FR2096529B1 - - Google Patents

Info

Publication number
FR2096529B1
FR2096529B1 FR7123381A FR7123381A FR2096529B1 FR 2096529 B1 FR2096529 B1 FR 2096529B1 FR 7123381 A FR7123381 A FR 7123381A FR 7123381 A FR7123381 A FR 7123381A FR 2096529 B1 FR2096529 B1 FR 2096529B1
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
FR7123381A
Other versions
FR2096529A1 (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.)
Aeronca Inc
Original Assignee
Aeronca Inc
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 Aeronca Inc filed Critical Aeronca Inc
Publication of FR2096529A1 publication Critical patent/FR2096529A1/fr
Application granted granted Critical
Publication of FR2096529B1 publication Critical patent/FR2096529B1/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
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • 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
    • F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine
    • 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)
  • Testing Of Engines (AREA)
  • Window Of Vehicle (AREA)
FR7123381A 1970-06-26 1971-06-25 Expired FR2096529B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5022470A 1970-06-26 1970-06-26

Publications (2)

Publication Number Publication Date
FR2096529A1 FR2096529A1 (fr) 1972-02-18
FR2096529B1 true FR2096529B1 (fr) 1975-07-11

Family

ID=21964044

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7123381A Expired FR2096529B1 (fr) 1970-06-26 1971-06-25

Country Status (3)

Country Link
US (1) US3616648A (fr)
FR (1) FR2096529B1 (fr)
GB (1) GB1358078A (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3794246A (en) * 1973-04-11 1974-02-26 Aeronca Inc Thrust reversing cascade assembly
GB1542642A (en) * 1975-07-15 1979-03-21 Rolls Royce Thrust reverser for by-pass gas turbine engine
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
GB1545089A (en) * 1976-09-11 1979-05-02 Rolls Royce Jet engine thrust reverser and cowl structure
US4185798A (en) * 1978-03-13 1980-01-29 Rohr Industries, Inc. Thrust reverser-cascade two door pre-exit
US4340178A (en) * 1980-05-05 1982-07-20 Rohr Industries, Inc. Thrust reverser - cascade type
US5224342A (en) * 1992-02-13 1993-07-06 Lair Jean Pierre Latching and sealing arrangement for jet engine thrust reverser
US6311928B1 (en) 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
US6584763B2 (en) 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system
FR3060660B1 (fr) * 2016-12-20 2019-05-17 Safran Nacelles Nacelle de turboreacteur d'aeronef, ensemble propulsif et aeronef comportant une telle nacelle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2950595A (en) * 1954-11-01 1960-08-30 Marquardt Corp Thrust reverser
US3002343A (en) * 1956-10-29 1961-10-03 Aerojet General Co Thrust-reversing mechanism for jet aircraft
US3059426A (en) * 1957-03-22 1962-10-23 Marquardt Corp Thrust reverser utilizing aft end mechanical blockage
US2955418A (en) * 1958-08-06 1960-10-11 Ryan Aeronautical Co Combination augmenter, sound suppressor and thrust reverser for jet engines

Also Published As

Publication number Publication date
GB1358078A (en) 1974-06-26
US3616648A (en) 1971-11-02
FR2096529A1 (fr) 1972-02-18

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Legal Events

Date Code Title Description
ST Notification of lapse