JPS52139816A - Thrust reversing device for jet engine - Google Patents

Thrust reversing device for jet engine

Info

Publication number
JPS52139816A
JPS52139816A JP4746677A JP4746677A JPS52139816A JP S52139816 A JPS52139816 A JP S52139816A JP 4746677 A JP4746677 A JP 4746677A JP 4746677 A JP4746677 A JP 4746677A JP S52139816 A JPS52139816 A JP S52139816A
Authority
JP
Japan
Prior art keywords
jet engine
reversing device
thrust reversing
thrust
jet
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.)
Pending
Application number
JP4746677A
Other languages
Japanese (ja)
Inventor
Meson Herumintoraa Oogasutasu
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JPS52139816A publication Critical patent/JPS52139816A/en
Pending 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
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP4746677A 1976-04-28 1977-04-26 Thrust reversing device for jet engine Pending JPS52139816A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68090876A 1976-04-28 1976-04-28

Publications (1)

Publication Number Publication Date
JPS52139816A true JPS52139816A (en) 1977-11-22

Family

ID=24733013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4746677A Pending JPS52139816A (en) 1976-04-28 1977-04-26 Thrust reversing device for jet engine

Country Status (5)

Country Link
JP (1) JPS52139816A (en)
BE (1) BE853946A (en)
DE (1) DE2718643A1 (en)
FR (1) FR2349738A1 (en)
IT (1) IT1203685B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010529346A (en) * 2007-06-01 2010-08-26 エアバス・オペレーションズ Aircraft propulsion assembly with sliding nacelle
CN112996998A (en) * 2018-11-09 2021-06-18 赛峰短舱公司 Sealing joint for aircraft turbojet engine nacelle

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2669679B1 (en) * 1990-11-28 1994-04-29 Sud Ouest Conception Aeronauti GAS EJECTION NOZZLE FOR A REACTION ENGINE AND A REACTION ENGINE EQUIPPED WITH SUCH A NOZZLE, PARTICULARLY A SEPARATE FLOW TYPE ENGINE.
FR2812035B1 (en) * 2000-07-24 2003-08-29 Hurel Dubois Avions IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE
GB0025666D0 (en) * 2000-10-19 2000-12-06 Short Brothers Plc Aircraft propulsive power unit
US6824101B2 (en) * 2003-02-17 2004-11-30 The Boeing Company Apparatus and method for mounting a cascade support ring to a thrust reverser
BR112016013122A2 (en) * 2013-12-23 2017-08-08 Gen Electric AIRCRAFT AND INJECTION COOLING SYSTEM
FR3077847B1 (en) * 2018-02-09 2020-02-14 Safran Nacelles SHUTTER INVERTER FOR PROPULSIVE AIRCRAFT ASSEMBLY

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010529346A (en) * 2007-06-01 2010-08-26 エアバス・オペレーションズ Aircraft propulsion assembly with sliding nacelle
CN112996998A (en) * 2018-11-09 2021-06-18 赛峰短舱公司 Sealing joint for aircraft turbojet engine nacelle

Also Published As

Publication number Publication date
BE853946A (en) 1977-08-16
FR2349738A1 (en) 1977-11-25
DE2718643A1 (en) 1977-11-10
IT1203685B (en) 1989-02-15

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