FR1510762A - Moteur à turbine à gaz - Google Patents

Moteur à turbine à gaz

Info

Publication number
FR1510762A
FR1510762A FR94470A FR94470A FR1510762A FR 1510762 A FR1510762 A FR 1510762A FR 94470 A FR94470 A FR 94470A FR 94470 A FR94470 A FR 94470A FR 1510762 A FR1510762 A FR 1510762A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine
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
FR94470A
Other languages
English (en)
Inventor
Leslie John Brooks
Geoffrey William Morris
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
Application granted granted Critical
Publication of FR1510762A publication Critical patent/FR1510762A/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
    • 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
    • F02K1/56—Reversing jet main flow
    • F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage
    • 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
    • F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
    • F02K1/42—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet the means being movable into an inoperative position
    • 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
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
FR94470A 1966-02-14 1967-02-10 Moteur à turbine à gaz Expired FR1510762A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6461/66A GB1111219A (en) 1966-02-14 1966-02-14 Gas turbine engine

Publications (1)

Publication Number Publication Date
FR1510762A true FR1510762A (fr) 1968-01-19

Family

ID=9814900

Family Applications (1)

Application Number Title Priority Date Filing Date
FR94470A Expired FR1510762A (fr) 1966-02-14 1967-02-10 Moteur à turbine à gaz

Country Status (3)

Country Link
US (1) US3422624A (fr)
FR (1) FR1510762A (fr)
GB (1) GB1111219A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2068695A1 (fr) * 1969-11-28 1971-08-27 Gen Electric

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2241695B1 (fr) * 1973-08-21 1978-03-17 Bertin & Cie
US4073440A (en) * 1976-04-29 1978-02-14 The Boeing Company Combination primary and fan air thrust reversal control systems for long duct fan jet engines
US4216923A (en) * 1977-03-30 1980-08-12 Boeing Commercial Airplane Company Target type thrust reverser
GB2207468A (en) * 1987-06-01 1989-02-01 Secr Defence Vortex silencing in gas turbine engines
FR2766522B1 (fr) * 1997-07-24 1999-09-03 Hispano Suiza Sa Inverseur de poussee de turbosoufflante a obstacle a guidage axial lies au capot primaire
DE602006019925D1 (de) * 2006-10-12 2011-03-10 United Technologies Corp Translatorisch bewegbare innenhaube mit aerodynamischen klappenabschnitten
WO2008045089A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Profil aérodynamique pour capot de corps central de turbine à gaz
US7797944B2 (en) * 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
US7870721B2 (en) 2006-11-10 2011-01-18 United Technologies Corporation Gas turbine engine providing simulated boundary layer thickness increase
US8408491B2 (en) * 2007-04-24 2013-04-02 United Technologies Corporation Nacelle assembly having inlet airfoil for a gas turbine engine
US8205430B2 (en) * 2007-05-16 2012-06-26 United Technologies Corporation Variable geometry nacelle assembly for a gas turbine engine
US8402739B2 (en) * 2007-06-28 2013-03-26 United Technologies Corporation Variable shape inlet section for a nacelle assembly of a gas turbine engine
US9004399B2 (en) 2007-11-13 2015-04-14 United Technologies Corporation Nacelle flow assembly
US8186942B2 (en) * 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
US8192147B2 (en) * 2007-12-14 2012-06-05 United Technologies Corporation Nacelle assembly having inlet bleed

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032981A (en) * 1957-02-11 1962-05-08 Boeing Co Noise suppressor and thrust reverser for jet engine nozzles
US2938335A (en) * 1958-04-14 1960-05-31 Boeing Co Noise suppressor and thrust reverser
US3280561A (en) * 1965-06-07 1966-10-25 Gen Electric Thrust reverser mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2068695A1 (fr) * 1969-11-28 1971-08-27 Gen Electric

Also Published As

Publication number Publication date
DE1576782B1 (de) 1971-01-14
GB1111219A (en) 1968-04-24
US3422624A (en) 1969-01-21

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