FR2959280B1 - Procede de demarrage d'un moteur a turbine a gaz - Google Patents

Procede de demarrage d'un moteur a turbine a gaz Download PDF

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Publication number
FR2959280B1
FR2959280B1 FR1152781A FR1152781A FR2959280B1 FR 2959280 B1 FR2959280 B1 FR 2959280B1 FR 1152781 A FR1152781 A FR 1152781A FR 1152781 A FR1152781 A FR 1152781A FR 2959280 B1 FR2959280 B1 FR 2959280B1
Authority
FR
France
Prior art keywords
starting
gas turbine
turbine engine
engine
gas
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR1152781A
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English (en)
Other versions
FR2959280A1 (fr
Inventor
Kenneth Winston
Andre Ajami
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand Corp
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 Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of FR2959280A1 publication Critical patent/FR2959280A1/fr
Application granted granted Critical
Publication of FR2959280B1 publication Critical patent/FR2959280B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/262—Restarting after flame-out
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2220/00—Application
    • F05B2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Eletrric Generators (AREA)
FR1152781A 2010-04-23 2011-04-01 Procede de demarrage d'un moteur a turbine a gaz Expired - Fee Related FR2959280B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/765,916 US9086018B2 (en) 2010-04-23 2010-04-23 Starting a gas turbine engine to maintain a dwelling speed after light-off
US12/765916 2010-04-23

Publications (2)

Publication Number Publication Date
FR2959280A1 FR2959280A1 (fr) 2011-10-28
FR2959280B1 true FR2959280B1 (fr) 2018-03-30

Family

ID=44774280

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1152781A Expired - Fee Related FR2959280B1 (fr) 2010-04-23 2011-04-01 Procede de demarrage d'un moteur a turbine a gaz

Country Status (3)

Country Link
US (1) US9086018B2 (fr)
FR (1) FR2959280B1 (fr)
RU (1) RU2467192C1 (fr)

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Also Published As

Publication number Publication date
RU2467192C1 (ru) 2012-11-20
FR2959280A1 (fr) 2011-10-28
US20110259016A1 (en) 2011-10-27
US9086018B2 (en) 2015-07-21

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