DK0544817T3 - Udstrømningsdyse med variabel trykretning - Google Patents

Udstrømningsdyse med variabel trykretning

Info

Publication number
DK0544817T3
DK0544817T3 DK91917208.0T DK91917208T DK0544817T3 DK 0544817 T3 DK0544817 T3 DK 0544817T3 DK 91917208 T DK91917208 T DK 91917208T DK 0544817 T3 DK0544817 T3 DK 0544817T3
Authority
DK
Denmark
Prior art keywords
variable pressure
pressure direction
outflow nozzle
outflow
nozzle
Prior art date
Application number
DK91917208.0T
Other languages
English (en)
Inventor
Raymond J Bruchez Jr
George E Mount
James T Dixon
Wayne T Movick
Jim D Stewart
Russel H Hagerman
Aldo Arena
Original Assignee
United Technologies Corp
Grumman 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, Grumman Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DK0544817T3 publication Critical patent/DK0544817T3/da

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
    • F02K1/002—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
    • F02K1/008—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 in any rearward direction
    • 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
    • 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
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • 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)
  • Exhaust Silencers (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supporting Of Heads In Record-Carrier Devices (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
DK91917208.0T 1990-08-23 1991-08-22 Udstrømningsdyse med variabel trykretning DK0544817T3 (da)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/571,797 US5082182A (en) 1990-08-23 1990-08-23 Thrust vectoring exhaust nozzle

Publications (1)

Publication Number Publication Date
DK0544817T3 true DK0544817T3 (da) 1996-10-21

Family

ID=24285098

Family Applications (1)

Application Number Title Priority Date Filing Date
DK91917208.0T DK0544817T3 (da) 1990-08-23 1991-08-22 Udstrømningsdyse med variabel trykretning

Country Status (10)

Country Link
US (1) US5082182A (da)
EP (1) EP0544817B1 (da)
JP (1) JPH06500611A (da)
KR (1) KR0160317B1 (da)
DE (1) DE69120082T2 (da)
DK (1) DK0544817T3 (da)
ES (1) ES2091944T3 (da)
IL (1) IL99276A (da)
NO (1) NO180424C (da)
WO (1) WO1992003648A1 (da)

Families Citing this family (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5235808A (en) * 1990-02-12 1993-08-17 General Electric Company Exhaust nozzle including idle thrust spoiling
GB2464330B (en) * 1991-02-19 2010-09-29 Rolls Royce Plc Exhaust nozzle for thrust vectoring
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
US5176323A (en) * 1991-04-15 1993-01-05 General Electric Company Reduced weight nozzle actuation mechanism
US5174502A (en) * 1991-05-10 1992-12-29 General Electric Company Support for a translating nozzle vectoring ring
DE69232222T2 (de) * 1991-05-16 2002-08-22 Gen Electric Hitzeschild für achsymmetrische schwenkbare Schubdüse
US5239815A (en) * 1991-09-23 1993-08-31 United Technologies Corporation Sync-ring assembly for a gas turbine engine exhaust nozzle
US5245823A (en) * 1991-09-23 1993-09-21 United Technologies Corporation External flap vectoring mechanism
ES2075782B1 (es) * 1992-02-20 1998-03-16 Sener Ing & Sist Tobera orientable de geometria variable para turbinas de gas.
US5215257A (en) * 1992-07-16 1993-06-01 United Technologies Corporation Divergent seal arrangement for a convergent/divergent nozzle
US5238189A (en) * 1992-07-16 1993-08-24 United Technologies Corporation Convergent-to-divergent seal hinge for a convergent/divergent nozzle
US5215256A (en) * 1992-07-16 1993-06-01 Barcza W Kevin Flap hinge arrangement for a convergent/divergent nozzle
US5232158A (en) * 1992-08-11 1993-08-03 United Technologies Corporation Convergent/divergent nozzle with seal centering
US5261606A (en) * 1992-10-26 1993-11-16 United Technologies Corporation Crossed strut divergent flap vectoring mechanism
US5351888A (en) * 1993-05-14 1994-10-04 General Electric Company Multi-axis vectorable exhaust nozzle
US5328098A (en) * 1993-07-09 1994-07-12 United Technologies Corporation Thrust vectoring ejector nozzle
US5335489A (en) * 1993-07-09 1994-08-09 United Technologies Corporation Gas turbine vectoring exhaust nozzle
US5364029A (en) * 1993-08-30 1994-11-15 United Technologies Corporation Axisymmetric convergent/divergent nozzle with external flaps
US5511376A (en) * 1993-08-31 1996-04-30 United Technologies Corporation Axisymmetric vectoring nozzle
ES2105929B1 (es) * 1993-11-23 1998-05-01 Sener Ing & Sist Tobera axisimetrica orientable de geometria variable para propulsores de turbina de gas.
FR2715192B1 (fr) * 1994-01-20 1996-02-16 Snecma Tuyère d'éjection de turboréacteur.
US5442909A (en) * 1994-05-13 1995-08-22 General Electric Company Control system for limiting the vector angle in an axisymmetric vectoring exhaust nozzle
US5820024A (en) * 1994-05-16 1998-10-13 General Electric Company Hollow nozzle actuating ring
ES2136475B1 (es) * 1994-05-20 2000-05-16 Sener Ing & Sist Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadas a propulsores de turbina de gas.
US5484105A (en) * 1994-07-13 1996-01-16 General Electric Company Cooling system for a divergent section of a nozzle
US5667140A (en) * 1994-12-02 1997-09-16 United Technologies Corporation Engine exhaust nozzle seal
US5683034A (en) * 1995-05-22 1997-11-04 United Technologies Corporation Engine exhaust nozzle seal
US5794851A (en) * 1995-12-07 1998-08-18 United Technologies Corporation Nozzle sealing apparatus
US5897120A (en) * 1997-04-15 1999-04-27 General Electric Company Outer flap elastic seal assembly
US6070830A (en) * 1997-09-29 2000-06-06 General Electric Company Faceted exhaust nozzle
FR2781254B1 (fr) * 1998-07-17 2000-08-18 Snecma Tuyere d'ejection de turboreacteur a masquage du jet de gaz
FR2790792B1 (fr) * 1999-03-10 2003-11-14 Klimov Corp Tuyere vectorielle
FR2796422B1 (fr) 1999-07-12 2001-09-07 Snecma Tuyere d'ejection de turboreacteur axisymetrique, convergente divergente a deviation de jet
US6622472B2 (en) * 2001-10-17 2003-09-23 Gateway Space Transport, Inc. Apparatus and method for thrust vector control
US7251941B2 (en) * 2004-03-10 2007-08-07 General Electric Company Ablative afterburner
US7587899B2 (en) * 2004-08-27 2009-09-15 University Of Houston Shape memory alloy actuated adaptive exhaust nozzle for jet engine
KR100625852B1 (ko) * 2004-10-07 2006-09-20 한국항공우주연구원 발사체의 고체모터 가동노즐 추력벡터제어용구동장치시스템의 보상제어방법 및 그 보상제어회로부
US7377099B2 (en) * 2005-05-27 2008-05-27 United Technologies Corporation System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
WO2007129937A1 (en) * 2006-05-04 2007-11-15 Volvo Aero Corporation A device for pivoting at least one pivotable element in a gas turbine engine
KR100782114B1 (ko) * 2007-01-03 2007-12-05 삼성전자주식회사 배기 장치 및 방법, 그리고 상기 배기 장치를 가지는반도체 제조 설비
US7721549B2 (en) * 2007-02-08 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
US7845176B2 (en) * 2007-03-20 2010-12-07 United Technologies Corporation Mode strut and divergent flap interface
US8931281B2 (en) * 2010-06-07 2015-01-13 United Technologies Corporation External flap retaining mechanism
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
US8443931B2 (en) 2011-04-06 2013-05-21 Lockheed Martin Corporation Noise reduction of supersonic jet engines
WO2014160509A1 (en) * 2013-03-13 2014-10-02 Rolls-Royce North American Technologies, Inc. Gas turbine engine with three stream, variable area, vectorable nozzle
CN103423025B (zh) * 2013-08-07 2016-01-20 中国航空工业集团公司沈阳发动机设计研究所 一种收敛喷管
US10837402B2 (en) 2020-01-09 2020-11-17 Guanhao Wu Thrust vector nozzle
CN114017198A (zh) * 2021-11-12 2022-02-08 中国航发沈阳发动机研究所 一种轴对称收扩喷管
CN114687886A (zh) * 2022-04-14 2022-07-01 中国航发沈阳发动机研究所 一种轴对称收扩喷管

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US3004385A (en) * 1958-06-25 1961-10-17 Gen Motors Corp Variable convergent-divergent jet nozzle
US3794244A (en) * 1971-12-20 1974-02-26 United Aircraft Corp Seal centering and retention means
US3792815A (en) * 1972-11-24 1974-02-19 United Aircraft Corp Balanced flap converging/diverging nozzle
FR2277239A2 (fr) * 1974-07-04 1976-01-30 Snecma Dispositif de commande de volets de tuyere d'ejection
US4181260A (en) * 1977-03-17 1980-01-01 General Electric Company Hydraulic actuation ring
DE2719439C2 (de) * 1977-04-30 1984-01-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Schubdüse zur Vektorsteuerung
US4128208A (en) * 1977-07-11 1978-12-05 General Electric Company Exhaust nozzle flap seal arrangement
US4176792A (en) * 1977-07-11 1979-12-04 General Electric Company Variable area exhaust nozzle
FR2437499A1 (fr) * 1978-09-27 1980-04-25 Snecma Perfectionnement aux tuyeres orientables pour propulseurs a reaction
US4245787A (en) * 1978-12-01 1981-01-20 General Electric Company Variable area nozzle system
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
US4440347A (en) * 1981-12-28 1984-04-03 United Technologies Corporation Simplified means for balancing the loads on a variable area nozzle
US4447009A (en) * 1981-12-28 1984-05-08 United Technologies Corporation Three-dimensional axially translatable convergent/divergent nozzle assembly
US4440346A (en) * 1981-12-28 1984-04-03 United Technologies Corporation Axially translatable variable area convergent/divergent nozzle
US4456178A (en) * 1982-12-27 1984-06-26 United Technologies Corporation Exhaust nozzle assembly with dual unison ring structure
DE3619652C1 (en) * 1986-06-11 1990-10-11 Messerschmitt Boelkow Blohm Jet aircraft manoeuvring aid - has three movable flaps each suspended from four point linkage
US4994660A (en) * 1989-04-11 1991-02-19 Hitachi, Ltd. Axisymmetric vectoring exhaust nozzle

Also Published As

Publication number Publication date
KR0160317B1 (ko) 1999-01-15
DE69120082D1 (de) 1996-07-11
IL99276A (en) 1994-11-28
US5082182A (en) 1992-01-21
ES2091944T3 (es) 1996-11-16
DE69120082T2 (de) 1997-01-23
IL99276A0 (en) 1992-07-15
NO180424B (no) 1997-01-06
NO930577D0 (no) 1993-02-18
EP0544817A1 (en) 1993-06-09
EP0544817B1 (en) 1996-06-05
JPH06500611A (ja) 1994-01-20
WO1992003648A1 (en) 1992-03-05
KR930702605A (ko) 1993-09-09
NO180424C (no) 1997-04-16
NO930577L (no) 1993-02-18

Similar Documents

Publication Publication Date Title
DK0544817T3 (da) Udstrømningsdyse med variabel trykretning
NO168882C (no) Munnstykke med trykkpaavirkning i vertikal retning.
DE69128325T2 (de) Hochdruck-Injektordüse
FI97902B (fi) Päistä avoin puristuskangas
DE69102330D1 (de) Teilapparat.
GB9001822D0 (en) Vectorable variable area nozzle
DK0546003T3 (da) Trykomskifter
FI911566A0 (fi) Suutin
DK90492D0 (da) Procaterolholdigt praeparat til paafoering paa huden
FI91038C (fi) Suutinpää
FI933671A (fi) Rainanmuodostuskudos
IT8819287A0 (it) Cabina per doccia di larghezza regolabile.
BR9100451A (pt) Valvula de seguranca
IT219633Z2 (it) Bocchetta per doccia con mezzi per la regolazione del getto
GB2249158B (en) Flow restrictor
DK72490A (da) Hoejtryksrenser
BR9107022A (pt) Conversor de pressao
FI912331A (fi) Suutin
FI923138A (fi) Tryckmedium-stoedanordning.
ES1007248Y (es) Tobera antigoteo.
FI955890A0 (fi) Suutinjärjestely
FI910280A (fi) Venttiililaite
NO923213L (no) Dysesystem
KR910019294U (ko) 선미노즐
BR7001051U (pt) Controlador de vazao