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Engines and Energy Conversion Laboratory DOE Project DE-FC26-04NT42270: Systematic Engine Uprate Technology Development and Deployment through Increased Torque “Engine Uprates” DOE/ NETL Project Kickoff April 21, 2005

DOE Project DE-FC26-04NT42270: Systematic Engine Uprate ...“The overall objective of this project is to develop new engine up- rate technologies that will be applicable to a large

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  • Engines and Energy Conversion Laboratory

    DOE Project DE-FC26-04NT42270:Systematic Engine Uprate Technology Development and Deployment through

    Increased Torque

    “Engine Uprates”

    DOE/ NETL Project KickoffApril 21, 2005

  • Engines and Energy Conversion Laboratory

    Outline

    • Executive Summary (Ted)• Previous Work done with GTI Funds (Dan)• DOE Year 1 Results To-Date (Dan)• Planned Research Activities (Dan)

  • Engines and Energy Conversion Laboratory

    “The overall objective of this project is to develop new engine up-rate technologies that will be applicable to a large inventory of existing pipeline compressor units for the purpose of increasing pipeline

    throughput with the same footprint of existing facilities”

    •Increase Output by 10% •Target Cost ~ $500/HP

    Engine Uprates: Motivation

  • Engines and Energy Conversion Laboratory

    Objectives by Year

    • Year 1: Laboratory Demonstration of Candidate Technologies– Demonstrate that the technologies developed during the

    background research phase to achieve the performance targets under controlled, laboratory conditions and using the Engines and Energy Conversion Laboratory's (EECL's) Clark TLA research engine.

    • Year 2 (Phase 2): Demonstration of Optimal Technologies– Demonstrate that the technologies tested under phase 1 can

    migrate to an operating engine in pipeline service with similar, or better, performance and that the durability of the retrofit equipment will be acceptable.

  • Engines and Energy Conversion Laboratory

    Issues to Keep in Balance

    • OEM Business Strategy– Dresser-Rand– Cooper Compression

    • Enabling Technologies• Air Emissions Permits• FERC Capacity Certification

  • Engines and Energy Conversion Laboratory

    Guidance from manufacturer

    perspective

    Guidance from user perspective

    Engine Manufacturer, Dresser-Rand

    (Doug Bird)

    PRCI CAPSTC

    Project Lead: Ken Gilbert, Dominion Pipeline

    Department of Energy

    Colorado State University

    PI: Dan Olsen

    Reporting

    Project Team

  • Engines and Energy Conversion Laboratory

    Year 1 Project Schedule

    Task O04

    N04

    D04

    JO5

    FO5

    M05

    A05

    M05

    J05

    J05

    A05

    S05

    O05

    1.1 Research Management Plan complete

    1.2 Technology Assessment complete

    1.3 Optical Engine Evaluations

    1.4 Component Procure & Fab

    1.5 System Test Plan M1

    1.6 Uprate Systems Installation

    1.7 Testing of Uprate Systems M2

    1.8 Annual Contractor Review

    Semi-Annual Progress Report

  • Engines and Energy Conversion Laboratory

    Year 2 Project Schedule

    Task O05

    N05

    D05

    JO6

    FO6

    M06

    A06

    M06

    J06

    J06

    A06

    S06

    O06

    2.1 Selection of Field Test Unit

    2.2 Component Procure/ Fab

    2.3 Field Test Plan

    2.4 Component Procure & Fab

    2.5 Uprate System Field Install

    2.6 Uprate System Field Test

    2.7 Technology Transfer Plan

    2.8 Annual Contractor Review

    Semi-Annual Progress Report

  • Engines and Energy Conversion Laboratory

    Funding Sources

    2003 2004 2005 2006GTI Only $240,000(FERC funds)GTI Cost-Share$100,000(FERC funds)

    1 1

    PRCI$160,000(Industry funds)

    2 2 2 2

    DOE$150,000 (Yr 1)$250,000 (Yr 2)

    1 1 1 1 2 2 2 2

  • Engines and Energy Conversion Laboratory

    Expenditures

    DOE Project DE-FC26-04NT42270CSU Expenditures of DOE Funds

    0

    20000

    40000

    60000

    80000

    100000

    120000

    140000

    160000

    1 2 3 4 5 6 7 8 9 10 11 12

    Months

    Cum

    mul

    ativ

    e Fu

    nds,

    $

    BudgetedActual

    Chart1

    1250012500

    2500025000

    3750037500

    5000050000

    6250074858

    7500099720

    87500124575

    100000

    112500

    125000

    137500

    150000

    Budgeted

    Actual

    Months

    Cummulative Funds, $

    DOE Project DE-FC26-04NT42270CSU Expenditures of DOE Funds

    Sheet1

    MonthsBudgetedActual

    11250012500

    22500025000

    33750037500

    45000050000

    56250074,858

    67500099,720

    787500124,575

    8100000

    9112500

    10125000

    11137500

    12150000

    Sheet2

    Sheet3

  • Engines and Energy Conversion Laboratory

    Outline

    • Executive Summary• Previous Work done with GTI Funds• DOE Year 1 Results To-Date• Planned Research Activities

  • Engines and Energy Conversion Laboratory

    Identify Potential Engines: Engine Candidates

    Desired Engine Candidate Requirements• BMEP vs. Quantity

    Want to find engines with:• Low BMEP• Significant Installed Base• 2-Stroke

  • Engines and Energy Conversion Laboratory

    Identify Potential Engines: Engine Uprates Survey Table

    Manufacturer Family #Units Total HP Type (2/4 stroke) Cyl. Dims.Cylinder

    Configurations Air Delivery BMEP

    BA 145 203507 2 17x17 5,6,8,10 Piston Scavenged 68.3HBA 245 410644 2 17x17 5,6,8,10 Piston Scavenged 75.3HLA 44 91950 2 17x19 5,6,8,10 Nat. Asp. 76.5TLA 284 665074 2 17x19 5,6,8,10 Turbocharged 103.3KVG 286 310588 4 15.25x18 6,8,10,12 Nat. Asp. 80.34KVS 225 411235 4 15.25x18 6,8,10,12 Elliott Turbo. 121.7GMV 305 305219 2 14x14 4,6,8,10 Piston Scavenged 61.3

    GMVA 136 170539 2 14x14 4,6,8,10,12 Blower 79.2-84.3GMW 189 422080 2 18x20 6,8,10 Blower 74.5

    GMWA 216 453100 2 18x20 6,8,10,12 Blower 77.5

    Clark

    Ingersoll-Rand

    Cooper-Bessemer

    Sheet1

    Engine Uprates Survey Table

    ManufacturerFamily#UnitsTotal HPType (2/4 stroke)Cyl. Dims.Cylinder ConfigurationsAir DeliveryBMEP

    ClarkBA145203507217x175,6,8,10Piston Scavenged68.3

    HBA245410644217x175,6,8,10Piston Scavenged75.3

    HLA4491950217x195,6,8,10Nat. Asp.76.5

    TLA284665074217x195,6,8,10Turbocharged103.3

    Ingersoll-RandKVG286310588415.25x186,8,10,12Nat. Asp.80.34

    KVS225411235415.25x186,8,10,12Elliott Turbo.121.7

    Cooper-BessemerGMV305305219214x144,6,8,10Piston Scavenged61.3

    GMVA136170539214x144,6,8,10,12Blower79.2-84.3

    GMW189422080218x206,8,10Blower74.5

    GMWA216453100218x206,8,10,12Blower77.5

    Sheet2

    ManufacturerFamily#UnitsTotal HPType (2/4 stroke)Cyl. Dims.Cylinder ConfigurationsAir DeliveryBMEPCost

    ClarkBA145203507217x175,6,8,10Piston Scavenged68.3

    HBA245410644217x175,6,8,10Piston Scavenged75.3

    HLA4491950217x195,6,8,10Nat. Asp.76.5

    TLA284665074217x195,6,8,10Turbocharged103.3

    K5X11652218.5x196 (3 disabled)Turbocharged129.2

    Ingersoll-RandKVG286310588415.25x186,8,10,12Nat. Asp.80.34

    KVS225411235415.25x186,8,10,12Elliott Turbo.121.7

    Cooper-BessemerGMV305305219214x144,6,8,10Piston Scavenged61.3

    GMVA136170539214x144,6,8,10,12Blower79.2-84.3

    GMW189422080218x206,8,10Blower74.5

    GMWA216453100218x206,8,10,12Blower77.5

    Sheet3

  • Engines and Energy Conversion Laboratory

    Identify Potential Engines: Target Engines

    Based upon the engine survey table, the following engines meet the requirements:•Clark HBA•Clark TLA•Cooper-Bessemer GMV series

  • Engines and Energy Conversion Laboratory

    • Turbocharger Upgrade or Installation• High Pressure Fuel Injection• Micro Pilot Injection• Pre-Combustion Chambers• Intercooling• Piston Crown Re-design• Exhaust Tuning

    Technical Considerations: Potential Technologies

  • Engines and Energy Conversion Laboratory

    Block Diagram

  • Engines and Energy Conversion Laboratory

    B.S. NOx vs Load

    0

    2

    4

    6

    8

    10

    12

    14

    240 290 340 390 440 490

    Load (BHP)

    B.S

    . NO

    x (g

    /bhp

    -hr)

    MGAV @ 7.5"HPFI @ 7.5"HPFI @ 12"Adv. Ign. Sys. @ 16"

    MGAV -> HPFI

    Turbo Upgrade

    Adv. Ign. Sys.& More Boost

    IncreasedLoad

    Overall Reduction in NOx

    Final OperatingPoint

    Projected Reduction In NOx After Uprating Methods

    Data

    BS NOx @ 7.5" BoostBSFC @ 7.5" Boost

    LoadHPFI @ 7.5"MGAV @ 7.5"HPFI @ 7.5"MGAV @ 7.5"

    2650.41.91085011800

    3100.72.2955010300

    35512.586009300

    3802.13.184008800

    4003.24.582508600

    4409.711.881008400

    BS NOx @ 12" BoostBSFC @ 12" Boost

    LoadHPFI @ 12"MGAV @ 12"LoadHPFI @ 12"

    3150.25330012000

    3600.52.33309500

    4151.22.73609000

    4302.13.13908300

    4402.43.54208100

    4503.24.54408030

    4909.711.8

    Adv. Ign. Sys. @ 16"

    3150.05

    3600.15

    4150.25

    4300.45

    4400.75

    4702.2

    4904

    BHPBFSC

    4408100HPFI @ 7.5"

    8400MGAV @ 7.5"

    8050Adv. Ign. Sys. @ 12"

    8010Adv. Ign. Sys. @ 16"

    8200Adv. Ign. Sys. @ 20"

    8400MGAV @ 16"

    4847850Adv. Ign. Sys. @ 16" & 484 bhp

    Data

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Load (BHP)

    BSFC (btu/bhp-hr)

    BSFC vs Load

    BS NOx vs Load Graph

    265265315315

    310310360360

    355355415415

    380380430430

    400400440440

    440440450470

    490490

    MGAV -> HPFI

    Turbo Upgrade

    Adv. Ign. Sys.& More Boost

    IncreasedLoad

    Overall Reduction in NOx

    Final OperatingPoint

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Adv. Ign. Sys. @ 16"

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Adv. Ign. Sys. @ 16"

    Load (BHP)

    B.S. NOx (g/bhp-hr)

    B.S. NOx vs Load

    0.4

    1.9

    0.25

    0.05

    0.7

    2.2

    0.5

    0.15

    1

    2.5

    1.2

    0.25

    2.1

    3.1

    2.1

    0.45

    3.2

    4.5

    2.4

    0.75

    9.7

    11.8

    3.2

    2.2

    9.7

    4

    BSFC Bar Chart

    840081008050801082007850

    Potential Fuel SavingsAfter IncreasedBoost & Load

    MGAV @ 7.5"440 bhp

    HPFI @ 7.5"440 bhp

    Adv. Ign.Sys. @ 12"440 bhp

    Adv. Ign.Sys. @ 16"440 bhp

    Adv. Ign.Sys. @ 20"440 bhp

    Adv. Ign.Sys. @ 16"484 bhp

    MGAV @ 7.5"

    HPFI @ 7.5"

    Adv. Ign. Sys. @ 12"

    Adv. Ign. Sys. @ 16"

    Adv. Ign. Sys. @ 20"

    Adv. Ign. Sys. @ 16" & 484 bhp

    BSFC (btu/bhp-hr)

    Brake Specific Fuel Consumption

  • Engines and Energy Conversion Laboratory

    Brake Specific Fuel Consumption

    7700

    7800

    7900

    8000

    8100

    8200

    8300

    8400

    8500

    BSF

    C (b

    tu/b

    hp-h

    r) Potential Fuel Savings

    After IncreasedBoost & Load

    MGAV @ 7.5"440 bhp

    HPFI @ 7.5"440 bhp

    Adv. Ign.Sys. @ 12"

    440 bhp Adv. Ign.Sys. @ 16"

    440 bhp

    Adv. Ign.Sys. @ 20"

    440 bhp

    Adv. Ign.Sys. @ 16"

    484 bhp

    Projected Fuel Savings withUprating Methods

    Data

    BS NOx @ 7.5" BoostBSFC @ 7.5" Boost

    LoadHPFI @ 7.5"MGAV @ 7.5"HPFI @ 7.5"MGAV @ 7.5"

    2650.41.91085011800

    3100.72.2955010300

    35512.586009300

    3802.13.184008800

    4003.24.582508600

    4409.711.881008400

    BS NOx @ 12" BoostBSFC @ 12" Boost

    LoadHPFI @ 12"MGAV @ 12"LoadHPFI @ 12"

    3150.25330012000

    3600.52.33309500

    4151.22.73609000

    4302.13.13908300

    4402.43.54208100

    4503.24.54408030

    4909.711.8

    Adv. Ign. Sys. @ 16"

    3150.05

    3600.15

    4150.25

    4300.45

    4400.75

    4702.2

    4904

    BHPBFSC

    4408100HPFI @ 7.5"

    8400MGAV @ 7.5"

    8050Adv. Ign. Sys. @ 12"

    8010Adv. Ign. Sys. @ 16"

    8200Adv. Ign. Sys. @ 20"

    8400MGAV @ 16"

    4847850Adv. Ign. Sys. @ 16" & 484 bhp

    Data

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Load (BHP)

    BSFC (btu/bhp-hr)

    BSFC vs Load

    BS NOx vs Load Graph

    265265315315

    310310360360

    355355415415

    380380430430

    400400440440

    440440450470

    490490

    MGAV -> HPFI

    Turbo Upgrade

    Adv. Ign. Sys.& More Boost

    IncreasedLoad

    Overall Reduction in NOx

    Final OperatingPoint

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Adv. Ign. Sys. @ 16"

    HPFI @ 7.5"

    MGAV @ 7.5"

    HPFI @ 12"

    Adv. Ign. Sys. @ 16"

    Load (BHP)

    B.S. NOx (g/bhp-hr)

    B.S. NOx vs Load

    0.4

    1.9

    0.25

    0.05

    0.7

    2.2

    0.5

    0.15

    1

    2.5

    1.2

    0.25

    2.1

    3.1

    2.1

    0.45

    3.2

    4.5

    2.4

    0.75

    9.7

    11.8

    3.2

    2.2

    9.7

    4

    BSFC Bar Chart

    840081008050801082007850

    Potential Fuel SavingsAfter IncreasedBoost & Load

    MGAV @ 7.5"440 bhp

    HPFI @ 7.5"440 bhp

    Adv. Ign.Sys. @ 12"440 bhp

    Adv. Ign.Sys. @ 16"440 bhp

    Adv. Ign.Sys. @ 20"440 bhp

    Adv. Ign.Sys. @ 16"484 bhp

    MGAV @ 7.5"

    HPFI @ 7.5"

    Adv. Ign. Sys. @ 12"

    Adv. Ign. Sys. @ 16"

    Adv. Ign. Sys. @ 20"

    Adv. Ign. Sys. @ 16" & 484 bhp

    BSFC (btu/bhp-hr)

    Brake Specific Fuel Consumption

  • Engines and Energy Conversion Laboratory

    The Effect of Combustion Stabilization

    Combustion stabilization through enhanced ignition

    ReducedVariability

    Variability

    Potential increase in average peak pressure without increasing

    maximum peak pressure

  • Engines and Energy Conversion Laboratory

    Micro Pilot Ignition System

    Using a micro-liter quantity of a compression ignitable pilot fuelas the ignitionsource

  • Engines and Energy Conversion Laboratory

    Micro Pilot Ignition System

    • No Misfires• Lower THC• Lower BSFC• Achieved

  • Engines and Energy Conversion Laboratory

    Misfire Elimination

    0.0

    0.5

    1.0

    1.5

    2.0

    2.5

    3.0

    3.5

    4.0

    4.5

    100 90 80 70Load (%)

    Misfi

    res (

    %)

    φ=

    0.85

    φ=

    0.85

    Pilot IgnitionSpark Ignition

    φ=

    0.78

    φ=

    0.78

    φ=

    0.73

    φ=

    0.73

    φ=

    0.71

    φ=

    0.67

    Micro Pilot Ignition System

  • Engines and Energy Conversion Laboratory

    THC Reduction

    0

    2

    4

    6

    8

    10

    12

    14

    100 90 80 70Load (%)

    THC

    (g/h

    p-hr

    )

    φ=

    0.85

    φ=

    0.85

    Pilot Ignition

    Spark Ignition

    φ=

    0.78

    φ=

    0.78

    φ=

    0.73

    φ=

    0.73

    φ=

    0.71

    φ=

    0.67

    Micro Pilot Ignition System

  • Engines and Energy Conversion Laboratory

    7000

    7500

    8000

    8500

    9000

    9500

    100 90 80 70Load (%)

    BSFC

    (BTU

    /hp-h

    r)

    BSFC Reductionφ

    = 0.

    85

    φ=

    0.85

    Pilot IgnitionSpark Ignition

    φ=

    0.78

    φ=

    0.78

    φ=

    0.73

    φ=

    0.73

    φ=

    0.71

    φ=

    0.67

    0.8% Pilot

    Micro Pilot Ignition System

  • Engines and Energy Conversion Laboratory

    Micro Pilot Ignition System

    Currently, key components are provided by Woodward and Delphi

  • Engines and Energy Conversion Laboratory

    The current injectors used will work better for the Clark engine than for the GMV

    Micro Pilot Ignition System

    Impinging Sprays

    No Impingement

    This was shown to reduce pilot fuel quantity with custom fuel injector testing

  • Engines and Energy Conversion Laboratory

    Clark TLA Piston Crown Re-Design Example

  • Engines and Energy Conversion Laboratory

    • Developed using Ricardo WAVE– Engine simulation software– Models compressible flow effects (1-D)– Computes emissions – 2-zone combustion model

    • Engine is first modeled under nominal operating conditions, matching efficiency, cylinder pressure profile, NOx emissions, and other parameters

    • Manifold is optimized using 7 variable Design of Experiments technique, adapted for this application

    Clark TLA Exhaust Tuning Example

  • Engines and Energy Conversion Laboratory

    Tuned Exhaust Manifoldfor Clark TLA Engine

    Original Exhaust Manifold New Exhaust Manifold Design

  • Engines and Energy Conversion Laboratory

    Tuned Exhaust Manifoldfor Clark TLA Engine

  • Engines and Energy Conversion Laboratory

    Parameters Nominal Optimized ModifiedDelivery Ratio 1.771 1.777 1.77

    Scavenging Efficiency 0.87 0.871 0.869Trapping Efficiency 0.491 0.49 0.491

    IMEP (psi) 120.3 120.3 121.4Peak Pressure (psi) 752.7 765.8 758.6Location of PP (CA) 18.01 18.02 17.97

    Brake Power (hp) 2000 2000 2020BMEP (psi) 102 102 103.1

    Mass Flow of Fresh Air (lb/hr) 34580 35640 35090Trapped Equivalence Ratio 0.7259 0.7016 0.7212

    Fuel (g) 3.275 3.23 3.275NOx (g/bkW-hr) 12.81 8.45 10.59

    • The first optimized case produced NOx reduction of 34%• The modified optimized case produced NOx reduction of 17.3%

    Tuned Exhaust Results

    Sheet1

    ParametersNominalOptimizedModified

    Delivery Ratio1.7711.7771.77

    Scavenging Efficiency0.870.8710.869

    Trapping Efficiency0.4910.490.491

    IMEP (psi)120.3120.3121.4

    Peak Pressure (psi)752.7765.8758.6

    Location of PP (CA)18.0118.0217.97

    Brake Power (hp)200020002020

    BMEP (psi)102102103.1

    Mass Flow of Fresh Air (lb/hr)345803564035090

    Trapped Equivalence Ratio0.72590.70160.7212

    Fuel (g)3.2753.233.275

    NOx (g/bkW-hr)12.818.4510.59

    Sheet2

    Sheet3

  • Engines and Energy Conversion Laboratory

    CFD Modeling of D-R Research Engine, K5X

  • Engines and Energy Conversion Laboratory

    Cost Analysis

    • Project target cost was to achieve

  • Engines and Energy Conversion Laboratory

    EECL’s Clark TLA Engine –Donated by Dresser-Rand

    • Currently being modified from 3-cylinder to 6-cylinder configuration

  • Engines and Energy Conversion Laboratory

    Engine Specific Uprate Strategy

    Family Type (2/4 stroke) Original Air Delivery Method

    BMEP Enhanced Mixing

    Improved Air

    Delivery

    Improved Ignition

    Exhaust Tuning

    BA 2 Piston Scavenged 68.3 HPFI TC X1 TBDHBA 2 Piston Scavenged 75.3 HPFI TC X1 TBDHLA 2 Piston Scavenged 76.5 HPFI TC X1 TBDTLA 2 Turbocharged 103.3 HPFI TU X1 XK5X 2 Turbocharged 129.2KVG 4 Nat. Asp. 80.34 HPFI TC X1 TBDGMV 2 Piston Scavenged 61.3 HPFI TC X1 TBD

    GMVA 2 Blower 79.2-84.3 HPFI TC X1 TBDGMW 2 Blower 74.5 HPFI TC X1 TBD

    GMWA 2 Blower 77.5 HPFI TC X1 TBDNote:1 If CR > 8.5:1 Then pilot injection

    TC = Turbocharger

    If CR < 8.5:1 Then PCC's

    Ingersoll-Rand

    Cooper-Bessemer

    N/A

    Engine Uprates Technique Table

    Manufacturer

    Clark

    Sheet1

    Engine Uprates Survey TableEngine Uprates Technique Table

    ManufacturerFamily#UnitsTotal HPType (2/4 stroke)Cyl. Dims.Cylinder ConfigurationsAir DeliveryBMEPManufacturerFamilyType (2/4 stroke)Original Air Delivery MethodBMEPEnhanced MixingImproved Air DeliveryImproved IgnitionExhaust Tuning

    ClarkBA145203507217x175,6,8,10Piston Scavenged68.3ClarkBA2Piston Scavenged68.3HPFITCX1TBD

    HBA245410644217x175,6,8,10Piston Scavenged75.3HBA2Piston Scavenged75.3HPFITCX1TBD

    HLA4491950217x195,6,8,10Nat. Asp.76.5HLA2Piston Scavenged76.5HPFITCX1TBD

    TLA284665074217x195,6,8,10Turbocharged103.3TLA2Turbocharged103.3HPFITUX1X

    K5X11652218.5x196 (3 disabled)Turbocharged129.2K5X2Turbocharged129.2N/A

    Ingersoll-RandKVG286310588415.25x186,8,10,12Nat. Asp.80.34Ingersoll-RandKVG4Nat. Asp.80.34HPFITCX1TBD

    Cooper-BessemerGMV305305219214x144,6,8,10Piston Scavenged61.3Cooper-BessemerGMV2Piston Scavenged61.3HPFITCX1TBD

    GMVA136170539214x144,6,8,10,12Blower79.2-84.3GMVA2Blower79.2-84.3HPFITCX1TBD

    GMW189422080218x206,8,10Blower74.5GMW2Blower74.5HPFITCX1TBD

    GMWA216453100218x206,8,10,12Blower77.5GMWA2Blower77.5HPFITCX1TBD

    Note:TC = Turbocharger

    1If CR > 8.5:1 Then pilot injection

    If CR < 8.5:1 Then PCC's

    Sheet2

    ManufacturerFamily#UnitsTotal HPType (2/4 stroke)Cyl. Dims.Cylinder ConfigurationsAir DeliveryBMEPCost

    ClarkBA145203507217x175,6,8,10Piston Scavenged68.3

    HBA245410644217x175,6,8,10Piston Scavenged75.3

    HLA4491950217x195,6,8,10Nat. Asp.76.5

    TLA284665074217x195,6,8,10Turbocharged103.3

    K5X11652218.5x196 (3 disabled)Turbocharged129.2

    Ingersoll-RandKVG286310588415.25x186,8,10,12Nat. Asp.80.34

    KVS225411235415.25x186,8,10,12Elliott Turbo.121.7

    Cooper-BessemerGMV305305219214x144,6,8,10Piston Scavenged61.3

    GMVA136170539214x144,6,8,10,12Blower79.2-84.3

    GMW189422080218x206,8,10Blower74.5

    GMWA216453100218x206,8,10,12Blower77.5

    Sheet3

  • Engines and Energy Conversion Laboratory

    Industry Involvement

    • Dresser-Rand support – TLA engine donation, engineering drawings, and commitment for some conversion parts

    • Altronic, Enginuity, and Hoerbiger commitment for hardware support/donations

    • Industry personnel assistance –interviews, documentation, etc.

  • Engines and Energy Conversion Laboratory

    Industry Experience (Summary)

    • Large bore NG 2-stroke engines are believed to have large safety factors

    • Field data demonstrates safe operation at greater than 100% load

    • Many of the large bore NG 2-stroke engines capable of increased speeds and loads without structural modifications

    • No increase in failures noted for these engines

  • Engines and Energy Conversion Laboratory

    Industry Experience (Interviews)

    • Power Cylinder Porting Change• New Heads & Pistons• Scavenging Air Elbow• No Turbo Upgrade• 110% of Rated Load• Ran Better, No Increased Failure Rates

    Chevron-Texaco - Clark RA Series

  • Engines and Energy Conversion Laboratory

    Industry Experience (Interviews)

    • Installed ABB Marine Turbocharger (19” Hg Boost)

    • Intercooler w/ Wet Cooling Tower – Intake Air Temp. of 97°F

    • Peak Pressure Balance w/ Std. Dev. < 30 psi.• 115% of Rated Load Since 1958 w/ No

    Increase in Failure Rates or Maintenance

    SoCal Gas – Clark TLA-6 (7)

  • Engines and Energy Conversion Laboratory

    Industry Experience (Interviews)

    • Std. Turbocharger• Intercooler Upgrade w/ Cooling Towers• 105% of Rated Load for 20 yrs w/ No

    Increase in Failure Rates

    Williams Pipeline – Clark TLA-6 (12)

  • Engines and Energy Conversion Laboratory

    Industry Experience

    • Reviewed TLA-6 crankcase and upper block solid models

    • Provided feedback on common TLA-6 failure modes and locations

    • Will provide similar input for GMV and HBA engines

    Terry Smith – Industry Field Repair Expert

  • Engines and Energy Conversion Laboratory

    OEM Communications

    • Memo from Clark to Texaco (1959) communicated results from a vibration analysis for an RA-6.

    • Results indicated a resonant frequency exists at 340-350 RPM with a 7°amplitude.

    • Clark recommended a max. speed of 320 RPM or flywheel modifications.

  • Engines and Energy Conversion Laboratory

    OEM Communications

    • Report from Cooper-Bessemer to Texaco(1989) regarding increasing speeds of GMV-6 (3) and GMVL-6 (1).

    • Increased speed from 300 – 330 RPM.• Balance study indicated that one of the

    GMV-6 engines needed to have additional reciprocating weight added.

  • Engines and Energy Conversion Laboratory

    • Increasing torque, not speed, can avoid approaching critical speeds.

    • Industry data supports the conclusion that the engines have a large factor of safety, which will allow for the safe operation at the increased loads.

    • Improved air delivery has long been demonstrated to reduce fuel consumption and emissions through leaner operation.

    GTI Project Conclusions (1/2)

  • Engines and Energy Conversion Laboratory

    • Enhanced mixing can help reduce emissions, increase combustion stability, extend the lean limit, and decrease fuel consumption.

    • Improved ignition techniques can reduce emissions, improve combustion stability, extend the lean limit, and decrease fuel consumption.

    • HPFI, micro pilot ignition, and increased boost are proven technologies and are planned for implementation in Year 1 of the DOE program.

    • Exhaust tuning benefits are engine specific and would have to be analyzed for each case.

    GTI Project Conclusions (2/2)

  • Engines and Energy Conversion Laboratory

    Year 1 Project Schedule

    Task O04

    N04

    D04

    JO5

    FO5

    M05

    A05

    M05

    J05

    J05

    A05

    S05

    O05

    1.1 Research Management Plan complete

    1.2 Technology Assessment complete

    1.3 Optical Engine Evaluations

    1.4 Component Procure & Fab

    1.5 System Test Plan M1

    1.6 Uprate Systems Installation

    1.7 Testing of Uprate Systems M2

    1.8 Annual Contractor Review

    Semi-Annual Progress Report

  • Engines and Energy Conversion Laboratory

    Outline

    • Executive Summary • Previous Work done with GTI Funds• DOE Year 1 Results To-Date• Planned Research Activities

  • Engines and Energy Conversion Laboratory

    Task 1.2: Technology Assessment Summary Table

    ENGINE MODEL

    (Percent of Overall Fleet)BA, HBAHLA

    TLA KVG KVS GMV, GMVA

    GMW, GMWA

    (7.5) (7.1) (3.1) (4.4) (5.1) (9.3)

    UPRATE TECHNOLOGY Indicates Uprate Technology is applicable to engine model (subject to change per study)Turbo Installation/ Upgrade•Pro: can help reduce emissions, increase engine output and extend the lean limit.•Con: may not be economical for units

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (1/15): Description

  • Engines and Energy Conversion Laboratory

    Laser Sheet

    Acetone SeedingSystem

    Laser

    ICCD Camera

    OpticalEngine

    Fuel Valve

    Task 1.3: Optical Engine (2/15): PLIF Imaging Setup

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (3/15): CFD Validation

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (4/15): Clark TLA CFD Analysis

    • Optical engine has 14” bore; TLA has 17” bore• Not practical to modify for larger bore• Performed mixing studies using CFD, previously

    validated with optical engine results– Case #1 - OEM TLA with standard mixing model– Case #2 - TLA with enhanced mixing model and OEM

    piston– Case #3 - TLA with enhanced mixing model with

    modified crown piston

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (5/15): CFD Flow Field @ IGNITION

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (6/15): CFD Fuel Distribution @ IGNITION

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (7/15): CFD Flame Propagation & Fuel Consumption

    -6 -2 2 6

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (8/15): CFD Flame Propagation & Fuel Consumption

    10 14 18 22

  • Engines and Energy Conversion Laboratory

    0 10 20 30

    Task 1.3: Optical Engine (9/15): CFD Temperature & NO

  • Engines and Energy Conversion Laboratory

    40 50 60 70

    Task 1.3: Optical Engine (10/15): CFD Temperature & NO

  • Engines and Energy Conversion Laboratory

    90° BTDC100° BTDC110° BTDC120° BTDC

    HPFI

    HPFI w/ modified piston

    Nominal TLA

    Task 1.3: Optical Engine (11/15): Mixing Comparison

  • Engines and Energy Conversion Laboratory

    50° BTDC60° BTDC70° BTDC80° BTDC

    Nominal TLA

    HPFI

    HPFI w/ modified piston

    Task 1.3: Optical Engine (12/15): Mixing Comparison

  • Engines and Energy Conversion Laboratory

    10° BTDC20° BTDC30° BTDC40° BTDC

    Nominal TLA

    HPFI

    HPFI w/ modified piston

    Task 1.3: Optical Engine (13/15): Mixing Comparison

  • Engines and Energy Conversion Laboratory

    • CFD work provides required information on mixing

    • To examine micropilot ignition, utilize combustion test chamber (CTC)

    • CTC will allow imaging of pilot injection with new injectors prior to engine testing

    Task 1.3: Optical Engine (14/15)

  • Engines and Energy Conversion Laboratory

    Task 1.3: Optical Engine (15/15): Combustion Test Chamber

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (1/15)

    • Request for OEM components has been submitted to Dresser-Rand

    • Hoerbiger and Enginuity have offered to provide high pressure fuel injection systems

    • Enginuity is donating an Impact cylinder pressure monitoring system

    • Altronic is donating CPU 2000 spark ignition system with add-on module for micropilot injection control

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (2/15): Modal and Dynamic Stress Analysis

    • Modal analysis (Pro Mechanica) performed to assess possibility of utilizing speed increases

    • Stress analysis performed to examine effects of increasing torque

    • Dynamic forces accounted for by utilizing Working Model and simulation feature in Pro Mechanica

    • High stress locations identified using Finite Element Analysis

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (3/15): TLA Crankshaft Modal Analysis• Added ‘mass’ (lobes) to

    crankshaft to simulate piston/connecting rod weight.

    • Constrained bearing at non-flywheel end to 1 rotational DOF, all other bearing supports to 1 rotational and 1 translational DOF.

    • Modal Analysis results indicate the first resonant frequency occurs at 34Hz (2040RPM).– The 5th, 6th, and 7th order critical speeds are 408, 340,

    and 291 RPM, respectively.

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (4/15): TLA-6 Stress Analysis

    • Given the forces of the power and compressor pistons, the frame stresses are examined.

    • The frame stresses of standard TLA configuration are compared to the frame stresses of the uprated TLA configuration.

    GMV crankcaseSuperior crankcase(Reynolds-French)

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (5/15): TLA-6 Dynamic Analysis

    • Developed dynamic model using Working Model 2D software

    • Determined dynamic forces on crankshaft bearings

    • These forces used as the loading forces for the crankcase FEA modeling

  • Engines and Energy Conversion Laboratory

    Task 1.4: Component Procurement & Fabrication (6/15): TLA-6 Dynamic Analysis

    Working Model Simulation of TLA Power Piston and Compressor Piston Forces on Crankshaft Bearings

    -80000

    -60000

    -40000

    -20000

    0

    20000

    40000

    60000

    80000

    100000

    120000

    140000

    160000

    0 30 60 90 120 150 180 210 240 270 300 330 360

    Crank Angle (deg)

    Forc

    e (lb

    )

    FxFyCombustion ForceCompression ForceSuction Force

    Chart3

    00000

    0.250.250.250.250.25

    0.50.50.50.50.5

    0.750.750.750.750.75

    11111

    1.251.251.251.251.25

    1.51.51.51.51.5

    1.751.751.751.751.75

    22222

    2.252.252.252.252.25

    2.52.52.52.52.5

    2.752.752.752.752.75

    33333

    3.253.253.253.253.25

    3.53.53.53.53.5

    3.753.753.753.753.75

    44444

    4.254.254.254.254.25

    4.54.54.54.54.5

    4.754.754.754.754.75

    55555

    5.255.255.255.255.25

    5.55.55.55.55.5

    5.755.755.755.755.75

    66666

    6.256.256.256.256.25

    6.56.56.56.56.5

    6.756.756.756.756.75

    77777

    7.257.257.257.257.25

    7.57.57.57.57.5

    7.757.757.757.757.75

    88888

    8.258.258.258.258.25

    8.58.58.58.58.5

    8.758.758.758.758.75

    99999

    9.259.259.259.259.25

    9.59.59.59.59.5

    9.759.759.759.759.75

    1010101010

    10.2510.2510.2510.2510.25

    10.510.510.510.510.5

    10.7510.7510.7510.7510.75

    1111111111

    11.2511.2511.2511.2511.25

    11.511.511.511.511.5

    11.7511.7511.7511.7511.75

    1212121212

    12.2512.2512.2512.2512.25

    12.512.512.512.512.5

    12.7512.7512.7512.7512.75

    1313131313

    13.2513.2513.2513.2513.25

    13.513.513.513.513.5

    13.7513.7513.7513.7513.75

    1414141414

    14.2514.2514.2514.2514.25

    14.514.514.514.514.5

    14.7514.7514.7514.7514.75

    1515151515

    15.2515.2515.2515.2515.25

    15.515.515.515.515.5

    15.7515.7515.7515.7515.75

    1616161616

    16.2516.2516.2516.2516.25

    16.516.516.516.516.5

    16.7516.7516.7516.7516.75

    1717171717

    17.2517.2517.2517.2517.25

    17.517.517.517.517.5

    17.7517.7517.7517.7517.75

    1818181818

    18.2518.2518.2518.2518.25

    18.518.518.518.518.5

    18.7518.7518.7518.7518.75

    1919191919

    19.2519.2519.2519.2519.25

    19.519.519.519.519.5

    19.7519.7519.7519.7519.75

    2020202020

    20.2520.2520.2520.2520.25

    20.520.520.520.520.5

    20.7520.7520.7520.7520.75

    2121212121

    21.2521.2521.2521.2521.25

    21.521.521.521.521.5

    21.7521.7521.7521.7521.75

    2222222222

    22.2522.2522.2522.2522.25

    22.522.522.522.522.5

    22.7522.7522.7522.7522.75

    2323232323

    23.2523.2523.2523.2523.25

    23.523.523.523.523.5

    23.7523.7523.7523.7523.75

    2424242424

    24.2524.2524.2524.2524.25

    24.524.524.524.524.5

    24.7524.7524.7524.7524.75

    2525252525

    25.2525.2525.2525.2525.25

    25.525.525.525.525.5

    25.7525.7525.7525.7525.75

    2626262626

    26.2526.2526.2526.2526.25

    26.526.526.526.526.5

    26.7526.7526.7526.7526.75

    2727272727

    27.2527.2527.2527.2527.25

    27.527.527.527.527.5

    27.7527.7527.7527.7527.75

    2828282828

    28.2528.2528.2528.2528.25

    28.528.528.528.528.5

    28.7528.7528.7528.7528.75

    2929292929

    29.2529.2529.2529.2529.25

    29.529.529.529.529.5

    29.7529.7529.7529.7529.75

    3030303030

    30.2530.2530.2530.2530.25

    30.530.530.530.530.5

    30.7530.7530.7530.7530.75

    3131313131

    31.2531.2531.2531.2531.25

    31.531.531.531.531.5

    31.7531.7531.7531.7531.75

    3232323232

    32.2532.2532.2532.2532.25

    32.532.532.532.532.5

    32.7532.7532.7532.7532.75

    3333333333

    33.2533.2533.2533.2533.25

    33.533.533.533.533.5

    33.7533.7533.7533.7533.75

    3434343434

    34.2534.2534.2534.2534.25

    34.534.534.534.534.5

    34.7534.7534.7534.7534.75

    3535353535

    35.2535.2535.2535.2535.25

    35.535.535.535.535.5

    35.7535.7535.7535.7535.75

    3636363636

    36.2536.2536.2536.2536.25

    36.536.536.536.536.5

    36.7536.7536.7536.7536.75

    3737373737

    37.2537.2537.2537.2537.25

    37.537.537.537.537.5

    37.7537.7537.7537.7537.75

    3838383838

    38.2538.2538.2538.2538.25

    38.538.538.538.538.5

    38.7538.7538.7538.7538.75

    3939393939

    39.2539.2539.2539.2539.25

    39.539.539.539.539.5

    39.7539.7539.7539.7539.75

    4040404040

    40.2540.2540.2540.2540.25

    40.540.540.540.540.5

    40.7540.7540.7540.7540.75

    4141414141

    41.2541.2541.2541.2541.25

    41.541.541.541.541.5

    41.7541.7541.7541.7541.75

    4242424242

    42.2542.2542.2542.2542.25

    42.542.542.542.542.5

    42.7542.7542.7542.7542.75

    4343434343

    43.2543.2543.2543.2543.25

    43.543.543.543.543.5

    43.7543.7543.7543.7543.75

    4444444444

    44.2544.2544.2544.2544.25

    44.544.544.544.544.5

    44.7544.7544.7544.7544.75

    4545454545

    45.2545.2545.2545.2545.25

    45.545.545.545.545.5

    45.7545.7545.7545.7545.75

    4646464646

    46.2546.2546.2546.2546.25

    46.546.546.546.546.5

    46.7546.7546.7546.7546.75

    4747474747

    47.2547.2547.2547.2547.25

    47.547.547.547.547.5

    47.7547.7547.7547.7547.75

    4848484848

    48.2548.2548.2548.2548.25

    48.548.548.548.548.5

    48.7548.7548.7548.7548.75

    4949494949

    49.2549.2549.2549.2549.25

    49.549.549.549.549.5

    49.7549.7549.7549.7549.75

    5050505050

    50.2550.2550.2550.2550.25

    50.550.550.550.550.5

    50.7550.7550.7550.7550.75

    5151515151

    51.2551.2551.2551.2551.25

    51.551.551.551.551.5

    51.7551.7551.7551.7551.75

    5252525252

    52.2552.2552.2552.2552.25

    52.552.552.552.552.5

    52.7552.7552.7552.7552.75

    5353535353

    53.2553.2553.2553.2553.25

    53.553.553.553.553.5

    53.7553.7553.7553.7553.75

    5454545454

    54.2554.2554.2554.2554.25

    54.554.554.554.554.5

    54.7554.7554.7554.7554.75

    5555555555

    55.2555.2555.2555.2555.25

    55.555.555.555.555.5

    55.7555.7555.7555.7555.75

    5656565656

    56.2556.2556.2556.2556.25

    56.556.556.556.556.5

    56.7556.7556.7556.7556.75

    5757575757

    57.2557.2557.2557.2557.25

    57.557.557.557.557.5

    57.7557.7557.7557.7557.75

    5858585858

    58.2558.2558.2558.2558.25

    58.558.558.558.558.5

    58.7558.7558.7558.7558.75

    5959595959

    59.2559.2559.2559.2559.25

    59.559.559.559.559.5

    59.7559.7559.7559.7559.75

    6060606060

    60.2560.2560.2560.2560.25

    60.560.560.560.560.5

    60.7560.7560.7560.7560.75

    6161616161

    61.2561.2561.2561.2561.25

    61.561.561.561.561.5

    61.7561.7561.7561.7561.75

    6262626262

    62.2562.2562.2562.2562.25

    62.562.562.562.562.5

    62.7562.7562.7562.7562.75

    6363636363

    63.2563.2563.2563.2563.25

    63.563.563.563.563.5

    63.7563.7563.7563.7563.75

    6464646464

    64.2564.2564.2564.2564.25

    64.564.564.564.564.5

    64.7564.7564.7564.7564.75

    6565656565

    65.2565.2565.2565.2565.25

    65.565.565.565.565.5

    65.7565.7565.7565.7565.75

    6666666666

    66.2566.2566.2566.2566.25

    66.566.566.566.566.5

    66.7566.7566.7566.7566.75

    6767676767

    67.2567.2567.2567.2567.25

    67.567.567.567.567.5

    67.7567.7567.7567.7567.75

    6868686868

    68.2568.2568.2568.2568.25

    68.568.568.568.568.5

    68.7568.7568.7568.7568.75

    6969696969

    69.2569.2569.2569.2569.25

    69.569.569.569.569.5

    69.7569.7569.7569.7569.75

    7070707070

    70.2570.2570.2570.2570.25

    70.570.570.570.570.5

    70.7570.7570.7570.7570.75

    7171717171

    71.2571.2571.2571.2571.25

    71.571.571.571.571.5

    71.7571.7571.7571.7571.75

    7272727272

    72.2572.2572.2572.2572.25

    72.572.572.572.572.5

    72.7572.7572.7572.7572.75

    7373737373

    73.2573.2573.2573.2573.25

    73.573.573.573.573.5

    73.7573.7573.7573.7573.75

    7474747474

    74.2574.2574.2574.2574.25

    74.574.574.574.574.5

    74.7574.7574.7574.7574.75

    7575757575

    75.2575.2575.2575.2575.25

    75.575.575.575.575.5

    75.7575.7575.7575.7575.75

    7676767676

    76.2576.2576.2576.2576.25

    76.576.576.576.576.5

    76.7576.7576.7576.7576.75

    7777777777

    77.2577.2577.2577.2577.25

    77.577.577.577.577.5

    77.7577.7577.7577.7577.75

    7878787878

    78.2578.2578.2578.2578.25

    78.578.578.578.578.5

    78.7578.7578.7578.7578.75

    7979797979

    79.2579.2579.2579.2579.25

    79.579.579.579.579.5

    79.7579.7579.7579.7579.75

    8080808080

    80.2580.2580.2580.2580.25

    80.580.580.580.580.5

    80.7580.7580.7580.7580.75

    8181818181

    81.2581.2581.2581.2581.25

    81.581.581.581.581.5

    81.7581.7581.7581.7581.75

    8282828282

    82.2582.2582.2582.2582.25

    82.582.582.582.582.5

    82.7582.7582.7582.7582.75

    8383838383

    83.2583.2583.2583.2583.25

    83.583.583.583.583.5

    83.7583.7583.7583.7583.75

    8484848484

    84.2584.2584.2584.2584.25

    84.584.584.584.584.5

    84.7584.7584.7584.7584.75

    8585858585

    85.2585.2585.2585.2585.25

    85.585.585.585.585.5

    85.7585.7585.7585.7585.75

    8686868686

    86.2586.2586.2586.2586.25

    86.586.586.586.586.5

    86.7586.7586.7586.7586.75

    8787878787

    87.2587.2587.2587.2587.25

    87.587.587.587.587.5

    87.7587.7587.7587.7587.75

    8888888888

    88.2588.2588.2588.2588.25

    88.588.588.588.588.5

    88.7588.7588.7588.7588.75

    8989898989

    89.2589.2589.2589.2589.25

    89.589.589.589.589.5

    89.7589.7589.7589.7589.75

    9090909090

    90.2590.2590.2590.2590.25

    90.590.590.590.590.5

    90.7590.7590.7590.7590.75

    9191919191

    91.2591.2591.2591.2591.25

    91.591.591.591.591.5

    91.7591.7591.7591.7591.75

    9292929292

    92.2592.2592.2592.2592.25

    92.592.592.592.592.5

    92.7592.7592.7592.7592.75

    9393939393

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    356356356356356

    356.25356.25356.25356.25356.25

    356.5356.5356.5356.5356.5

    356.75356.75356.75356.75356.75

    357357357357357

    357.25357.25357.25357.25357.25

    357.5357.5357.5357.5357.5

    357.75357.75357.75357.75357.75

    358358358358358

    358.25358.25358.25358.25358.25

    358.5358.5358.5358.5358.5

    358.75358.75358.75358.75358.75

    359359359359359

    359.25359.25359.25359.25359.25

    359.5359.5359.5359.5359.5

    359.75359.75359.75359.75359.75

    360360360360360

    Fx

    Fy

    Combustion Force

    Compression Force

    Suction Force

    Crank Angle (deg)

    Force (lb)

    Working Model Simulation of TLA Power Piston and Compressor Piston Forces on Crankshaft Bearings

    90200

    0

    0

    -12.743

    90200

    0

    0

    322.235

    90930

    0

    0

    658.011

    91700

    0

    0

    994.748

    92490

    0

    0

    1332.472

    93270

    0

    0

    1671.167

    94040

    0

    0

    2011.076

    94900

    0

    0

    2351.948

    95720

    0

    0

    2694.065

    96580

    0

    0

    3037.423

    97470

    0

    0

    98330

    0

    0

    3727.603

    20500

    99240

    0

    0

    21460

    100200

    0

    0

    22390

    101100

    0

    0

    23370

    102000

    0

    0

    24340

    103000

    0

    0

    5475.951

    25320

    103900

    0

    0

    26360

    104900

    0

    0

    27370

    105900

    0

    0

    106900

    0

    0

    29520

    108000

    0

    0

    7260.842

    30580

    109000

    0

    0

    31650

    110000

    0

    0

    32720

    111000

    0

    0

    33830

    112100

    0

    0

    8715.235

    34950

    113100

    0

    0

    9083.19

    36090

    114200

    0

    0

    37240

    115300

    0

    0

    9822.449

    38340

    116400

    0

    0

    10200

    39510

    117500

    0

    0

    40660

    118600

    0

    0

    41790

    119600

    0

    0

    11320

    42950

    120700

    0

    0

    121800

    0

    0

    45310

    123000

    0

    0

    46450

    124000

    0

    0

    12840

    47610

    125100

    0

    0

    13220

    48770

    126200

    0

    0

    49940

    127300

    0

    0

    51060

    128300

    0

    0

    52230

    129400

    0

    0

    53360

    130500

    0

    0

    54420

    131400

    0

    0

    55580

    132500

    0

    0

    56710

    133600

    0

    0

    57780

    134500

    0

    0

    58870

    135500

    0

    0

    59940

    136500

    0

    0

    60970

    137400

    0

    0

    61980

    138300

    0

    0

    62990

    139300

    0

    0

    18690

    140100

    0

    0

    141000

    0

    0

    141900

    0

    0

    142700

    0

    0

    143500

    0

    0

    144200

    0

    0

    144900

    0

    0

    21430

    145700

    0

    0

    21830

    146300

    0

    0

    147000

    0

    0

    147600

    0

    0

    148100

    0

    0

    148700

    0

    0

    149200

    0

    0

    149700

    0

    0

    150100

    0

    0

    24900

    150500

    0

    0

    150900

    0

    0

    25650

    151200

    0

    0

    151500

    0

    0

    151800

    0

    0

    152000

    0

    0

    152200

    0

    0

    152300

    0

    0

    152400

    0

    0

    152400

    0

    0

    152400

    0

    0

    152400

    0

    0

    152400

    0

    0

    152300

    0

    0

    152100

    0

    0

    152000

    0

    0

    30630

    151800

    0

    0

    151500

    0

    0

    151200

    0

    0

    150900

    0

    0

    150600

    0

    0

    150200

    0

    0

    149800

    0

    0

    149400

    0

    0

    148900

    0

    0

    148400

    0

    0

    77770

    147800

    0

    0

    147300

    0

    0

    146700

    0

    0

    146100

    0

    0

    145400

    0

    0

    144800

    0

    0

    144100

    0

    0

    143400

    0

    0

    142700

    0

    0

    141900

    0

    0

    141100

    0

    0

    36830

    140300

    0

    0

    139500

    0

    0

    138700

    0

    0

    137900

    0

    0

    137000

    0

    0

    38080

    136100

    0

    0

    135300

    0

    0

    38560

    134400

    0

    0

    133500

    0

    0

    132600

    0

    0

    131700

    0

    0

    130800

    0

    0

    129800

    0

    0

    128900

    0

    0

    63020

    127900

    0

    0

    126900

    0

    0

    126000

    0

    0

    125100

    0

    0

    40990

    124100

    0

    0

    123100

    0

    0

    122200

    0

    0

    121200

    0

    0

    120200

    0

    0

    119300

    0

    0

    55790

    118300

    0

    0

    117400

    0

    0

    116400

    0

    0

    115500

    0

    0

    42950

    114500

    0

    0

    113600

    0

    0

    112600

    0

    0

    111700

    0

    0

    43680

    110700

    0

    0

    49600

    109800

    0

    0

    108900

    0

    0

    108000

    0

    0

    44400

    107100

    0

    0

    106200

    0

    0

    105300

    0

    0

    104400

    0

    0

    103500

    0

    0

    102600

    0

    0

    101800

    0

    0

    43270

    100800

    0

    0

    45750

    100000

    0

    0

    99140

    0

    0

    46080

    41560

    98310

    0

    0

    46250

    97490

    0

    0

    96670

    0

    0

    39950

    95850

    0

    0

    46730

    95010

    0

    0

    94220

    0

    0

    93450

    0

    0

    47210

    92650

    0

    0

    91840

    0

    0

    91060

    0

    0

    90290

    0

    0

    89520

    0

    0

    47990

    88770

    0

    0

    88020

    0

    0

    87270

    0

    0

    86550

    0

    0

    48590

    85820

    0

    0

    85120

    0

    0

    84410

    0

    0

    83710

    0

    0

    83010

    0

    0

    82300

    0

    0

    49490

    81640

    0

    0

    49640

    80960

    0

    0

    80280

    0

    0

    30230

    79600

    0

    0

    78970

    0

    0

    29580

    78330

    0

    0

    77700

    0

    0

    50510

    77060

    0

    0

    28600

    76400

    0

    0

    75790

    0

    0

    27990

    75150

    0

    0

    74560

    0

    0

    73970

    0

    0

    73380

    0

    0

    26910

    72790

    0

    0

    72200

    0

    0

    71630

    0

    0

    71090

    0

    0

    52050

    70520

    0

    0

    52180

    69930

    0

    0

    69390

    0

    0

    52450

    68840

    0

    0

    68280

    0

    0

    67750

    0

    0

    24630

    67230

    0

    0

    66710

    0

    0

    66160

    0

    0

    24050

    65640

    0

    0

    65140

    0

    0

    64640

    0

    0

    64140

    0

    0

    63670

    0

    0

    63170

    0

    0

    54040

    23110

    62670

    0

    0

    22980

    62190

    0

    0

    61720

    0

    0

    61240

    0

    0

    54560

    60790

    0

    0

    60310

    0

    0

    59880

    0

    0

    59420

    0

    0

    59010

    0

    0

    22140

    58580

    0

    0

    58110

    0

    0

    21930

    57680

    0

    0

    57240

    0

    0

    56840

    0

    0

    21740

    56430

    0

    0

    21660

    56000

    0

    0

    21600

    55590

    0

    0

    21550

    55180

    0

    0

    21520

    54790

    0

    0

    21490

    54410

    0

    0

    21440

    54000

    0

    0

    21390

    53590

    0

    0

    53200

    0

    0

    56900

    21360

    52840

    0

    0

    21350

    52480

    0

    0

    21330

    52090

    0

    0

    21330

    51730

    0

    0

    21320

    51370

    0

    0

    57500

    51030

    0

    0

    50640

    0

    0

    21340

    50300

    0

    0

    21370

    49960

    0

    0

    21390

    49620

    0

    0

    21390

    49250

    0

    0

    21400

    48890

    0

    0

    21420

    48550

    0

    0

    58410

    21470

    48230

    0

    0

    21500

    47890

    0

    0

    21550

    47580

    0

    0

    58750

    21600

    47260

    0

    0

    46940

    0

    0

    46620

    0

    0

    46300

    0

    0

    46010

    0

    0

    45710

    0

    0

    45400

    0

    0

    22000

    45080

    0

    0

    22100

    44810

    0

    0

    22160

    44490

    0

    0

    22230

    44190

    0

    0

    43920

    0

    0

    22410

    43630

    0

    0

    22490

    43330

    0

    0

    43060

    0

    0

    42810

    0

    0

    22790

    42510

    0

    0

    22920

    42260

    0

    0

    23000

    41970

    0

    0

    41700

    0

    0

    41450

    0

    0

    23330

    41170

    0

    0

    23430

    40900

    0

    0

    23580

    40670

    0

    0

    23700

    40430

    0

    0

    40130

    0

    0

    39880

    0

    0

    24040

    39630

    0

    0

    24190

    39400

    0

    0

    39180

    0

    0

    38950

    0

    0

    24590

    38680

    0

    0

    24720

    38430

    0

    0

    24890

    38220

    0

    0

    25040

    38000

    0

    0

    25190

    37770

    0

    0

    25350

    37540

    0

    0

    25500

    37320

    0

    0

    25650

    37090

    0

    0

    25800

    36860

    0

    0

    25950

    36630

    0

    0

    26120

    36430

    0

    0

    26270

    36200

    0

    0

    26430

    35980

    0

    0

    35790

    0

    0

    26820

    35610

    0

    0

    26970

    35390

    0

    0

    27140

    35180

    0

    0

    27320

    34980

    0

    0

    27490

    34770

    0

    0

    27690

    34590

    0

    0

    63750

    27860

    34390

    0

    0

    28030

    34180

    0

    0

    28230

    34000

    0

    0

    28430

    33820

    0

    0

    28600

    33620

    0

    0

    28800

    33430

    0

    0

    28990

    33250

    0

    0

    29190

    33070

    0

    0

    29380

    32890

    0

    0

    29580

    32710

    0

    0

    32530

    0

    0

    32340

    0

    0

    30160

    32160

    0

    0

    30360

    31980

    0

    0

    30580

    31820

    0

    0

    30770

    31640

    0

    0

    64990

    30990

    31480

    0

    0

    65050

    31180

    31300

    0

    0

    65130

    31400

    31140

    0

    0

    65200

    31610

    30980

    0

    0

    65270

    31830

    30820

    0

    0

    65340

    32050

    30670

    0

    0

    65410

    32260

    30510

    0

    0

    65470

    32480

    30350

    0

    0

    65540

    30190

    0

    0

    65610

    32910

    30030

    0

    0

    65670

    33120

    29870

    0

    0

    65730

    33330

    29710

    0

    0

    65800

    33550

    29550

    0

    0

    65860

    33780

    29420

    0

    0

    65920

    34000

    29260

    0

    0

    65990

    34230

    29120

    0

    0

    66050

    34470

    28990

    0

    0

    66110

    34680

    28830

    0

    0

    66170

    28690

    0

    0

    66220

    35130

    28530

    0

    0

    66280

    28400

    0

    0

    66340

    35590

    28260

    0

    0

    66390

    35820

    28120

    0

    0

    66440

    27960

    0

    0

    66500

    27850

    0

    0

    66560

    36520

    27710

    0

    0

    66610

    36750

    27580

    0

    0

    66660

    36980

    27440

    0

    0