DE3882761D1 - Verfahren und gelenkgetriebe zur positionierung einer konvergierenden klappe und eines koaxialen bogenfoermigen ventils. - Google Patents

Verfahren und gelenkgetriebe zur positionierung einer konvergierenden klappe und eines koaxialen bogenfoermigen ventils.

Info

Publication number
DE3882761D1
DE3882761D1 DE8888630037T DE3882761T DE3882761D1 DE 3882761 D1 DE3882761 D1 DE 3882761D1 DE 8888630037 T DE8888630037 T DE 8888630037T DE 3882761 T DE3882761 T DE 3882761T DE 3882761 D1 DE3882761 D1 DE 3882761D1
Authority
DE
Germany
Prior art keywords
valve
positioning
arc shaped
joint transmission
converging
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
DE8888630037T
Other languages
English (en)
Other versions
DE3882761T2 (de
Inventor
Eric Jonathan Ward
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
Publication of DE3882761D1 publication Critical patent/DE3882761D1/de
Application granted granted Critical
Publication of DE3882761T2 publication Critical patent/DE3882761T2/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
    • F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/323—Arrangement of components according to their shape convergent
    • 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)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Exhaust Silencers (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Arc Welding In General (AREA)
DE88630037T 1987-03-27 1988-03-03 Verfahren und Gelenkgetriebe zur Positionierung einer konvergierenden Klappe und eines koaxialen bogenförmigen Ventils. Expired - Fee Related DE3882761T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/030,794 US4767055A (en) 1987-03-27 1987-03-27 Method and linkage for positioning a convergent flap and coaxial arc valve

Publications (2)

Publication Number Publication Date
DE3882761D1 true DE3882761D1 (de) 1993-09-09
DE3882761T2 DE3882761T2 (de) 1993-11-25

Family

ID=21856079

Family Applications (1)

Application Number Title Priority Date Filing Date
DE88630037T Expired - Fee Related DE3882761T2 (de) 1987-03-27 1988-03-03 Verfahren und Gelenkgetriebe zur Positionierung einer konvergierenden Klappe und eines koaxialen bogenförmigen Ventils.

Country Status (6)

Country Link
US (1) US4767055A (de)
EP (1) EP0284540B1 (de)
JP (1) JPS63253160A (de)
KR (1) KR960013104B1 (de)
CN (1) CN1015322B (de)
DE (1) DE3882761T2 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4830519A (en) * 1987-04-06 1989-05-16 United Technologies Corporation Annular seal assembly
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
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
US5188292A (en) * 1991-06-28 1993-02-23 The United States Of America As Represented By The Secretary Of The Air Force Thermal shields for rotating members in a gas flow path
FR2704907B1 (fr) * 1993-05-06 1995-06-09 Hispano Suiza Sa Systeme auto-bloquant de commande des portes d'inverseur de poussee d'un turboreacteur.
US6386829B1 (en) 1999-07-02 2002-05-14 Power Technology, Incorporated Multi-valve arc inlet for steam turbine
US7721550B2 (en) 2005-08-10 2010-05-25 United Technologies Corporation Aircraft engine exhaust flap curved strut slot
FR2900980B1 (fr) * 2006-05-10 2011-08-19 Aircelle Sa Nacelle pour turboreacteur double flux a grand taux de dilution
FR2912189B1 (fr) * 2007-02-01 2012-02-17 Airbus France Nacelle d'aeronef incorporant un dispositif pour inverser la poussee
US9719370B2 (en) * 2007-03-30 2017-08-01 United Technologies Corporation Linkage system with wear reduction
FR2929998B1 (fr) * 2008-04-14 2011-08-12 Aircelle Sa Nacelle de turboreacteur a double flux
CN101737919B (zh) * 2008-11-07 2013-01-16 Lg电子株式会社 空调机
FR2952128B1 (fr) * 2009-11-05 2011-11-04 Aircelle Sa Dispositif d'inverseur de poussee
FR2958910B1 (fr) * 2010-04-20 2012-04-27 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
US8931281B2 (en) 2010-06-07 2015-01-13 United Technologies Corporation External flap retaining mechanism
FR3042226B1 (fr) * 2015-10-13 2019-06-07 Safran Nacelles Tuyere de section variable pour nacelle d'aeronef et nacelle pour un turboreacteur d'aeronef comportant une telle tuyere
FR3092819A1 (fr) * 2019-02-18 2020-08-21 Airbus Operations Nacelle d’un turboreacteur comportant une porte de blocage et un systeme de deploiement de la porte de blocage
CN113492988B (zh) * 2020-04-02 2023-06-20 中国航发商用航空发动机有限责任公司 反推力装置和航空发动机
US20220018309A1 (en) * 2020-05-15 2022-01-20 Rohr, Inc. Passively actuated variable area nozzle for an aircraft propulsion system

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1481543A1 (de) * 1967-01-31 1969-10-23 Entwicklungsring Sued Gmbh Duese fuer Strahltriebwerk
GB1211923A (en) * 1968-08-30 1970-11-11 Rolls Royce Thrust reverser for gas turbine jet propulsion engine
US3558058A (en) * 1969-03-14 1971-01-26 Us Air Force Thrust vectorable supersonic nozzle
US3667680A (en) * 1970-04-24 1972-06-06 Boeing Co Jet engine exhaust nozzle system
US4052007A (en) * 1975-11-25 1977-10-04 United Technologies Corporation Flap-type two-dimensional nozzle
US4375276A (en) * 1980-06-02 1983-03-01 General Electric Company Variable geometry exhaust nozzle
GB2155552B (en) * 1981-02-24 1986-02-26 Rolls Royce Adjustable jet propulsion nozzle
US4605169A (en) * 1983-12-27 1986-08-12 United Technologies Corporation Exhaust nozzle construction
US4591097A (en) * 1984-05-16 1986-05-27 The United States Of America As Represented By The Secretary Of The Air Force Thrust reverser/exhaust nozzle assembly for a gas turbine engine
US4753392A (en) * 1984-11-02 1988-06-28 United Technologies Corporation Two dimensional gas turbine engine exhaust nozzle
US4690329A (en) * 1984-11-02 1987-09-01 United Technologies Corporation Exhaust nozzle coupled with reverser exhaust door

Also Published As

Publication number Publication date
US4767055A (en) 1988-08-30
EP0284540A2 (de) 1988-09-28
KR880011458A (ko) 1988-10-28
EP0284540A3 (en) 1990-02-07
CN1015322B (zh) 1992-01-22
EP0284540B1 (de) 1993-08-04
DE3882761T2 (de) 1993-11-25
CN88101725A (zh) 1988-10-19
JPS63253160A (ja) 1988-10-20
KR960013104B1 (ko) 1996-09-30

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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