DE3870702D1 - Gestaenge fuer ein schubumlenkgitter mit geregeltem querschnitt. - Google Patents

Gestaenge fuer ein schubumlenkgitter mit geregeltem querschnitt.

Info

Publication number
DE3870702D1
DE3870702D1 DE8888630099T DE3870702T DE3870702D1 DE 3870702 D1 DE3870702 D1 DE 3870702D1 DE 8888630099 T DE8888630099 T DE 8888630099T DE 3870702 T DE3870702 T DE 3870702T DE 3870702 D1 DE3870702 D1 DE 3870702D1
Authority
DE
Germany
Prior art keywords
rod
section
drawer grid
regulated cross
regulated
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 - Fee Related
Application number
DE8888630099T
Other languages
English (en)
Inventor
Eric Jonathan Ward
Philip Russell Scott
Edward Boyd Thayer
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE3870702D1 publication Critical patent/DE3870702D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • 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
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • 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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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
    • 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)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE8888630099T 1987-05-22 1988-05-19 Gestaenge fuer ein schubumlenkgitter mit geregeltem querschnitt. Expired - Fee Related DE3870702D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/053,289 US4760960A (en) 1987-05-22 1987-05-22 Linkage for area controlled, thrust vectoring vane cascade

Publications (1)

Publication Number Publication Date
DE3870702D1 true DE3870702D1 (de) 1992-06-11

Family

ID=21983188

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888630099T Expired - Fee Related DE3870702D1 (de) 1987-05-22 1988-05-19 Gestaenge fuer ein schubumlenkgitter mit geregeltem querschnitt.

Country Status (5)

Country Link
US (1) US4760960A (de)
EP (1) EP0292422B1 (de)
KR (1) KR960003686B1 (de)
CN (1) CN1026022C (de)
DE (1) DE3870702D1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2196911B (en) * 1986-10-30 1990-03-14 Rolls Royce Plc Thrust reverser
US5161752A (en) * 1991-01-11 1992-11-10 United Technologies Corporation In-flight reverser
US5150862A (en) * 1991-01-11 1992-09-29 United Technologies Corporation In-flight reverser
NL9101782A (nl) * 1991-10-24 1993-05-17 Philip Rijk Koudijs Afvoersysteem voor verbrandingsgassen.
US5485958A (en) * 1994-06-06 1996-01-23 Rolls-Royce, Incorporated Mechanism for operating a cascade of variable pitch vanes
DE4426195C2 (de) * 1994-07-23 1998-02-05 Daimler Benz Aerospace Ag Schubdüse in Rechteckbauweise für Strahltriebwerke
US5706649A (en) * 1995-04-03 1998-01-13 Boeing North American, Inc. Multi axis thrust vectoring for turbo fan engines
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
DE10313729B4 (de) * 2003-03-27 2007-11-29 Airbus Deutschland Gmbh Luftauslaßventil für ein Flugzeug
US7568348B2 (en) * 2005-11-28 2009-08-04 Aerojet-General Corporation Nozzle assembly for rocket and ramjet applications
US7836681B2 (en) * 2006-06-13 2010-11-23 Rolls-Royce Corporation Mechanism for a vectoring exhaust nozzle
US8365515B2 (en) 2006-10-12 2013-02-05 United Technologies Corporation Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle
US8109467B2 (en) * 2009-04-24 2012-02-07 United Technologies Corporation Thrust reverser assembly with shaped drag links
US9874176B2 (en) * 2015-01-14 2018-01-23 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US10018151B2 (en) * 2015-01-14 2018-07-10 The Boeing Company Methods and apparatus to vary reverse thrust of aircraft engines
US10077740B2 (en) * 2015-10-16 2018-09-18 The Boeing Company Folding door thrust reversers for aircraft engines
FR3073493B1 (fr) * 2017-11-12 2020-06-19 Michel Aguilar Dispositif multiplicateur de poussee

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2964905A (en) * 1960-12-20 Aircraft control means
US3100377A (en) * 1960-11-14 1963-08-13 Northrop Corp Deflecting means for jet aircraft and the like
US3081597A (en) * 1960-12-06 1963-03-19 Northrop Corp Variable thrust vectoring systems defining convergent nozzles
US3292880A (en) * 1964-09-01 1966-12-20 Gen Electric Thrust deflecting mechanism
US3292864A (en) * 1965-01-21 1966-12-20 Gen Electric Thrust reverser and deflector
US3335960A (en) * 1965-03-04 1967-08-15 Gen Electric Louver actuation system
US3344604A (en) * 1965-12-14 1967-10-03 Gen Dynamics Corp Apparatus for selectively reversing the thrust of front fan jet engines
US3380661A (en) * 1966-04-12 1968-04-30 United Aircraft Corp Thrust deflector
DE1284851B (de) * 1967-07-26 1968-12-05 Ver Flugtechnische Werke Flugzeug mit zumindest einem Hubtriebwerk, dessen Auslass durch zwei hintereinanderliegende Klappen verschliessbar ist
US3601992A (en) * 1970-06-10 1971-08-31 Rohr Corp Thrust reversing apparatus
US3770227A (en) * 1971-09-10 1973-11-06 Us Air Force Jet wing with multiple thrust augmentors
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
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser
US4241647A (en) * 1979-08-20 1980-12-30 Dayco Corporation Air damper valve
GB2155552B (en) * 1981-02-24 1986-02-26 Rolls Royce Adjustable jet propulsion nozzle

Also Published As

Publication number Publication date
EP0292422A2 (de) 1988-11-23
CN1026022C (zh) 1994-09-28
CN1032218A (zh) 1989-04-05
EP0292422B1 (de) 1992-05-06
EP0292422A3 (en) 1989-11-15
KR960003686B1 (ko) 1996-03-21
US4760960A (en) 1988-08-02
KR880013768A (ko) 1988-12-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee