WO2002036952A3 - Minimum fuel flow schedule adjustment method for turbine engine control - Google Patents

Minimum fuel flow schedule adjustment method for turbine engine control Download PDF

Info

Publication number
WO2002036952A3
WO2002036952A3 PCT/US2001/048228 US0148228W WO0236952A3 WO 2002036952 A3 WO2002036952 A3 WO 2002036952A3 US 0148228 W US0148228 W US 0148228W WO 0236952 A3 WO0236952 A3 WO 0236952A3
Authority
WO
WIPO (PCT)
Prior art keywords
fuel flow
minimum fuel
turbine engine
flow schedule
engine control
Prior art date
Application number
PCT/US2001/048228
Other languages
French (fr)
Other versions
WO2002036952A2 (en
Inventor
Mohamad Hanif Vhora
Original Assignee
Honeywell Int Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell Int Inc filed Critical Honeywell Int Inc
Priority to AU2002220278A priority Critical patent/AU2002220278A1/en
Publication of WO2002036952A2 publication Critical patent/WO2002036952A2/en
Publication of WO2002036952A3 publication Critical patent/WO2002036952A3/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00Mathematical features
    • F05D2200/10Basic functions
    • F05D2200/13Product
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/07Purpose of the control system to improve fuel economy

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

A control and method is provided that continuously adjusts minimum fuel flow schedules in the electronic control unit of a gas turbine engine. The control and method includes the steps of generating a fuel command signal; a sensed fuel flow signal and a minimum fuel flow schedule. The minimum fuel flow schedule is then multiplied by the ratio of the fuel command signal to the sensed fuel flow signal to provide an adjusted minimum fuel flow schedule.
PCT/US2001/048228 2000-10-31 2001-10-29 Minimum fuel flow schedule adjustment method for turbine engine control WO2002036952A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2002220278A AU2002220278A1 (en) 2000-10-31 2001-10-29 Minimum fuel flow schedule adjustment method for turbine engine control

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US70341000A 2000-10-31 2000-10-31
US09/703,410 2000-10-31

Publications (2)

Publication Number Publication Date
WO2002036952A2 WO2002036952A2 (en) 2002-05-10
WO2002036952A3 true WO2002036952A3 (en) 2003-01-09

Family

ID=24825268

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2001/048228 WO2002036952A2 (en) 2000-10-31 2001-10-29 Minimum fuel flow schedule adjustment method for turbine engine control

Country Status (3)

Country Link
AU (1) AU2002220278A1 (en)
TW (1) TW534949B (en)
WO (1) WO2002036952A2 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3962863A (en) * 1973-11-28 1976-06-15 Nissan Motor Co., Ltd. Gas turbine engine fuel supply control
US4464895A (en) * 1982-05-26 1984-08-14 Chandler Evans Inc. Gas turbine engine starting technique and control
US4716719A (en) * 1985-04-17 1988-01-05 Hitachi, Ltd. Method of and apparatus for controlling fuel of gas turbine
EP0324633A2 (en) * 1988-01-15 1989-07-19 ROLLS-ROYCE plc Fuel control system
US5303541A (en) * 1991-10-11 1994-04-19 Alliedsignal Inc. Closed loop fuel control method

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3962863A (en) * 1973-11-28 1976-06-15 Nissan Motor Co., Ltd. Gas turbine engine fuel supply control
US4464895A (en) * 1982-05-26 1984-08-14 Chandler Evans Inc. Gas turbine engine starting technique and control
US4716719A (en) * 1985-04-17 1988-01-05 Hitachi, Ltd. Method of and apparatus for controlling fuel of gas turbine
EP0324633A2 (en) * 1988-01-15 1989-07-19 ROLLS-ROYCE plc Fuel control system
US5303541A (en) * 1991-10-11 1994-04-19 Alliedsignal Inc. Closed loop fuel control method

Also Published As

Publication number Publication date
TW534949B (en) 2003-06-01
AU2002220278A1 (en) 2002-05-15
WO2002036952A2 (en) 2002-05-10

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