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NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
New Technology for Dramatically
Improving Reciprocating Compressor Performance
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Brief Technical Background
2013: Commercial release of Virtual Pumping Station & Design Software;Project opportunity at Williams sta. 85.
2006: OPT & El Paso cooperate to model Ariel compressor cylinder.
2007: OPT & ACI cooperate to model a cylinder compressor; GMC Paper on Tuned Loops and Tuning Section Transitions
2008: Lab testing of PAN for 2 DA cyl. air compressor;GMC Paper on Air Compressor Test Rig
2009: 2 throw proof of concept test on Superior MH64 at TGT Ellisburg station;GMC Paper comparing PAN simulation & field test results.
2010: Designed PAN for El Paso Sta. 96; Project cancelled due changing pipeline flows.Continued research on PAN tuned manifolds.
2012: Kinder Morgan acquired El Paso & withdrew Batesville.
2011: Research to increase compressor efficiency via tuning;GMC Paper on Performance Augmentation Networks;El Paso Batesville Sta. design & GMRC project. initiated.
2014: Sta. 85 field installation & testing.GMRC Paper on test results.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
The History of Unsteady Gas Dynamics in Pipes• Initial development in Europe in the mid 20th Century.• Queens University of Belfast took the academic research lead.• Professor Gordon P. Blair, CBE became its leading spokesperson publishing over
100 SAE papers and two reference text books.• High performance racing engine simulation and design was his passion.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
The Development of Virtual Engines andVirtual Pumping Stations• 1993 OPTIMUM Power Technology entered into a development partnership with QUB
and developed its Virtual Engines design software based on this physics.– VE was licensed to Honda, Toyota Racing Development (TRD), Ilmor, Hendrick
Motorsports and others who used it very successfully for racing engine design.– VE was licensed to Cameron for natural gas engine development.– Because engines breathe air at 1 atmosphere, the thermodynamics of VE is based
on ideal gas laws.• OPTIMUM Pumping Technology enhanced VE to accurately simulate natural gas
reciprocating compressors – Virtual Pumping Station.– Virtual Pumping Station was enhanced to use real gas physics based on NIST data.– Dynamic (mass‐spring) check‐valve support was added.– Infinite step unloader support.– Loop PAN pulsation comb filter technology was developed.– Manifold PAN technology was developed.– Cameron became the 1st VPS customer.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Principles of Unsteady Gas Dynamics in Pipes• Finite amplitude unsteady gas dynamics is fundamentally different from
and far more complex than steady state gas flow theory.• It is as different as electrical AC circuit theory is from DC circuit theory.• Finite amplitude unsteady gas dynamics is fundamentally different from
and far more complex than acoustic theory.• Finite amplitude pressure waves change the media as they propagate.• They transmit and reflect at pipe area changes and everywhere the
media in the pipe changes its properties.• In any pipe that is experiencing unsteady-pulsing flow, there are 2
waves propagating in opposite directions. The convention is to call them the Right wave and the Left wave.
• The sum of these 2 waves is the superposition pressure that we measure with pressure transducers.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
PAN Virtual Pumping Station Animation of Cylinder 1Head End, Crank End, Check Valves and Header Pipe
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
PAN Virtual Pumping Station Flow Diagram
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Bottles and PANs are FUNDAMENTALLY DifferentBottle systems• Reduce pulsation to acceptable levels• DISSIPATE 95% of pulsation energy• Process each throw INDIVIDUALLY• Components
• Primary and secondary bottle volumes• Choke tubes• Orifice plates
• Problems:• Pressure loss• Poorly phased cyclical flange pressure
that reduces adiabatic efficiency of the compressor
• Bottle vibration problems
• Bottles CANNOT be modified to perform like a PAN
PANs• Reduce pulsation to acceptable levels• RECOVER 95% of pulsation energy• Process ALL throws as a SYSTEM• Components
• Primary TST W or Y junction recovers pulsation energy
• Secondary Y TST junction to join flow from both sides of compressor to reduce pulsation
• Standard pipe• OPTIMIZED TSTs, pipe diameters and
lengths• Benefits:
• NO pressure loss• Greatly improved cyclical flange
pressure significantly increases compressor adiabatic efficiency
• Reduced operation cost• Reduced power/engine emissions• Increased flow• Reduced vibration caused failures
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
2008: Laboratory (2) DA Cylinder Air Test
1000 RPM, 21 PSIA, Y with 15' & 10' loopsFull load
17.518
18.519
19.520
20.521
21.522
22.523
23.524
24.525
25.526
26.5
-180 -135 -90 -45 0 45 90 135 180Crank angle (deg.)
Pres
sure
(PSI
)
Head 1 Head 2 After Y After 1st loop After 2nd loop
0.7% P/P discharge pulsation
2 x Quincy single stage500 ‐ 1000 rpm2 DA cylinder discharge PAN
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
2009: El Paso Ellisburg Field Test – 2nd Generation
PAN Side vs BOTTLE Side Pressure Drop ComparisonPressure drop (PR = 1.1)
896 psig Avg. Discharge Pressure
0
1
2
3
4
5
6
7
8
9
10
11
860 880 900 920 940 960 980 1000Speed (RPM)
Pres
sure
dro
p (P
SI)
BOT Cyl 1 to LINE PAN Cyl 2 to LINE BOT Cyl 3 to LINE PAN Cyl 4 to LINELinear (PAN Cyl 2 to LINE) Linear (PAN Cyl 4 to LINE) Linear (BOT Cyl 1 to LINE) Linear (BOT Cyl 3 to LINE)
Traditional Bottle System - Cyl. 1 & 3
Bottle-less Pan System - Cyl. 2 & 4
Cyl. 3
Cyl. 1
Cyl. 2
Cyl. 4
1000 RPM Fully Loaded
870.0
880.0
890.0
900.0
910.0
920.0
930.0
940.0
0 45 90 135 180 225 270 315 360 405 450 495 540 585 630 675 720Angle
Pres
sure
(PSI
)
NozzleStart of 1st loopAfter PAN
5.5 psig less discharge pressure drop 0.4% P/P discharge pulsation
Superior MH64 single‐stage750 ‐ 1000 rpm2 DA cylinder discharge PAN
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
2010: El Paso Sta. 96 Conversion Design – 3rd Generation
Flange ‐> W‐TST ‐> Side Pipe ‐> Y‐TST ‐> Pipeline
Ariel KVB/6 single‐stage720 rpm constant speed6 DA cylinder PAN manifoldInfinite step unloading
Cancelled due to PL flow demand change.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
2011: El Paso Batesville Conversion Design – 4th Generation
Ariel KVB/6 single‐stage500 ‐ 750 rpm6 DA cylinder PAN manifold8 symmetric unloading steps
GMRC & El Paso Project Objectives– No Compressor Modifications– Variable Speed– 8 Load Steps with ACI Pockets – CONTINUOUS Unloading– Less than 1% P/P pulsation under all operating conditions– 90% Reduction in system pressure Loss– Acceptable vibration– Demonstrate that PANs can significantly improve the efficiency far beyond
the benefits of reduced pressure loss
Cancelled due to KM acquisition.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
4th Generation PAN Improved Adiabatic Efficiency
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
2013 Progress & Status• GMRC Royalty Agreements have been negotiated with OPTIMUM Pumping• A second Virtual Pumping Station 6‐throw baseline bottle compressor model has
been 90% validated• New test site at Williams Sta. 85 identified May 2013
‐ 2 identical units to be re‐cylindered: one with PAN; one with new bottles.‐ Project schedule is fast track and has to move forward right away to meet the
station’s contractual needs. ‐ Project has been planned to accomplish GMRC Project’s objectives, with
sequence adapted from El Paso project.‐ Modeling & simulation completed and presented herein.‐ Mechanical design nearly completed.‐ System mechanical analysis ready to start after review meeting. ‐ TST production ready to start.‐ Williams project team $$ approval pending – (now
the pacing item in schedule).
2 identical Cat G3616 & Ariel JGZ/6 Packages Requiring Re‐cylindering‐ 1 unit to have PAN‐ 1 unit to have new bottles
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Williams Sta. 85 – New Cylinders & Unloading
Unloading selected based on bottle system.HE FVCPs on each cylinder.No CE FVCPs required.No SACE load steps required.
Cat G3616 & Ariel JGZ/6 with (6) 9.75” ZL cylinders
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Primary Project Objectives• Total system pressure drop from suction line to discharge line less than 2 psig at
all operating points.• Control of pulsation to less than 1.5% of line pressure level at all operating
conditions.• Control of mechanical vibrations and stress levels consistent with API 618 M5
requirements.• A 10% reduction in compressor BHP/MMSCFD at the high flow operating
condition (compared to bottle system).
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Secondary Project Objectives• The ability of OPTIMUM’s Virtual Pumping Station software to predict the pressure
drop, pulsation and BHP/MMSCFD of the re‐cylindered compressor with the PAN installed.
• The ability of the Virtual Pumping Station software to predict the pressure drop, pulsation and BHP/MMSCFD of the re‐cylindered compressor with the Bottles installed.
• The ability of OPTIMUM’s design optimization software to create a PAN that simultaneously achieves all of the primary objectives of the project.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Project TeamACI Services Inc.• Norm Shade – ACI (executive project management)• John Bazaar – ACI (project management; mechanical design, analysis)• Tyler Clark – ACI (mechanical design, analysis, CAD modeling)• Jessica Gilcher – ACI (design, CAD modeling)• Joe Mosely – ACI (CAD modeling)• Nak Nortey – ACI (FEA)• Beta Machinery Analysis – (system mechanical analysis)
OPTIMUM Power Technology• Glen Chatfield – OPT (project management; simulation & PAN design)• Dale Wells – OPT (simulation & PAN design)• Malcom Ashe – OPT (valve modeling/simulation)
Williams• Patrick Jacobs• Scott Schubring
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Project Schedule with MilestonesCylinder selection (Williams) ‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐5/15/13 DoneFinal cost estimate & schedule to Williams‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐5/31/13 DoneDraft contract to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐6/7/13 8/31/13 est.Initial PAN model development & simulation (OPT)‐‐‐‐‐‐‐‐‐‐‐‐6/15/13 DoneGMRC contract signed‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐6/30/13 10/7/13Invoice #1 to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐7/23/13 10/7/13Begin solicitation of co‐funding‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐7/1/13 9/1/13Mechanical layout (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐6/30/13 DoneFinal PAN model (ACI/OPT)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐7/8/13 DonePresent PAN Model results to Williams & PSC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐7/12/13 8/13/13Williams & GMRC decision to proceed‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐7/16/13 8/15/13Complete TST design & FEA (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/7/13 9/16/13Complete detailed mechanical design (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/15/13 8/30/13Finalize support & pier/foundation design (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/15/13 8/30/13Begin TST patterns (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/16/13 10/1/13Complete valve analysis‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐9/16/13 10/15/13Complete system mechanical analysis (ACI/contractor)‐‐‐‐‐‐‐‐9/16/13 10/15/13Present mechanical analysis results to Williams & PSC‐‐‐‐‐‐‐‐‐9/18/13 10/17/13Williams & GMRC decision to proceed‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐9/20/13 10/19/13Invoice #2 to GMRC 9/22/13 10/19/13
* l / /
5/12* Schedule
CurrentSchedule
Current
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Project Schedule with Milestones5/12*
ScheduleCurrentSchedule
Order PAN material (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐9/23/13 10/21/13 Complete new #2 unit bottle design (Enerflex)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐10/31/13 10/31/13Model & simulate new bottles (OPT)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐11/30/13 11/30/13Complete test protocol & define instrumentation‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐N/A 12/15/13Invoice #3 to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐1/7/14 1/7/14Complete TSTs (ACI)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐1/15/14 1/15/14Complete PAN & supports fabrication (ACI/contractor)‐‐‐‐‐‐‐2/28/14 2/28/14Invoice #4 to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐3/1/14 3/1/14Remove existing bottle system & install piers (Williams)‐‐‐‐‐‐3/31/14 3/31/14Install new cylinders (Williams)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐4/8/14 4/8/14Install PAN on Unit #1 & bottles on Unit #2 (Williams)‐‐‐‐‐‐‐‐‐4/22/14 4/22/14Hydrostatic testing and support installation (Williams)‐‐‐‐‐‐‐‐4/30/14 4/30/14Onsite static mechanical test (team)‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐5/7/14 5/7/14Mechanical & performance testing (ACI/OPT/contractor)‐‐‐‐‐5/24/14 5/24/14Acceptance‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐5/31/14 5/31/14Invoice #5 to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐6/14/14 6/14/14Final report to Williams & GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/?/14 8/12/14Invoice #6 to GMRC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐8/31/14 8/12/14Report results at 2014 GMC‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐‐10/?/14 10/6/14
* Preliminary estimate 5/12/13
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – As Is
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – 5th Generation PAN
8”
8”
12”
12”
16”
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Preliminary Supports & Platform
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Top View
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Top View
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Site Work
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Site Work
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Site Work
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design – Site Work
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Mechanical Design ‐ Prefabrication
Disch W-TST
Suct W-TST
Suct Y-TST
Disch Y-TST
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction Pressure vs. Crank Angle @ 950 RPMDesign Pt. 3: 850 psig (864.7 psia) suction / 1307 psig (1321.7 psia) discharge – fully loaded
@ Cyl. Flange
After W-TST
After Y-TST
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction Pressure Animation @950rpmDesign Pt. 3: 850psig (864.7 psia) suction / 1307psig (1321.7 psia) discharge – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge Pressure vs. Crank Angle @ 950 RPMDesign Pt. 3: 850 psig (864.7 psia) suction / 1307 psig (1321.7 psia) discharge – fully loaded
After W-TST
@ Cyl. Flange
After Y-TST
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge Pressure Animation @950rpmDesign Pt. 3: 850psig (864.7 psia) suction / 1307psig (1321.7 psia) discharge – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionPV Chart @950rpmDesign Pt. 3: 850psig (864.7 psia) suction / 1307psig (1321.7 psia) discharge – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance Comparison
• Comparison of eRCM Bottle** predictions to VPS PAN predictions• PAN Averages 17% Greater Efficiency and• PAN Averages 14% Greater Flow• Never Exceeded Rated BHP at Full Load (i.e., No Unloading)
** Bottle system pressure drop 2% suction and 1% discharge (lower than GMRC Guideline).
STATION 85 ‐ 6 VERY DIFFERENT DESIGN POINT OPERATING CONDITIONS
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionMMSCFD v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP/MMSCFD v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loadedVery good over entire speed range.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction P/P Pulsation v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded0.1 to 0.5%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge P/P Pulsation v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded0.1 to 0.6%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction Pressure Loss v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded0.4 to 0.2 psi pressure gain
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge Pressure Loss v. RPMDesign Pt. 3: 850 psig suction / 1307 psig discharge – fully loaded0.0 to 0.5 psi pressure loss [Total avg. Suct + Disch Pressure Loss = 0.06 psi]
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP v. RPMAll Design Points – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionMMSCFD v. RPMAll Design Points – fully loaded
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP/MMSCFD v. RPMAll Design Points – fully loadedVery good over entire speed range.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction P/P Pulsation v. RPMAll Design Points – fully loaded0.2 to 0.7%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge P/P Pulsation v. RPMAll Design Points – fully loaded0.1 to 0.6%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction Pressure Loss v. RPMAll Design Points – fully loaded0.4 to 0.1 psi pressure gain
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge Pressure Loss v. RPMAll Design Points – fully loaded‐0.6 to +0.6 psi pressure loss
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP v. RPMAll Design Points – fully unloaded (6 HE pockets open)
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionMMSCFD v. RPMAll Design Points – fully unloaded (6 HE pockets open)
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionBHP/MMSCFD v. RPMAll Design Points – fully unloaded (6 HE pockets open)Very good over entire speed range.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction P/P Pulsation v. RPMAll Design Points – fully unloaded (6 HE pockets open)0.6 to 1.3%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge P/P Pulsation v. RPMAll Design Points – fully unloaded (6 HE pockets open)0.3 to 1.2%
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionSuction Pressure Loss v. RPMAll Design Points – fully unloaded (6 HE pockets open)0.3 to 0.0 psi pressure gain
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Performance PredictionDischarge Pressure Loss v. RPMAll Design Points – fully unloaded (6 HE pockets open)0.0 to 0.5 psi pressure loss
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Primary Project Objectives Comparison• Total system pressure drop from suction line to discharge line less than 2 psi at all
operating points. – Simulation Results: All points less than 0.3 psi = Objective met.
• Control of pulsation to less than 1.5% of line pressure level at all operating conditions.– Simulation Results: Worst case 0.6% fully loaded / 1.3% with maximum
unloading = Objective met.• Control of mechanical vibrations and stress levels consistent with API 618 M5
requirements.– Next investigative phase (to be reported in October)
• A 10% reduction in compressor BHP/MMSCFD at the high flow operating condition (compared to bottle system).– Simulation Results: average 17% reduction at 6 design points = Objective met.
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Project Cost EstimateCost Estimated
CostACI/OPT
Contribut’nWilliams Cost*
GMRC Cost
System Modeling , Optimization & Eng. (OPT) $150,000 $0 $0 $150,000Previous uncompensated Batesville Sta. (OPT) $95,000 $95,000 $0 $0Previous uncompensated Batesville Sta. (ACI) $67,000 $67,000 $0 $0
System Design and Drwg Development (ACI) $72,000 $72,000 $0 $0System Mechanical Analysis (contractor) $27,500 $0 $0 $27,500Project Management Services (ACI ) $32,000 $32,000 $0 $0 TSTs including P&T for new designs (ACI) 229,200 $71,500 $0 $157,700Remove Existing System (Williams) $28,300 $0 $28,300 $0Procure/Fabricate PAN & supports (ACI) 283,250 $0 $0 $283,250Install New PAN System (Williams) 298,700 $0 $298,700 $0Site Engineering Support (ACI & OPT) $96,000 $96,000 $0 $0 Field Mech & Perf Testing/Analys (contractor) $55,000 $0 TBD $55,000Travel Expenses for site support (ACI and OPT) $66,550 $0 $0 $66,550Contingency Modifications $100,000 $0 $0 $100,000PROJECT TOTAL $1,650,500 $433,500 $327,000 $840,000
*Approval Pending
NEW TECHNOLOGY FOR CONTROLLINGRECIPROCATING COMPRESSOR PULSATIONS
Performance Augmentation Network Technology (PAN) Full‐scale Field Test
08/13/2013 Report
Project Cost EstimateInvoice Schedule to GMRC Amount DateGMRC Invoice 1 – 15% $126,000 10/7/13GMRC Invoice 2 – 10% $84,000 10/19/13GMRC Invoice 3 – 25% $210,000 1/7/14GMRC Invoice 4 – 20% $168,000 3/1/14GMRC Invoice 5 – 25% $210,000 6/1/14GMRC Invoice 6 – 5% $42,000 8/31/14GMRC TOTAL $840,000
GMRC Funding Sources & ScheduleGMRC approved maximum 2012 $250,000 AvailableAriel Co‐funding $100,000 AvailableCaterpillar Co‐funding $100,000 AvailableGE Water & Power Co‐funding $50,000 AvailableDresser‐Rand Co‐funding $20,000 AvailableAdditional GMRC request 2013 $150,000 10/11/13Additional Co‐funding TBD $170,000 3/31/13GMRC TOTAL $840,000Contingency Co‐funding TBD $100,000