GB1249609A - Powerplant comprising a gas turbine engine - Google Patents

Powerplant comprising a gas turbine engine

Info

Publication number
GB1249609A
GB1249609A GB8164/70A GB816470A GB1249609A GB 1249609 A GB1249609 A GB 1249609A GB 8164/70 A GB8164/70 A GB 8164/70A GB 816470 A GB816470 A GB 816470A GB 1249609 A GB1249609 A GB 1249609A
Authority
GB
United Kingdom
Prior art keywords
thrust
engine
intake
turbine
reverse
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
GB8164/70A
Other languages
English (en)
Inventor
Jack Britt
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8164/70A priority Critical patent/GB1249609A/en
Priority to FR7109324A priority patent/FR2081027B1/fr
Publication of GB1249609A publication Critical patent/GB1249609A/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • 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)
  • Control Of Turbines (AREA)
GB8164/70A 1970-02-20 1970-02-20 Powerplant comprising a gas turbine engine Expired GB1249609A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB8164/70A GB1249609A (en) 1970-02-20 1970-02-20 Powerplant comprising a gas turbine engine
FR7109324A FR2081027B1 (enExample) 1970-02-20 1971-03-17

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8164/70A GB1249609A (en) 1970-02-20 1970-02-20 Powerplant comprising a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1249609A true GB1249609A (en) 1971-10-13

Family

ID=9846998

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8164/70A Expired GB1249609A (en) 1970-02-20 1970-02-20 Powerplant comprising a gas turbine engine

Country Status (2)

Country Link
FR (1) FR2081027B1 (enExample)
GB (1) GB1249609A (enExample)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3123946B1 (fr) 2021-06-13 2023-05-26 Safran Aircraft Engines Entrée d’air d’ensemble propulsif d’aéronef comprenant des organes mobiles pour favoriser une phase d’inversion de poussée et procédé d’utilisation d’une telle entrée d’air

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3019600A (en) * 1959-08-03 1962-02-06 United Aircraft Corp Turbo-fan engine thrust reverser

Also Published As

Publication number Publication date
FR2081027B1 (enExample) 1975-08-22
FR2081027A1 (enExample) 1971-11-26

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