structural analysis terex demax latice crane
TRANSCRIPT
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
1/163
CC 8800-1
Structural Analysis
CC 8800-1
HSSL 60.0 m
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
2/163
CC 8800-1
1. Explanation of analysis method
A FORTRAN program system is used for the static calculation of the boo
A pre-processor program generates a finite element model of the cran
generates automatically the load cases and loads in accordance with DIN
The finite element program STAB88 (Technical University Munich)
forces, inner moments and the deflection in compliance with the geome
(equilibrium at the deformed system).
A post-processor program accesses on the STAB88 output and perform
analysis and the verification of stability.
2. Standards and specifications used
[1] DIN 15018 part 3
[2] DIN 18800, part 2, State of consultation November 1990
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
3/163
CC 8800-1
3. Design loads
The loads acting on the structure are subdivided into main loads, additio
loads.
Main loads are:
- self weigths
- lifted loads
- dynamic effects arising from lifting and lowering
- inertia forces arising from drives
Additional loads are:
- wind loads
Special loads are:
- test loads
The above loads are grouped into load cases. For the calculation in
geometric non-linear theory, the loads are multiplied by the pa(DIN 15018 part 3 table 5).
Loads partial safety factors
Load case H Load case HZ
Self weigths 1,20 1.09
Liftet loads 1.35 1.20
Test loads - -
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
4/163
CC 8800-1
4. General stress analysis
The general stress analysis against attaining the yield strength shall be ac
the load cases, in order to demonstrate that the limiting stresses in accord
part 3 will not be exceeded under the action of the loads multiplied
factors.
5. Verification of Stability
The verification of the required safety against buckling for chord an
according to DIN 15018, part 3 [1], by using the buckling curve acco
part 2 [2].
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
5/163
CC 8800-1
6. Example
The calculation was made for the boom length 60 m. The load causes a m
deflection, stress and buckling.
Radius [m] Lifting capacity [t]
10 1541
Load case H
10 1541
Load case HZ
10 1541Load case HZ1 (rated load)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
6/163
CC 8800-1
Appendix A
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
7/163
CC 8800-1
BEAM NUMBERS
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
8/163
CC 8800-1
BOOM HEAD (BEAM NUMBERS)
BOOM FOOT (BEAM NUMBERS)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
9/163
CC 8800-1
NODE NUMBERS
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
10/163
CC 8800-1
BOOM HEAD (NODE NUMBERS)
BOOM FOOT (NODE NUMBERS)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
11/163
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
12/163
CC 8800-1
PRESTAB_V6, Version V5.5h 22.11.2007:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
: load control part 1 * 5.12.2007 8:51:56 *** 57545:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CC 8800-1 Projekt SSL 60 s_mr2615.09.2006 Zimmer
Control output of the variable input------------------------------------------1. radius = 9.82. loadcase =
3. rated load = 1541.04. reeving = 5. number of hoist lines back to the winch = 6. loads mass(n): ----------------------
node no. Radius[m] ----------------------
32 -24.000 Control output of the non variable input-----------------------------1. maximum torque = 480.02. minimum time of deceleration = 5.03. number of revolutions = 0.34. hoisting speed = 72.05. hoisting class = 6. node number of load = 7. windpressure on load = 60.08. counterweight = 220.09. distance between rotation axis/counterweight = 900.010.weight of superstructure = 36.811.distance between rotation axis/superstructure = 120.012.lateral inclination of boom system = 0.313.weight of hoist rope = 7.8
14.Guidance of hoist rope..........node numbers : 14, 13, 18, 26, 36
15.load factors : -----------------------------------load- | loads :case | dead lifted test a
-----------------------------------H | 1.20 1.35 0.00 1HZ | 1.09 1.20 0.00 1HS | 1.09 0.00 1.09 1HZ*1 | 1.00 1.00 0.00 1-----------------------------------
Control output of the results
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
13/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 2 * 5.12.2007 8:51:56 *** 57545
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
node masss and node loads / loadcase H--------------------------------------------------
node masss node loads---------------- -----------------------------
node - boom - lifted vertical horizontalno. loads acceleration
system Y X Z
-----------------------------------------------------------[t] [t] [kN] [kN] [kN]
===========================================================1 8.350 -- -98.88 6.75 0.04 02 13.000 -- -153.94 10.50 0.07 03 0.000 -- 0.00 0.00 0.00 04 0.000 -- 0.00 0.00 0.00 05 11.400 -- -134.99 9.21 0.07 06 16.550 -- -195.98 13.37 0.11 07 19.050 -- -225.58 15.39 0.16 0
8 14.150 -- -167.56 11.43 0.15 09 9.800 -- -116.05 7.92 0.11 0
10 13.600 -- -161.05 10.99 0.17 011 12.700 -- -150.39 10.26 0.19 012 5.700 -- -68.75 3.11 0.09 013 3.545 -- -44.41 0.58 0.04 014 23.822 1541.00 -21784.90 0.00 29.41 015 5.500 -- -67.19 -3.72 0.01 016 16.550 -- -202.66 -4.54 -0.08 017 4.400 -- -54.76 1.97 -0.03 0
18 1.150 -- -13.53 0.93 -0.01 019 10.330 -- -126.19 -6.99 -0.07 020 9.660 -- -118.00 -6.53 -0.19 021 7.730 -- -94.43 -5.23 -0.25 022 4.300 -- -52.53 -2.91 -0.18 023 6.800 -- -82.83 -0.80 -0.30 024 3.000 -- -36.70 -1.75 -0.14 025 2.000 -- -23.55 1.62 -0.09 026 2.000 -- -25.07 -0.53 -0.09 027 0.250 -- -3.11 0.11 -0.01 028 8.979 -- -108.36 -4.79 -0.45 029 5.500 -- -67.96 -3.07 -0.07 030 8.266 -- -101.29 -5.17 -0.23 031 0.000 -- 0.00 0.00 0.00 032 3.483 640.00 -6317.40 -2.82 -29.50 033 0.464 -- -5.64 -0.33 -0.01 034 0.000 -- 0.00 0.00 0.00 0
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
14/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 3 * 5.12.2007 8:51:56 *** 57545
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CW-Value 1.60 [/]
beam- node- angle length weight windareano. numbers t.horiz
-----------------------------------------------------------[degr] [cm] [t] [qm/lfm]
===========================================================1 1 2 84.79 400.0 16.700 2.018
2 5 6 84.79 375.0 13.500 2.0833 2 3 174.79 137.5 0.000 0.0004 2 4 165.77 159.5 0.000 0.0005 2 5 84.79 225.0 9.300 2.2066 6 7 84.79 1200.0 19.600 1.9527 7 8 84.79 1200.0 18.500 1.9568 8 9 84.79 600.0 9.800 2.1029 9 10 84.79 600.0 9.800 2.10210 10 11 84.79 1200.0 17.400 1.95211 11 12 84.79 200.0 8.000 1.500
12 12 13 174.79 180.0 3.400 0.00013 12 14 -5.21 190.0 0.000 0.00014 15 16 123.50 685.0 11.000 1.25015 16 19 123.50 215.0 11.000 1.44016 16 17 -146.50 138.5 8.800 0.00017 16 18 89.95 114.0 2.300 0.00018 19 20 123.50 1200.0 9.660 1.43119 20 21 123.50 1200.0 9.660 1.43120 21 22 123.50 800.0 5.800 1.49021 22 23 123.50 274.0 2.800 1.505
22 23 24 123.50 416.0 2.800 1.23023 24 28 123.50 210.0 2.700 0.60024 23 25 89.37 125.6 4.000 0.00025 23 26 161.07 131.2 4.000 0.00026 24 27 -146.50 65.0 0.500 0.00027 29 30 136.49 1165.0 11.000 1.00028 31 32 -180.00 1300.0 0.000 0.00029 13 28 -151.93 3689.6 3.689 0.35030 30 33 -62.01 1031.4 0.928 0.35031 28 30 -70.94 3540.5 4.603 0.35032 28 32 -86.83 4337.9 6.966 0.45033 3 34 -124.53 387.0 0.000 0.00034 17 35 -99.46 495.5 0.000 0.000
===========================================================SUM : 228.206
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
15/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 4 * 5.12.2007 8:51:56 *** 57545
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
results of basic load determination :node loads without factors in STAB84-global-components
node loads in [ kN ] :no. node mass beam mass acceleration forces
Y Y Y X Z -----------------------------------------------------------1 0.00 -81.89 -0.410 4.497 0.018 0
2 0.00 -127.49 -0.638 7.001 0.032 03 0.00 0.00 0.000 0.000 0.000 04 0.00 0.00 0.000 0.000 0.000 05 0.00 -111.80 -0.560 6.140 0.030 06 0.00 -162.30 -0.813 8.913 0.048 07 0.00 -186.82 -0.935 10.260 0.073 08 0.00 -138.76 -0.695 7.621 0.067 09 0.00 -96.11 -0.481 5.278 0.051 010 0.00 -133.37 -0.668 7.325 0.077 011 0.00 -124.54 -0.624 6.840 0.084 0
12 0.00 -55.90 -1.112 2.071 0.038 013 0.00 -34.76 -1.796 0.386 0.019 014 0.00 -233.61 0.000 0.000 13.072 015 0.00 -53.94 -1.642 -2.480 0.006 016 0.00 -162.30 -5.268 -3.025 -0.036 017 0.00 -43.15 -1.984 1.313 -0.014 018 0.00 -11.28 -0.001 0.622 -0.003 019 0.00 -101.30 -3.084 -4.658 -0.033 020 0.00 -94.73 -2.884 -4.356 -0.085 021 0.00 -75.81 -2.308 -3.486 -0.112 0
22 0.00 -42.17 -1.284 -1.939 -0.078 023 0.00 -66.69 -1.871 -0.532 -0.132 024 0.00 -29.42 -0.934 -1.165 -0.064 025 0.00 -19.61 -0.012 1.082 -0.039 026 0.00 -19.61 -1.023 -0.351 -0.041 027 0.00 -2.45 -0.113 0.075 -0.005 028 0.00 -88.06 -1.794 -3.196 -0.201 029 0.00 -53.94 -2.157 -2.048 -0.030 030 0.00 -81.06 -2.681 -3.446 -0.104 031 0.00 0.00 0.000 0.000 0.000 032 0.00 -34.16 -0.104 -1.881 -13.112 033 0.00 -4.55 -0.118 -0.222 -0.004 034 0.00 0.00 0.000 0.000 0.000 035 0.00 0.00 0.000 0.000 0.000 0
-----------------------------------------------------------SUM : 0.00 -2471.55 -37.991 36.638 -0.282 0
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
16/163
CC 8800-1
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %
% E I N Z E L S T A B - A N A L Y S I S %% =================================== %% ( 5.12.2007 8:51:57) %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% CC 8800-1 Projekt SSL 60 s_mr26 %% 15.09.2006 Zimmer %% **************************************** %% E I N G A B E K O N T R O L L E : %% crane part 4 declin. 180.000 [deg]%
% crane part 2 radius -26.400 [m] %% crane part 1 radius 9.840 [m] %% loadcase H nom. load 1541.000 [t] %% reeving 25 %% node num. 32 add. mass 640.000 [t] %% **************************************** %% F R E I E T E X T E I N G A B E : %% variante 1 , superlift %% **************************************** %% * 5.12.2007 8:51:56 *** 575457564857 * %
% %%%%%%%%%%%% Version 5.0g vom 18.06.2007 %%%%
number of beams 34number of nodes 35
beam node length Ndiag section no. sectionnumber KA KE (cm) Stab84 Einzel
( 1) 1 2 399.99 2 1 1 tapered( 2) 5 6 374.99 2 2 2 standar( 3) 2 3 137.50 0 3 0 -------( 4) 2 4 159.47 0 4 0 -------( 5) 2 5 224.99 1 5 3 standar( 6) 6 7 1199.98 7 6 4 standar( 7) 7 8 1200.00 7 7 5 standar( 8) 8 9 600.01 4 8 6 standar( 9) 9 10 600.02 4 9 6 standar( 10) 10 11 1200.07 7 10 7 standar( 11) 11 12 200.01 0 11 0 -------( 12) 12 13 180.00 0 12 0 -------( 13) 12 14 190.00 0 13 0 -------( 14) 15 16 684.99 6 14 8 tapered( 15) 16 19 215.00 1 15 9 standar( 16) 16 17 138.50 0 16 0 -------( 17) 16 18 113.99 0 17 0 -------
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
17/163
CC 8800-1
SECTION PROPERTIES=================================
section type : standard lattice mast [cm,kN]=====================================
( 2) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 3.75m paral. Teil Nr.2 R2
LV LW field length cantilev-A cantil275.0 320.0 330.3 0.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 3) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 2.25m paral. Teil Nr.1 R2
LV LW field length cantilev-A cantil
275.0 320.0 441.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 4) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-45-12CC8800-1 16.03.2006 W.Zim. Projekt ZW 12m 3227-45 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 5) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-40-12
CC8800-1 12.9.2006 W.Zim. Entwurf ZW 12m 3227-40 3.5 FelderLV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.00 29.85*4.00 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
18/163
CC 8800-1
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62area 296.88 296.88 38.08 42.
----------------------------------------------------------( 9) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 5.90 paralleler Teil 2621
LV LW field length cantilev-A cantil
210.0 260.0 421.4 0.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 10) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-30-12CC8800-1 08.12.2005 W.Zim. ZW 12m 2621-30 4 Felder 2621-30
LV LW field length cantilev-A cantil210.0 260.0 281.8 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 11) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-22-80
CC8800-1 08.12.2005 W.Zim. ZW 8m 2621-22.2 3.0 Felder 2621-2LV LW field length cantilev-A cantil210.0 260.0 245.0 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41area 137.32 137.32 20.11 20.
----------------------------------------------------------
( 12) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze paralleler Teil 2.75m
LV LW field length cantilev-A cantil210.0 260.0 244.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
19/163
CC 8800-1
section type : tapered part (o.ae.) [cm,kN]========================================
( 1) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-foot 4.0m konischer Teil R298.
LVA LVE LWA LWE field length cantil35.0 275.0 320.0 320.0 345.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62
area 358.38 358.38 38.08 42.
----------------------------------------------------------( 8) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 4.6m konischer Teil 2621-
LVA LVE LWA LWE field length cantil14.0 210.0 260.0 260.0 215.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 13) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze 4.16m 2.0 Feld 2621-22
LVA LVE LWA LWE field length cantil210.0 86.4 260.0 185.0 203.8 0.0
upp. chord low. chord upp. diags low. dia
pipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41
area 137.32 137.32 20.11 20.
----------------------------------------------------------
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
20/163
CC 8800-1
NODE DISPLACEMENTS :======================
NODE X Y ZNUMBER (CM) (CM) (CM)
( 1) 0.00 0.00 0.00( 2) -1.32 -0.34 8.24( 3) -1.34 -0.50 7.81( 4) -1.42 -0.73 8.29( 5) -2.22 -0.54 13.55( 6) -3.67 -0.91 23.49
( 7) -7.06 -2.52 63.85( 8) -6.31 -5.31 116.43( 9) -3.42 -7.30 146.81( 10) 1.72 -9.70 179.41( 11) 19.93 -15.70 248.59( 12) 26.09 -18.57 263.23( 13) 26.95 -13.48 250.67( 14) 18.55 -56.45 276.38( 15) 0.00 0.00 0.00( 16) 6.42 3.81 1.33
( 17) 5.77 4.82 1.30( 18) 7.23 3.82 1.62( 19) 7.74 4.52 2.07( 20) 12.77 6.93 9.25( 21) 15.48 7.71 20.76( 22) 16.58 7.52 30.28( 23) 16.84 7.37 33.78( 24) 17.30 7.26 39.23( 25) 16.92 7.34 35.03( 26) 16.73 6.93 35.02
( 27) 17.27 7.29 39.23( 28) 17.56 7.22 42.01( 29) 0.00 0.00 0.00( 30) 1.49 1.54 0.46( 31) 0.00 0.00 0.00( 32) -0.10 0.11 4.84( 33) 0.00 0.00 0.00( 34) 0.00 0.00 0.00( 35) 0.00 0.00 0.00
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
21/163
CC 8800-1
BEARING FORCES=================================================
node X (KN) Y (KN) number XX (KN*cm) YY (KN*cm)
( 1) 2494.3242 25012.6895 -6509702.0000 803591.8750
( 15) -4077.6113 4999.9277 -791196.2500 -509034.4062
( 29) -95.7696 162.1747 -5868.1787 -6159.3008
( 31) 301.4645 0.2236 -5.2385 -47062.4336
( 33) 298.2805 -557.6107 0.0000 0.0000
( 34) 452.0176 659.8839
0.0000 0.0000
( 35) 139.1291 787.8088 0.0000 0.0000
INNER FORCES AND MOMENTS=========================================
1) foot main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 1) -25035.67 -230404.25 309.43 6555095.00 -6421351.00 0.00 -1
( 2) -25443.28 -234405.33 757.22
6326841.00 -6140894.00 231140.98 -5
( 3) -391.09 0.00 -697.83 -851.65 -0.66 95950.82
( 4) 0.00 0.00 0.01 -0.77 -0.77 -0.51
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
22/163
CC 8800-1
( 8) -24836.33 -236926.42 589.20 3975367.00 -3199237.50 2366885.50 -27
( 9) -24716.30 -238535.81 501.46 3184231.75 -2331916.75 2737382.25 -30
( 10) -24552.85 -237034.14 346.86 2307841.00 -470284.78 3056413.75 -34
3) head main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 11) -24383.05 -285642.66 -79.51 421996.28 -40571.57 3474981.00 -34
( 12) 1889.73 0.19 2835.33 23342.01 -0.38 -510652.62
( 13) 5456.94 -19.31 -20888.77
227508.97 -40.34 3975483.50
4) Superliftmast=============
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 14) -6358.04 -2038.80 -750.11 940806.50 -847418.00 0.00 5
( 15) -8207.62 -454.73 219.91 842313.56 -820891.25 -546264.31 4
( 16) -517.65 0.00 -537.85 -872.10 0.05 74489.03
( 17) 1529.93 0.00 366.16 5983.04 -0.02 -41743.02
( 18) -8104.84 -121.66 163.74 820925.19 -658855.75 -499002.78 3
( 19) -8008.11 764.09 112.28 658832.25 -420946.81 -302664.25 1
( 20) -7930.78 1229.13 65.62
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
23/163
CC 8800-1
( 26) 1.62 0.00 2.66 2.72 0.01 -172.75
5) A-frame========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 27) -136.51 0.00 0.00 8507.31 -0.06 0.00
6) misc. parts==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 28) 301.60 0.02 0.00 47063.55 2.43 0.00
( 33) -800.00 0.00 0.00
0.00 0.00 0.00
( 34) -800.00 0.00 0.00 0.00 0.00 0.00
7) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 30) 637.21 0.00 0.00 0.00 0.00 0.00
( 32) 5844.22 0.00 0.00 0.00 0.00 0.00
8) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 29) 3281.79 0.00 0.00 0.00 0.00 0.00
( 31) 602.51 0.00 0.00
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
24/163
CC 8800-1
G E N E R A L S T R E S S - A N A L Y S I S===================================================
stress = force in pipe/areasafety = stress/calculated stress limit
safety = 88.888 --> force in pipe = 0.00 or pressursafety = 99.999 --> safety > 100.0
stresses [KN/cm**2] and safeties (section type
===============================================
beam upper chord | upper chord | lower chord (min) | (max) | (min)
| | 1 -44.24 1.363 | 9.19 6.565 | -50.44 1.196 2 -44.33 1.360 | 11.27 5.350 | -47.87 1.260 5 -45.89 1.314 | 10.28 5.865 | -47.89 1.259 6 -41.55 1.451 | 11.90 5.065 | -50.23 1.201 7 -35.83 1.759 | 14.41 4.373 | -54.41 1.158
8 -26.95 2.337 | 14.29 4.408 | -57.49 1.096 9 -20.34 3.098 | 12.42 5.071 | -55.43 1.137
10 -13.43 4.692 | 9.69 6.500 | -52.72 1.195 14 -14.04 4.167 | 7.36 7.951 | -25.13 2.328 15 -13.87 4.218 | 4.67 12.539 | -27.70 2.112 18 -14.51 4.032 | 3.95 14.828 | -26.68 2.192 19 -14.51 4.032 | -0.38 99.999 | -22.07 2.650 20 -17.55 3.590 | -6.05 10.418 | -22.81 2.762 21 -15.60 4.040 | -9.63 6.544 | -19.07 3.303 22 -14.04 4.486 | -9.90 6.367 | -12.50 5.041
beam diagonals | diagonals | diagonalsupper(min) | lower (min) | vertical(min)
| |1 2.81 22.121 | -6.86 9.053 | -5.49 11.3212 -3.38 18.365 | -16.16 3.843 | -24.64 2.5205 4.96 12.513 | 16.33 3.802 | 1.73 35.8216 0.00 99.999 | -18.79 3.304 | -24.15 2.5717 -5.00 12.424 | -23.28 2.667 | -23.13 2.6858 -7.99 7.774 | -25.66 2.420 | -20.96 2.963
9 -9.72 6.388 | -27.33 2.272 | -19.77 3.14110 -11.76 5.279 | -29.69 2.091 | -18.23 3.40614 -3.71 11.153 | -3.67 11.292 | -5.35 7.74515 3.12 13.254 | -3.02 13.717 | -3.28 12.61218 -3.85 10.745 | -3.83 10.818 | -4.95 8.36119 -5.55 7.453 | -5.72 7.240 | -3.49 11.86020 -6.58 6.289 | -6.84 6.054 | -2.06 20.052
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
25/163
CC 8800-1
- A N A L Y S I S O F B U C K L I N G -===================================================
analysis: "buckling stress" = Sigma/KappaKappa Lambdaquer < 0.2safety = 88.888 --> force in pipe = 0.00safety = 99.999 --> safety > 100.0safety = 111.111 --> tension, no buckling
diagonals : buckling length sk = 0.8 * length
buckling stresses [KN/cm**2] and safeties (section buckling curve "a", Alpha = 0.170===================================================
beam upper chord | lower chord|
1 52.52 1.148 | 60.30 1.000
2 51.01 1.182 | 55.09 1.0955 48.66 1.239 | 50.78 1.1886 47.13 1.279 | 56.97 1.0587 40.71 1.548 | 61.82 1.0198 29.20 2.158 | 62.28 1.0129 22.03 2.860 | 60.04 1.04910 15.20 4.144 | 59.69 1.05614 15.57 3.756 | 27.87 2.09915 15.28 3.829 | 30.52 1.91718 17.49 3.345 | 32.16 1.819
19 17.49 3.345 | 26.61 2.19920 20.10 3.134 | 26.13 2.41121 17.84 3.531 | 21.82 2.88722 15.43 4.084 | 13.73 4.589
beam diagonals | diagonals | diagoupper | lower | ve
| |1 2.81 111.111 | 9.59 6.475 | 6.542 4.53 13.715 | 21.61 2.874 | 30.69
5 4.96 111.111 | 16.33 111.111 | 1.736 0.00 99.999 | 24.94 2.490 | 29.887 6.64 9.347 | 30.89 2.010 | 28.618 10.37 5.990 | 33.23 1.869 | 25.399 12.62 4.922 | 35.40 1.754 | 23.9410 15.63 3.972 | 39.40 1.576 | 22.5614 4.49 9.213 | 4.44 9.327 | 5.53
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
26/163
CC 8800-1
S U M M A R Y O F B O O M S Y S T E M===================================================
section type 1 + 2=====================
upper chords lower chords min max min max upper
Sigma -45.89 14.41 -57.49 -28.17 -11.76 -safety 1.314 4.373 1.096 2.237 5.279 beamnunber ( 5) ( 7) ( 8) ( 10) ( 10)
Sigma/Kappa 52.52 60.30 15.63 safety 1.148 1.000 3.972 beamnunber ( 1) ( 1) ( 10)
minimum safety of boom system===================================
1.000 decisive : buckling (beam-/node
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
27/163
CC 8800-1
Appendix B
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
28/163
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
29/163
CC 8800-1
PRESTAB_V6, Version V5.5h 22.11.2007:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
: load control part 1 * 5.12.2007 8:51:57 *** 49565:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CC 8800-1 Projekt SSL 60 s_mr2615.09.2006 Zimmer
Control output of the variable input------------------------------------------1. radius = 9.82. loadcase =
3. rated load = 1541.04. reeving = 5. number of hoist lines back to the winch = 6. loads mass(n): ----------------------
node no. Radius[m] ----------------------
32 -24.000 Control output of the non variable input-----------------------------1. maximum torque = 480.0
2. minimum time of deceleration = 5.03. number of revolutions = 0.34. hoisting speed = 72.05. hoisting class = 6. node number of load = 7. windpressure on load = 60.08. counterweight = 220.09. distance between rotation axis/counterweight = 900.010.weight of superstructure = 36.811.distance between rotation axis/superstructure = 120.0
12.lateral inclination of boom system = 0.313.weight of hoist rope = 7.8
14.Guidance of hoist rope..........node numbers : 14, 13, 18, 26, 36
15.load factors : -----------------------------------load- | loads :case | dead lifted test a-----------------------------------H | 1.20 1.35 0.00 1HZ | 1.09 1.20 0.00 1HS | 1.09 0.00 1.09 1HZ*1 | 1.00 1.00 0.00 1-----------------------------------
C t l t t f th lt
CC
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
30/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 2 * 5.12.2007 8:51:57 *** 49565
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
node masss and node loads / loadcase HZ--------------------------------------------------
node masss node loads---------------- -----------------------------
node - boom - lifted vertical horizontalno. loads acceleration
system Y X Z
-----------------------------------------------------------[t] [t] [kN] [kN] [kN] ===========================================================
1 8.350 -- -89.81 6.07 0.04 02 13.000 -- -139.82 9.45 0.06 03 0.000 -- 0.00 0.00 0.00 04 0.000 -- 0.00 0.00 0.00 05 11.400 -- -122.61 8.29 0.06 06 16.550 -- -178.00 12.03 0.10 07 19.050 -- -204.89 13.85 0.15 0
8 14.150 -- -152.19 10.29 0.14 09 9.800 -- -105.40 7.13 0.10 0
10 13.600 -- -146.28 9.89 0.16 011 12.700 -- -136.60 9.23 0.17 012 5.700 -- -62.43 2.80 0.08 013 3.545 -- -40.31 0.52 0.04 014 23.822 1541.00 -19369.81 0.00 26.47 015 5.500 -- -61.01 -3.35 0.01 016 16.550 -- -184.02 -4.08 -0.07 017 4.400 -- -49.71 1.77 -0.03 0
18 1.150 -- -12.29 0.84 -0.01 019 10.330 -- -114.58 -6.29 -0.07 020 9.660 -- -107.15 -5.88 -0.17 021 7.730 -- -85.74 -4.71 -0.23 022 4.300 -- -47.70 -2.62 -0.16 023 6.800 -- -75.21 -0.72 -0.27 024 3.000 -- -33.33 -1.57 -0.13 025 2.000 -- -21.39 1.46 -0.08 026 2.000 -- -22.76 -0.47 -0.08 027 0.250 -- -2.82 0.10 -0.01 0
28 8.979 -- -98.40 -4.32 -0.41 029 5.500 -- -61.70 -2.76 -0.06 030 8.266 -- -91.97 -4.65 -0.21 031 0.000 -- 0.00 0.00 0.00 032 3.483 640.00 -6313.63 -2.54 -26.55 033 0.464 -- -5.12 -0.30 -0.01 034 0.000 -- 0.00 0.00 0.00 0
CC 8800 1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
31/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 3 * 5.12.2007 8:51:57 *** 49565:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CW-Value 1.60 [/]
beam- node- angle length weight windareano. numbers t.horiz
-----------------------------------------------------------[degr] [cm] [t] [qm/lfm]
===========================================================1 1 2 84.79 400.0 16.700 2.018
2 5 6 84.79 375.0 13.500 2.0833 2 3 174.79 137.5 0.000 0.0004 2 4 165.77 159.5 0.000 0.0005 2 5 84.79 225.0 9.300 2.2066 6 7 84.79 1200.0 19.600 1.9527 7 8 84.79 1200.0 18.500 1.9568 8 9 84.79 600.0 9.800 2.1029 9 10 84.79 600.0 9.800 2.10210 10 11 84.79 1200.0 17.400 1.95211 11 12 84.79 200.0 8.000 1.500
12 12 13 174.79 180.0 3.400 0.00013 12 14 -5.21 190.0 0.000 0.00014 15 16 123.50 685.0 11.000 1.25015 16 19 123.50 215.0 11.000 1.44016 16 17 -146.50 138.5 8.800 0.00017 16 18 89.95 114.0 2.300 0.00018 19 20 123.50 1200.0 9.660 1.43119 20 21 123.50 1200.0 9.660 1.43120 21 22 123.50 800.0 5.800 1.49021 22 23 123.50 274.0 2.800 1.505
22 23 24 123.50 416.0 2.800 1.23023 24 28 123.50 210.0 2.700 0.60024 23 25 89.37 125.6 4.000 0.00025 23 26 161.07 131.2 4.000 0.00026 24 27 -146.50 65.0 0.500 0.00027 29 30 136.49 1165.0 11.000 1.00028 31 32 -180.00 1300.0 0.000 0.00029 13 28 -151.93 3689.6 3.689 0.35030 30 33 -62.01 1031.4 0.928 0.35031 28 30 -70.94 3540.5 4.603 0.350
32 28 32 -86.83 4337.9 6.966 0.45033 3 34 -124.53 387.0 0.000 0.00034 17 35 -99.46 495.5 0.000 0.000
===========================================================SUM : 228.206
CC 8800 1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
32/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 4 * 5.12.2007 8:51:57 *** 49565:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
results of basic load determination :node loads without factors in STAB84-global-components
node loads in [ kN ] :no. node mass beam mass acceleration forces
Y Y Y X Z -----------------------------------------------------------1 0.00 -81.89 -0.410 4.497 0.018 0
2 0.00 -127.49 -0.638 7.001 0.032 03 0.00 0.00 0.000 0.000 0.000 04 0.00 0.00 0.000 0.000 0.000 05 0.00 -111.80 -0.560 6.140 0.030 06 0.00 -162.30 -0.813 8.913 0.048 07 0.00 -186.82 -0.935 10.260 0.073 08 0.00 -138.76 -0.695 7.621 0.067 09 0.00 -96.11 -0.481 5.278 0.051 010 0.00 -133.37 -0.668 7.325 0.077 011 0.00 -124.54 -0.624 6.840 0.084 0
12 0.00 -55.90 -1.112 2.071 0.038 013 0.00 -34.76 -1.796 0.386 0.019 014 0.00 -233.61 0.000 0.000 13.072 015 0.00 -53.94 -1.642 -2.480 0.006 016 0.00 -162.30 -5.268 -3.025 -0.036 017 0.00 -43.15 -1.984 1.313 -0.014 018 0.00 -11.28 -0.001 0.622 -0.003 019 0.00 -101.30 -3.084 -4.658 -0.033 020 0.00 -94.73 -2.884 -4.356 -0.085 021 0.00 -75.81 -2.308 -3.486 -0.112 0
22 0.00 -42.17 -1.284 -1.939 -0.078 023 0.00 -66.69 -1.871 -0.532 -0.132 024 0.00 -29.42 -0.934 -1.165 -0.064 025 0.00 -19.61 -0.012 1.082 -0.039 026 0.00 -19.61 -1.023 -0.351 -0.041 027 0.00 -2.45 -0.113 0.075 -0.005 028 0.00 -88.06 -1.794 -3.196 -0.201 029 0.00 -53.94 -2.157 -2.048 -0.030 030 0.00 -81.06 -2.681 -3.446 -0.104 031 0.00 0.00 0.000 0.000 0.000 0
32 0.00 -34.16 -0.104 -1.881 -13.112 033 0.00 -4.55 -0.118 -0.222 -0.004 034 0.00 0.00 0.000 0.000 0.000 035 0.00 0.00 0.000 0.000 0.000 0
-----------------------------------------------------------SUM : 0.00 -2471.55 -37.991 36.638 -0.282 0
CC 8800 1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
33/163
CC 8800-1
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% E I N Z E L S T A B - A N A L Y S I S %% =================================== %% ( 5.12.2007 8:51:58) %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% CC 8800-1 Projekt SSL 60 s_mr26 %% 15.09.2006 Zimmer %% **************************************** %% E I N G A B E K O N T R O L L E : %% crane part 4 declin. 180.000 [deg]%
% crane part 2 radius -26.400 [m] %% crane part 1 radius 9.840 [m] %% loadcase HZ nom. load 1541.000 [t] %% reeving 25 %% node num. 32 add. mass 640.000 [t] %% **************************************** %% F R E I E T E X T E I N G A B E : %% variante 1 , superlift %% **************************************** %% * 5.12.2007 8:51:57 *** 495657565748 * %
% %%%%%%%%%%%% Version 5.0g vom 18.06.2007 %%%%
number of beams 34number of nodes 35
beam node length Ndiag section no. sectionnumber KA KE (cm) Stab84 Einzel
( 1) 1 2 399.99 2 1 1 tapered( 2) 5 6 374.99 2 2 2 standar( 3) 2 3 137.50 0 3 0 -------( 4) 2 4 159.47 0 4 0 -------( 5) 2 5 224.99 1 5 3 standar( 6) 6 7 1199.98 7 6 4 standar( 7) 7 8 1200.00 7 7 5 standar( 8) 8 9 600.01 4 8 6 standar( 9) 9 10 600.02 4 9 6 standar( 10) 10 11 1200.07 7 10 7 standar
( 11) 11 12 200.01 0 11 0 -------( 12) 12 13 180.00 0 12 0 -------( 13) 12 14 190.00 0 13 0 -------( 14) 15 16 684.99 6 14 8 tapered( 15) 16 19 215.00 1 15 9 standar( 16) 16 17 138.50 0 16 0 -------( 17) 16 18 113.99 0 17 0 -------
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
34/163
CC 8800 1
SECTION PROPERTIES=================================
section type : standard lattice mast [cm,kN]=====================================
( 2) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 3.75m paral. Teil Nr.2 R2
LV LW field length cantilev-A cantil275.0 320.0 330.3 0.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 3) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 2.25m paral. Teil Nr.1 R2
LV LW field length cantilev-A cantil
275.0 320.0 441.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 4) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-45-12CC8800-1 16.03.2006 W.Zim. Projekt ZW 12m 3227-45 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 5) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-40-12
CC8800-1 12.9.2006 W.Zim. Entwurf ZW 12m 3227-40 3.5 FelderLV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.00 29.85*4.00 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
35/163
CC 8800 1
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62area 296.88 296.88 38.08 42.
----------------------------------------------------------( 9) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 5.90 paralleler Teil 2621
LV LW field length cantilev-A cantil210.0 260.0 421.4 0.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 10) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-30-12CC8800-1 08.12.2005 W.Zim. ZW 12m 2621-30 4 Felder 2621-30
LV LW field length cantilev-A cantil210.0 260.0 281.8 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 11) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-22-80
CC8800-1 08.12.2005 W.Zim. ZW 8m 2621-22.2 3.0 Felder 2621-2LV LW field length cantilev-A cantil210.0 260.0 245.0 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41area 137.32 137.32 20.11 20.
----------------------------------------------------------
( 12) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze paralleler Teil 2.75m
LV LW field length cantilev-A cantil210.0 260.0 244.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
36/163
CC
section type : tapered part (o.ae.) [cm,kN]========================================
( 1) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-foot 4.0m konischer Teil R298.
LVA LVE LWA LWE field length cantil35.0 275.0 320.0 320.0 345.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 8) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 4.6m konischer Teil 2621-
LVA LVE LWA LWE field length cantil14.0 210.0 260.0 260.0 215.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 13) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze 4.16m 2.0 Feld 2621-22
LVA LVE LWA LWE field length cantil210.0 86.4 260.0 185.0 203.8 0.0
upp. chord low. chord upp. diags low. dia
pipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41area 137.32 137.32 20.11 20.
----------------------------------------------------------
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
37/163
NODE DISPLACEMENTS :======================
NODE X Y ZNUMBER (CM) (CM) (CM)
( 1) 0.00 0.00 0.00( 2) -1.04 -0.33 8.46( 3) -1.05 -0.43 8.04( 4) -1.12 -0.64 8.53( 5) -1.79 -0.52 13.90( 6) -3.00 -0.88 24.05( 7) -5.89 -2.43 65.01( 8) -5.34 -5.08 117.93( 9) -2.94 -6.95 148.34( 10) 1.40 -9.20 180.87( 11) 16.99 -14.75 249.67( 12) 22.25 -17.32 264.04( 13) 23.06 -12.76 251.63( 14) 15.82 -51.22 277.27( 15) 0.00 0.00 0.00( 16) 5.96 3.56 1.26
( 17) 5.35 4.50 1.23( 18) 6.71 3.57 1.54( 19) 7.17 4.22 1.96( 20) 11.69 6.39 8.63( 21) 13.97 6.99 19.22( 22) 14.79 6.72 27.94( 23) 14.97 6.55 31.13( 24) 15.28 6.39 36.11( 25) 15.01 6.53 32.28( 26) 14.85 6.14 32.26
( 27) 15.27 6.41 36.11( 28) 15.46 6.33 38.66( 29) 0.00 0.00 0.00( 30) 1.28 1.32 0.47( 31) 0.00 0.00 0.00( 32) -0.09 0.03 2.83( 33) 0.00 0.00 0.00( 34) 0.00 0.00 0.00( 35) 0.00 0.00 0.00
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
38/163
BEARING FORCES=================================================
node X (KN) Y (KN) number XX (KN*cm) YY (KN*cm)
( 1) 2160.7771 22195.8594 -6622024.0000 815562.2500
( 15) -3635.7307 4375.3892 -737769.5000 -475137.4375
( 29) -78.7201 139.3425 -6003.1689 -6304.3428
( 31) 270.4721 0.1399 -1.0185 -27507.2070
( 33) 255.6697 -477.3058 0.0000 0.0000
( 34) 452.3451 659.6484
0.0000 0.0000
( 35) 138.5744 787.9066 0.0000 0.0000
INNER FORCES AND MOMENTS=========================================
1) foot main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 1) -22206.39 -227819.59 206.80 6668152.00 -6486338.50 0.00 -
( 2) -22640.06 -232118.45 650.56
6367183.50 -6143487.00 166874.84 -4
( 3) -391.13 0.00 -697.85 -816.05 -0.04 95952.35
( 4) 0.01 0.00 -0.02 -0.03 -0.02 1.26
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
39/163
( 8) -22086.31 -234412.59 531.54 3863714.50 -3091433.00 2041549.12 -23
( 9) -21977.23 -235873.92 465.14 3078351.75 -2241217.50 2377196.75 -26
( 10) -21828.98 -234703.34 346.23 2219990.00 -433918.09 2674154.00 -30
3) head main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 11) -21673.12 -274693.44 20.23 391297.78 -32320.87 3091899.75 -30
( 12) 1681.43 0.05 2506.68 19635.95 -0.34 -451456.78
( 13) 4455.55 -1.44 -18674.00
227875.14 -16.83 3552888.50
4) Superliftmast=============
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 14) -5599.19 -2168.90 -710.15 877534.31 -784123.88 0.00 4
( 15) -7304.07 -661.74 208.52 779605.56 -757489.12 -524177.09 4
( 16) -520.14 0.00 -542.26 -879.97 0.00 75100.71
( 17) 1359.76 0.00 325.50 5303.72 0.00 -37107.09
( 18) -7210.75 -307.01 156.54 757504.31 -599507.31 -479350.22 2
( 19) -7122.97 578.19 108.89 599501.12 -379321.03 -291613.78 1
( 20) -7052.82 1031.59 66.03
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
40/163
( 26) 1.47 0.00 2.41 2.32 0.01 -156.76
5) A-frame========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 27) -112.51 0.00 0.00 8705.44 0.00 0.00
6) misc. parts==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 28) 270.52 0.00 0.00 27507.86 0.21 0.00
( 33) -800.00 0.00 0.00 0.00 0.00 0.00
( 34) -800.00 0.00 0.00 0.00 0.00 0.00
7) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 30) 545.86 0.00 0.00 0.00 0.00 0.00
( 32) 5205.17 0.00 0.00 0.00 0.00 0.00
8) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 29) 2914.47 0.00 0.00 0.00 0.00 0.00
( 31) 524.87 0.00 0.00
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
41/163
G E N E R A L S T R E S S - A N A L Y S I S===================================================
stress = force in pipe/areasafety = stress/calculated stress limit
safety = 88.888 --> force in pipe = 0.00 or pressursafety = 99.999 --> safety > 100.0
stresses [KN/cm**2] and safeties (section type ===============================================
beam upper chord | upper chord | lower chord (min) | (max) | (min)
| | 1 -42.83 1.408 | 11.38 5.301 | -48.45 1.245 2 -42.80 1.409 | 12.83 4.699 | -45.67 1.320 5 -44.31 1.361 | 12.21 4.938 | -45.88 1.314 6 -40.09 1.504 | 13.26 4.549 | -46.87 1.287 7 -34.55 1.824 | 14.81 4.255 | -50.54 1.247 8 -26.04 2.419 | 13.99 4.503 | -52.54 1.199 9 -19.69 3.200 | 11.95 5.274 | -50.32 1.252
10 -13.04 4.830 | 9.19 6.855 | -47.61 1.323 14 -12.55 4.662 | 7.41 7.897 | -23.01 2.543 15 -12.19 4.798 | 4.95 11.811 | -25.45 2.298 18 -12.77 4.581 | 4.26 13.743 | -24.49 2.389 19 -12.77 4.582 | 0.09 99.999 | -20.07 2.915 20 -15.49 4.067 | -5.11 12.319 | -20.55 3.065 21 -13.82 4.560 | -8.44 7.461 | -17.08 3.689 22 -12.44 5.064 | -8.72 7.229 | -11.19 5.629
beam diagonals | diagonals | diagonalsupper(min) | lower (min) | vertical(min)
| |1 4.72 13.156 | -8.52 7.291 | -5.11 12.1532 -1.78 34.845 | -17.40 3.569 | -22.87 2.7155 3.07 20.211 | 17.81 3.486 | 3.39 18.3366 -1.16 53.700 | -19.67 3.157 | -22.50 2.7607 -5.48 11.324 | -23.56 2.636 | -21.77 2.8538 -8.01 7.757 | -25.48 2.437 | -19.99 3.107
9 -9.48 6.553 | -26.91 2.308 | -19.10 3.25110 -11.23 5.527 | -29.03 2.139 | -18.10 3.43214 -3.71 11.147 | -3.67 11.294 | -5.07 8.16115 3.25 12.751 | -3.09 13.383 | -3.10 13.37018 -3.78 10.963 | -3.71 11.157 | -4.76 8.69619 -5.15 8.031 | -5.28 7.843 | -3.36 12.31220 -5.97 6.938 | -6.18 6.698 | -2.05 20.195
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
42/163
- A N A L Y S I S O F B U C K L I N G -===================================================
analysis: "buckling stress" = Sigma/KappaKappa Lambdaquer < 0.2safety = 88.888 --> force in pipe = 0.00safety = 99.999 --> safety > 100.0safety = 111.111 --> tension, no buckling
diagonals : buckling length sk = 0.8 * length
buckling stresses [KN/cm**2] and safeties (section buckling curve "a", Alpha = 0.170===================================================
beam upper chord | lower chord|
1 50.85 1.186 | 57.52 1.0482 49.25 1.224 | 52.55 1.1475 46.97 1.284 | 48.64 1.2406 45.48 1.326 | 53.16 1.1347 39.25 1.605 | 57.42 1.0978 28.21 2.233 | 56.92 1.1079 21.33 2.954 | 54.51 1.15610 14.77 4.267 | 53.91 1.16914 13.92 4.203 | 25.52 2.29215 13.43 4.355 | 28.05 2.08618 15.39 3.800 | 29.52 1.982
19 15.39 3.801 | 24.19 2.41820 17.74 3.550 | 23.54 2.67621 15.81 3.986 | 19.54 3.22422 13.67 4.610 | 12.29 5.125
beam diagonals | diagonals | diagoupper | lower | ve
| |1 4.72 111.111 | 11.91 5.215 | 6.092 2.39 26.023 | 23.26 2.669 | 28.48
5 3.07 111.111 | 17.81 111.111 | 3.396 1.54 40.401 | 26.10 2.380 | 27.837 7.29 8.520 | 31.26 1.987 | 26.938 10.39 5.977 | 33.00 1.882 | 24.219 12.30 5.050 | 34.84 1.782 | 23.1310 14.93 4.159 | 38.53 1.612 | 22.3914 4.50 9.207 | 4.44 9.329 | 5.25
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
43/163
S U M M A R Y O F B O O M S Y S T E M===================================================
section type 1 + 2=====================
upper chords lower chords min max min max upper
Sigma -44.31 14.81 -52.54 -23.97 -11.23 -safety 1.361 4.255 1.199 2.628 5.527 beamnunber ( 5) ( 7) ( 8) ( 10) ( 10)
Sigma/Kappa 50.85 57.52 14.93 safety 1.186 1.048 4.159 beamnunber ( 1) ( 1) ( 10)
minimum safety of boom system===================================
1.048 decisive : buckling (beam-/node
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
44/163
Appendix C
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
45/163
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
46/163
PRESTAB_V6, Version V5.5h 22.11.2007:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 1 * 5.12.2007 8:51:58 *** 53575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CC 8800-1 Projekt SSL 60 s_mr2615.09.2006 Zimmer
Control output of the variable input------------------------------------------1. radius = 9.82. loadcase = HZ3. rated load = 1541.04. reeving = 5. number of hoist lines back to the winch = 6. loads mass(n): ----------------------
node no. Radius[m] ----------------------
32 -24.000 Control output of the non variable input-----------------------------1. maximum torque = 480.0
2. minimum time of deceleration = 5.03. number of revolutions = 0.34. hoisting speed = 72.05. hoisting class = 6. node number of load = 7. windpressure on load = 60.08. counterweight = 220.09. distance between rotation axis/counterweight = 900.010.weight of superstructure = 36.811.distance between rotation axis/superstructure = 120.0
12.lateral inclination of boom system = 0.313.weight of hoist rope = 7.8
14.Guidance of hoist rope..........node numbers : 14, 13, 18, 26, 36
15.load factors : -----------------------------------load- | loads :case | dead lifted test a-----------------------------------
H | 1.20 1.35 0.00 1HZ | 1.09 1.20 0.00 1HS | 1.09 0.00 1.09 1HZ*1 | 1.00 1.00 0.00 1-----------------------------------
Control output of the results
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
47/163
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 2 * 5.12.2007 8:51:58 *** 53575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
node masss and node loads / loadcase HZ*1--------------------------------------------------
node masss node loads---------------- -----------------------------
node - boom - lifted vertical horizontalno. loads acceleration
system Y X Z -----------------------------------------------------------
[t] [t] [kN] [kN] [kN] ===========================================================
1 8.350 -- -82.30 4.50 0.03 02 13.000 -- -128.12 7.00 0.05 03 0.000 -- 0.00 0.00 0.00 04 0.000 -- 0.00 0.00 0.00 05 11.400 -- -112.36 6.14 0.04 06 16.550 -- -163.11 8.91 0.07 07 19.050 -- -187.75 10.26 0.11 08 14.150 -- -139.46 7.62 0.10 09 9.800 -- -96.59 5.28 0.08 0
10 13.600 -- -134.04 7.32 0.12 011 12.700 -- -125.17 6.84 0.13 012 5.700 -- -57.01 2.07 0.06 013 3.545 -- -36.56 0.39 0.03 014 23.822 1541.00 -16162.92 0.00 19.61 015 5.500 -- -55.58 -2.48 0.01 016 16.550 -- -167.57 -3.02 -0.05 017 4.400 -- -45.13 1.31 -0.02 018 1.150 -- -11.28 0.62 0.00 019 10.330 -- -104.39 -4.66 -0.05 020 9.660 -- -97.62 -4.36 -0.13 021 7.730 -- -78.11 -3.49 -0.17 022 4.300 -- -43.45 -1.94 -0.12 023 6.800 -- -68.56 -0.53 -0.20 024 3.000 -- -30.35 -1.17 -0.10 025 2.000 -- -19.63 1.08 -0.06 026 2.000 -- -20.64 -0.35 -0.06 027 0.250 -- -2.56 0.07 -0.01 0
28 8.979 -- -89.85 -3.20 -0.30 029 5.500 -- -56.09 -2.05 -0.04 030 8.266 -- -83.74 -3.45 -0.16 031 0.000 -- 0.00 0.00 0.00 032 3.483 640.00 -6310.52 -1.88 -19.67 033 0.464 -- -4.67 -0.22 -0.01 034 0.000 -- 0.00 0.00 0.00 0
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
48/163
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 3 * 5.12.2007 8:51:58 *** 53575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CW-Value 1.60 [/]
beam- node- angle length weight windareano. numbers t.horiz
-----------------------------------------------------------[degr] [cm] [t] [qm/lfm]
===========================================================1 1 2 84.79 400.0 16.700 2.0182 5 6 84.79 375.0 13.500 2.083
3 2 3 174.79 137.5 0.000 0.0004 2 4 165.77 159.5 0.000 0.0005 2 5 84.79 225.0 9.300 2.2066 6 7 84.79 1200.0 19.600 1.9527 7 8 84.79 1200.0 18.500 1.9568 8 9 84.79 600.0 9.800 2.1029 9 10 84.79 600.0 9.800 2.10210 10 11 84.79 1200.0 17.400 1.95211 11 12 84.79 200.0 8.000 1.50012 12 13 174.79 180.0 3.400 0.000
13 12 14 -5.21 190.0 0.000 0.00014 15 16 123.50 685.0 11.000 1.25015 16 19 123.50 215.0 11.000 1.44016 16 17 -146.50 138.5 8.800 0.00017 16 18 89.95 114.0 2.300 0.00018 19 20 123.50 1200.0 9.660 1.43119 20 21 123.50 1200.0 9.660 1.43120 21 22 123.50 800.0 5.800 1.49021 22 23 123.50 274.0 2.800 1.50522 23 24 123.50 416.0 2.800 1.23023 24 28 123.50 210.0 2.700 0.60024 23 25 89.37 125.6 4.000 0.00025 23 26 161.07 131.2 4.000 0.00026 24 27 -146.50 65.0 0.500 0.00027 29 30 136.49 1165.0 11.000 1.00028 31 32 -180.00 1300.0 0.000 0.00029 13 28 -151.93 3689.6 3.689 0.35030 30 33 -62.01 1031.4 0.928 0.35031 28 30 -70.94 3540.5 4.603 0.35032 28 32 -86.83 4337.9 6.966 0.45033 3 34 -124.53 387.0 0.000 0.00034 17 35 -99.46 495.5 0.000 0.000
===========================================================SUM : 228.206
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
49/163
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 4 * 5.12.2007 8:51:58 *** 53575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
results of basic load determination :node loads without factors in STAB84-global-components
node loads in [ kN ] :no. node mass beam mass acceleration forces
Y Y Y X Z -----------------------------------------------------------1 0.00 -81.89 -0.410 4.497 0.018 02 0.00 -127.49 -0.638 7.001 0.032 0
3 0.00 0.00 0.000 0.000 0.000 04 0.00 0.00 0.000 0.000 0.000 05 0.00 -111.80 -0.560 6.140 0.030 06 0.00 -162.30 -0.813 8.913 0.048 07 0.00 -186.82 -0.935 10.260 0.073 08 0.00 -138.76 -0.695 7.621 0.067 09 0.00 -96.11 -0.481 5.278 0.051 010 0.00 -133.37 -0.668 7.325 0.077 011 0.00 -124.54 -0.624 6.840 0.084 012 0.00 -55.90 -1.112 2.071 0.038 0
13 0.00 -34.76 -1.796 0.386 0.019 014 0.00 -233.61 0.000 0.000 13.072 015 0.00 -53.94 -1.642 -2.480 0.006 016 0.00 -162.30 -5.268 -3.025 -0.036 017 0.00 -43.15 -1.984 1.313 -0.014 018 0.00 -11.28 -0.001 0.622 -0.003 019 0.00 -101.30 -3.084 -4.658 -0.033 020 0.00 -94.73 -2.884 -4.356 -0.085 021 0.00 -75.81 -2.308 -3.486 -0.112 022 0.00 -42.17 -1.284 -1.939 -0.078 023 0.00 -66.69 -1.871 -0.532 -0.132 024 0.00 -29.42 -0.934 -1.165 -0.064 025 0.00 -19.61 -0.012 1.082 -0.039 026 0.00 -19.61 -1.023 -0.351 -0.041 027 0.00 -2.45 -0.113 0.075 -0.005 028 0.00 -88.06 -1.794 -3.196 -0.201 029 0.00 -53.94 -2.157 -2.048 -0.030 030 0.00 -81.06 -2.681 -3.446 -0.104 031 0.00 0.00 0.000 0.000 0.000 032 0.00 -34.16 -0.104 -1.881 -13.112 033 0.00 -4.55 -0.118 -0.222 -0.004 034 0.00 0.00 0.000 0.000 0.000 035 0.00 0.00 0.000 0.000 0.000 0
-----------------------------------------------------------SUM : 0.00 -2471.55 -37.991 36.638 -0.282 0
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
50/163
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% E I N Z E L S T A B - A N A L Y S I S %
% =================================== %% ( 5.12.2007 8:51:58) %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% CC 8800-1 Projekt SSL 60 s_mr26 %% 15.09.2006 Zimmer %% **************************************** %% E I N G A B E K O N T R O L L E : %% crane part 4 declin. 180.000 [deg]%% crane part 2 radius -26.400 [m] %
% crane part 1 radius 9.840 [m] %% loadcase HZ*1 nom. load 1541.000 [t] %% reeving 25 %% node num. 32 add. mass 640.000 [t] %% **************************************** %% F R E I E T E X T E I N G A B E : %% variante 1 , superlift %% **************************************** %% * 5.12.2007 8:51:58 *** 535755485452 * %% %
%%%%%%%%%%% Version 5.0g vom 18.06.2007 %%%%
number of beams 34number of nodes 35
beam node length Ndiag section no. sectionnumber KA KE (cm) Stab84 Einzel
( 1) 1 2 399.99 2 1 1 tapered( 2) 5 6 374.99 2 2 2 standar( 3) 2 3 137.50 0 3 0 -------( 4) 2 4 159.47 0 4 0 -------( 5) 2 5 224.99 1 5 3 standar( 6) 6 7 1199.98 7 6 4 standar( 7) 7 8 1200.00 7 7 5 standar( 8) 8 9 600.01 4 8 6 standar( 9) 9 10 600.02 4 9 6 standar( 10) 10 11 1200.07 7 10 7 standar( 11) 11 12 200.01 0 11 0 -------( 12) 12 13 180.00 0 12 0 -------( 13) 12 14 190.00 0 13 0 -------( 14) 15 16 684.99 6 14 8 tapered( 15) 16 19 215.00 1 15 9 standar( 16) 16 17 138.50 0 16 0 -------( 17) 16 18 113.99 0 17 0 -------
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
51/163
SECTION PROPERTIES=================================
section type : standard lattice mast [cm,kN]=====================================
( 2) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 3.75m paral. Teil Nr.2 R2
LV LW field length cantilev-A cantil275.0 320.0 330.3 0.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 3) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 2.25m paral. Teil Nr.1 R2
LV LW field length cantilev-A cantil275.0 320.0 441.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 4) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-45-12CC8800-1 16.03.2006 W.Zim. Projekt ZW 12m 3227-45 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 5) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-40-12CC8800-1 12.9.2006 W.Zim. Entwurf ZW 12m 3227-40 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.00 29.85*4.00 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
52/163
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62area 296.88 296.88 38.08 42.
----------------------------------------------------------( 9) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 5.90 paralleler Teil 2621
LV LW field length cantilev-A cantil210.0 260.0 421.4 0.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 10) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-30-12CC8800-1 08.12.2005 W.Zim. ZW 12m 2621-30 4 Felder 2621-30
LV LW field length cantilev-A cantil
210.0 260.0 281.8 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41area 178.22 178.22 20.11 20.
----------------------------------------------------------( 11) /berechnung/stab84/gerdaten/cc8800-1/teile/2621-22-80CC8800-1 08.12.2005 W.Zim. ZW 8m 2621-22.2 3.0 Felder 2621-2
LV LW field length cantilev-A cantil210.0 260.0 245.0 25.0 2
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41area 137.32 137.32 20.11 20.
----------------------------------------------------------( 12) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze paralleler Teil 2.75m
LV LW field length cantilev-A cantil210.0 260.0 244.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
53/163
section type : tapered part (o.ae.) [cm,kN]========================================
( 1) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-foot 4.0m konischer Teil R298.
LVA LVE LWA LWE field length cantil35.0 275.0 320.0 320.0 345.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 8) /berechnung/stab84/gerdaten/cc8800-1/teile/fussma2621CC8800-1 06.04.2006 W.Zim. Mastfu 4.6m konischer Teil 2621-
LVA LVE LWA LWE field length cantil14.0 210.0 260.0 260.0 215.0 25.0
upp. chord low. chord upp. diags low. diapipe 21.91*3.00 21.91*3.00 13.30*0.50 13.30*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 46.0/ 41.4 46.0/ 41
area 178.22 178.22 20.11 20.
----------------------------------------------------------( 13) /berechnung/stab84/gerdaten/cc8800-1/teile/spima2621-CC8800-1 06.04.2006 W.Zim. Mastspitze 4.16m 2.0 Feld 2621-22
LVA LVE LWA LWE field length cantil210.0 86.4 260.0 185.0 203.8 0.0
upp. chord low. chord upp. diags low. diapipe 21.91*2.22 21.91*2.22 13.30*0.50 13.30*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 46.0/ 41.4 46.0/ 41area 137.32 137.32 20.11 20.
----------------------------------------------------------
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
54/163
NODE DISPLACEMENTS :======================
NODE X Y ZNUMBER (CM) (CM) (CM)
( 1) 0.00 0.00 0.00( 2) -0.51 -0.26 4.85( 3) -0.51 -0.22 4.62( 4) -0.55 -0.42 4.90( 5) -0.97 -0.40 7.96( 6) -1.73 -0.65 13.77( 7) -3.44 -1.63 37.18
( 8) -2.51 -3.20 67.40( 9) -0.36 -4.31 84.76( 10) 3.35 -5.64 103.32( 11) 16.41 -9.02 142.56( 12) 20.73 -10.84 150.70( 13) 21.14 -7.37 143.53( 14) 16.05 -38.95 158.45( 15) 0.00 0.00 0.00( 16) 5.30 3.19 0.62( 17) 4.75 4.03 0.58
( 18) 5.96 3.20 0.77( 19) 6.35 3.77 0.97( 20) 10.17 5.62 4.35( 21) 11.90 6.07 9.83( 22) 12.41 5.79 14.39( 23) 12.50 5.63 16.07( 24) 12.66 5.48 18.69( 25) 12.50 5.62 16.69( 26) 12.39 5.27 16.64( 27) 12.66 5.49 18.67
( 28) 12.77 5.42 20.02( 29) 0.00 0.00 0.00( 30) 1.02 1.06 0.26( 31) 0.00 0.00 0.00( 32) -0.08 -0.01 1.11( 33) 0.00 0.00 0.00( 34) 0.00 0.00 0.00( 35) 0.00 0.00 0.00
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
55/163
BEARING FORCES=================================================
node X (KN) Y (KN) number XX (KN*cm) YY (KN*cm)
( 1) 1742.9998 18531.8965 -3787089.7500 469304.6250
( 15) -3068.8716 3596.8789 -370942.5625 -237576.9688
( 29) -58.3606 113.6053
-3285.7363 -3452.7588
( 31) 228.3494 0.0597 0.0487 -10806.4004
( 33) 205.0605 -381.9803 0.0000 0.0000
( 34) 452.9670 659.3528 0.0000 0.0000
( 35) 137.7719 788.0474 0.0000 0.0000
INNER FORCES AND MOMENTS=========================================
1) foot main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 1) -18529.95 -128214.97 87.93 3813908.00 -3703388.00 0.00 -
( 2) -18987.38 -130728.77 527.19 3632973.00 -3502604.00 66336.67 -2
( 3) -391.06 0.00 -697.88 -804.39 -0.06 95957.41
( 4) 0.00 0.00 0.00 -0.06 -0.06 0.29
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
56/163
( 8) -18493.21 -135467.09 479.98 2205453.00 -1763185.25 1568969.25 -18
( 9) -18396.12 -137523.81 442.36 1757230.88 -1276521.38 1862241.25 -21
( 10) -18262.83 -138553.17 370.74 1266569.62 -237438.16 2133385.50 -25
3) head main boom==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Q
number MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 11) -18134.57 -158089.02 171.56 216699.28 -15765.01 2578692.75 -26
( 12) 1416.92 0.03 2082.67 9323.37 0.13 -375046.34
( 13) 3224.80 -1.79 -15721.53 128626.43 -11.65 2989998.50
4) Superliftmast=============
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 14) -4642.59 -2685.64 -648.35 440496.31 -400667.56 0.00 4
( 15) -6145.29 -1348.43 197.03 398247.28 -389304.66 -488727.59 4
( 16) -522.11 0.00 -546.47 -938.92 0.01 75683.04
( 17) 1132.67 0.00 270.85 2815.55 0.00 -30876.17
( 18) -6060.03 -756.16 148.46 389336.38 -318322.94 -446363.50 2
( 19) -5980.18 232.55 103.58 318331.69 -205865.95 -268287.75 1
( 20) -5916.37 684.37 63.84
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
57/163
( 26) 1.35 0.00 2.18 1.48 0.00 -141.67
5) A-frame========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 27) -83.39 0.00 0.00 4766.36 0.00 0.00
6) misc. parts==================
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 28) 228.36 0.00 0.00 10806.66 0.14 0.00
( 33) -800.00 0.00 0.00 0.00 0.00 0.00
( 34) -800.00 0.00 0.00 0.00 0.00 0.00
7) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Qnumber MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 30) 437.57 0.00 0.00 0.00 0.00 0.00
( 32) 4359.53 0.00 0.00 0.00 0.00 0.00
8) ropes=========
beam PU ( KN ) MU(KNcm) QV ( KN ) Q
number MAV(KNcm) MEV(KNcm) MAW(KNcm) M
( 29) 2438.98 0.00 0.00 0.00 0.00 0.00
( 31) 436.32 0.00 0.00
CC 8800-1
G E N E R A L S T R E S S A N A L Y S I S
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
58/163
G E N E R A L S T R E S S - A N A L Y S I S===================================================
stress = force in pipe/areasafety = stress/calculated stress limit
safety = 88.888 --> force in pipe = 0.00 or pressursafety = 99.999 --> safety > 100.0
stresses [KN/cm**2] and safeties (section type ===============================================
beam upper chord | upper chord | lower chord (min) | (max) | (min)
| | 1 -28.82 2.092 | 2.20 27.455 | -31.85 1.893 2 -28.79 2.095 | 3.06 19.694 | -30.27 1.992 5 -29.83 2.021 | 2.60 23.226 | -30.32 1.989 6 -26.96 2.237 | 3.73 16.164 | -31.95 1.887 7 -23.14 2.723 | 5.16 12.198 | -35.29 1.785 8 -17.35 3.631 | 5.64 11.175 | -37.57 1.677
9 -13.07 4.818 | 5.12 12.304 | -36.90 1.707 10 -8.62 7.312 | 4.23 14.903 | -35.96 1.752 14 -7.05 8.298 | 3.83 15.279 | -16.64 3.515 15 -6.90 8.473 | 2.11 27.720 | -19.37 3.020 18 -8.20 7.131 | 1.57 37.325 | -18.58 3.149 19 -8.75 6.684 | -1.51 38.648 | -15.26 3.833 20 -11.29 5.581 | -5.59 11.262 | -15.94 3.953 21 -10.72 5.875 | -7.76 8.117 | -13.64 4.619 22 -9.83 6.408 | -7.82 8.061 | -8.88 7.096
beam diagonals | diagonals | diagonalsupper(min) | lower (min) | vertical(min)
| |1 2.98 20.857 | -5.08 12.225 | -2.79 22.2932 -0.83 74.749 | -9.95 6.238 | -15.36 4.0445 1.48 41.999 | 10.25 6.057 | -0.72 86.5076 -0.73 85.273 | -11.19 5.552 | -15.28 4.0647 -3.12 19.920 | -13.45 4.618 | -15.07 4.1228 -4.53 13.711 | -14.64 4.242 | -14.07 4.4159 -5.35 11.610 | -15.53 3.999 | -13.63 4.557
10 -6.32 9.825 | -16.86 3.683 | -13.21 4.70014 -1.60 25.823 | -1.54 26.827 | -4.67 8.86615 1.44 28.793 | -1.13 36.782 | -2.88 14.40018 -1.76 23.481 | -1.60 25.850 | -4.58 9.03919 -2.64 15.685 | -2.69 15.395 | -3.15 13.12520 -3.21 12.884 | -3.36 12.339 | -1.94 21.342
CC 8800-1
A N A L Y S I S O F B U C K L I N G
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
59/163
- A N A L Y S I S O F B U C K L I N G -===================================================
analysis: "buckling stress" = Sigma/KappaKappa Lambdaquer < 0.2safety = 88.888 --> force in pipe = 0.00safety = 99.999 --> safety > 100.0safety = 111.111 --> tension, no buckling
diagonals : buckling length sk = 0.8 * length
buckling stresses [KN/cm**2] and safeties (section buckling curve "a", Alpha = 0.170===================================================
beam upper chord | lower chord|
1 34.21 1.762 | 37.81 1.5952 33.13 1.820 | 34.84 1.731
5 31.63 1.906 | 32.14 1.8766 30.58 1.972 | 36.24 1.6647 26.29 2.396 | 40.09 1.5718 18.80 3.352 | 40.69 1.5489 14.16 4.448 | 39.97 1.57610 9.75 6.458 | 40.72 1.54714 7.82 7.481 | 18.46 3.16915 7.61 7.690 | 21.34 2.74118 9.89 5.916 | 22.39 2.61319 10.55 5.545 | 18.39 3.180
20 12.93 4.873 | 18.26 3.45121 12.27 5.135 | 15.60 4.03722 10.80 5.834 | 9.75 6.461
beam diagonals | diagonals | diagoupper | lower | ve
| |1 2.98 111.111 | 7.10 8.744 | 3.322 1.11 55.823 | 13.31 4.666 | 19.135 1.48 111.111 | 10.25 111.111 | 0.95
6 0.97 64.155 | 14.84 4.184 | 18.917 4.14 14.987 | 17.84 3.481 | 18.648 5.88 10.565 | 18.96 3.276 | 17.049 6.94 8.947 | 20.11 3.088 | 16.5010 8.40 7.391 | 22.37 2.776 | 16.3514 1.94 21.331 | 1.87 22.160 | 4.83
CC 8800-1
S U M M A R Y O F B O O M S Y S T E M
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
60/163
S U M M A R Y O F B O O M S Y S T E M===================================================
section type 1 + 2=====================
upper chords lower chords min max min max upper
Sigma -29.83 -7.82 -37.57 -22.62 -6.32 -safety 2.021 8.061 1.677 2.786 9.825 beamnunber ( 5) ( 22) ( 8) ( 10) ( 10)
Sigma/Kappa 34.21 40.72 8.40 safety 1.762 1.547 7.391 beamnunber ( 1) ( 10) ( 10)
minimum safety of boom system===================================
1.547 decisive : buckling (beam-/node
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
61/163
Structural Analysis
CC 8800-1
SWSL 96.0 + 36.0 m
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
62/163
1. Explanation of analysis method
A FORTRAN program system is used for the static calculation of the boo
A pre-processor program generates a finite element model of the cran
generates automatically the load cases and loads in accordance with DIN
The finite element program STAB88 (Technical University Munich) forces, inner moments and the deflection in compliance with the geome
(equilibrium at the deformed system).
A post-processor program accesses on the STAB88 output and perform
analysis and the verification of stability.
2. Standards and specifications used
[1] DIN 15018 part 3
[2] DIN 18800, part 2, State of consultation November 1990
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
63/163
3. Design loads
The loads acting on the structure are subdivided into main loads, additio
loads.
Main loads are:
- self weigths- lifted loads
- dynamic effects arising from lifting and lowering
- inertia forces arising from drives
Additional loads are:
- wind loads
Special loads are:
- test loads
The above loads are grouped into load cases. For the calculation in
geometric non-linear theory, the loads are multiplied by the pa
(DIN 15018 part 3 table 5).
Loads partial safety factors
Load case H Load case HZ
Self weigths 1,20 1.09
Liftet loads 1.35 1.20
Test loads - -
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
64/163
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
65/163
6. Example
The calculation was made for the boom length 96 m and the jib length 36
a maximium of deflection, stress and buckling.
Radius [m] Lifting capacity [t]
40 257Load case H
40 257
Load case HZ
40 257
Load case HZ1 (rated load)
CC 8800-1
Appendix A
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
66/163
Appendix A
CC 8800-1
BEAM NUMBERS
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
67/163
CC 8800-1
JIB HEAD (BEAM NUMBERS)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
68/163
LUFFING MASTS (BEAM NUMBERS)
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
69/163
BOOM FOOT AND MAST (BEAM NUMBERS)
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
70/163
CC 8800-1
NODE NUMBERS
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
71/163
CC 8800-1
JIB HEAD (NODE NUMBERS)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
72/163
LUFFING MASTS (NODE NUMBERS)
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
73/163
CC 8800-1
BOOM FOOT AND MAST (NODE NUMBERS)
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
74/163
CC 8800-1
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
75/163
CC 8800-1
PRESTAB_V6, Version V5.5h 22.11.2007:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 1 * 5.12.2007 13:38:55 *** 56575
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
76/163
p:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
CC 8800-1 SWSL 96+36 mr2621.05.2007 Wilhelm
Control output of the variable input------------------------------------------1. radius = 39.52. loadcase = 3. rated load = 257.04. reeving = 5. number of hoist lines back to the winch = 6. loads mass(n): ----------------------
node no. Radius[m] ----------------------
60 -22.000 Control output of the non variable input-----------------------------1. maximum torque = 480.02. minimum time of deceleration = 5.0
3. number of revolutions = 0.34. hoisting speed = 72.05. hoisting class = 6. node number of load = 7. windpressure on load = 60.08. counterweight = 220.09. distance between rotation axis/counterweight = 900.010.weight of superstructure = 36.811.distance between rotation axis/superstructure = 120.012.lateral inclination of boom system = 0.3
13.weight of hoist rope = 7.8
14.Guidance of hoist rope..........node numbers : 32, 31, 33, 38, 46, 5
15.load factors : -----------------------------------load- | loads :case | dead lifted test a-----------------------------------H | 1.20 1.35 0.00 1
HZ | 1.09 1.20 0.00 1HS | 1.09 0.00 1.09 1HZ*1 | 1.00 1.00 0.00 1-----------------------------------
Control output of the results
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 2 * 5.12.2007 13:38:55 *** 56575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
77/163
node masss and node loads / loadcase H--------------------------------------------------
node masss node loads---------------- -----------------------------
node - boom - lifted vertical horizontalno. loads acceleration
system Y X Z -----------------------------------------------------------
[t] [t] [kN] [kN] [kN] ===========================================================
1 8.350 -- -98.57 8.81 0.03 02 13.000 -- -153.46 13.72 0.05 03 0.000 -- 0.00 0.00 0.00 04 4.785 -- -57.50 -4.91 0.01 05 11.400 -- -134.58 12.03 0.04 06 16.550 -- -195.37 17.47 0.06 07 19.600 -- -231.37 20.68 0.08 08 19.050 -- -224.88 20.10 0.09 0
9 14.150 -- -167.04 14.93 0.08 010 9.800 -- -115.69 10.34 0.06 011 13.600 -- -160.55 14.35 0.08 012 16.700 -- -197.14 17.62 0.11 013 16.000 -- -188.88 16.89 0.11 014 8.000 -- -94.44 8.44 0.06 015 5.600 -- -66.11 5.91 0.04 016 5.600 -- -66.11 5.91 0.04 017 2.867 -- -35.15 2.68 0.02 018 0.100 -- -1.28 -0.01 0.00 0
19 0.000 -- 0.00 0.00 0.00 020 0.000 -- 0.00 0.00 0.00 021 0.000 -- 0.00 0.00 0.00 022 2.600 -- -33.04 1.25 0.03 023 6.100 -- -77.52 2.92 0.10 024 1.275 -- -15.50 -1.25 0.01 025 0.000 -- 0.00 0.00 0.00 026 8.950 -- -113.75 4.29 0.18 027 8.575 -- -108.98 4.11 0.30 028 6.250 -- -79.43 3.00 0.26 0
29 8.075 -- -102.62 3.87 0.40 030 7.200 -- -90.47 0.26 0.37 031 4.365 -- -54.65 -2.54 0.22 032 8.800 257.00 -3745.50 0.00 13.95 033 2.150 -- -26.14 -2.11 0.01 034 2.075 -- -25.23 -2.04 0.01 0
CC 8800-1
52 3.000 -- -36.89 -2.45 -0.08 053 2.000 -- -23.77 2.10 -0.05 054 2.000 -- -25.45 -0.89 -0.05 0
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
78/163
55 0.250 -- -3.18 0.12 -0.01 056 10.192 -- -122.67 -4.80 -0.30 057 5.500 -- -67.68 -5.00 -0.05 058 8.312 -- -101.55 -7.87 -0.14 059 0.000 -- 0.00 0.00 0.00 060 3.673 640.00 -6319.48 -3.88 -18.79 061 0.511 -- -6.12 -0.53 -0.01 062 0.000 -- 0.00 0.00 0.00 063 0.000 -- 0.00 0.00 0.00 0
===========================================================loads -20.55
SUM : 389.150 640.00 -14630.96 122.75 16.84 0-3.71
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 3 * 5.12.2007 13:38:55 *** 56575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
79/163
CW-Value 1.60 [/]
beam- node- angle length weight windareano. numbers t.horiz
-----------------------------------------------------------[degr] [cm] [t] [qm/lfm]
===========================================================1 1 2 88.00 400.0 16.700 2.0182 5 6 88.00 375.0 13.500 2.0833 2 3 178.00 137.5 0.000 0.0004 2 4 168.98 159.5 0.000 0.0005 2 5 88.00 225.0 9.300 2.2066 6 7 88.00 1200.0 19.600 1.9527 7 8 88.00 1200.0 19.600 1.9528 8 9 88.00 1200.0 18.500 1.9569 9 10 88.00 600.0 9.800 2.10210 10 11 88.00 600.0 9.800 2.10211 11 12 88.00 1200.0 17.400 1.95212 12 13 88.00 1200.0 16.000 1.952
13 13 14 88.00 1200.0 16.000 1.95214 14 15 88.00 200.0 0.000 2.00015 15 16 88.00 55.0 11.200 2.00016 15 17 178.00 130.0 0.000 0.00017 17 18 178.00 50.0 0.000 0.00018 17 19 19.10 68.6 0.000 0.00019 16 20 -2.00 75.0 0.000 0.00020 20 21 26.99 14.0 0.000 1.62021 21 22 26.99 246.0 0.000 1.62022 22 23 26.99 440.0 5.200 1.620
23 23 26 26.99 300.0 7.000 1.62024 21 24 116.99 140.0 0.000 0.00025 22 25 116.99 140.0 0.000 0.00026 26 27 26.99 1200.0 10.900 1.84627 27 28 26.99 600.0 6.250 1.96928 28 29 26.99 600.0 6.250 1.96929 29 30 26.99 200.0 9.900 1.50030 30 31 116.99 180.0 4.500 0.00031 30 32 -63.01 190.0 0.000 0.00032 24 33 111.64 330.0 2.550 1.013
33 33 34 111.64 192.0 1.750 1.15634 34 35 111.64 328.0 2.400 1.13235 35 36 111.64 1200.0 3.750 1.06436 36 37 111.64 600.0 4.200 1.02137 18 38 177.03 231.0 0.200 0.50038 38 39 177.03 296.0 2.200 0.650
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
80/163
CC 8800-1
:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: load control part 4 * 5.12.2007 13:38:55 *** 56575:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
81/163
results of basic load determination :node loads without factors in STAB84-global-components
node loads in [ kN ] :no. node mass beam mass acceleration forces
Y Y Y X Z -----------------------------------------------------------1 0.00 -81.89 -0.205 5.875 0.012 02 0.00 -127.49 -0.319 9.146 0.020 03 0.00 0.00 0.000 0.000 0.000 04 0.00 -46.92 -0.792 -3.274 0.003 05 0.00 -111.80 -0.280 8.021 0.018 06 0.00 -162.30 -0.407 11.644 0.028 07 0.00 -192.21 -0.482 13.790 0.038 08 0.00 -186.82 -0.468 13.403 0.041 09 0.00 -138.76 -0.348 9.956 0.034 010 0.00 -96.11 -0.241 6.895 0.025 011 0.00 -133.37 -0.334 9.569 0.036 012 0.00 -163.77 -0.410 11.750 0.049 013 0.00 -156.91 -0.393 11.257 0.051 014 0.00 -78.45 -0.197 5.629 0.027 015 0.00 -54.92 -0.138 3.940 0.019 016 0.00 -54.92 -0.138 3.940 0.019 017 0.00 -28.12 -0.935 1.789 0.008 018 0.00 -0.98 -0.070 -0.004 0.000 019 0.00 0.00 0.000 0.000 0.000 020 0.00 0.00 0.000 0.000 0.000 021 0.00 0.00 0.000 0.000 0.000 022 0.00 -25.50 -1.631 0.831 0.014 0
23 0.00 -59.82 -3.827 1.949 0.046 024 0.00 -12.50 -0.331 -0.834 0.005 025 0.00 0.00 0.000 0.000 0.000 026 0.00 -87.77 -5.614 2.860 0.082 027 0.00 -84.09 -5.379 2.740 0.133 028 0.00 -61.29 -3.921 1.997 0.116 029 0.00 -79.19 -5.066 2.580 0.176 030 0.00 -70.61 -3.824 0.170 0.164 031 0.00 -42.81 -2.181 -1.693 0.098 032 0.00 -86.30 0.000 0.000 6.202 0
33 0.00 -21.08 -0.558 -1.407 0.006 034 0.00 -20.35 -0.539 -1.358 0.005 035 0.00 -30.16 -0.798 -2.012 0.005 036 0.00 -38.98 -1.032 -2.601 -0.003 037 0.00 -66.22 -3.039 -0.198 -0.015 038 0.00 -11.77 -0.844 -0.044 0.001 0
CC 8800-1
56 0.00 -99.95 -1.819 -3.197 -0.132 057 0.00 -53.94 -1.970 -3.333 -0.021 058 0.00 -81.52 -2.487 -5.244 -0.060 059 0.00 0.00 0.000 0.000 0.000 0
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
82/163
59 0.00 0.00 0.000 0.000 0.000 0
60 0.00 -36.02 0.000 -2.586 -8.352 061 0.00 -5.01 -0.073 -0.352 -0.003 062 0.00 0.00 0.000 0.000 0.000 063 0.00 0.00 0.000 0.000 0.000 0
-----------------------------------------------------------SUM : 0.00 -3816.25 -88.835 81.833 -1.443 0
CC 8800-1
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% E I N Z E L S T A B - A N A L Y S I S %% =================================== %
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
83/163
% ( 5.12.2007 13:38:57) %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% CC 8800-1 SWSL 96+36 mr26 %% 21.05.2007 Wilhelm %% **************************************** %% E I N G A B E K O N T R O L L E : %% crane part 7 declin. 180.000 [deg]%% crane part 5 radius -22.000 [m] %% crane part 1 declin. 88.000 [deg]%% crane part 2 radius 39.560 [m] %% loadcase H nom. load 257.000 [t] %% reeving 5 %% node num. 60 add. mass 640.000 [t] %% **************************************** %% F R E I E T E X T E I N G A B E : %% variante 1 , wippbarer hilfsausleger %% **************************************** %% * 5.12.2007 13:38:55 *** 565757555350 * %% %%%%%%%%%%%% Version 5.0g vom 18.06.2007 %%%%
number of beams 66number of nodes 63
beam node length Ndiag section no. sectionnumber KA KE (cm) Stab84 Einzel
( 1) 1 2 399.99 2 1 1 tapered( 2) 5 6 374.99 2 2 2 standar( 3) 2 3 137.50 0 3 0 -------( 4) 2 4 159.47 0 4 0 -------( 5) 2 5 225.00 1 5 3 standar( 6) 6 7 1199.98 7 6 4 standar( 7) 7 8 1199.98 7 7 5 standar( 8) 8 9 1199.99 7 8 6 standar( 9) 9 10 600.00 4 9 7 standar( 10) 10 11 600.01 4 10 8 standar
( 11) 11 12 1200.03 7 11 9 standar( 12) 12 13 1200.05 7 12 10 standar( 13) 13 14 1200.07 7 13 11 standar( 14) 14 15 200.01 0 14 0 -------( 15) 15 16 55.00 0 15 0 -------( 16) 15 17 130.00 0 16 0 -------
CC 8800-1
( 34) 34 35 328.01 3 34 19 standar( 35) 35 36 1199.99 10 35 20 standar( 36) 36 37 599.99 5 36 21 tapered( 37) 18 38 231.00 0 37 0 -------
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
84/163
( 38) 38 39 296.00 3 38 22 tapered( 39) 39 40 223.00 2 39 23 standar( 40) 40 41 1200.00 10 40 24 standar( 41) 41 42 600.01 5 41 25 tapered( 42) 43 44 684.99 6 42 26 tapered( 43) 44 47 215.00 1 43 27 standar( 44) 44 45 138.50 0 44 0 -------( 45) 44 46 113.99 0 45 0 -------( 46) 47 48 1199.98 8 46 28 standar( 47) 48 49 1200.01 8 47 29 standar
( 48) 49 50 800.03 6 48 30 standar( 49) 50 51 274.01 2 49 31 standar( 50) 51 52 416.02 4 50 32 tapered( 51) 52 56 210.01 0 51 0 -------( 52) 51 53 125.65 0 52 0 -------( 53) 51 54 131.21 0 53 0 -------( 54) 52 55 65.00 0 54 0 -------( 55) 57 58 1165.00 0 55 0 -------( 56) 59 60 1100.00 0 56 0 -------( 57) 17 56 5735.13 0 57 0 -------( 58) 58 61 1135.54 0 58 0 -------( 59) 4 42 9570.42 0 59 0 -------( 60) 37 42 3072.88 0 60 0 -------( 61) 31 37 4230.60 0 61 0 -------( 62) 56 58 3540.50 0 62 0 -------( 63) 56 60 4591.18 0 63 0 -------( 64) 3 62 369.21 0 64 0 -------( 65) 45 63 553.12 0 65 0 -------( 66) 19 25 409.94 0 66 0 -------
CC 8800-1
SECTION PROPERTIES=================================
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
85/163
section type : standard lattice mast [cm,kN]=====================================
( 2) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 3.75m paral. Teil Nr.2 R2
LV LW field length cantilev-A cantil275.0 320.0 330.3 0.0 3
upp. chord low. chord upp. diags low. dia
pipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62
area 358.38 358.38 38.08 42.
----------------------------------------------------------( 3) /berechnung/stab84/gerdaten/cc8800-1/teile/fussha3227CC8800-1 17.03.2006 W.Zim. HA-Fu 2.25m paral. Teil Nr.1 R2
LV LW field length cantilev-A cantil275.0 320.0 441.0 0.0
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 4) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-45-12CC8800-1 16.03.2006 W.Zim. Projekt ZW 12m 3227-45 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62area 358.38 358.38 38.08 42.
----------------------------------------------------------( 5) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-45-12CC8800-1 16.03.2006 W.Zim. Projekt ZW 12m 3227-45 3.5 Felder
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*4.50 29.85*4.50 17.78*0.71 17.78*0.
Beta-S/limit 67.0/ 60.3 67.0/ 60.3 69.0/ 62.1 69.0/ 62
CC 8800-1
LV LW field length cantilev-A cantil275.0 320.0 256.8 38.0 3
upp. chord low. chord upp. diags low. dia
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
86/163
pipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62
area 296.88 296.88 38.08 42.
----------------------------------------------------------( 8) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-36-60ZW 6m 3227-36 2 Felder CC8800 13.7.2000 W.Zim. Gurtrohre StE
StE690LV LW field length cantilev-A cantil275.0 320.0 256.8 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62area 296.88 296.88 38.08 42.
----------------------------------------------------------( 9) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-36-12CC8800-1 16.3.2006 W.Zim. ZW 12m 3227-36 3.5 Felder 3227-36
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.60 29.85*3.60 17.78*0.71 17.78*0.
Beta-S/limit 70.0/ 63.0 70.0/ 63.0 69.0/ 62.1 69.0/ 62area 296.88 296.88 38.08 42.
----------------------------------------------------------( 10) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-30-12CC8800-1 16.3.2006 W.Zim. ZW 12m 3227-30 3.5 Felder 3227-30
LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*3.00 29.85*3.00 17.78*0.71 17.78*0.
Beta-S/limit 65.0/ 58.5 65.0/ 58.5 69.0/ 62.1 69.0/ 62area 253.06 253.06 38.08 42.
----------------------------------------------------------
( 11) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-30-12CC8800-1 16.3.2006 W.Zim. ZW 12m 3227-30 3.5 Felder 3227-30LV LW field length cantilev-A cantil275.0 320.0 314.7 38.0 3
upp. chord low. chord upp. diags low. dia
CC 8800-1
----------------------------------------------------------( 16) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-20-60CC8800-1 16.03.2006 W.Zim. ZW 6m 3227-20.0 2 Felder 3227-20
LV LW field length cantilev-A cantil
275 0 320 0 256 8 38 0 3
-
7/29/2019 Structural Analysis Terex Demax Latice Crane
87/163
275.0 320.0 256.8 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*2.00 29.85*2.00 15.24*0.56 15.24*0.
Beta-S/limit 75.0/ 67.5 75.0/ 67.5 46.0/ 41.4 46.0/ 41area 174.99 174.99 25.83 32.
----------------------------------------------------------( 17) /berechnung/stab84/gerdaten/cc8800-1/teile/3227-20-60CC8800-1 16.03.2006 W.Zim. ZW 6m 3227-20.0 2 Felder 3227-20
LV LW field length cantilev-A cantil275.0 320.0 256.8 38.0 3
upp. chord low. chord upp. diags low. diapipe 29.85*2.00 29.85*2.00 15.24*0.56 15.24*0.
Beta-S/limit 75.0/ 67.5 75.0/ 67.5 46.0/ 41.4 46.0/ 41area 174.99 174.99 25.83 32.
--------------------------------------------------