DCB19106 - Installation, operation and maintenance manualAirflex 29DCB clutch/brake assembly drawing LA-11219 (Stolle P/N 094950) - on Standun B6 bodymaker 204194 Rev. B

LF

X

E

T

R

I

AN

OA

E

D CB

9

2

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 20162

General information

Warning

Forward this manual to the person responsible for Installation, Operation and Maintenance of the product described herein. Without access to this information, faulty Installation, Operation or Maintenance may result in personal injury or equipment damage.

Caution

Use only genuine Airflex replacement parts. The Airflex division of Eaton Corporation recommends the use of genuine Airflex replacement parts. The use of non-genuine Airflex replacement parts could result in substandard product performance, and may void your Eaton warranty. For optimum performance, contact Airflex:

In the U.S.A. and Canada: (800) 233-5926

Outside the U.S.A. and Canada: (216) 281-2211

www.eaton.com/Airflex

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 3

Table of contents

Section Description Page no

1.0 Introduction 41.1 Description 51.2 How it works 52.0 Installation 52.1 Preparation 52.2 Flywheel sub-assembly 52.3 29 DCB installation 72.4 Start up procedure 83.0 Operation 93.1 Pressure and speed limits 93.2 Initial operation 93.3 Periodic maintenance 94.0 Maintenance 94.1 Wear limits 94.2 Air manifold repair 94.3 Removal of the DCB 104.4 Friction disc replacement 11 4.5 Cylinder seal replacement 134.6 Disassembly 134.7 Reassembly 144.8 Flywheel bearing replacement 144.9 Bushing replacement 155.0 Technical assistance 156.0 Wear limit tables 167.0 Parts lists 168.0 Revisions 18

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 20164

DCB19106

Figure 1

1.0 Introduction

Throughout this manual there are a number of HAZARD Warnings that must be read and adhered to in order to prevent possible personal injury and/ or damage to equipment. Three signal words

Danger, Warning and Caution are used to indicate the severity of a hazard, and are preceded by the safety alert symbol

Danger Denotes the most serious injury hazard, and is used when serious injury or death WILL result from misuse or failure to follow specific instructions.

Warning Used when serious injury or death MAY result from misuse or failure to follow specific instructions.

Caution Used when injury or product/ equipment damage may result from misuse or failure to follow specific instructions. It is the responsibility and duty of all personnel involved in the installation, operation, and maintenance of the equipment on which this device is used to fully understand the Danger, the Warning and the Caution procedures by which hazards are to be avoided.

Item

Qty.

Description

Part number

Stolle part number

1 1 Hub 514213 094457

2 1 End plate 513107

3 16 Spring 000071X0131

4 16 Socket head cap screw

000030X0720

5 16 Clamp tube 000153X1105

6 2 Strap 307918

7 1 Clutch friction disc assembly

513131 088074

8 12 Hex head screw 000342X0607 094726

9 1 Pressure plate 513109

10 1 Polypak seal 000402X0015 088072

11 1 Cylinder 513099 090357

12 32 Washer 000153X0990 093168

13 1 Polypak seal 000402X0017 088073

14 32 Socket head cap screw

000030X0417 093169

15 1 Warning label 307577

16 1 Rotor sub-assembly

513110

17 16 Lockwasher 000068X0025

18 16 Hex head screw 000197X0712

19 16 Hi collar washer 000031X0005

20 4 Self-tap screw 000153X0644

21 1 Brake friction disc assembly

513134 088075

22 4 Flatwasher 000067X0009

23 4 Hex head screw 000197X0716

24 1 Air manifold sub assembly

415757 090150

25 8 Rubber washer 000350X0014 000350

26 2 Strap 307931

27 12 Safety washer - 5/8"

000404X0007 072750

2518 17

15 20

14 12

24

23

222

34

516

19

1

13

11

10

216

726

27 8

9

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 5

DCB19106

1.1 Description

1.1.1 The Airflex® Model 29DCB clutch and brake unit was designed to provide optimal clutch/ brake performance required on the Standun B6 Bodymaker.

1.2 How it works

1.2.1 Referring to Figure 1, the hub (1) is secured to the machine drive shaft. The rotor sub-assembly (16) is attached to the hub which are axially stationary. As air pressure is introduced into the cylinder (11) cavity, the cylinder, pressure plate (9) and end plate (2), which are fixed to each other with screws (4) and clamp tubes (5), move away from the machine, clamping the clutch friction disc assembly (7) between the end plate and rotor subassembly and compressing the springs (3). The clutch friction disc is resiliently bushing supported on the flywheel. At the same time, the pressure plate (9), by virtue of its being fixed to the end plate, draws away from the brake friction disc assembly (21). As air pressure is exhausted from the cylinder cavity, the springs (3) force the end plate in the opposite direction, clamping the brake friction disc assembly between the pressure plate and rotor subassembly. The brake friction disc assembly is bushing supported on stationary reaction members bolted to the bearing quill.

2.0 Installation Caution

Prior to performing any work, read this manual carefully, paying particular attention to the figures and attached drawing LA-11219. Do not risk injury or equipment damage.

Note: All part numbers referred to in this section can be found on Airflex Drawing LA-11219, which is a part of this manual.

2.1 Preparation

2.1.1 Prior to attempting installation, ensure the shaft and reference dimensions compare to those shown on drawing LA-11219. Make sure the shaft is clean and free of nicks or burrs.

2.2 Flywheel sub-assembly

2.2.1 Thoroughly clean the bores in the flywheel (515226) and remove any nicks or burrs.

2.2.2 Install the bearing cups (000348x0078) in the flywheel. It may be necessary to freeze the cups

to ease installation. Refer to drawing LA-11219 for proper orientation of the cups.

Note: The bearing cups may have been pre-installed at the factory.

2.2.3 Carefully tap the grease seals (000113x0461) into the flywheel. Refer to drawing LA-11219 for proper orientation of the seal lips.

2.2.4 Install the SpirOlox® seal retainers (000190x0090) by separating the coils and inserting one end of the ring into the groove. Keep the coil separated and spiral each turn progressively into the housing groove. When the last turn enters the groove there will be a snap indicating that ring is assembled properly.

2.2.5 Install the grease fitting and relief fitting per drawing LA-11219. Use a good quality sealant on all pipe threads.

2.2.5.1 Install pipe plugs in flywheel. Use Loctite® #262.

Caution

Loctite® #262 must be shaken prior to application.

Caution

Loctite® #262 may irritate sensitive skin. Refer to the product label for proper safety precautions.

2.2.6 Install the SpirOlox® seal retainer (000190x0095) in the brake reaction plate by separating the coils and inserting one end of the ring into the groove. Keep the coil separated and spiral each turn progressively into the housing groove. When the last turn enters the groove there will be a snap indicating that ring is assembled properly. Install bearing oil seal (000113x0464) into the brake reaction plate (513361). See drawing LA-11219 for proper orientation.

2.2.7 Insert bushings (308554) into the holes in the brake reaction plate.

2.2.8 Apply Never-Seez® to the first three to four threads and Loctite® #262 to the next three to four threads of the bushing mounting screws (000342x0620). Install and torque to 156 ft. lbs. Because the Loctite will set rapidly, apply Loctite and then tighten one screw at a time. This will avoid the Loctite from setting prior to tightening.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 20166

DCB19106

NOTE: Loctite® and Never-Seez® are compatible. Loctite® will provide a removable threadlock & the Never-Seez® prevents corrosion without interfering with the Loctite® holding capabilities.

2.2.9 Install flywheel bushing ring (513359) onto the flywheel. Install 16 screws (000197x0720) and safety washers (000404x0005), lubricate the first 3-4 threads with Never-Seez® and the next 3-4 threads apply Loctite® #262 and torque to 245 ft.lbs. Use a crosswise pattern. Because the Loctite will set rapidly, apply Loctite and then tighten one screw at a time. This will avoid the Loctite from setting prior to tightening.

Caution

Use only Airflex-supplied screws.

2.2.10 Hand pack one of the bearing cones (000347x0146) with grease (Mobilgrease XHP222 special or equivalent) and slide it onto the bearing quill and against the quill shoulder. See drawing LA-11219 for proper orientation of the bearing cone.

2.2.11 Slide the bearing spacer (308507) onto the bearing quill and against the bearing cone.

Note: Bearing spacers are custom fit to length for each flywheel. Do not interchange spacers with those from other flywheels.

2.2.12 Grease the bearing cups and the seal surface on the bearing quill. Fill the grease seal lips with grease. Use a grease gun and pre-fill the grease inlet passages. DO NOT fill the relief passage. Fill area between bearing cone and seal surfaces as shown in Figure 2. Rig the flywheel into position and slide it over the shaft until the inner cup is against the cone on the sleeve. Take care not to damage the inner grease seal as it passes over the bearing cone. Hold the flywheel in position.

2.2.13 Hand pack the remaining bearing cone with grease (Mobilgrease XHP222 special or equivalent) and, while still supporting the flywheel, tap it onto the sleeve.

2.2.14 Grease the seal surface ONLY on the bearing retainer (415906) and slide it onto the shaft. Grease the seal and slide the brake reaction plate on to the bearing quill lining up the three roll pins (000382x0041) with the retainer plate. Fasten with clamp ring, and 16 screws (supplied by customer). Tighten the screws until only snug. Remove the flywheel support and, using a crosswise tightening sequence, torque the screws to 75 ft.- lbs.(lubed).2.2.15 Using a depth micrometer through the holes in the brake reaction plate, measure and record the distance from the outer surface of the brake reaction plate to the face of the flywheel bearing quill ("D" on Figure 3).

2.2.16 Remove the brake reaction plate, making sure the flywheel remains in position, and measure and record the thickness of the brake reaction plate flange ("T" on Figure 3). Use the average of these values.

2.2.17 Subtract "T" from "D". Grind the spacer ring (supplied by customer) to achieve total thickness equal to (+.000/-.001") the difference between "D" and "T". Grind equal amounts of material from both sides of the spacer ring.

2.2.18 Reinstall the brake reaction plate with the spacer ring in place. Using a crosswise pattern, uniformly torque the 7/8-14 UNF x 5" Lg. screws (lubed) to 300 ft.lbs. then repeat crosswise pattern to 600 ft.lbs. Install retainers and snap rings after achieving proper orientation of the screws. To achieve proper orientation for retainers, vary screw torque from 550 ft. lbs. to 650 ft.lbs., maximum.

Figure 3

“D”

“T”

Figure 2

Fill with grease tolevel shown

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 7

DCB19106

Caution

The Brake Reaction Plate mounting screws must be Grade 8, minimum.

2.2.19 Pump 1 oz. - approximately 20 pumps from a hand grease gun - of (Mobilgrease XHP222 special or equivalent) grease into the flywheel bearing cavity. Remove excess grease from fittings. The bearing cavity should be about 1/3 to 1/2 full. Refer to Figure 2.

2.3 29 DCB Installation

Note: The air manifold (415747) may be attached to the DCB for shipping purposes. If so, remove it prior to installation of the DCB.

2.3.1 Make sure the shaft is clean and free of nicks or burrs.

Caution

Ensure that NO moly-based grease contaminates the shaft area where the locking assembly clamps.

2.3.2 Apply Molybdenum disulfide grease or equivalent to the shaft between the hub and shaft. Reference note 16 on Eaton drawing LA-11219.

2.3.3 Installation instructions for clutch hub item #1 and B'Loc locking assembly item #2. Reference Stolle Drawing 715081 for the following 11 steps.

1. Clean and lightly oil (D.T.E. light Hyd. oil ISO VG 32 or equal) shaft, hub bore and locking assembly. Make sure to always oil threads and head of SOC head cap screws. It is important not to use molybdenum disulfide, e.g. Molykote, Never-seeze or similar lubricants in any locking assembly installation.

2. Use installation fixture tool assembly 741042 for following procedures.

3. Install locking assembly (item #2) into the ă6-1/2" bore of the clutch/brake hub (item #1) seating locking assembly on bore shoulder as shown. It may be necessary to secure position of inner wedge during this procedure. Utilize screw positions (view a-a) 1, 6, & 11 as jacking screws to hold inner wedge position. Remove these bolts from current position and thread to appropriate depth on adjacent holes to secure inner wedge.

4. Attach the tool plate (item #15) 741043 to the clutch/brake hub (item #1) by tightening (4) SOC head cap screws 3/4-10 unc x 2-3/4 long (item #19) to 170 ft-lbs.

5. Install clutch/brake assembly with locking device and tool plate mounted onto the crank shaft dia. As shown using overhead lifting device fitted slings or other equivalent supporting device, be sure to fully seat the tool plate against the end of the crankshaft by tightening (3) socket head cap screws 5/8-11unc x 2-1/2" long (item #17) to 30 ft-lb - do not relieve lifting support.

6. Install clutch/brake tool bolt (item #16) in center threaded hole of tooling plate (item #15). Tighten tool bolt (item #16) to 45 ft. lbs. do not relieve lifting support.

7. Measure through slot provided to determine distance "W" between clutch/brake hub and crankshaft journal at the four positions provided. Center the clutch/brake unit to the crankshaft within .005" or less by adjusting the tooling bolt (item #16) torque and tooling plate mounting bolts (item #17) in combination with clutch/brake support mechanism in use. Complete tightening of (3) socket head cap screws 5/8-11unc x 2-1/2" long (item #17) to 125 ft. lbs. upon achieving centering specification of "w" dimension variation of .005" or less.

8. Remove slings and other clutch/brake unit lifting devices - recheck "W" dimension in slots through tool plate (item #15) for any movement from centering specification - repeat step 7 if movement is determined. 9. Stages following the sequence shown in the partial end view a-a on sheet 2 of 3. Reference Stolle drawing 715081.

Stage 1: tighten screws evenly and in sequence shown by turning the screws approximately 1/4 turn at a time evenly until 40 ft-lbs. Each is reached as measured with a torque wrench.

Stage 2: remove tool plate (item #15) by unscrewing all SOC head cap screws from hub and from crankshaft. Remove any slings or straps (crane). Pay attention to the clamp collar split-line and make necessary torque corrections to the screws (position 7 & 8) adjacent to the split-line to ensure no more than .015" offset exists, check "Channel" width "W" at (8) places and enter each measurement to the chart. If difference (W max / -W min ) is more than .005", recheck all locking screw torque (40 ft. lbs.), if necessary disassemble, check components for burrs & foreign matter and reassemble per the above procedure, if (W max / -W min) is .005" or less proceed tightening all screws evenly & in sequence shown by turning the screws approx. 1/4 turn at a time until 60/80/100 ft. lbs. each is reached as measured with a torque wrench. Make "Channel" width "W" check after each screw tightening step. Maximum variation acceptable is .005 in.

Stage 3: recheck final screw tightening torque of 100 ft. lbs. in clockwise sequence until no screw can be turned any more. Make final "Channel" width "W" check and enter the measurements to the chart.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 20168

DCB19106

10. Remove (item #15) tool plate and re-verify "w" dimension variation less than .005". Repeat step above and correct any deviation.

11. Removal instructions: reference drawing 741042 sheet 2.

A. Use tool bolt (item #16) for removal of clutch/brake unit from crankshaft journal. Remove socket head cap screw (item #17) and install (4) socket head cap screws (item #19).

B. Install proper lifting and support mechanisms (straps & blocks) to support the weight of the clutch/brake unit during removal (850 lbs).

C. Remove (14) locking device mounting screws. Rotate tooling plate (item #15) 90° in either direction and re-install the locking device mounting screws in the adjacent threaded holes to seperate locking device wedges. Once screws are seated tighten in clockwise pattern 1/4 turn each until wedges are seperated.

D. Turn tool bolt (item #16) to seperate clutch/brake unit from crankshaft journal.

2.3.4 Install and tension the drive belts.

2.3.5 Attach the air manifold subassembly (415757) to the DCB hub with four screws (000197x 0716) and flat washers (000067x0009), making sure the rubber washers (000350x0014) are in place at the air inlets. Use Loctite® #262 on the screws and torque to 110 ft.-lb.(lubed)

2.3.6 Attach the 1" RH rotorseal (145488AB) to the air manifold with four screws (000030x0207) and lockwashers (000031x0006), making sure the rubber face seal is in place. Using a crosswise pattern, torque the mounting screws to 28 ft. lbs., lubed.

2.3.7 Connect a regulated air supply to the rotorseal and apply enough air pressure to release the brake (80-90 psi).

Warning

Maximum applied air pressure for set up purposes is 90 psi. Air pressure exceeding maximum allowable will result in damage to the DCB components.

Warning

A pinch point exists between the rotor, pressure plate and brake friction disc assembly.

2.3.8 Remove the screws, serrated safety washers and straps attaching the brake friction disc assembly halves together and reinstall with Loctite® #262. Torque the screws to 156 ft.- lb., making sure the brake friction disc slides freely on the bushing assemblies.

Caution

The brake friction disc assembly MUST slide freely on the bushings. If the disc binds, excessive heat will be generated during machine operation.

2.3.9 Exhaust the air pressure and remove the temporary air supply.

2.3.10 Connect the air piping using a flexible hose between the rotorseal and the dual valve.

Warning

Maximum applied air pressure is 90 psi. Maximum operating air pressure is 85 psi. Operation with air pressure greater than the maximum allowable may result in damage to DCB components.

2.3.11 Remove the screws and straps attaching the clutch friction disc assembly halves together and reinstall with Loctite® #262. Torque the screws to 156 ft.-lb., making sure the clutch friction disc slides freely on the bushing assemblies.

Caution

The clutch friction disc assembly MUST slide freely on the bushings. If the disc binds, excessive heat will be generated during machine operation.

2.4 Start up procedure

Warning

Excessive machine cycling or jogging during die set up may cause internal damage to the DCB clutch/brake, and accordingly, degrade clutch/brake performance, with potential subsequent damage to the machine and/or related equipment.

2.4.1 Start the main drive motor and allow it to idle at slow speed (if so equipped) for approximately one hour. Cycle the machine several times during this period to check clutch/brake operation.

Note: Some grease may be thrown out through the relief fitting, which is no cause for alarm.

2.4.2 Turn the main drive motor off and check for excessive temperatures at the flywheel bearing hub (at slow speed the hub should be relatively cool). Check that the clutch & brake friction discs slide freely on the bushings. Correct if necessary by loosening the screws attaching the friction disc halves together, reapplying Loctite® #262 and retightening.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 9

2.4.3 Start the main drive motor and allow to idle at full speed for approximately one hour, again cycling the machine periodically. Turn the drive motor off and repeat the above checks.

3.0 Operation

3.1 Pressure and speed limits

3.1.1 Maximum applied air pressure is 90 psi. Maximum operating air pressure is 85 psi. Minimum operating air pressure is 80 psi, operation below 80 psi will result in insufficient torque development and possible friction disc slippage.

Warning

Maximum applied air pressure is 90 psi. Maximum operating air pressure is 85 psi. Operation with air pressure greater than the maximum allowable may result in damage to DCB components.

3.1.2 Maximum operating speed of the 29 DCB clutch/ brake is 750 rpm.

3.2 Initial operation

Warning

Excessive machine cycling or jogging during die set up may cause internal damage to the DCB clutch/ brake, and accordingly, degrade clutch/brake performance, with potential subsequent damage to the machine and/or related equipment.

3.2.1 Insure that the clutch and brake friction discs slide freely on the bushings. Excessive heat will be generated during machine operation if the disc binds. If binding is evident refer to paragraph 2.3.13 - 2.3.16.

3.3 Periodic maintenance

3.3.1 Perform all operations in section 3.2.

3.3.2 Inspect the friction material for signs of wear (refer to table 1).

3.3.3 Inspect the flywheel bushings and brake reaction plate bushings for signs of wear (fretting).

3.3.4 Check drive belts for proper tensioning.

3.3.5 Check for air leaks in the air system and at the clutch.

3.3.6 Check the rotorseal bearings for freedom of movement.

3.3.7 Insure that the guards are free from the flywheel and clutch/brake assembly.

3.3.8 Lubricate the flywheel bearings on a weekly basis using 1 oz. - approximately 20 pumps from a hand grease gun - of (Mobilgrease XHP222 special or equivalent) grease.

DCB19106

4.0 Maintenance

Warning

Prior to performing any work on the DCB, make sure the machinery is in, and will remain in, a safe condition.

4.1 Wear limits

4.1.1 Wear limits for the normal wearing components of the DCB are listed on Table 1. If any wear limit has been reached or exceeded, that component must be replaced. In addition, if any friction surface has been contaminated with oil or grease, that friction disc assembly must be replaced.

4.2 Air manifold repair

Airflex repair kit 145141DQ is available for repair of the air manifold quick release valves. Each kit contains an end cap, diaphragm, muffler and a tube of Loctite® #222. Item numbers in the following instructions are shown on Figure 4.

NOTE: It is not necessary to remove DCB from shaft to repair the air manifold.

Warning

Follow the repair instructions closely. Improperly installed QRV end caps may work loose during operation resulting in exposure to personal injury or equipment damage.

Figure 4

3

4

6

2

1

5

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201610

4.2.1 Remove the rotorseal from the manifold. It may be necessary to disconnect the air supply line.

4.2.2 Remove the air manifold assembly and transport to a clean work area.

4.2.3 Remove the mufflers (6), end caps (2) and diaphragms (3), taking care not to damage the sealing surfaces in the QRV housings (4). If a QRV housing comes loose when removing the end caps, replace per the following instructions.

4.2.3.1 Thoroughly clean all holes in the manifold housing (1).

4.2.3.2 Install the end cap (2) into the QRV housing (4) hand tight. Do not use any Loctite® on the end cap threads.

4.2.3.3 Install the o-ring (5), lubricated with Parker O-Lube®, into the manifold housing.

4.2.3.4 Apply Loctite® #271 to the external threads on the QRV housing and screw it into the manifold until the QRV housing is flush with the O.D. of the manifold. Align the air inlet holes.

4.2.3.5 Allow the Loctite® #271to cure for 24hrs. For faster cure allow the Loctite® to cure at 200°F for a minimum of one hour.

4.2.4 With the end caps removed, thoroughly clean the internal threads in the QRV housings.

4.2.5 Place a diaphragm in the housing and install the end cap and muffler using Loctite® #222 on the threads. Torque the end cap to no more than 10 ft.-lb.

4.2.6 After the Loctite® has cured minimum 24hrs (for faster cure allow the Loctite® to cure at 200°F for a minimum of one hour), apply counter-clockwise torque of 15 ft.-lb. to each end cap and muffler. If any end cap or muffler comes loose, remove and repeat 4.2.5.

4.2.7 Reinstall per 2.3.5 and 2.3.6.

4.3 Removal of the DCB

Note: It is not necessary to remove either of the friction disc assemblies to remove and overhaul the DCB.

4.3.1 Disconnect the air supply and remove the rotorseal and QRV manifold assembly from the DCB hub.

4.3.2 Attach an overhead support to the DCB.

4.3.3 Refer to Figure 5. Loosen the shaft locking assembly screws gradually in a diametrically opposed sequence (crosswise pattern). Remove all of the screws. Install screws into push-off threads provided in the outer clamp collar (A), until they bottom against the center collar (B). Tighten the screws crosswise in 1/4 turn increments until the outer clamp collar loosens. Remove the outer clamp collar. Install screws into push-off threads provided in the center collar. Tighten the screws crosswise in 1/4 turn increments until the center collar loosens from the inner clamp collar (C).

4.3.4 Carefully slide the DCB off of the shaft and transport to a clean work area.

4.3.5 Remove the remaining clamp collars from the DCB hub and re-assemble the shaft locking assembly for later use.

DCB19106

Figure 5

A C

B

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 11

4.4 Friction disc replacement

Note: Removal of the DCB Clutch/Brake is required to remove clutch & brake friction discs(see section 4.3).The shaft locking assemblies may be removed, allowing the DCB to be slid away from the machine to obtain the required clearance to remove the clutch friction disc halves. When using this procedure, make sure the DCB is supported to avoid personal injury. Refer to the INSTALLATION section of this manual for reassembly. Note the orientation of the offset on the friction disc’s metal core, and remember to install the straps attaching the friction disc halves.

Note: The wear limit for the clutch/brake friction disc surfaces, shown on Table 1, is approximately .060" per surface. Due to the offset on the disc cores, a direct measurement of friction material thickness is not possible. Figure 6 shows the measurements to be taken between the outboard clutch friction surface (measured with air on) and the end plate, and between the inboard brake friction surface (measured with air off) and the pressure plate.

Warning

Operation of the DCB with the friction material worn to less than the gap measurements shown on Figure 6 will result in a significant reduction of clutch and/or brake torque.

4.4.1 Remove the screws attaching the straps to the clutch friction disc assembly halves and remove the clutch friction disc assembly. If not replacing, set aside in a clean area.

4.4.2 Apply air regulated (90 psi Max.) pressure to the DCB to release the brake.

Warning

Pressure above 90 psi may cause internal damage to the components of the clutch/brake.

4.4.3 Remove the screws attaching the straps to the brake friction disc assembly halves and remove the brake friction disc assembly. If not replacing, set aside in a clean area.

4.4.4 Exhaust the air to release the clutch.

Warning

With the brake friction disc assembly removed, a pinch point exists between the pressure plate and rotor.

4.4.5 Friction lining replacement: If the bushing holes in the Clutch/Brake disc have not worn to the limit shown on Table 1 and the friction disc cores are in good condition, the cores may be relined with new friction material. Airflex lining kit 146293YF contains enough friction material and rivets to repair one clutch or brake friction disc assembly. Replace the friction linings per the following instructions.

Warning

Before beginning replacement of parts supplied in the friction disc kit, carefully read the following instructions and make sure what is stated in each step is understood. Failure to follow these instructions may result in personal injury.

Caution

Use only Airflex supplied replacement friction material. Use of material not of Airflex origin may result in reduced clutch or brake torque or accelerated wear of the iron components.

4.4.5.1 Drill out the old rivets using a .250" drill. Remove and discard the used friction discs.

4.4.5.2 Refer to Figure 7 and carefully examine the counterbored holes in the friction disc segments (513084). One set of counterbored holes is tapered and designed to accept the rivet head, while the other set of counterbored holes is flat-bottomed and designed to accept the clinched end of the rivet.

DCB19106

Figure 6

Figure 7

.010" min.(air on)

.010" min.(air off)

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201612

DCB19106

4.4.5.3 Position the friction discs on both sides of the friction disc core, as shown on figures 8, 9 &10, and align the rivet holes in the friction discs with the rivet holes in the core plate.

Caution

Each friction disc (513084) is molded in a continuous ring and saw cut prior to shipment from Airflex. Matching friction disc segments are wired together after cutting. Make sure each friction disc set is riveted to the same face of the clutch or brake disc core.

Caution

Manual setting of the rivets using a punch very frequently results in splitting of the clinched end of the rivet. When this occurs, the rivet will ultimately fail in service due to fatigue. It is therefore recommended that rivets be set using an automatic rivet setting machine.

4.4.5.4 Insert the first rivet (000130x0090) through any hole adjacent to the split line (end of lining segment). Be sure to note the type of counterbored hole to determine the position of the rivet head. See Figure 7.

Caution

When working with any friction material, regardless of material type, always wear approved safety equipment.

4.4.5.5 Set the rivet using a washer (000153x0985) on the clinched end of the rivet. See figures 9 and 10. Figure 9 shows machine-setting and Figure 10 shows setting the rivet manually. When setting manually, use an arbor press and keep the setting tool square to avoid splitting the rivet. The rivet setting tool optional and available from Airflex as part number 000153X1092. (Stolle part # 089800).

Caution

The clinched end of the rivet must have a washer (000153x0985) in place prior to clinching. Failure to use the washer will allow the rivet to fracture the friction lining. Also, use of excessive force to clinch the rivet will fracture the friction lining.

4.4.5.6 Insert a second rivet on the opposite end of the friction lining and repeat 4.4.5.5.

4.4.5.7 Insert a third rivet at the center of the friction lining and repeat 4.4.5.5.

4.4.5.8 The remaining rivets may be installed in any reasonable sequence following 4.4.5.5.

4.4.5.9 After all rivets are clinched, check to make sure that a washer has been used on each rivet. Inspect the clinched end of each rivet and replace any that are cracked or split. Look closely at the lining and make sure there are no cracks. If a .005" feeler gauge can be inserted further than .375" between the friction discs and core plate, the rivets in that area must be reclinched.

Figure 9

Figure 10

Anvil pinClutch or brakeFriction disc core

Washer

Frictiondisc

RivetDriver

Frictiondisc

Anvil

Washer

PunchRivet

Clutch or brakeFriction disc core

Figure 8

Split line

Clinched end ofrivet / washer

Rivethead

Split line

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 13

4.4.6 Apply air regulated pressure to the DCB to release the brake. (90 psi Max.)

Warning

Pressure above 90 psi may cause damage to the components of the clutch/brake.

4.4.7 Install the brake friction discs, straps washers and screws. Hand tighten screws.

4.4.8 Exhaust the air to release the clutch.

4.4.9 Install the clutch friction discs, straps washers and screws. Hand tighten screws.

4.4.10 Inspect the bushings for wear. Replace if necessary per section 4.9.

4.4.11 Re-install the DCB per section 2.3.

4.5 Cylinder Seal Replacement

Note: Remove the DCB per section 4.3.

Refer to Figure 1 for location of the following numbered items.

4.5.1 Match-mark the cylinder (11) to the pressure plate (9) and remove the cylinder attaching screws (14) and lockwashers (12).

4.5.2 Carefully slide the cylinder (11) off of the DCB.

Warning

DO NOT use air pressure to force the cylinder off of the DCB. Application of air pressure with the cylinder attaching screws (14) removed will result in exposure to personal injury or equipment damage.

4.5.3 Check the seal surfaces on the cylinder (11). If the wear reaches or exceeds the specification on Table 1, the cylinder (11) must be replaced.

4.5.4 Remove the PolyPak® seals (10)(13) from the hub (1) Install new seals (10)(13) noting the orientation of the seal lips.

4.5.5 Lubricate the seal surfaces on the cylinder (11) with a light coat of Parker O- Lube® and slide the cylinder (11) into position.

4.5.6 Align the match marks and attach the cylinder (11) to the pressure plate (9). Torque the screws to 70 ft.-lb., lubed. Use Loctite® #272 on the screws.

DCB19106

4.6 Disassembly

Note: Remove the DCB per section 4.3.

Refer to Figure 1 for location of the following numbered items.

Danger

High spring forces exist within the DCB. Read the following instructions carefully before attempting to disassemble the unit.

4.6.1 Lay the DCB on a clean, flat work surface, cylinder (11) down.

4.6.2 Remove four equally spaced screws (4) and lockwashers (19) attaching the end plate (2) to the pressure plate (9) and reinstall without the lockwashers (19) in place.

4.6.3 Remove the remaining 12 screws (4) and lockwashers (19).

4.6.4 Loosen the four screws (4) in a crosswise pattern, one turn at a time, until all of the spring force has been relieved.

Danger

The four screws (4) must be loosened gradually. Failure to follow this procedure will result in over stressing and possible failure of the end plate (2).

4.6.5 Lift the end plate (2) off of the springs (3) and check the friction surface. See Table 1.

Danger

The wear surface on the end plate (2) cannot be renewed by machining. If the wear limit shown on Table 1 has been reached or exceeded, the end plate (2) MUST be replaced.

4.6.6 Remove the clutch friction disc assembly (7), note the wear on the friction surfaces and set aside.

4.6.7 Remove the springs (3) and check the free height. If any one of the springs (3) has a free height less than the value shown on Table 1, the entire complement of springs (3) must be replaced.

4.6.8 Lift the clamp tubes (5) out of the holes in the rotor (16) and check for wear. If any clamp tube (5) has worn to the specification on Table 1, it is advised that the entire set be replaced.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201614

DCB19106

4.6.9 Remove the screws (18) and lockwashers (17) attaching the rotor (16) to the hub and lift off the rotor (16). Inspect the friction surfaces and bushing bores. If any of the wear limits on Table 1 have been reached or exceeded, the rotor subassembly (16) must be replaced.

Caution

If the wear limits on the rotor friction surfaces have been reached or exceeded, the rotor subassembly must be replaced. The friction surfaces cannot be renewed by machining.

Caution

If the wear limit for the bushings in the rotor has been reached or exceeded, the rotor must be replaced. The bushings are normally not replaceable items. Consult the factory prior to attempting replacement of the bushings.

4.6.10 Remove the brake friction disc assembly (21), note the wear on the friction surfaces and set aside.

4.6.11 Note the wear on the friction surface on the pressure plate.(9) If the wear exceeds the limit shown on Table 1, the pressure plate (9) must be replaced. To replace, remove the cylinder (11) per 4.5.

Caution

If wear of the friction surface on the pressure plate (9) exceeds the value shown on Table 1, the pressure plate (9) must be replaced.

4.7 Reassembly

Refer to Figure 1 for location of the following numbered items.

4.7.1 With the cylinder (11) assembled to the pressure plate (9) and hub (1), lay the unit on a flat work surface, cylinder (11) down.

4.7.2 Place the brake friction disc assembly (21) on the pressure plate (9), noting the orientation of the step on the friction disc core.

4.7.3 Position the rotor (16) onto the hub (1) so the two sets of holes are aligned and the register on the rotor (16) engages the DCB hub (1).

4.7.4 Attach the rotor (16) to the hub (1) with screws (18) and lockwashers (17). Coat the screws (18) with an Never-seez® and, using a crosswise pattern, torque the screws (18) to 245 ft.-lb.

4.7.5 Coat the O.D. of the clamp tubes (5) with a light coat of Never-seez® and insert into the holes in the rotor (16).

4.7.6 Insert the springs (3) into the pockets in the hub (1).

4.7.7 Place the clutch friction disc assembly (7) on the rotor (16), noting the orientation of the step on the disc core.

4.7.8 Place the end plate (2) over the springs (3) so the mounting holes are aligned and the springs (3) engage the bosses on the end plate (2).

4.7.9 Apply a coat of Never-seez® to the threads and under the heads of four end plate mounting screws (4) and install evenly spaced. Do not install the lockwashers (19) at this time.

4.7.10 Tighten the four screws (4) one turn at a time, in an alternating sequence, until the springs (3) are fully compressed.

Danger

The four screws (4) must be tightened gradually. Failure to follow this procedure will result in over stressing and possible failure of the end plate (2).

4.7.11 Install the remaining end plate mounting screws (4) and lockwashers (19). Apply a coat of Never-seez® to the screw threads and, using a crosswise pattern, torque the screws (4) to 245 ft.-lb.

4.7.12 Remove the four screws (4) installed in 4.7.9 and reinstall and torque with the lockwashers (19) in place.

4.7.13 Install the DCB per section 2.3.

4.8 Flywheel bearing replacement

Caution

The flywheel bearing cups and cones must be replaced in sets. It is not a good practice to install a new cone against a worn cup. Also, when replacing bearings, it is extremely important that the bearing spacer length be checked to ensure porper bearing clearance.

4.8.1 Remove the DCB from the shaft per 4.3 and remove the drive belts.

4.8.2 While supporting the flywheel, remove the screws, clamp rings, retainers and snap rings attaching the brake reaction plate (513361) to the bearing quill. Remove the brake reaction plate. Examine the seal surface on the quill bearing retainer (415906). Insure it is free from nicks and burrs. Replace if necessary.

4.8.3 Carefully slide the flywheel off of the bearing quill. The bearings and spacer will pull off the quill along with the flywheel.

4.8.4 Slide the bearing cones(000347x0146) and spacer(308507) out of the bore.

4.8.5 Examine the grease seal surface of the quill. Insure it is free of nicks and burrs. Repair or replace if necessary.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 15

DCB19106

4.8.6 Remove the SpirOlox® seal retainers and carefully tap the grease seals (000113x0461) and the bearing cups (000348x0078) out of the flywheel.

4.8.7 Remove any nicks or burrs from the flywheel bore and carefully tap in the new bearing cups. Freezing the cups will ease insertion. See LA-11219 for proper orientation.

4.8.8 Replacement of the bearings requires that the spacer length be re-evaluated. Determine the spacer length per the following instructions:

4.8.8.1 Allow the bearing cups to warm to ambient temperature if they have been chilled during assembly.

4.8.8.2 Apply a light coat of grease to the cups and insert the cones into the flywheel, holding them into position with a three pronged fixture, similar to that shown on Figure 11.

4.8.8.3 Rotate the fixture while tightening the fixture clamp screw. Tighten just until the rollers are seated in the cups so that no rollers are loose.

4.8.8.4 Measure the space between the inner bearing races ("M" on Figure 11) at three positions approximately 120 degrees apart. If the difference between the three readings is less than 0.010", calculate the average of the three readings. If the difference between the three readings is greater than 0.010", the bearings are not seated. Loosen the fixture and re-seat the cones, tightening the fixture per 4.8.8.3.

4.8.8.5 Calculate the spacer width: Minimum spacer width = M + 0.014". Maximum spacer length = M + 0.015".

Figure 11

4.8.8.6 Grind the spacer to the proper length. If necesarry, weld and re-grind the spacer, or replace the spacer and grind to length as required.

4.8.9 Reinstall per Section 2.0.

4.9 Bushing replacement

4.9.1 Remove DCB from Shaft per 4.3

4.9.2 Remove the screws (000197X0720) and washers (000404X0005) attaching the flywheel bushing ring to the flywheel and remove bushing ring.

4.9.3 Support the flywheel and remove customer supplied screws (7/8-14 UNF x 5.00) from the brake reaction plate and remove. Do not remove overhead support from the flywheel.

4.9.4 Removal of the bushings from the flywheel bushing ring and brake reaction plate requires Airflex Kit #146220XE, which includes two screws (000032x0612 & 307657) and a pin (307654-01).

4.9.5 Remove each bushing per the following instructions:

4.9.5.1 Remove the (000342x0620) securing the bushing to the flywheel bushing ring and/or brake reaction plate.

4.9.5.2 Slide the pin (307654-01) into the bushing and thread the screw (307657) into the tapped hole in the end of the bushing until it seats.

4.9.5.3 Apply Never-Seez® to the threads of the screw (000032x0612) and thread it into the tapped bushing mounting hole.

4.9.5.4 Tighten the screw to push the bushing out.

4.9.5.5 Repeat the above procedure for the remaining bushings.

4.9.6 Re-install the bushings per section 2.0 and DCB per section 2.3.

5.0 Technical information

5.1 In any correspondence regarding Airflex equipment, refer to the part number and description on the product nameplate and call or write:

Eaton Corporation Airex Division 9919 Clinton Road Cleveland, Ohio 44144 Tel.: (216) 281-2211 Fax: (216) 281-3890 Toll Free: (800) 233-5926 www.eaton.com/airflex

Loctite is a registered trademark of Henkle Consumer Adhesives. Molykote is a registered trademark of Dow Corning Corporation. Mobilgrease is a registered trademark of Mobil Oil Corporation. PolyPak and Parker O-Lube are registered trademarks of Parker Hannifin Corporation. Never-Seez is a registered trademark of Bostik, Inc. SpirOlox is a trademark of Ramsey Corporation.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201616

7.0 Recommended spare parts list Standun bodymaker per Airflex drawing LA-11219 (108100A) / (Stolle 094950)

DCB19106

Quantity Description Airflex part number Stolle part number

1 29DCB clutch/brake assembly 146293E 0893461 Piston polypak seal 000402X0015 0880721 Piston polypak seal 000402X0017 08807316 Brake apply spring 000071X0131 0887651 Bearing retainer, grease seal wear surface 415906 0887661 Clutch friction disc assembly 513131 0880741 Brake friction disc assembly 513134 0880752 Friction disc and rivet replacement kit 146293YF 0887672 Flywheel grease seal 000113X0461 0880772 Flywheel bearing (Cone) 000347X0146 0949512 Flywheel bearing (Cup) 000348X0078 0949521 Flywheel bearing spacer 308507 0949531 1" RH rotorseal 145488AB 0955801 1" RH rotorseal rebuild kit 145488XA 0887688 Manifold mounting seal washers 000350X0014 0887698 Manifold QRV repair kits 145141DQ 09003232 Bushings 308554 0951481 Shaft seal 000113X0464 0880711 Shaft locking assembly 000403x0105 7150668 Rubber washers 000350x0014 086712

6.0 Wear limits

TABLE 1 (See figure 1 for Item Numbers)Item Description Wear limit Remarks

11 Cylinder Visual Replace when aluminum is visible.

7, 21 Friction disc assemblyFriction materialExceeding wear limit will result in clutch/brake failure.

Minimum friction disc assembly overall thickness is **.785".

Replace friction disc assembly when overall thickness is worn to wear limit. New friction disc assembly is approximately .850 - .880" thick.

2, 9 16 Friction Disc GapExceeding wear limit will result in clutch/ brake failure.

Maximum friction disc gap not to exceed **.815"Both discs removed.

End plate to rotor gap measured with air applied. Pressure plate to rotor gap measured without air applied. Inspect components for wear if gap limit is exceeded. A pinch point exists when air is applied or released.

3 Spring 4.500" free height Original spring free height is 4.455".

2 End plate friction surface .020" on surface Wear will be evident as a step worn into the friction surface along with some grooving.

5 Clamp tube .010" on diameter Wear will typically be in the form of a notch in the driving direction. Original diameter is 1.366".

16 Rotor bushing .015" on diameter Wear will be in the form of elongation of the bushing. Original bushing I.D. is 1.377".

16 Rotor friction surfaces .020" per surface Wear will be evident as a step worn into the friction surface along with some grooving.

9 Pressure plate friction surface .020" on surface Wear will be evident as a step worn into the friction surface along with some grooving.

7 Friction disc metal core .030" on diameter Wear will be in the form of elongation of the holes which mate with the flywheel bushings. Original hole diameter is 1.655/1.660".

* Bushings 308554 .020" on diameter Wear will be in the form of a groove on the O.D. of the bushing. New diameter 1.613/1.623"

* Shown on drawing LA-11219 at end of this manual.** The friction disc gap includes a combination of iron surface wear of the End Plate, Rotor and Pressure Plate. The friction disc must be at least .010" thicker than the friction disc gap.

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 17

29DCB clutch/brake application material list Standun bodymaker per Airflex drawing LA-11219 (108100A) / (Stolle 094950)

DCB19106

Quantity Description Airflex part number Stolle part number

2 Pipe Plug, countersunk hex, steel, 1/8" 000077X00012 Pipe Plug, countersunk hex, steel, 3/8" 000077X00042 Oil seal 000113X0461 0880771 Oil seal 000113X0464 0880711 Grease fitting 000145X00021 Relief fitting 000145X00052 Snap ring 000190X0090 0880801 Snap ring 000190X009516 Hex head screw, GR8, 3/4-10NC2 x 4.5 long 000197X0720 09036316 Hex head screw, GR8, 5/8-18NC2 x 4.5 long 000342X0620 0898352 Bearing cone 000190x0090 0949512 Bearing cup 000190x0095 0949521 Locking assembly 000403X0105 71506616 Serrated safety washer, 3/4 000404X0005 0386001 1" RH rotorseal 145488AB 0955801 Bushing installation and removal kit 146220XE 0898541 29DCB clutch/brake assembly 146293E 0893461 Flywheel bushing ring and bushing sub-assembly 146367 0900271 Bearing spacer 308507 0949531 Bushing sub-assembly 308554 0951481 Bearing retainer 415906 0900001 Brake reaction plate 513361 7150581 Flywheel 515226 094954

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201618

Revision

Original publication date: August 2006

Revision date Change Pages

11 February 2016 Converted to new IOM format All

308554 was 307677 5

Mobilgrease XHP222 special was Mobilith AW 2 6, 7, 9

29DCB installation revised to include detail on Stolle drawing 715081 7,8

145488AB was 145488K 8

customer supplied screws (7/8-14 UNF x 5.00 was (000197X0611) 15

Table 6.0 -- 4.500 was 4.188, 4.455 was 4.366, 1.366 was 1.000, 1.377 was 1.005 and 308554 was 307677 15

Table 7. -- 145488AB was 145488K, 145488XA was 145488X. 308554 was 307677, 095580 was 086622, 095148 was 086731 16

Included current drawings 18, 19, 20, 21

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 19

DCB19106 clutch/brake application for Standun B6 bodymaker

XX

PAR

TIA

L E

ND

VIE

W S

HO

WIN

G F

LYW

HE

EL,

R

ETA

INE

RS

, BU

SH

ING

MTG

RIN

G &

LO

CK

ING

AS

SY

(W/T

IGH

TEN

ING

SE

QU

EN

CE

FO

R L

OC

KIN

G A

SS

Y S

CR

EW

S) S

EE

NO

TE 9

CENTERLINE OF MACHINE

0000

77X

0004

PIP

E P

LUG

(3/8

-18

NP

T)2

RE

QD

, 90°

APA

RT

AS

SE

MB

LE W

ITH

LO

CTI

TE 2

62

0001

13X

0461

,2

RE

QD

(CR

137

5230

)

OIL

SE

AL

CA

RR

IER

BY

CU

STO

ME

R

0001

90X

0090

, 2 R

EQ

D(S

PIR

OLO

X R

RN

-150

0)

0003

47X

0146

(TIM

KE

N C

ON

E M

2497

49)

0003

48X

0078

(TIM

KE

N C

UP

M24

9710

)2

RE

QD

3085

07S

EE

NO

TE 1

7

5152

26 F

LYW

HE

EL

3/4-

10N

C X

1.5

0 D

EE

P3

LIFT

ING

HO

LES

EQ

SPA

CE

DO

N 3

8.50

B.C

.

5 "C

" GR

OO

VE

S

0001

97X

0720

(3/4

-10N

C X

4.5

0 LG

SC

R G

R 8

)00

0404

X00

05 S

AFE

TY W

AS

HE

R16

RE

QD

, AS

SE

MB

LE W

ITH

LO

CTI

TE 2

62TO

RQ

UE

TO

245

FT.

LBS

.(LU

BE

D, S

EE

NO

TE 1

3)

3/4-

10N

C-2

X 1

.50

DE

EP

LIFT

ING

HO

LE

0001

13X

0464

OIL

SE

AL

(NAT

ION

AL

4173

65)

0001

90X

0095

SN

AP

RIN

G(S

PIR

OLO

X R

R-7

12)

4 S

CR

EW

S &

WA

SH

ER

S (P

AR

TS O

F 14

6293

E)

0001

97X

0716

(3/4

-10N

C X

3.2

5 LG

GR

8)

0000

67X

0009

FLA

T W

AS

HE

RA

SS

EM

BLE

WIT

H L

OC

TITE

262

AT

FIN

AL

AS

SY

TOR

QU

E T

O 1

10 F

T.LB

S.(L

UB

ED

, SE

E N

OTE

13)

0003

50X

0014

, 8 R

EQ

D(P

AR

T O

F 14

6293

A)

4157

57 (P

AR

T O

F 14

6293

E)

1" 1

1-1/

2 N

PT

SP

LIT

LIN

E IN

CLA

MP

CO

LLA

R

1454

88A

B (4

1702

2)1"

RH

RO

TOR

SE

AL

4 S

CR

EW

S &

LO

CK

WA

SH

ER

S (P

AR

TS O

F 14

5488

AB

)00

0030

X02

07 (3

/8-1

6NC

X 1

.00

LG)

0000

31X

0006

LO

CK

WA

SH

ER

TO

RQ

UE

TO

28

FT.L

BS

.(LU

BE

D, S

EE

NO

TE 1

3)

1462

93E

(514

212)

29D

CB

CL/

BR

AS

SY

(STO

LLE

089

346)

RE

TAIN

ER

(8 R

EQ

D)

SN

AP

RIN

G (1

6 R

EQ

D)

SU

PP

LIE

D B

Y C

US

TOM

ER

0004

03X

0105

BIK

ON

LO

CK

ING

AS

SY

DO

BIK

ON

SE

RIE

S B

112

(120

X16

5)IN

STA

LL P

ER

NO

TE 9

7/8-

14U

NF

X 5

.00

LG G

RA

DE

-8 S

CR

EW

S16

RE

QD

, BY

CU

STO

ME

R (S

EE

NO

TE 1

4)

1211

10 9 87

65

4321

1413

0000

77X

0001

PIP

E P

LUG

(1/8

-27

NP

T)2

RE

QD

, 90°

APA

RT

AS

SE

MB

LE W

ITH

LOC

TITE

262

5133

59 F

LYW

HE

EL

BU

SH

ING

RIN

G

5133

61 B

RA

KE

RE

AC

TIO

N P

LATE

3085

54 B

US

HIN

G S

/A, 1

6 R

EQ

DIN

STA

LL P

ER

NO

TE 1

1

0003

42X

0620

(5/8

-18N

F X

4.5

0 LG

GR

8)

16 R

EQ

D, A

SS

EM

BLE

WIT

H L

OC

TITE

262

TO

RQ

UE

TO

156

FT.

LBS

.(LU

BE

D, S

EE

NO

TE 1

3)

SPA

CE

R R

ING

SU

PP

LIE

D B

Y C

US

TOM

ER

INS

TALL

SPA

CE

R R

ING

PE

R N

OTE

14

4159

06

CLA

MP

RIN

G B

Y C

US

TOM

ER

0003

82X

0041

RO

LL P

IN(.3

75 Ø

X 1

.000

LG

) 3 R

EQ

D

0001

45X

0002

GR

EA

SE

FIT

TIN

G (A

LEM

ITE

161

0-B

L)00

0145

X00

05 R

ELI

EF

FITT

ING

(ALE

MIT

E 4

7640

) 90

° C

LOC

KW

ISE

FR

OM

GR

EA

SE

FIT

TIN

GA

S V

IEW

ED

FR

OM

C/B

SID

E O

F FL

YW

HE

EL

3085

54 B

US

HIN

G S

/A, 1

6 R

EQ

DIN

STA

LL P

ER

NO

TE 1

2

0003

42X

0620

(5/8

-18N

F X

4.5

0 LG

GR

8)

16 R

EQ

D, A

SS

EM

BLE

WIT

H L

OC

TITE

262

TOR

QU

E T

O 1

56 F

T.LB

S.(L

UB

ED

, SE

E N

OTE

13)

NO

TE!

FOR

AP

PLI

CAT

ION

WIT

H D

IFFE

RE

NT

TIM

KE

N B

EA

RIN

GS

,S

EE

LA

-104

53-0

2

DE

SC

RIP

TIO

N

29D

CB

CL/

BR

AP

PL.

29D

CB

CL/

BR

AP

PL.

WIT

H

BU

SH

ING

RIN

G &

BU

SH

ING

S/A

1081

00A

1081

00

BU

SH

. RIN

G &

BU

SH

. S/A

NO

NE

1463

67

MAT

L LI

ST

SE

E N

OTE

16

---

---

EC

O. N

O.

LTR

.ZO

NE

CH

AN

GE

BY

& D

ATE

CH

KD

.

5177

4--

---

--R

ELE

AS

E5-

19-0

6--

--51

794

A1D

WA

S D

CB

1910

5TK

6-8

-06

SG

5184

9C

5BA

DD

ED

NO

TE #

17A

J 8/

25/0

6TC

K52

230

D7C

WA

S 1

4548

8K (4

1202

7)A

J 11

/5/0

7TC

K52

281

E3D

RE

VIS

ED

NO

TE #

7A

J 2/

25/0

8R

ST

0033

985

F7D

WA

S 3

0767

7 (2

PLA

CE

S)

AJ

8/14

/09

RS

0119

391

G1

---

RE

VIS

ED

AN

D R

ED

RAW

N

IN A

UTO

CA

DR

BA

1/28

/16

DC

29D

CB

CLU

TCH

/BR

AK

E A

PP

LIC

ATIO

NFO

R S

TAN

DU

N B

6 B

OD

YM

AK

ER

SE

E D

ETA

ILS

TCK

5-1

8-06

SG

5-1

9-06

TC

K

9918

53G

LA

-112

19S

HE

ET

NO

.

1 O

F 4

1/

4

SE

E T

AB

1) C

LUTC

H R

ATE

D T

OR

QU

E =

160

,000

LB

. IN

S. A

T 85

PS

IG (E

XA

CT

TOR

QU

E R

ATIN

G IS

D

EP

EN

DE

NT

UP

ON

AP

PLI

ED

AIR

PR

ES

SU

RE

AN

D O

PE

RAT

ING

SP

EE

D).

2) E

ATO

N W

AR

RA

NTI

ES

AR

E V

OID

IF T

HE

SE

SP

EC

IFIC

ATIO

NS

AR

E E

XC

EE

DE

D. E

ATO

N

A

CC

EP

TS N

O R

ES

PO

NS

IBIL

ITY

AN

D E

XTE

ND

S N

O W

AR

RA

NTY

UN

LES

S IT

HA

S A

PP

RO

VE

D

AN

Y VA

RIA

TIO

N IN

AD

VAN

CE

.3)

ALL

RO

TATI

NG

EQ

UIP

ME

NT

MU

ST

BE

PR

OTE

CTE

D T

O C

OM

PLY

WIT

H O

SH

A S

TAN

DA

RD

S.

4) W

HE

N R

EQ

UE

STI

NG

INFO

RM

ATIO

N, A

LWAY

S ID

EN

TIFY

TH

E A

PP

LIC

ATIO

N B

Y TH

IS

DR

AWIN

G N

UM

BE

R, M

ATE

RIA

L LI

ST

NU

MB

ER

, AN

D A

IRFL

EX

FIL

E N

UM

BE

R.

5) M

IN. R

EC

OM

ME

ND

ED

SH

AFT

MAT

ER

IAL

TO B

E S

AE

414

0/41

42 A

LLO

Y R

OU

ND

, HE

AT

TRE

ATE

D T

O 2

48-3

21 B

RIN

ELL

.6)

VE

ND

OR

PA

RT

NU

MB

ER

SH

OW

N M

AY B

E S

UB

STI

TUTE

D W

ITH

AN

EQ

UIV

ALE

NT

ALT

ER

NAT

E.

7) H

AN

D P

AC

K B

EA

RIN

GS

AN

D F

ILL

SE

AL

LIP

S ,F

LYW

HE

EL

GR

EA

SE

INLE

T H

OLE

, A

ND

AR

EA

S

MA

RK

ED

"X" W

ITH

MO

BIL

GR

EA

SE

XH

P 22

2 S

PE

CIA

L O

R E

QU

IVA

LEN

T AT

AS

SE

MB

LY.

FOLL

OW

-UP

BY

PU

MP

ING

1 O

Z. (A

PP

RO

X. 2

0 P

UM

PS

HA

ND

GR

EA

SE

GU

N) O

F G

RE

AS

E IN

TO

THE

FLY

WH

EE

L B

EA

RIN

G C

AVIT

Y. R

EM

OV

E E

XC

ES

S G

RE

AS

E. R

ELU

BR

ICAT

E W

EE

KLY

WIT

H 1

O

Z. O

F M

OB

ILG

RE

AS

E X

HP

222

SP

EC

IAL

OR

EQ

UIV

ALE

NT.

8) F

OR

INS

TALL

ATIO

N, O

PE

RAT

ION

AN

D M

AIN

TEN

AN

CE

, RE

QU

ES

T FO

RM

: DC

B 1

9106

.9)

SE

E IN

STA

LLAT

ION

INS

TRU

CTI

ON

S O

N S

HE

ET

2, 3

AN

D 4

.10

) PR

OC

ED

UR

E A

ND

PA

RTS

FO

R IN

STA

LLAT

ION

AN

D R

EM

OVA

L O

F 29

DC

B B

US

HIN

GS

FR

OM

B

US

HIN

G R

ING

AR

E S

UP

PLI

ED

WIT

H T

HE

BU

SH

ING

INS

TALL

ATIO

N A

ND

RE

MO

VAL

KIT

14

6220

XE

(IN

CLU

DE

D W

ITH

MAT

L LI

ST

#107

686D

).11

) PR

OC

ED

UR

E F

OR

INS

TALL

ATIO

N O

F 29

DC

B B

US

HIN

GS

INTO

TH

E F

LYW

HE

EL

BU

SH

ING

R

ING

513

359.

A

) A

PP

LY "N

EV

ER

-SE

EZ"

TO

TH

E IN

SID

ES

OF

THE

BU

SH

ING

CO

UN

TER

BO

RE

HO

LES

IN T

HE

FLY

WH

EE

L B

US

HIN

G R

ING

. B

) U

SIN

G A

ON

E IN

CH

DIA

ME

TER

SO

FT S

TEE

L R

OD

/BR

AS

S D

RIF

T, C

AR

EFU

LLY

TAP

T

HE

BU

SH

ING

S IN

TO T

HE

CO

UN

TER

BO

RE

D H

OLE

S O

F T

HE

FLY

WH

EE

L B

US

HIN

G

R

ING

, UN

TIL

THE

BU

SH

ING

S A

RE

FU

LLY

SE

ATE

D.

C)

AP

PLY

"NE

VE

R-S

EE

Z" T

O T

HE

FIR

ST

THR

EE

TO

FO

UR

TH

RE

AD

S A

ND

LO

CTI

TE 2

62

T

O T

HE

NE

XT

THR

EE

TO

FO

UR

TH

RE

AD

S O

F TH

E B

US

HIN

G M

OU

NTI

NG

SC

RE

WS

(00

0342

X06

20).

D)

INS

TALL

AN

D T

OR

QU

E T

O 1

56 F

T. L

BS

. TH

E A

BO

VE

BU

SH

ING

MO

UN

TIN

G S

CR

EW

S;

P

ER

FOR

M T

HIS

PR

OC

ED

UR

E O

NE

SC

RE

W A

T A

TIM

E.

12) P

RO

CE

DU

RE

FO

R IN

STA

LLAT

ION

OF

29D

CB

BU

SH

ING

S IN

TH

E B

RA

KE

RE

AC

TIO

N

B

RA

CK

ET

(513

361)

. A

) AP

PLY

"NE

VE

R-S

EE

Z" T

O T

HE

INS

IDE

S O

F TH

E B

US

HIN

G C

OU

NTE

RB

OR

E H

OLE

S IN

TH

E B

RA

KE

RE

AC

TIO

N P

LATE

. B

) IN

SE

RT

THE

BU

SH

ING

S IN

TO T

HE

CO

UN

TER

BO

RE

D H

OLE

S O

F TH

E

BR

AK

E R

EA

CTI

ON

PLA

TE, U

NTI

L TH

E B

US

HIN

GS

AR

E F

ULL

Y S

EAT

ED

. C

) AP

PLY

"NE

VE

R-S

EE

Z" T

O T

HE

FIR

ST

THR

EE

TO

FO

UR

TH

RE

AD

S A

ND

LO

CTI

TE 2

62

T

O T

HE

NE

XT

THR

EE

TO

FO

UR

TH

RE

AD

S O

F TH

E B

US

HIN

G M

OU

NTI

NG

SC

RE

WS

(000

342X

0620

). D

) IN

STA

LL A

ND

TO

RQ

UE

TO

156

FT.

LB

S. T

HE

AB

OV

E B

US

HIN

G M

OU

NTI

NG

SC

RE

WS

;

PE

RFO

RM

TH

IS P

RO

CE

DU

RE

ON

E S

CR

EW

AT

A TI

ME

. 13

) FO

R "L

UB

ED

" BO

LT, L

UB

RIC

ATE

FIR

ST

3-4

THR

EA

DS

WIT

H S

AE

30

OIL

, "N

EV

ER

-SE

EZ"

, OR

E

QU

IV. N

OTE

, WH

EN

US

ING

LO

CTI

TE W

ITH

"LU

BE

D" B

OLT

, LU

BR

ICAT

E F

IRS

T 3-

4 TH

RE

AD

S

AS

IND

ICAT

ED

, AN

D T

HA

N A

PP

LY L

OC

TITE

TO

NE

XT

3-4

THR

EA

DS

.14

) US

ING

A C

RO

SS

WIS

E P

ATTE

RN

, UN

IFO

RM

LY T

OR

QU

E 1

6 B

RA

KE

RE

AC

TIO

N P

LATE

S

CR

EW

S T

O 7

5 FT

. LB

S.(L

UB

ED

) TH

EN

, US

ING

A D

EP

TH M

ICR

OM

ETE

R T

HR

OU

GH

TH

E H

OLE

S

IN T

HE

BR

AK

E R

EA

CTI

ON

BR

AC

KE

T, M

EA

SU

RE

TH

E D

ISTA

NC

E "D

" FR

OM

TH

E O

UTE

R

SU

RFA

CE

OF

THE

BR

AK

E R

EA

CTI

ON

PLA

TE T

O T

HE

FA

CE

OF

THE

FLY

WH

EE

L B

EA

RIN

G

QU

ILL.

ME

AS

UR

E "T

",AV

ER

AG

E T

HE

NU

MB

ER

S.A

ND

SU

BTR

AC

T FR

OM

TH

E A

VE

RA

GE

OF

"D".

THIS

IS T

HE

SPA

CE

R R

ING

TH

ICK

NE

SS

(+.0

00/-.

001)

. G

RIN

D T

HE

SPA

CE

R R

ING

TO

PR

OP

ER

TH

ICK

NE

SS

.(RE

MO

VE

AP

PR

OX

IMAT

ELY

TH

E S

AM

E A

MO

UN

T O

F M

ATE

RIA

L FR

OM

BO

TH

SID

ES

OF

THE

SPA

CE

R R

ING

TO

OB

TAIN

TH

E P

RO

PE

R T

HIC

KN

ES

S).

RE

INS

TALL

BR

AK

E

RE

AC

TIO

N P

LATE

WIT

H T

HE

SPA

CE

R R

ING

IN P

LAC

E. U

SIN

G A

CR

OS

SW

ISE

PAT

TER

N,

UN

IFO

RM

LY T

OR

QU

E T

HE

7/8

-14

X 5

" LG

SC

RE

WS

(LU

BE

D) T

O 3

00 F

T.LB

S. T

HE

N R

EP

EAT

C

RO

SS

WIS

E P

ATTE

RN

TO

600

FT.

LB

S. I

NS

TALL

RE

TAIN

ER

S A

ND

SN

AP

RIN

GS

AFT

ER

P

RO

PE

R O

RIE

NTA

TIO

N O

F R

ETA

INE

RS

. TO

AC

HIE

VE

PR

OP

ER

OR

IEN

TATI

ON

FO

R

RE

TAIN

ER

S, V

AR

Y S

CR

EW

TO

RQ

UE

FR

OM

550

FT.

LB

S. T

O 6

50 F

T. L

BS

. MA

X.

15) A

LL P

AR

TS N

OT

IDE

NTI

FIE

D W

ITH

AIR

FLE

X P

AR

T N

O. &

SH

OW

N IN

PH

AN

TOM

AR

E

FUR

NIS

HE

D B

Y C

US

TOM

ER

.16

) AP

PLY

MO

LYB

DE

NU

M D

ISU

LFID

E G

RE

AS

E O

R E

QU

IVA

LEN

T TO

TH

E S

HA

FT F

OR

O

NLY

TH

IS L

EN

GTH

TO

PR

EV

EN

T FR

ETT

ING

BE

TWE

EN

TH

E H

UB

AN

D S

HA

FT.

17) T

O E

STA

BLI

SH

SPA

CE

R L

EN

GTH

SE

E S

K-1

394

OR

IOM

.

5.25

0

10.3

75

21.2

5 R

EF

.750

1.00

0 TY

P8.38

.250

3.50

5.87

5

4.63

.250

1.00

2.94

1.63

1.50

.75

1.30

24.

522

1.00

7.

45 6.75

0

9.25

1.75

4.784 4.782 SHAFT4.785 4.780 BORE

1.81

2 R

EF

8.00

0 R

EF

6.000 REF

10.000 9.999 QUILL

"T"

"D"

6.62

5 R

EF

13.0

00

RE

F

.967

.7

17

.562

1.

375

9.81

2

1.00

4.12

5.1

88.9

4

R.25

REF

Ø42.000

Ø41.600 P.D.

Ø35.750

8.500 B.C.

D

FF

E C

A

.XX

= ±

.X

XX

= ±

.0

10X

°=

±

0° 3

0 '

1.A

LL D

IME

NS

ION

S A

RE

IN IN

CH

ES

[mm

]2.

.010

- .0

20 B

RE

AK

ON

ED

GE

S A

ND

C

OR

NE

RS

.3.

MIC

RO

FIN

ISH

EATO

N C

OR

POR

ATIO

N -

CO

NFI

DEN

TIA

L A

ND

PR

OPR

IETA

RYN

OTI

CE

TO

PE

RS

ON

S R

EC

EIV

ING

TH

IS D

OC

UM

EN

T A

ND

/OR

TE

CH

NIC

AL

INFO

RM

ATIO

NTH

IS D

OC

UM

EN

T, IN

CLU

DIN

G T

HE

DR

AWIN

G A

ND

INFO

RM

ATIO

N C

ON

TAIN

ED

TH

ER

EO

N, I

S C

ON

FID

EN

TIA

L A

ND

IS

THE

EX

CLU

SIV

E P

RO

PE

RTY

OF

EAT

ON

CO

RP

OR

ATIO

N, A

ND

IS M

ER

ELY

ON

LO

AN

AN

D S

UB

JEC

T TO

RE

CA

LL B

Y E

ATO

N A

T A

NY

TIM

E. B

Y TA

KIN

G P

OS

SE

SS

ION

OF

THIS

DO

CU

ME

NT,

TH

E R

EC

IPIE

NT

AC

KN

OW

LED

GE

S A

ND

A

GR

EE

S T

HAT

TH

IS D

OC

UM

EN

T C

AN

NO

T B

E U

SE

D IN

AN

Y M

AN

NE

R A

DV

ER

SE

TO

TH

E IN

TER

ES

TS O

F E

ATO

N,

AN

D T

HAT

NO

PO

RTI

ON

OF

THIS

DO

CU

ME

NT

MAY

BE

CO

PIE

D O

R O

THE

RW

ISE

RE

PR

OD

UC

ED

WIT

HO

UT

THE

P

RIO

R W

RIT

TEN

CO

NS

EN

T O

F E

ATO

N. I

N T

HE

CA

SE

OF

CO

NFL

ICTI

NG

CO

NTR

AC

TUA

L P

RO

VIS

ION

S, T

HIS

NO

TIC

E

SH

ALL

GO

VE

RN

TH

E S

TATU

S O

F TH

IS D

OC

UM

EN

T.©

200

8 E

aton

Cor

pora

tion

- All

Rig

hts

Res

erve

d.

DO

NO

T S

CA

LE T

HIS

DR

AWIN

G

CR

ITIC

AL

CH

AR

AC

TER

ISTI

CS

100%

INS

PE

CTI

ON

BY

AIR

FLE

X

THIR

D A

NG

LE P

RO

JEC

TIO

N

UN

LESS

OTH

ERW

ISE

SPEC

IFIE

D:

TOLE

RA

NC

ES:

GEO

MET

RIC

SY

MB

OLS

PE

R A

SME

Y14.

5

MAT

'L.

CO

DE

SCA

LE:

CO

DE

IDEN

T.IT

EM C

LASS

SALE

S O

RD

ER N

O.

DR

AWIN

G N

O.

DR

AWN

:C

HEC

KED

:PE

:A

PPD

:

MA

KE

FRO

M:

MAT

ERIA

L:

NEX

TA

SSY.

MAT

'L.

LISTE

aton

Cor

pora

tion

Airf

lex

Div

isio

n99

19 C

linto

n R

oad

Cle

vela

nd, O

hio

4414

4®

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201620

DCB19106 clutch/brake application for Standun B6 bodymaker

"W"

"W"

C

11

IDEN

TIFI

CATI

ON C

HART

STEE

L STA

MP

INK

STAM

P

ELEC

TRO

CHEM

ETC

H

BAG

AND

TAG

ELEC

TRIC

PEN

CIL

B6

1/2

32

CD

7150

81CL

UTCH

, BRA

KE F

LYW

HEEL

PART

NO.

IDEN

TIFI

ER

TOLE

RA

NC

E U

NLE

SS

OTH

ER

WIS

ES

PE

CIF

IED

125

± 1/8

± 0°3

0'

±.000

5

±.005

± 1/32

±.010

MACH

INED

FINI

SHES

WEL

DMEN

TS

ANGL

ES

4 PLA

CE

3 PLA

CE

2 PLA

CE

FRAC

TION

S

QTY.

PER

DWG.

ASSY

.DW

G.

ITEM

NO.

SPAR

E C

ODE

ITEM

DES

CRIP

TION

STAN

DUN

PART

NO.

COMD

.CO

DEDW

G.SI

ZE

MACH

.SP

EC.

NEXT

ASS

Y.

REV.

DWG.

NO.

SHT.

O

FSC

ALE

SIZE

TITL

E

MACH

INE

MODE

L NO.

APPD

.

CHK.

DET.

DES.

BILLIN

GS

MART

LARO

MART

LARO

EATO

N06

-12-06

06-12

-06

06-12

-06

06-12

-06

STO

LLE

MAC

HINE

RY C

OM

PANY

, LLC

6

949

S. P

OTO

MAC

STR

EET

C

ENTE

NNIA

L, C

O 8

0112

CA

NFO

RM

ING

SY

STE

MS

R

STO

LLE

CMD

This

drawin

g and

all th

e info

rmati

on on

it is

the ex

clusiv

e prop

erty o

f Stol

le M

achin

ery.

The d

rawing

is co

nfide

ntial

and g

iven t

o you

for a

limite

d purp

ose d

eterm

ined b

y Stol

lein

its so

le dis

cretio

n. Th

e lim

ited p

urpos

e may

be re

voke

d by S

tolle

in its

sole

discre

tion

witho

ut no

tice t

o you

and t

he dr

awing

mus

t be r

eturne

d to S

tolle

on re

ques

t. You

do no

t hav

epe

rmiss

ion to

crea

te de

rivati

ve w

orks f

rom, c

opy,

distrib

ute, e

xhibi

t, furn

ish to

othe

rs or

reprod

uce t

he dr

awing

, any

part o

f the d

rawing

and a

ny in

forma

tion o

n the

draw

ing. Y

ou al

so do

not h

ave p

ermiss

ion to

take

photo

graph

s of a

ny ar

ticle

fabric

ated o

r ass

emble

d from

this

drawin

g.

6

REF

115161718

19

GNINETHGIT

WER

CS

20.000

SH

AFT

RE

F

Ø

4.72

44.

722

SPLI

T-LI

NE

CR

ANKS

HAF

T

REF

TOP

411

1413

12 10

98

76

53

2

1

RE

F2R

EF1R

EF

15

VIE

WA

-A

A A

1/2-

13 U

NC

TH

RU

(4) P

LAC

ES (L

IFTI

NG

HO

LES)

20

+.00

5-.0

00Ø

4.7

80P

ILO

T B

OR

E

RE

F

-13.

000

32.250

30.438

22.438

CR

ANKS

HAF

T

(CL

OCK

WISE

)

CR

ANK

REF

2 REF

0.18

8

BE

SU

RE

TO

FU

LLY

SE

AT T

HE

TO

OL

PLA

TE A

GA

INS

T TH

E E

ND

OF

THE

CLU

TCH

/BR

AK

E H

UB

AN

D C

RA

NK

SH

AFT

JO

UR

NA

L AT

TH

E F

OU

R P

OS

ITIO

NS

PR

OV

IDE

D. C

EN

TER

TH

E C

LUTC

H/B

RA

KE

UN

IT T

O T

HE

CR

AN

KS

HA

FT W

ITH

IN.0

05" O

R L

ES

S B

Y A

DJU

STI

NG

TH

E T

OO

LIN

G B

OLT

(ITE

M #

16) T

OR

QU

E A

ND

TOO

LIN

G P

LATE

MO

UN

TIN

G B

OLT

S (I

TEM

#17

) IN

CO

MB

INAT

ION

WIT

HC

LUTC

H/B

RA

KE

SU

PP

OR

T M

EC

HA

NIS

M IN

US

E. C

OM

PLE

TE T

IGH

TEN

ING

OF

(3) S

OC

KE

T H

EA

D C

AP

SC

RE

WS

5/8

-11U

NC

x 2

-1/2

" LO

NG

(ITE

M #

17) T

O

125

FT-L

BS

UP

ON

AC

HIE

VIN

G C

EN

TER

ING

SP

EC

IFIC

ATIO

N O

F "W

" DIM

INS

ION

VAR

IATI

ON

OF

.005

" OR

LE

SS

.

7. M

EA

SU

RE

TH

RO

UG

H S

LOT

PR

OV

IDE

D T

O D

ETE

RM

INE

DIS

TAN

CE

"W" B

ETW

EE

N

DO

NO

T R

ELI

EV

E L

IFTI

NG

SU

PP

OR

T.O

F TO

OLI

NG

PLA

TE (I

TEM

#15

). TI

GH

TEN

TO

OL

BO

LT (I

TEM

#16

) TO

45

FT-L

BS

6. IN

STA

LL C

LUTC

H/B

RA

KE

TO

OL

BO

LT (I

TEM

#16

) IN

CE

NTE

R T

HR

EA

DE

D H

OLE

3/4-

10 U

NC

x 2

-3/4

LO

NG

(ITE

M #

19) T

O 1

70 F

T-LB

S.

CLU

TCH

/BR

AK

E H

UB

(ITE

M #

1) B

Y TI

GH

TEN

ING

(4) S

OC

HE

AD

CA

P S

CR

EW

S4.

ATT

AC

H T

HE

TO

OL

PLA

TE (I

TEM

#15

) 741

043

TO T

HE

DE

VIC

E F

ITTE

D S

LIN

GS

OR

OTH

ER

EQ

UIV

ALE

NT

SU

PP

OR

TIN

G D

EV

ICE

,M

OU

NTE

D O

NTO

TH

E C

RA

NK

SH

AFT

DIA

. AS

SH

OW

N U

SIN

G O

VE

RH

EA

D L

IFTI

NG

5. IN

STA

LL C

LUTC

H/B

RA

KE

AS

SE

MB

LY W

ITH

LO

CK

ING

DE

VIC

E A

ND

TO

OL

PLA

TE

2 U

SE

INS

TALL

ATIO

N F

IXTU

RE

TO

OL

AS

SE

MB

LY 7

4104

2 FO

R F

OLL

OW

ING

PR

OC

ED

UR

ES

.

LUB

RIC

AN

TS IN

AN

Y LO

CK

ING

AS

SE

MB

LY IN

STA

LLAT

ION

.U

SE

MO

LYB

DE

NU

M D

ISU

LFID

E, E

.G. M

OLY

KO

TE, N

EV

ER

-SE

EZE

or S

IMIL

AR

THR

EA

DS

AN

D H

EA

D O

F S

OC

HE

AD

CA

P S

CR

EW

S. I

T IS

IMP

OR

TAN

T N

OT

TOS

HA

FT, H

UB

BO

RE

AN

D L

OC

KIN

G A

SS

EM

BLY

. MA

KE

SU

RE

TO

ALW

AYS

OIL

1. C

LEA

N A

ND

LIG

HTL

Y O

IL (D

.T.E

. LIG

HT

HY

D. O

IL IS

O V

G 3

2 or

EQ

UA

L)

NO

TES

: IN

STA

LLAT

ION

INS

TRU

CTI

ON

S F

OR

CLU

TCH

HU

B IT

EM

#1

AN

D

B'L

OC

LO

CK

ING

AS

SE

MB

LY IT

EM

#2.

3. IN

STA

LL L

OC

KIN

G A

SS

EM

BLY

(ITE

M #

2) IN

TO T

HE

Ø6-

1/2"

BO

RE

OF

THE

C

LUTC

H/B

RA

KE

HU

B (I

TEM

#1)

SE

ATIN

G L

OC

KIN

G A

SS

EM

BLY

ON

BO

RE

SH

OU

LDE

R

AS

SH

OW

N. I

T M

AY B

E N

EC

ES

SA

RY

TO S

EC

UR

E P

OS

ITIO

N O

F IN

NE

R W

ED

GE

D

UR

ING

TH

IS P

RO

CE

DU

RE

. UTI

LIZE

SC

RE

W P

OS

ITIO

NS

(VIE

W A

-A) 1

, 6, &

11

A

S J

AC

KIN

G S

CR

EW

S T

O H

OLD

INN

ER

WE

DG

E P

OS

ITIO

N. R

EM

OV

E T

HE

SE

BO

LTS

FR

OM

CU

RR

EN

T P

OS

ITIO

N A

ND

TH

RE

AD

TO

AP

PR

OP

RIA

TE D

EP

TH O

N A

DJA

CE

NT

H

OLE

S T

O S

EC

UR

E IN

NE

R W

ED

GE

.

x 2-

1/2"

LO

NG

(ITE

M #

17) T

O 3

0 FT

-LB

- D

O N

OT

RE

LIE

VE

LIF

TIN

G S

UP

PO

RT.

CR

AN

KS

HA

FT B

Y TI

GH

TEN

ING

(3) S

OC

KE

T H

EA

D C

AP

SC

RE

WS

5/8

-11U

NC

8. R

EM

OV

E S

LIN

GS

AN

D O

THE

R C

LUTC

H/B

RA

KE

UN

IT L

IFTI

NG

DE

VIC

ES

- R

EC

HE

CK

"W" D

IME

NS

ION

IN S

LOTS

TH

RO

UG

H T

OO

L P

LATE

(ITE

M #

15) F

OR

AN

Y M

OV

EM

EN

TFR

OM

CE

NTE

RIN

G S

PE

CIF

ICAT

ION

- R

EP

EAT

STE

P 7

IF M

OV

EM

EN

T IS

DE

TER

MIN

ED

.

INS

TALL

ATIO

N IN

STR

UC

TIO

NS

CO

NTI

NU

ED

ON

PA

GE

3 O

F 3.

23 22 211

SN73

0114

RELI

EF V

ALVE

, 3/4

MPT

,90

PSI

,.018

JET

CSE

E PN

EUM

ATIC

ASS

Y FO

R LO

CATI

ON

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 21

DCB19106 clutch/brake application for Standun B6 bodymaker

7818

0M

RMM

RM03

-18-

09RE

MO

VED

NAM

EPLA

TES

7300

14 &

272

141

C02

-02-

09G

REAS

E CA

LLO

UT M

OBI

L XH

P222

WAS

MO

BILI

TH A

W2

RPA

MRM

7723

8B

B

16) A

PPLY

MO

LYBD

ENU

M D

ISU

LFID

E G

REA

SE O

R E

QU

IVAL

ENT

TO T

HE

SHAF

T

FO

R O

NLY

TH

IS L

ENG

TH T

O P

REV

ENT

FRET

TIN

G B

ETW

EEN

TH

E H

UB

AND

SH

AFT.

15) A

LL P

ARTS

NO

T ID

ENTI

FIED

WIT

H A

IRFL

EX P

ART

NO

. &

SH

OW

N IN

PH

ANTO

M A

RE

FUR

NIS

HED

BY

CU

STO

MER

.

REF

REF

REF

REF

REF

REF

REF

REF

REF

REF

REF

REF

C

14) U

SIN

G A

CR

OSS

WIS

E PA

TTER

N, U

NIF

OR

MLY

TO

RQ

UE

16 B

RAK

E R

EAC

TIO

N P

LATE

S

CR

EWS

TO 7

5 FT

. LBS

.(LU

BED

) TH

EN, U

SIN

G A

DEP

TH M

ICR

OM

ETER

TH

RO

UG

H

TH

E H

OLE

S IN

TH

E BR

AKE

REA

CTI

ON

BR

ACKE

T, M

EASU

RE

THE

DIS

TAN

CE

"D"

F

RO

M T

HE

OU

TER

SU

RFA

CE

OF

THE

BRAK

E R

EAC

TIO

N P

LATE

TO

TH

E FA

CE

OF

THE

F

LYW

HEE

L BE

ARIN

G Q

UIL

L. M

EASU

RE

"T",A

VER

AGE

THE

NU

MBE

RS.

AND

SU

BTR

ACT

FRO

M

TH

E AV

ERAG

E O

F "D

". TH

IS IS

TH

E SP

ACER

RIN

G T

HIC

KNES

S (+

.000

/-.00

1).

G

RIN

D T

HE

SPAC

ER R

ING

TO

PR

OPE

R T

HIC

KNES

S.(R

EMO

VE A

PPR

OXI

MAT

ELY

13) F

OR

"LU

BED

" BO

LT, L

UBR

ICAT

E FI

RST

3-4

TH

REA

DS

WIT

H S

AE 3

0 O

IL,

"N

EVER

-SEE

Z", O

R E

QU

IV. N

OTE

, WH

EN U

SIN

G L

OC

TITE

WIT

H "L

UBE

D"

B

OLT

, LU

BRIC

ATE

FIR

ST 3

-4 T

HR

EAD

S AS

IND

ICAT

ED, A

ND

TH

EN A

PPLY

L

OC

TITE

TO

NEX

T 3-

4 TH

REA

DS.

10) P

RO

CED

UR

E AN

D P

ARTS

FO

R IN

STAL

LATI

ON

AN

D R

EMO

VAL

OF

29D

CB

BUSH

ING

S

FR

OM

BU

SHIN

G R

ING

AR

E SU

PPLI

ED W

ITH

TH

E BU

SHIN

G IN

STAL

LATI

ON

AN

D

REM

OVA

L KI

T 14

6220

XE (I

NC

LUD

ED W

ITH

MAT

L LI

ST #

1076

86D

).

B) IN

SER

T TH

E BU

SHIN

GS

INTO

TH

E C

OU

NTE

RBO

RED

HO

LES

OF

THE

BR

AKE

REA

CTI

ON

PLA

TE, U

NTI

L TH

E BU

SHIN

GS

ARE

FULL

Y SE

ATED

.

A) A

PPLY

"NEV

ER-S

EEZ"

TO

TH

E IN

SID

ES O

F TH

E BU

SHIN

G C

OU

NTE

RBO

RE

H

OLE

S IN

TH

E BR

AKE

REA

CTI

ON

PLA

TE.

12) P

RO

CED

UR

E FO

R IN

STAL

LATI

ON

OF

29D

CB

BUSH

ING

S IN

TH

E BR

AKE

REA

CTI

ON

B

RAC

KET

(513

361)

.

D) I

NST

ALL

AND

TO

RQ

UE

TO 1

56 F

T. L

BS. T

HE

ABO

VE B

USH

ING

MO

UN

TIN

G

SCR

EWS;

PER

FOR

M T

HIS

PR

OC

EDU

RE

ON

E SC

REW

AT

A TI

ME.

C) A

PPLY

"NEV

ER-S

EEZ"

TO

TH

E FI

RST

TH

REE

TO

FO

UR

TH

REA

DS

AND

LO

CTI

TE 2

62 T

O T

HE

NEX

T TH

REE

TO

FO

UR

TH

REA

DS

OF

THE

BU

SHIN

G M

OU

NTI

NG

SC

REW

S (0

0034

2X06

20).

B) U

SIN

G A

ON

E IN

CH

DIA

MET

ER S

OFT

STE

EL R

OD

/BR

ASS

DR

IFT,

CAR

EFU

LLY

TA

P TH

E BU

SHIN

GS

INTO

TH

E C

OU

NTE

RBO

RED

HO

LES

OF

THE

FLYW

HEE

L

BUSH

ING

RIN

G, U

NTI

L TH

E BU

SHIN

GS

ARE

FULL

Y SE

ATED

.

A) A

PPLY

"NEV

ER-S

EEZ"

TO

TH

E IN

SID

ES O

F TH

E BU

SHIN

G C

OU

NTE

RBO

RE

H

OLE

S IN

TH

E FL

YWH

EEL

BUSH

ING

RIN

G.

11) P

RO

CED

UR

E FO

R IN

STAL

LATI

ON

OF

29D

CB

BUSH

ING

S IN

TO T

HE

FLYW

HEE

L

BU

SHIN

G R

ING

513

359.

9) F

OR

INST

ALLA

TIO

N A

ND

REM

OVA

L IN

STR

UC

TIO

NS

SEE

SHEE

TS 2

AN

D 3

.8)

FO

R O

PER

ATIO

N A

ND

MAI

NTE

NAN

CE,

REQ

UES

T FO

RM

: DC

B 19

105.

7) H

AND

PAC

K BE

ARIN

GS

AND

FIL

L SE

AL L

IPS

,FLY

WH

EEL

GR

EASE

INLE

T H

OLE

,

AND

AR

EAS

MAR

KED

"X" W

ITH

MO

BIL

XHP2

22 G

REA

SE O

R E

QU

IVAL

ENT

AT A

SSEM

BLY.

FO

LLO

W-U

P BY

PU

MPI

NG

1 O

Z. (A

PPR

OXI

MAT

ELY

20 P

UM

PS H

AND

GR

EASE

GU

N)

O

F G

REA

SE IN

TO T

HE

FLYW

HEE

L BE

ARIN

G C

AVIT

Y. R

EMO

VE E

XCES

S G

REA

SE.

R

ELU

BRIC

ATE

WEE

KLY

WIT

H 1

OZ.

OF

EXXO

N M

OBI

L M

OBI

LGR

EASE

XH

P222

OR

EQ

UIV

ALEN

T.

6) V

END

OR

PAR

T N

UM

BER

SH

OW

N M

AY B

E SU

BSTI

TUTE

D W

ITH

AN

EQ

UIV

ALEN

T AL

TER

NAT

E.

5) M

IN. R

ECO

MM

END

ED S

HAF

T M

ATER

IAL

TO B

E SA

E 41

40/4

142

ALLO

Y R

OU

ND

, HEA

T

TREA

TED

TO

248

-321

BR

INEL

L.

4) W

HEN

REQ

UES

TIN

G IN

FOR

MAT

ION

, ALW

AYS

IDEN

TIFY

TH

E AP

PLIC

ATIO

N B

Y TH

IS

DR

AWIN

G N

UM

BER

, MAT

ERIA

L LI

ST N

UM

BER

, AN

D A

IRFL

EX F

ILE

NU

MBE

R.

3) A

LL R

OTA

TIN

G E

QU

IPM

ENT

MU

ST B

E PR

OTE

CTE

D T

O C

OM

PLY

WIT

H O

SHA

STAN

DAR

DS.

2) E

ATO

N W

ARR

ANTI

ES A

RE

VOID

IF T

HES

E SP

ECIF

ICAT

ION

S AR

E EX

CEE

DED

. EAT

ON

AC

CEP

TS N

O R

ESPO

NSI

BILI

TY A

ND

EXT

END

S N

O W

ARR

ANTY

UN

LESS

IT H

AS

APPR

OVE

D A

NY

VAR

IATI

ON

IN A

DVA

NC

E.

C) A

PPLY

"NEV

ER-S

EEZ"

TO

TH

E FI

RST

TH

REE

TO

FO

UR

TH

REA

DS

AND

LO

CTI

TE 2

62 T

O T

HE

NEX

T TH

REE

TO

FO

UR

TH

REA

DS

OF

THE

BU

SHIN

G M

OU

NTI

NG

SC

REW

S (0

0034

2X06

20).

D) I

NST

ALL

AND

TO

RQ

UE

TO 1

56 F

T. L

BS. T

HE

ABO

VE B

USH

ING

MO

UN

TIN

G

SCR

EWS;

PER

FOR

M T

HIS

PR

OC

EDU

RE

ON

E SC

REW

AT

A TI

ME.

1) C

LUTC

H R

ATED

TO

RQ

UE

= 16

0,00

0 LB

. IN

S. A

T 85

PSI

G (E

XAC

T TO

RQ

UE

RAT

ING

IS

DEP

END

ENT

UPO

N A

PPLI

ED A

IR P

RES

SUR

E AN

D O

PER

ATIN

G S

PEED

).

THE

SAM

E AM

OU

NT

OF

MAT

ERIA

L FR

OM

BO

TH S

IDES

OF

THE

SPAC

ER R

ING

TO O

BTAI

N T

HE

PRO

PER

TH

ICKN

ESS)

. REI

NST

ALL

BRAK

E R

EAC

TIO

N P

LATE

WIT

H T

HE

SPAC

ER R

ING

IN P

LAC

E. U

SIN

G A

CR

OSS

WIS

E PA

TTER

N,

UN

IFO

RM

LY T

OR

QU

E TH

E 7/

8-14

X 5

" LG

SC

REW

S (L

UBE

D) T

O 3

00 F

T.LB

S.TH

EN R

EPEA

T C

RO

SSW

ISE

PATT

ERN

TO

600

FT.

LBS

. IN

STAL

L R

ETAI

NER

SAN

D S

NAP

RIN

GS

AFTE

R P

RO

PER

OR

IEN

TATI

ON

OF

RET

AIN

ERS.

TO

AC

HIE

VEPR

OPE

R O

RIE

NTA

TIO

N F

OR

RET

AIN

ERS,

VAR

Y SC

REW

TO

RQ

UE

FRO

M55

0 FT

. LBS

. TO

650

FT.

LBS

. MAX

.

NO

TES

NO

TES:

BY E

ATO

N

SEE

"EAT

ON" D

RAW

ING

#L

A-11

219

REF

14

EATO

N AI

RFLE

X #

LA-1

1219

0949

5004

211

1AS

SY, L

OCK

ING

(BIK

ON)

2SE

AL, O

IL (S

HAFT

)3

SEAL

, AIR

4SE

AL, A

IR5

ASSY

, CL/

FRIC

. DIS

K6

ASSY

, BR/

FRIC

. DIS

C7

SPAC

ER R

ING

8SE

AL O

IL9

CUP,

TIM

KEN

11CO

NE, T

IMKE

N10

SPIR

OLO

X12

SPAC

ER, B

EARI

NG13

7150

6604

2108

8071

0421

0421

0421

0421

0421

0421

0421

0421

0421

0880

7208

8073

0880

7408

8075

7600

1708

8077

0949

5109

4952

0880

8009

4953

IDEN

TIFI

CATI

ON C

HART

STEE

L STA

MP

INK

STAM

P

ELEC

TRO

CHEM

ETC

H

BAG

AND

TAG

ELEC

TRIC

PEN

CIL

B6

1/4

31

CD

7150

81CL

UTCH

, BRA

KE F

LYW

HEEL

PART

NO.

IDEN

TIFI

ER

TOLE

RA

NC

E U

NLE

SS

OTH

ER

WIS

ES

PE

CIF

IED

125

± 1/8

± 0°3

0'

±.000

5

±.005

± 1/32

±.010

MACH

INED

FINI

SHES

WEL

DMEN

TS

ANGL

ES

4 PLA

CE

3 PLA

CE

2 PLA

CE

FRAC

TION

S

QTY.

PER

DWG.

ASSY

.DW

G.

ITEM

NO.

SPAR

E C

ODE

ITEM

DES

CRIP

TION

STAN

DUN

PART

NO.

COMD

.CO

DEDW

G.SI

ZE

MACH

.SP

EC.

NEXT

ASS

Y.

REV.

DWG.

NO.

SHT.

O

FSC

ALE

SIZE

TITL

E

MACH

INE

MODE

L NO.

APPD

.

CHK.

DET.

DES.

7410

43CL

UTCH

BRA

KE T

OO

L-PL

ATE

1674

1044

CLUT

CH B

RAKE

TO

OL-

BOLT

171808

0100

4040

SOC

HD C

AP SC

R 5/8

-11x2

-1/2 L

G

1908

5901

5240

HARD

ENED

WAS

HER

5/8 ID

x 1/8

THK

2008

0100

4230

SOC

HD C

AP SC

R 3/4

-10x2

-3/4 L

G08

5908

4127

HARD

ENED

WAS

HER

3/4 ID

x 1/4

THK

REF

REF

REF

REF

REF

06-12

-06EA

TON

MART

LARO

06-12

-06

06-12

-06MA

RTLA

RO

BILLIN

GS06

-12-06

A59

723

RAB

RAB

ADDE

D IT

EMS

# 21

, # 2

2, #

23

ON

SHEE

T 2

OF

3EC

N#DW

NAP

PDDE

SCRI

PTIO

NDA

TERE

V05

-27-

08

PART

S LI

ST C

ONT

INUE

D O

N PA

GE

2 O

F 3

STO

LLE

MAC

HINE

RY C

OM

PANY

, LLC

6

949

S. P

OTO

MAC

STR

EET

C

ENTE

NNIA

L, C

O 8

0112

CA

NFO

RM

ING

SY

STE

MS

R

STO

LLE

CMD

This

drawin

g and

all th

e info

rmati

on on

it is

the ex

clusiv

e prop

erty o

f Stol

le M

achin

ery.

The d

rawing

is co

nfide

ntial

and g

iven t

o you

for a

limite

d purp

ose d

eterm

ined b

y Stol

lein

its so

le dis

cretio

n. Th

e lim

ited p

urpos

e may

be re

voke

d by S

tolle

in its

sole

discre

tion

witho

ut no

tice t

o you

and t

he dr

awing

mus

t be r

eturne

d to S

tolle

on re

ques

t. You

do no

t hav

epe

rmiss

ion to

crea

te de

rivati

ve w

orks f

rom, c

opy,

distrib

ute, e

xhibi

t, furn

ish to

othe

rs or

reprod

uce t

he dr

awing

, any

part o

f the d

rawing

and a

ny in

forma

tion o

n the

draw

ing. Y

ou al

so do

not h

ave p

ermiss

ion to

take

photo

graph

s of a

ny ar

ticle

fabric

ated o

r ass

emble

d from

this

drawin

g.

1413

12 11 109

87

6543

21

14

MUF

FLER

0899

5504

21RE

F15

.125

MACH

INE

42.000 Ø

PAR

TIAL

EN

D V

IEW

SH

OW

ING

FLYW

HEE

L, B

USH

ING

MTG

RIN

G &

LOC

KIN

G A

SSY

(W/T

IGH

TEN

ING

SEQ

UEN

CE

FOR

LO

CKI

NG

ASS

Y SC

REW

S)

"T"

"D"

.250

1" R

H R

OTO

RSE

AL

4 SC

REW

S &

LOC

KWAS

HER

S3/

8-16

NC

X 1

.00

LGLO

CKW

ASH

ERTO

RQ

UE

TO 2

8 FT

.LBS

.LU

BED

, SEE

NO

TE 1

3

(4) 3

/4-1

0NC

x 3

.25

LG, G

R 8

(4) F

LAT

WAS

HER

ASSE

MBL

E W

ITH

LO

CTI

TE 2

62

AT F

INAL

ASS

YTO

RQ

UE

TO 1

10 F

T.LB

S.(L

UBE

D, S

EE N

OTE

13)

29D

CB

CL/

BR A

SSY

INST

ALL

PER

NO

TE 9

3/4-

10N

C X

4.5

0 LG

SC

R G

R 8

SAFE

TY W

ASH

ER16

REQ

D,

ASSE

MBL

E W

ITH

LO

CTI

TE 2

62TO

RQ

UE

TO 2

45 F

T.LB

S.(L

UBE

D, S

EE N

OTE

13)

7/8-

14 U

NF

x 5.

00 L

G G

R 8

16 R

EQD

(SEE

NO

TE 1

4)

DR

IV-L

OK

PIN

(Ø .3

75 x

1" L

G, T

YPE

"D")

INST

ALL

SPAC

ER R

ING

PE

R N

OTE

14

5/8-

18N

F X

4.50

LG

GR

816

REQ

D, A

SSEM

BLE

WIT

H L

OC

TITE

262

TOR

QU

E TO

156

FT.

LBS.

(LU

BED

, SEE

NO

TE 1

3)

BUSH

ING

S/A

, 16

REQ

DIN

STAL

L PE

R N

OTE

12

5/8-

18N

F X

4.50

LG

GR

816

REQ

D, A

SSEM

BLE

WIT

H L

OC

TITE

262

TOR

QU

E TO

156

FT.

LBS.

(LU

BED

, SEE

NO

TE 1

3)

BUSH

ING

S/A

, 16

REQ

DIN

STAL

L PE

R N

OTE

11

BRAK

E R

EAC

TIO

N P

LATE

1" 1

1-1/

2 N

PT

SEE

NO

TE 9

2 3 5 6 7

981011

1213

1

4

WHE

N TH

IS G

AP R

EDUC

ES T

O .0

10 (A

IR O

N)TH

E FR

ICTI

ON

DISC

IS F

ULLY

WO

RN A

ND M

UST

BE R

EPLA

CED

OR

SIG

NIFI

CANT

RED

UCTI

ON

IN T

ORQ

UE W

ILL

RESU

LT.

WA

RN

ING

!

W

HEN

THIS

GAP

RED

UCES

TO

.010

(AIR

OFF

)TH

E FR

ICTI

ON

DISC

IS F

ULLY

WO

RN A

ND M

UST

BE R

EPLA

CED

OR

SIG

NIFI

CANT

RED

UCTI

ON

IN T

ORQ

UE W

ILL

RESU

LT.

WA

RN

ING

!

INSE

RT .0

30 F

EELE

R BE

TWEE

N FR

ICTI

ON

DISC

ASS

EMBL

Y AN

D EN

D PL

ATE

OR

ROTO

R.IF

FEE

LER

WIL

L NO

T EN

TER

MEA

SURE

THIC

KNES

S O

F FR

ICTI

ON

DISC

ASS

EMBL

Y

(S

HOUL

D NO

T EX

CEED

.880

) RE

PLAC

E IF

REQ

UIRE

D.

LUBR

ICAT

E CY

LIND

ER S

URFA

CES

THAT

CO

NTAC

T SE

ALS

WIT

H A

LIG

HT C

OAT

OF

PARK

ER "O

" LUB

E(S

K-12

60-1

1)

HIG

H SP

RING

FO

RCE

MAY

CAU

SE P

ERSO

NAL

INJU

RY. R

EFER

TO

SK-

1350

FO

R PR

OPE

R A

SSEM

BLY

AND

DISA

SSEM

BLY

PRO

CEDU

RE.

WA

RN

ING

!

FLYW

HEEL

WEI

GHT

= 1

,670

lbs.

CLUT

CH/B

RAKE

ASS

Y W

EIGH

T = 85

0 lbs

.

REAC

TION

ASS

Y W

EIGH

T = 60

0 lbs

.

SPLI

T LI

NE

INC

LAM

P C

OLL

AR

FOR

MO

RE D

ETAI

LED

INFO

RMAT

ION

: S

EE M

AIN

BEAR

ING

ASS

EMBL

Y

21.25

00.0

00 C L

1 3/

4

SEE

NO

TE 1

6

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 201622

DCB19106 clutch/brake application for Standun B6 bodymaker

"W"

"W"

C

11

IDEN

TIFI

CATI

ON C

HART

STEE

L STA

MP

INK

STAM

P

ELEC

TRO

CHEM

ETC

H

BAG

AND

TAG

ELEC

TRIC

PEN

CIL

B6

1/2

32

CD

7150

81CL

UTCH

, BRA

KE F

LYW

HEEL

PART

NO.

IDEN

TIFI

ER

TOLE

RA

NC

E U

NLE

SS

OTH

ER

WIS

ES

PE

CIF

IED

125

± 1/8

± 0°3

0'

±.000

5

±.005

± 1/32

±.010

MACH

INED

FINI

SHES

WEL

DMEN

TS

ANGL

ES

4 PLA

CE

3 PLA

CE

2 PLA

CE

FRAC

TION

S

QTY.

PER

DWG.

ASSY

.DW

G.

ITEM

NO.

SPAR

E C

ODE

ITEM

DES

CRIP

TION

STAN

DUN

PART

NO.

COMD

.CO

DEDW

G.SI

ZE

MACH

.SP

EC.

NEXT

ASS

Y.

REV.

DWG.

NO.

SHT.

O

FSC

ALE

SIZE

TITL

E

MACH

INE

MODE

L NO.

APPD

.

CHK.

DET.

DES.

BILLIN

GS

MART

LARO

MART

LARO

EATO

N06

-12-06

06-12

-06

06-12

-06

06-12

-06

STO

LLE

MAC

HINE

RY C

OM

PANY

, LLC

6

949

S. P

OTO

MAC

STR

EET

C

ENTE

NNIA

L, C

O 8

0112

CA

NFO

RM

ING

SY

STE

MS

R

STO

LLE

CMD

This

drawin

g and

all th

e info

rmati

on on

it is

the ex

clusiv

e prop

erty o

f Stol

le M

achin

ery.

The d

rawing

is co

nfide

ntial

and g

iven t

o you

for a

limite

d purp

ose d

eterm

ined b

y Stol

lein

its so

le dis

cretio

n. Th

e lim

ited p

urpos

e may

be re

voke

d by S

tolle

in its

sole

discre

tion

witho

ut no

tice t

o you

and t

he dr

awing

mus

t be r

eturne

d to S

tolle

on re

ques

t. You

do no

t hav

epe

rmiss

ion to

crea

te de

rivati

ve w

orks f

rom, c

opy,

distrib

ute, e

xhibi

t, furn

ish to

othe

rs or

reprod

uce t

he dr

awing

, any

part o

f the d

rawing

and a

ny in

forma

tion o

n the

draw

ing. Y

ou al

so do

not h

ave p

ermiss

ion to

take

photo

graph

s of a

ny ar

ticle

fabric

ated o

r ass

emble

d from

this

drawin

g.

6

REF

115161718

19

GNINETHGITW

ERCS

20.000

SH

AFT

RE

F

Ø

4.72

44.

722

SPLI

T-LI

NE

CR

ANKS

HAF

T

REF

TOP

411

1413

12 10

98

76

53

2

1

RE

F2R

EF1R

EF

15

VIE

WA

-A

A A

1/2-

13 U

NC

TH

RU

(4) P

LAC

ES (L

IFTI

NG

HO

LES)

20

+.00

5-.0

00Ø

4.7

80P

ILO

T B

OR

E

RE

F

-13.

000

32.250

30.438

22.438

CR

ANKS

HAF

T

(C

L OCK

WISE )

CR

ANK

REF

2 REF

0.18

8

BE

SU

RE

TO

FU

LLY

SE

AT T

HE

TO

OL

PLA

TE A

GA

INS

T TH

E E

ND

OF

THE

CLU

TCH

/BR

AK

E H

UB

AN

D C

RA

NK

SH

AFT

JO

UR

NA

L AT

TH

E F

OU

R P

OS

ITIO

NS

PR

OV

IDE

D. C

EN

TER

TH

E C

LUTC

H/B

RA

KE

UN

IT T

O T

HE

CR

AN

KS

HA

FT W

ITH

IN.0

05" O

R L

ES

S B

Y A

DJU

STI

NG

TH

E T

OO

LIN

G B

OLT

(ITE

M #

16) T

OR

QU

E A

ND

TOO

LIN

G P

LATE

MO

UN

TIN

G B

OLT

S (I

TEM

#17

) IN

CO

MB

INAT

ION

WIT

HC

LUTC

H/B

RA

KE

SU

PP

OR

T M

EC

HA

NIS

M IN

US

E. C

OM

PLE

TE T

IGH

TEN

ING

OF

(3) S

OC

KE

T H

EA

D C

AP

SC

RE

WS

5/8

-11U

NC

x 2

-1/2

" LO

NG

(ITE

M #

17) T

O

125

FT-L

BS

UP

ON

AC

HIE

VIN

G C

EN

TER

ING

SP

EC

IFIC

ATIO

N O

F "W

" DIM

INS

ION

VAR

IATI

ON

OF

.005

" OR

LE

SS

.

7. M

EA

SU

RE

TH

RO

UG

H S

LOT

PR

OV

IDE

D T

O D

ETE

RM

INE

DIS

TAN

CE

"W" B

ETW

EE

N

DO

NO

T R

ELI

EV

E L

IFTI

NG

SU

PP

OR

T.O

F TO

OLI

NG

PLA

TE (I

TEM

#15

). TI

GH

TEN

TO

OL

BO

LT (I

TEM

#16

) TO

45

FT-L

BS

6. IN

STA

LL C

LUTC

H/B

RA

KE

TO

OL

BO

LT (I

TEM

#16

) IN

CE

NTE

R T

HR

EA

DE

D H

OLE

3/4-

10 U

NC

x 2

-3/4

LO

NG

(ITE

M #

19) T

O 1

70 F

T-LB

S.

CLU

TCH

/BR

AK

E H

UB

(ITE

M #

1) B

Y TI

GH

TEN

ING

(4) S

OC

HE

AD

CA

P S

CR

EW

S4.

ATT

AC

H T

HE

TO

OL

PLA

TE (I

TEM

#15

) 741

043

TO T

HE

DE

VIC

E F

ITTE

D S

LIN

GS

OR

OTH

ER

EQ

UIV

ALE

NT

SU

PP

OR

TIN

G D

EV

ICE

,M

OU

NTE

D O

NTO

TH

E C

RA

NK

SH

AFT

DIA

. AS

SH

OW

N U

SIN

G O

VE

RH

EA

D L

IFTI

NG

5. IN

STA

LL C

LUTC

H/B

RA

KE

AS

SE

MB

LY W

ITH

LO

CK

ING

DE

VIC

E A

ND

TO

OL

PLA

TE

2 U

SE

INS

TALL

ATIO

N F

IXTU

RE

TO

OL

AS

SE

MB

LY 7

4104

2 FO

R F

OLL

OW

ING

PR

OC

ED

UR

ES

.

LUB

RIC

AN

TS IN

AN

Y LO

CK

ING

AS

SE

MB

LY IN

STA

LLAT

ION

.U

SE

MO

LYB

DE

NU

M D

ISU

LFID

E, E

.G. M

OLY

KO

TE, N

EV

ER

-SE

EZE

or S

IMIL

AR

THR

EA

DS

AN

D H

EA

D O

F S

OC

HE

AD

CA

P S

CR

EW

S. I

T IS

IMP

OR

TAN

T N

OT

TOS

HA

FT, H

UB

BO

RE

AN

D L

OC

KIN

G A

SS

EM

BLY

. MA

KE

SU

RE

TO

ALW

AYS

OIL

1. C

LEA

N A

ND

LIG

HTL

Y O

IL (D

.T.E

. LIG

HT

HY

D. O

IL IS

O V

G 3

2 or

EQ

UA

L)

NO

TES

: IN

STA

LLAT

ION

INS

TRU

CTI

ON

S F

OR

CLU

TCH

HU

B IT

EM

#1

AN

D

B'L

OC

LO

CK

ING

AS

SE

MB

LY IT

EM

#2.

3. IN

STA

LL L

OC

KIN

G A

SS

EM

BLY

(ITE

M #

2) IN

TO T

HE

Ø6-

1/2"

BO

RE

OF

THE

C

LUTC

H/B

RA

KE

HU

B (I

TEM

#1)

SE

ATIN

G L

OC

KIN

G A

SS

EM

BLY

ON

BO

RE

SH

OU

LDE

R

AS

SH

OW

N. I

T M

AY B

E N

EC

ES

SA

RY

TO S

EC

UR

E P

OS

ITIO

N O

F IN

NE

R W

ED

GE

D

UR

ING

TH

IS P

RO

CE

DU

RE

. UTI

LIZE

SC

RE

W P

OS

ITIO

NS

(VIE

W A

-A) 1

, 6, &

11

A

S J

AC

KIN

G S

CR

EW

S T

O H

OLD

INN

ER

WE

DG

E P

OS

ITIO

N. R

EM

OV

E T

HE

SE

BO

LTS

FR

OM

CU

RR

EN

T P

OS

ITIO

N A

ND

TH

RE

AD

TO

AP

PR

OP

RIA

TE D

EP

TH O

N A

DJA

CE

NT

H

OLE

S T

O S

EC

UR

E IN

NE

R W

ED

GE

.

x 2-

1/2"

LO

NG

(ITE

M #

17) T

O 3

0 FT

-LB

- D

O N

OT

RE

LIE

VE

LIF

TIN

G S

UP

PO

RT.

CR

AN

KS

HA

FT B

Y TI

GH

TEN

ING

(3) S

OC

KE

T H

EA

D C

AP

SC

RE

WS

5/8

-11U

NC

8. R

EM

OV

E S

LIN

GS

AN

D O

THE

R C

LUTC

H/B

RA

KE

UN

IT L

IFTI

NG

DE

VIC

ES

- R

EC

HE

CK

"W" D

IME

NS

ION

IN S

LOTS

TH

RO

UG

H T

OO

L P

LATE

(ITE

M #

15) F

OR

AN

Y M

OV

EM

EN

TFR

OM

CE

NTE

RIN

G S

PE

CIF

ICAT

ION

- R

EP

EAT

STE

P 7

IF M

OV

EM

EN

T IS

DE

TER

MIN

ED

.

INS

TALL

ATIO

N IN

STR

UC

TIO

NS

CO

NTI

NU

ED

ON

PA

GE

3 O

F 3.

23 22 211

SN73

0114

RELI

EF V

ALVE

, 3/4

MPT

,90

PSI

,.018

JET

CSE

E PN

EUM

ATIC

ASS

Y FO

R LO

CATI

ON

EATON Airflex DCB19106 Installation, Operation and Maintenance Manual E-CLCL-II013-E February 2016 23

© 2016 Eaton All Rights Reserved Printed in USA Document No. E-CLCL-II013-E February 2016

EatonHydraulics Group USAAirflex Products9919 Clinton RoadCleveland, Ohio 44144USATel: 216-281-2211Fax: 216-281-3890www.eaton.com/airflex

EatonEaton Hydraulics Group ChinaAirflex Products281 Fa Sai RoadWaiGaoQiao Free Trade ZoneShanghai 200131ChinaTel: (+86 21) 5048 4811Fax: (+86 21) 5048 4911