FR1207598A - Enveloppe pour turbo-réacteur - Google Patents

Enveloppe pour turbo-réacteur

Info

Publication number
FR1207598A
FR1207598A FR1207598DA FR1207598A FR 1207598 A FR1207598 A FR 1207598A FR 1207598D A FR1207598D A FR 1207598DA FR 1207598 A FR1207598 A FR 1207598A
Authority
FR
France
Prior art keywords
turbo
reactor casing
reactor
casing
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
English (en)
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.)
LE MINISTRE de la DEFENSE NATIONALE DU CANADA
Original Assignee
LE MINISTRE de la DEFENSE NATIONALE DU CANADA
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 LE MINISTRE de la DEFENSE NATIONALE DU CANADA filed Critical LE MINISTRE de la DEFENSE NATIONALE DU CANADA
Application granted granted Critical
Publication of FR1207598A publication Critical patent/FR1207598A/fr
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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Supercharger (AREA)
FR1207598D 1957-02-04 1958-06-27 Enveloppe pour turbo-réacteur Expired FR1207598A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US637981A US2853854A (en) 1957-02-04 1957-02-04 Shroud assembly for gas turbine engines

Publications (1)

Publication Number Publication Date
FR1207598A true FR1207598A (fr) 1960-02-17

Family

ID=24558160

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1207598D Expired FR1207598A (fr) 1957-02-04 1958-06-27 Enveloppe pour turbo-réacteur

Country Status (2)

Country Link
US (1) US2853854A (fr)
FR (1) FR1207598A (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013385A (en) * 1957-09-27 1961-12-19 Rolls Royce Air intake for power plant of supersonic aircraft
US3032977A (en) * 1958-06-05 1962-05-08 Gen Electric Correlated bypass inlet and outlet control for a supersonic reaction powerplant
US3172253A (en) * 1959-01-02 1965-03-09 Garrett Corp Combination turbo and ramjet propulsion apparatus
US3358457A (en) * 1961-02-27 1967-12-19 Garrett Corp Engine cooling system
GB1090586A (en) * 1966-02-03 1967-11-08 Rolls Royce Improvements relating to jet engines
US4163366A (en) * 1977-05-23 1979-08-07 Avco Corporation Apparatus for disposal of leaking fluids in a turbofan engine
US4493184A (en) * 1983-03-07 1985-01-15 United Technologies Corporation Pressurized nacelle compartment for active clearance controlled gas turbine engines
GB2164706B (en) * 1984-09-25 1988-06-08 United Technologies Corp Pressurized nacelle compartment for active clearance controlled gas turbine engines
US5357742A (en) * 1993-03-12 1994-10-25 General Electric Company Turbojet cooling system
US5402638A (en) * 1993-10-04 1995-04-04 General Electric Company Spillage drag reducing flade engine
US5404713A (en) * 1993-10-04 1995-04-11 General Electric Company Spillage drag and infrared reducing flade engine
US6651929B2 (en) * 2001-10-29 2003-11-25 Pratt & Whitney Canada Corp. Passive cooling system for auxiliary power unit installation
US20050091963A1 (en) * 2003-10-30 2005-05-05 Gongling Li Aircraft turbine engine and an air ejection assembly for use therewith
US7373779B2 (en) * 2004-10-19 2008-05-20 General Electric Company Methods and apparatus for cooling gas turbine engines
US8099915B2 (en) 2005-06-02 2012-01-24 Snapsports Company Modular floor tile with resilient support members
US7958681B2 (en) 2005-06-02 2011-06-14 Moller Jr Jorgen J Modular floor tile with nonslip insert system
US7506839B2 (en) * 2005-11-30 2009-03-24 United Technologies Corporation Engine airframe J-seal damper
US9212623B2 (en) * 2007-12-26 2015-12-15 United Technologies Corporation Heat exchanger arrangement for turbine engine
GB201610958D0 (en) * 2016-06-23 2016-08-10 Rolls Royce Plc Gas turbine exhaust cooling system
US11242156B2 (en) * 2019-03-15 2022-02-08 Hamilton Sundstrand Corporation Plug in fluid cooled electrical connections for tail cone mounted generator
FR3107563A1 (fr) * 2020-02-25 2021-08-27 Airbus Operations Ensemble propulsif pour aeronef comportant un systeme de ventilation

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2612748A (en) * 1946-04-06 1952-10-07 Tenney Pulse jet mount
US2663517A (en) * 1949-10-11 1953-12-22 Lockheed Aircraft Corp Aircraft power plant installation

Also Published As

Publication number Publication date
US2853854A (en) 1958-09-30

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