FR1124095A - Gas turbine engine improvements - Google Patents

Gas turbine engine improvements

Info

Publication number
FR1124095A
FR1124095A FR1124095DA FR1124095A FR 1124095 A FR1124095 A FR 1124095A FR 1124095D A FR1124095D A FR 1124095DA FR 1124095 A FR1124095 A FR 1124095A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
gas
turbine
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
Other languages
French (fr)
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of FR1124095A publication Critical patent/FR1124095A/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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1124095D 1954-03-01 1955-03-01 Gas turbine engine improvements Expired FR1124095A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1124095X 1954-03-01

Publications (1)

Publication Number Publication Date
FR1124095A true FR1124095A (en) 1956-10-03

Family

ID=10875863

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1124095D Expired FR1124095A (en) 1954-03-01 1955-03-01 Gas turbine engine improvements

Country Status (1)

Country Link
FR (1) FR1124095A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095598B (en) * 1957-02-16 1960-12-22 Messerschmitt Ag Supersonic diffuser, especially for aircraft engines
DE1117953B (en) * 1957-10-03 1961-11-23 Bristol Siddeley Engines Ltd Device to prevent ice build-up in pipe bends
DE1283600B (en) * 1964-12-09 1968-11-21 Ver Flugtechnische Werke Ramjet engine with an intermittent jet engine arranged in its interior
EP0161561A1 (en) * 1984-05-15 1985-11-21 A. S. Kongsberg Väpenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
US4707981A (en) * 1986-01-27 1987-11-24 Rockwell International Corporation Variable expansion ratio reaction engine
EP0578951A1 (en) * 1992-07-11 1994-01-19 Daimler-Benz Aerospace Aktiengesellschaft Jet engine
US20140097271A1 (en) * 2012-10-10 2014-04-10 Eads Deutschland Gmbh Aircraft engine with an apparatus for pulsating expiration of gas into the exhaus nozzle

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095598B (en) * 1957-02-16 1960-12-22 Messerschmitt Ag Supersonic diffuser, especially for aircraft engines
DE1117953B (en) * 1957-10-03 1961-11-23 Bristol Siddeley Engines Ltd Device to prevent ice build-up in pipe bends
DE1283600B (en) * 1964-12-09 1968-11-21 Ver Flugtechnische Werke Ramjet engine with an intermittent jet engine arranged in its interior
EP0161561A1 (en) * 1984-05-15 1985-11-21 A. S. Kongsberg Väpenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
US4628687A (en) * 1984-05-15 1986-12-16 A/S Kongsberg Vapenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
US4707981A (en) * 1986-01-27 1987-11-24 Rockwell International Corporation Variable expansion ratio reaction engine
EP0578951A1 (en) * 1992-07-11 1994-01-19 Daimler-Benz Aerospace Aktiengesellschaft Jet engine
US20140097271A1 (en) * 2012-10-10 2014-04-10 Eads Deutschland Gmbh Aircraft engine with an apparatus for pulsating expiration of gas into the exhaus nozzle
US9193469B2 (en) * 2012-10-10 2015-11-24 Airbus Defence and Space GmbH Aircraft engine with an apparatus for pulsating expiration of gas into the exhaust nozzle

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