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8/6/2008 37th Turbomachinery Symposium 1 Start-up of Parallel Turbo Expander-Compressor Units Operating In Hydrocarbon Processing Plants 37 th Turbo machinery Symposium Houston, Texas September 7-11, 2008 Doug Bird bp Energy Canada Reza Agahi Atlas Copco Gas and Process Behrooz Ershaghi Mafi-Trench Co.

Start-up of Parallel Turbo Expander-Compressor Units Operating In Hydrocarbon ... · 2018. 12. 1. · • Capacity of cryogenic gas plants have increased over the last forty years

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  • 8/6/2008 37th Turbomachinery Symposium 1

    Start-up of Parallel Turbo Expander-Compressor Units OperatingIn

    Hydrocarbon Processing Plants

    37th Turbo machinery SymposiumHouston, Texas

    September 7-11, 2008

    Doug Bird bp Energy CanadaReza Agahi Atlas Copco Gas and ProcessBehrooz Ershaghi Mafi-Trench Co.

  • 8/6/2008 37th Turbomachinery Symposium 2

    •Capacity of hydrocarbon processing plants have increased since turbo expander-compressor technology was utilized in early 1960’s

    EXPANDER FLOW DEVELOPMENT

    0 . 0 0

    2 0 0 . 0 0

    4 0 0 . 0 0

    6 0 0 . 0 0

    8 0 0 . 0 0

    1 0 0 0 . 0 0

    1 2 0 0 . 0 0

    1 9 6 1 1 9 6 2 1 9 6 7 1 9 6 8 1 9 6 9 1 9 7 0 1 9 7 8 1 9 8 2 1 9 9 2 1 9 9 6 1 9 9 7 1 9 9 9 2 0 0 0 2 0 0 2

    Ye a r

    Expander Fl ow Li near (Expander Fl ow)

  • 8/6/2008 37th Turbomachinery Symposium 3

    EXPANDER POWER

    0

    2 0 0 0

    4 0 0 0

    6 0 0 0

    8 0 0 0

    10 0 0 0

    12 0 0 0

    14 0 0 0

    Ye a r

    EXPANDER POWER DEVELOPM E NT Li near (EXPANDE R POWER DEVE LOPM ENT )

    •Upper limit of installed experience for turbo expander-compressors poweris at 15,000 KW

  • 8/6/2008 37th Turbomachinery Symposium 4

    •Due to large capacity many plants have parallel turbo expander-compressor trains

  • 8/6/2008 37th Turbomachinery Symposium 5

    Operational Challenge:

    •Simultaneous Start-up

    Similar to a single train star-up

  • 8/6/2008 37th Turbomachinery Symposium 6

    Case Study Reference:

    For this case study a bp gas plant with two parallel turbo expander-compressor trains with the following gas dynamics performance was considered:

    14.70%Liquid Fraction

    7,7257,876HP

    615,000706,000Flow (lb./hr)

    172- 96T2 (oF)

    430350P2(Psia)

    107- 6T1 (oF)

    2901,080P1(Psia)

    18.2319.38Mw

    CompressorTurbo Expander

    50

    55

    60

    65

    70

    75

    80

    85

    90

    0.0 500000.0 1000000.0 1500000.0

    EXPANDER FLOW, lb/hr

    EXPANDER

    EFFICIENCY,

    %

    110%100% SP EED90%

    80%

    70%

    0

    2,000

    4,000

    6,000

    8,000

    10,000

    12,000

    14,000

    0.0 500000.0 1000000.0 1500000.0

    EXPANDER FLOW, lb/hr

    SHAFT

    POWER, hp

    110%

    100% SP EED

    90%

    80%

    70%

    0

    2,000

    4,000

    6,000

    8,000

    10,000

    12,000

    14,000

    0.0 200000.0 400000.0 600000.0 800000.0 1000000.0

    COMPRESSOR FLOW, lb/hrSHAFT POWER, hp

    110%

    100% SP EED

    90%

    80%

    70%

    Surg

    e lin

    e

    1.0

    1.1

    1.2

    1.3

    1.4

    1.5

    1.6

    1.7

    1.8

    0.0 200000.0 400000.0 600000.0 800000.0 1000000.0COMPRESSOR FLOW, lb/hr

    PRESSURE RATIO, P2/P1

    110%

    100% SP EED

    90%

    80%

    70%

    Surg

    e lin

    e

    cont

    rol l

    ine

  • 8/6/2008 37th Turbomachinery Symposium 7

    Case Study Reference:

    An efficiency curve for parallel EC could be developed to guide operation for one or two trains in service for the maximum efficiency

    Isentropic Efficiency of Expander

    0102030405060708090

    100

    0 50 100 150

    % Flow

    % E

    ffici

    ency

    1 unit2 units

  • 8/6/2008 37th Turbomachinery Symposium 8

    Operational Challenge:

    Start-up of one unit when the parallel unit is in full load operation:

    •Compressor cannot compress directly into discharge header and hence Requires recirculation.

    % COMP-Recycle flow

    020406080

    100120

    0 50 100 150

    % Mass flow

    % re

    cycl

    e flo

    w

    % COMP-Recycle

  • 8/6/2008 37th Turbomachinery Symposium 9

    Operational Challenge:

    The following conditions are to be monitored during start up of an EC while recycle valve open:

    • Compressor discharge process gas temperature•Axial Loads•Radial Loads

    Development of the above conditions depends on pressure ratio of the compressor. Two scenarios will be examined:

    •Low Pressure Ratio 1.2

  • 8/6/2008 37th Turbomachinery Symposium 10

    Operational Challenge:

    Low Pressure Ratio Compressor P2/P1

  • 8/6/2008 37th Turbomachinery Symposium 11

    Operational Challenge:

    Low Pressure Ratio Compressor P2/P1

  • 8/6/2008 37th Turbomachinery Symposium 12

    Operational Challenge:

    How Pressure Ratio Compressor P2/P1 >1.20

    14.70%Liquid Fraction

    7,7257,876HP

    615,000706,000Flow (lb./hr)

    172- 96T2 (oF)

    430350P2(Psia)

    107- 6T1 (oF)

    2901,080P1(Psia)

    18.2319.38Mw

    CompressorTurbo Expander

    50

    55

    60

    65

    70

    75

    80

    85

    90

    0.0 500000.0 1000000.0 1500000.0

    EXPANDER FLOW, lb/hr

    EXPANDER EFFICIENCY, %

    110%100% SP EED90%

    80%

    70%

    0

    2,000

    4,000

    6,000

    8,000

    10,000

    12,000

    14,000

    0.0 500000.0 1000000.0 1500000.0

    EXPANDER FLOW, lb/hr

    SHAFT POWER, hp

    110%

    100% SP EED

    90%

    80%

    70%

    0

    2,000

    4,000

    6,000

    8,000

    10,000

    12,000

    14,000

    0.0 200000.0 400000.0 600000.0 800000.0 1000000.0

    COMPRESSOR FLOW, lb/hr

    SHAFT POWER, hp

    110%

    100% SP EED

    90%

    80%

    70%

    Surg

    e lin

    e

    1.0

    1.1

    1.2

    1.3

    1.4

    1.5

    1.6

    1.7

    1.8

    0.0 200000.0 400000.0 600000.0 800000.0 1000000.0COMPRESSOR FLOW, lb/hr

    PRES

    SUR

    E R

    ATI

    O,

    P2/

    P1

    110%

    100% S P E E D

    90%

    80%

    70%

    Surg

    e lin

    e

    cont

    rol l

    ine

  • 8/6/2008 37th Turbomachinery Symposium 13

    Operational Challenge:

    High Pressure Ratio Compressor P2/P1 >1.20

    0

    2000

    4000

    6000

    8000

    10000

    12000

    14000

    16000

    18000

    -5000 -4000 -3000 -2000 -1000 0 1000 2000 3000 4000 5000

    Thrust load, Lb.

    Spee

    d, R

    PM

    Radial Load , Lb

    050

    100150200250300350400

    0 10000 20000

    RPM

    Radi

    al lo

    ad

    Radial Load , Lb

    Estimated Recycle Gas Temperature rise

    0

    100

    200

    300

    400

    500

    600

    0 5 10 15 20 25 30 35

    Time, Minute

    Tem

    pera

    ture

    , F

    P2/P1=1.4

    Bearing thrust capacityStart up axial load

    Valve close

    Valve open

  • 8/6/2008 37th Turbomachinery Symposium 14

    Estimated Recycle Gas Temperature rise

    0

    100

    200

    300

    400

    500

    600

    0 5 10 15 20 25 30 35

    Time, Minute

    Tem

    pera

    ture

    , F

    P2/P1=1.4

    P2/P1=1.2

    Alarm

    Comparison of compressor discharge gas temperature for low and high pressure ratio cases.

  • 8/6/2008 37th Turbomachinery Symposium 15

    Therefore the main operational problem associated with start up parallel turbo expander-compressor units is process gas temperature at the compressor discharge for high pressure ratio compressors

    The following remedies may be applied depending on circumstances. All these shall continue until the compressor discharge pressure approaches to compressor discharge header pressure:

    •Diluting closed loop warm recycle gas with cold gas

    •Venting compressor discharge to a lower pressure sink

    •Venting /flaring compressor discharge flow

  • 8/6/2008 37th Turbomachinery Symposium 16

    Diluting Closed Loop Warm Recycle Gas with Cold Gas

    Adding cooling gas from expander inlet to the recycle gas to maintain the discharge temperature below the Alarm Level

  • 8/6/2008 37th Turbomachinery Symposium 17

    Venting the recycle gas to expander discharge piping

    Venting Compressor Discharge to a Lower Pressure Sink

  • 8/6/2008 37th Turbomachinery Symposium 18

    More common in Older plants

    Venting /Flaring Compressor Discharge Flow

  • 8/6/2008 37th Turbomachinery Symposium 19

    Pros and Cons of the remedies:

    • Diluting closed loop warm recycle gas with cold gas:

    1. Loss of refrigeration2. Loss of condensate recovery3. Requires cold gas piping, valves, space, etc.

    1. No loss of process gas2. No environmental consequences

    • Venting compressor discharge to a lower pressure sink1. Loss of refrigeration2. Loss of condensate recovery3. Requires gas piping, valves, space, etc.

    1. No loss of process gas2. No environmental consequences

  • 8/6/2008 37th Turbomachinery Symposium 20

    Pros and Cons of the remedies:

    • Venting /flaring compressor discharge flow1. Loss of process gas2. Environmental consequences

    1. No piping loop2. Suitable for older plant with no expansion provisions

    • Because of loss of process gas and environmental consequences requires special attention

  • 8/6/2008 37th Turbomachinery Symposium 21

    Three start up alternatives will be evaluated:

    Alternate -1 Maintain flow of the operating unit at 100%

    Alternate-2 Increase flow of the operating unit to 130%

    Alternate-3 Decrease flow of the operating unit 70%

  • 8/6/2008 37th Turbomachinery Symposium 22

    Turboexpander Performance parameters during start up

    speed/design speed

    020406080

    100120

    0 50 100 150

    % Mass Flow

    Spee

    d

    % full speed

    Compressor pressure ratio

    11.11.21.31.41.51.6

    0 50 100 150

    % Mass Flow

    Pres

    sure

    Rat

    io

    Comp-P2/P1

    Pow er- KW/ per unit

    0

    2000

    4000

    6000

    8000

    0 50 100 150

    % Mass Flow

    KW Pow er- KW

    EXP- wt% liquid

    0

    5

    10

    15

    20

    0 50 100 150

    % Mass flow

    Wt %

    Liq

    uid

    EXP- w t% liq

  • 8/6/2008 37th Turbomachinery Symposium 23

    -600

    -400

    -200

    0

    200

    400

    600

    800

    1000

    1200

    1400

    0 5 10 15 20 25

    Poly. (100% Flow)

    Poly. (70% Flow)

    Poly. (130% Flow)

    Cumulative Economical Consequences

    Duration of start up, min

    $ 1,

    000

  • 8/6/2008 37th Turbomachinery Symposium 24

    Conclusions:

    • Capacity of cryogenic gas plants have increased over the last forty years • There are many cryogenic natural gas processing plants with parallel

    turbo expander-compressor units• Start up of one train EC while the other is in operation is an operational

    challenge• Compressor gas recycling is mandatory during start up• Several operational parameter of EC are to be monitored. Compressor

    discharge gas temperature is the critical parameter to be controlled• Two scenarios were considered, low pressure ratio (1.2) compressor• The former scenario does not impose any operational challenge during

    start up• The latter scenario demands special attention and procedures

    1. The most convenient method is to vent the recycle flow into the expander discharge stream

    2. The compressor recycle gas may be cooled down by diluting it with cold gas from the expander discharge

    3. If neither of the above is possible, the only remedy is to vent/flare gas- The most economical approach is to increase flow of the

    operating EC to 130% and then start up the parallel EC