FR1602870A - - Google Patents

Info

Publication number
FR1602870A
FR1602870A FR38880A FR1602870DA FR1602870A FR 1602870 A FR1602870 A FR 1602870A FR 38880 A FR38880 A FR 38880A FR 1602870D A FR1602870D A FR 1602870DA FR 1602870 A FR1602870 A FR 1602870A
Authority
FR
France
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
FR38880A
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 filed Critical
Application granted granted Critical
Publication of FR1602870A publication Critical patent/FR1602870A/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
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • 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
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR38880A 1964-07-01 1965-11-18 Expired FR1602870A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US37966964A 1964-07-01 1964-07-01
FR38880 1965-11-18
US66654667A 1967-08-31 1967-08-31

Publications (1)

Publication Number Publication Date
FR1602870A true FR1602870A (fr) 1971-02-08

Family

ID=27242734

Family Applications (1)

Application Number Title Priority Date Filing Date
FR38880A Expired FR1602870A (fr) 1964-07-01 1965-11-18

Country Status (4)

Country Link
US (1) US3533237A (fr)
DE (1) DE1526812C3 (fr)
FR (1) FR1602870A (fr)
GB (1) GB1211192A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2477100A1 (fr) * 1980-03-03 1981-09-04 Gen Electric Systeme d'ejection d'air de dilution de moteur a turbosoufflante

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4314681A (en) * 1979-08-31 1982-02-09 General Electric Company Drag-reducing component
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
US4410150A (en) * 1980-03-03 1983-10-18 General Electric Company Drag-reducing nacelle
AU555526B2 (en) * 1982-10-29 1986-09-25 General Electric Company Aircraft engine nacelle
US4799633A (en) * 1982-10-29 1989-01-24 General Electric Company Laminar flow necelle
FR2926536B1 (fr) * 2008-01-23 2010-07-30 Snecma Accrochage d'un systeme propulsif a un element de structure d'un aeronef
US9840917B2 (en) * 2011-12-13 2017-12-12 United Technologies Corporation Stator vane shroud having an offset

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3095166A (en) * 1963-06-25 briggs
US2416389A (en) * 1942-06-17 1947-02-25 Armstrong Siddeley Motors Ltd Torque balancing of jet propulsion turbine plant
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
FR1271544A (fr) * 1960-07-11 1961-09-15 Nord Aviation Combiné turboréacteur-statoréacteur
FR1325056A (fr) * 1962-03-15 1963-04-26 Nord Aviation Perfectionnements aux combinés turboréacteur-statoréacteur
US3241313A (en) * 1963-09-18 1966-03-22 Gen Electric Thrust deflector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2477100A1 (fr) * 1980-03-03 1981-09-04 Gen Electric Systeme d'ejection d'air de dilution de moteur a turbosoufflante

Also Published As

Publication number Publication date
GB1211192A (en) 1970-11-04
DE1526812B2 (de) 1978-02-02
DE1526812A1 (de) 1971-01-14
DE1526812C3 (de) 1978-09-28
US3533237A (en) 1970-10-13

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