CA1031170A - Start-up compressed air system for gas turbine engines - Google Patents

Start-up compressed air system for gas turbine engines

Info

Publication number
CA1031170A
CA1031170A CA238,902A CA238902A CA1031170A CA 1031170 A CA1031170 A CA 1031170A CA 238902 A CA238902 A CA 238902A CA 1031170 A CA1031170 A CA 1031170A
Authority
CA
Canada
Prior art keywords
compressed air
gas turbine
air system
turbine engines
engines
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
Application number
CA238,902A
Other languages
English (en)
French (fr)
Inventor
Willis E. Rose
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.)
Dresser Industries Inc
Original Assignee
Dresser Industries 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 Dresser Industries Inc filed Critical Dresser Industries Inc
Application granted granted Critical
Publication of CA1031170A publication Critical patent/CA1031170A/en
Expired legal-status Critical Current

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
    • F02C7/22—Fuel supply systems
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA238,902A 1975-01-22 1975-11-03 Start-up compressed air system for gas turbine engines Expired CA1031170A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/543,092 US3971210A (en) 1975-01-22 1975-01-22 Start-up compressed air system for gas turbine engines

Publications (1)

Publication Number Publication Date
CA1031170A true CA1031170A (en) 1978-05-16

Family

ID=24166545

Family Applications (1)

Application Number Title Priority Date Filing Date
CA238,902A Expired CA1031170A (en) 1975-01-22 1975-11-03 Start-up compressed air system for gas turbine engines

Country Status (6)

Country Link
US (1) US3971210A (OSRAM)
JP (1) JPS597016B2 (OSRAM)
CA (1) CA1031170A (OSRAM)
FR (1) FR2298694A1 (OSRAM)
GB (1) GB1530330A (OSRAM)
IT (1) IT1052479B (OSRAM)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4189914A (en) * 1978-06-19 1980-02-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Supercritical fuel injection system
EP0014075A1 (en) * 1979-01-22 1980-08-06 The Garrett Corporation Fuel atomising arrangements in gas turbine engines
JPS5915635A (ja) * 1982-07-15 1984-01-26 Hitachi Ltd 噴霧空気系統を有するガスタ−ビン
US5012646A (en) * 1988-11-28 1991-05-07 Machen, Inc. Turbine engine having combustor air precooler
US5136837A (en) * 1990-03-06 1992-08-11 General Electric Company Aircraft engine starter integrated boundary bleed system
US5125597A (en) * 1990-06-01 1992-06-30 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system
US5143329A (en) * 1990-06-01 1992-09-01 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed
US5137230A (en) * 1991-06-04 1992-08-11 General Electric Company Aircraft gas turbine engine bleed air energy recovery apparatus
WO1998020243A1 (en) * 1996-11-08 1998-05-14 Northern Research & Engineering Corporation Turbine engine with turbocompressor for supplying atomizing fluid to turbine engine fuel system
US6557337B1 (en) * 1998-09-25 2003-05-06 Alm Development, Inc. Gas turbine engine
US6324867B1 (en) * 1999-06-15 2001-12-04 Exxonmobil Oil Corporation Process and system for liquefying natural gas
GB9924545D0 (en) * 1999-10-19 1999-12-22 Rolls Royce Plc Vehicle main and auxiliary power units
JP3593488B2 (ja) 2000-02-25 2004-11-24 株式会社日立製作所 ガスタービン
US6499303B1 (en) * 2001-04-18 2002-12-31 General Electric Company Method and system for gas turbine power augmentation
US20040226299A1 (en) * 2003-05-12 2004-11-18 Drnevich Raymond Francis Method of reducing NOX emissions of a gas turbine
US8689562B2 (en) * 2009-09-13 2014-04-08 Donald W. Kendrick Combustion cavity layouts for fuel staging in trapped vortex combustors
US9086018B2 (en) 2010-04-23 2015-07-21 Hamilton Sundstrand Corporation Starting a gas turbine engine to maintain a dwelling speed after light-off
JP6290909B2 (ja) 2012-10-26 2018-03-07 パワーフェイズ・エルエルシー ガスタービンエネルギー補助システムおよび加熱システム、ならびに、その製造方法および使用方法
US10480418B2 (en) * 2012-10-26 2019-11-19 Powerphase Llc Gas turbine energy supplementing systems and heating systems, and methods of making and using the same
US10030580B2 (en) 2014-04-11 2018-07-24 Dynamo Micropower Corporation Micro gas turbine systems and uses thereof
CN105986846A (zh) * 2015-02-27 2016-10-05 福建三钢闽光股份有限公司 一种余热余能回收联合发电机组的对接式及空载冷却装置
CN107630754A (zh) * 2017-08-17 2018-01-26 俞平 燃气压缩机支持燃气轮机点火

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR972400A (OSRAM) * 1951-01-29
FR878970A (fr) * 1941-02-03 1943-02-10 Brown Dispositif pour le démarrage et la marche à vide de turbines à gaz à combustion continue et à refroidissement par air
US2303381A (en) * 1941-04-18 1942-12-01 Westinghouse Electric & Mfg Co Gas turbine power plant and method
DE768006C (de) * 1941-06-21 1955-05-05 Messerschmitt Boelkow Blohm Heissstrahltriebwerk zum Vortrieb von Luftfahrzeugen
US2394253A (en) * 1941-07-10 1946-02-05 Nettel Frederick Air expansion power system
US2813231A (en) * 1956-01-17 1957-11-12 Westinghouse Electric Corp Over-pressure protection of pipe lines
US2976683A (en) * 1958-09-08 1961-03-28 Gen Motors Corp Gas turbine fuel system with regenerator temperature compensation
FR1261487A (fr) * 1960-06-09 1961-05-19 Rover Co Ltd Système de mise en marche pour moteur à turbine à gaz
US3072058A (en) * 1961-08-18 1963-01-08 Socony Mobil Oil Co Inc Pipe line control system
US3577965A (en) * 1969-08-08 1971-05-11 Chandler Evans Inc Fuel atomization system having a compressor drive means
US3581493A (en) * 1969-12-12 1971-06-01 Avco Corp Air assist for fuel injector
US3722218A (en) * 1970-12-04 1973-03-27 Parker Hannifin Corp Air boost fuel atomizing system

Also Published As

Publication number Publication date
US3971210A (en) 1976-07-27
FR2298694A1 (fr) 1976-08-20
JPS597016B2 (ja) 1984-02-16
JPS5189917A (OSRAM) 1976-08-06
GB1530330A (en) 1978-10-25
FR2298694B1 (OSRAM) 1982-09-17
IT1052479B (it) 1981-06-20

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