FR1516562A - Bypass gas turbine engine - Google Patents

Bypass gas turbine engine

Info

Publication number
FR1516562A
FR1516562A FR99621A FR99621A FR1516562A FR 1516562 A FR1516562 A FR 1516562A FR 99621 A FR99621 A FR 99621A FR 99621 A FR99621 A FR 99621A FR 1516562 A FR1516562 A FR 1516562A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
bypass gas
bypass
engine
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
FR99621A
Other languages
French (fr)
Inventor
Sydney Ian Cowley
Geoffrey Light Wilde
Alfred John Honey
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Priority claimed from GB13419/66A external-priority patent/GB1139005A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR99621A priority Critical patent/FR1516562A/en
Application granted granted Critical
Publication of FR1516562A publication Critical patent/FR1516562A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR99621A 1966-03-25 1967-03-21 Bypass gas turbine engine Expired FR1516562A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR99621A FR1516562A (en) 1966-03-25 1967-03-21 Bypass gas turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB13419/66A GB1139005A (en) 1966-03-25 1966-03-25 Improvements in or relating to gas turbine by-pass engines
FR99621A FR1516562A (en) 1966-03-25 1967-03-21 Bypass gas turbine engine

Publications (1)

Publication Number Publication Date
FR1516562A true FR1516562A (en) 1968-03-08

Family

ID=26175014

Family Applications (1)

Application Number Title Priority Date Filing Date
FR99621A Expired FR1516562A (en) 1966-03-25 1967-03-21 Bypass gas turbine engine

Country Status (1)

Country Link
FR (1) FR1516562A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2628791A1 (en) * 1988-03-18 1989-09-22 Gen Electric FUEL DISPERSION BAR AND POSTCOMBUSTION CHAMBER COMPRISING SAME
FR2660736A1 (en) * 1990-04-04 1991-10-11 Gen Electric POOR STAGE COMBUSTION ASSEMBLY.
EP2096357A1 (en) * 2008-02-29 2009-09-02 Snecma Flame holder for reheat duct of a jet engine with separating flange, reheat duct and jet engine comprising a reheat duct
EP2472090A3 (en) * 2010-12-30 2014-03-05 Rolls-Royce North American Technologies, Inc. A gas engine turbine comprising a thrust augmentation system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2628791A1 (en) * 1988-03-18 1989-09-22 Gen Electric FUEL DISPERSION BAR AND POSTCOMBUSTION CHAMBER COMPRISING SAME
FR2660736A1 (en) * 1990-04-04 1991-10-11 Gen Electric POOR STAGE COMBUSTION ASSEMBLY.
EP2096357A1 (en) * 2008-02-29 2009-09-02 Snecma Flame holder for reheat duct of a jet engine with separating flange, reheat duct and jet engine comprising a reheat duct
FR2928202A1 (en) * 2008-02-29 2009-09-04 Snecma Sa FLAME HOOK FOR HEATER CHANNEL OF A TURBOJET ENGINE WITH A DISCHARGE SOLE, HEATING CHANNEL AND TURBOJET COMPRISING A HEATING CHANNEL.
US8307658B2 (en) 2008-02-29 2012-11-13 Snecma Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct
EP2472090A3 (en) * 2010-12-30 2014-03-05 Rolls-Royce North American Technologies, Inc. A gas engine turbine comprising a thrust augmentation system

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