ATE295475T1 - Eine auslasseinrichtung für einen strahlmotor - Google Patents

Eine auslasseinrichtung für einen strahlmotor

Info

Publication number
ATE295475T1
ATE295475T1 AT00989152T AT00989152T ATE295475T1 AT E295475 T1 ATE295475 T1 AT E295475T1 AT 00989152 T AT00989152 T AT 00989152T AT 00989152 T AT00989152 T AT 00989152T AT E295475 T1 ATE295475 T1 AT E295475T1
Authority
AT
Austria
Prior art keywords
outlet
jet engine
flow
jet
plane
Prior art date
Application number
AT00989152T
Other languages
English (en)
Inventor
Hans Berglund
Carleric Weiland
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Application granted granted Critical
Publication of ATE295475T1 publication Critical patent/ATE295475T1/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002Plants 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
    • F02K1/008Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Exhaust Silencers (AREA)
  • Valve Device For Special Equipments (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Massaging Devices (AREA)
AT00989152T 1999-12-22 2000-12-22 Eine auslasseinrichtung für einen strahlmotor ATE295475T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9904734A SE515379C2 (sv) 1999-12-22 1999-12-22 Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning
PCT/SE2000/002661 WO2001046580A1 (en) 1999-12-22 2000-12-22 An outlet device for a jet engine

Publications (1)

Publication Number Publication Date
ATE295475T1 true ATE295475T1 (de) 2005-05-15

Family

ID=20418262

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00989152T ATE295475T1 (de) 1999-12-22 2000-12-22 Eine auslasseinrichtung für einen strahlmotor

Country Status (8)

Country Link
US (1) US6681561B2 (de)
EP (1) EP1240420B1 (de)
AT (1) ATE295475T1 (de)
AU (1) AU2569501A (de)
DE (1) DE60020161T2 (de)
ES (1) ES2240227T3 (de)
SE (1) SE515379C2 (de)
WO (1) WO2001046580A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE527787C2 (sv) * 2004-11-05 2006-06-07 Volvo Aero Corp Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning
FR2887929B1 (fr) * 2005-06-30 2010-12-03 Soc Nat Detude Et De Construction De Moteurs Daviation Snecma Tuyere a orientation de poussee
US7568348B2 (en) * 2005-11-28 2009-08-04 Aerojet-General Corporation Nozzle assembly for rocket and ramjet applications
FR2900387B1 (fr) * 2006-04-28 2009-01-16 Snecma Sa Ensemble d'echappement des gaz de propulsion dans un aeronef avec deux elements coudes
FR2900389B1 (fr) * 2006-04-28 2009-01-16 Snecma Sa Ensemble d'echappement des gaz de propulsion dans un aeronef a coudage vrille
FR2900388B1 (fr) * 2006-04-28 2009-01-16 Snecma Sa Ensemble d'echappement des gaz de propulsion dans un aeronef formant un coude
CN105114206B (zh) * 2015-09-18 2017-06-16 中国航空工业集团公司沈阳发动机设计研究所 一种可降低红外和雷达信号特征的喷管

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB677973A (en) * 1951-02-22 1952-08-27 Blackburn & Gen Aircraft Ltd Improvements in and relating to variable area nozzles for turbo-jet engine installations
GB950288A (en) * 1959-08-18 1964-02-26 Bristol Siddeley Engines Ltd Improvements in nozzles for aircraft propulsion
GB1058933A (en) * 1963-10-02 1967-02-15 Bristol Siddeley Engines Ltd Improvements in jet propulsion nozzles
GB1253071A (de) * 1968-09-14 1971-11-10
US4627586A (en) * 1984-10-29 1986-12-09 The United States Of America As Represented By The Secretary Of The Navy Thrust vectoring apparatus for maneuvering missile in flight
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
US5050803A (en) * 1989-10-12 1991-09-24 General Electric Company Actuation system for positioning a vectoring exhaust nozzle
GB9915949D0 (en) * 1999-07-07 2000-06-21 British Aerospace Engine nozzle arrangement for an aircraft

Also Published As

Publication number Publication date
SE9904734L (sv) 2001-06-23
ES2240227T3 (es) 2005-10-16
DE60020161T2 (de) 2006-01-26
EP1240420A1 (de) 2002-09-18
WO2001046580A1 (en) 2001-06-28
US6681561B2 (en) 2004-01-27
SE515379C2 (sv) 2001-07-23
EP1240420B1 (de) 2005-05-11
SE9904734D0 (sv) 1999-12-22
AU2569501A (en) 2001-07-03
US20020189232A1 (en) 2002-12-19
DE60020161D1 (de) 2005-06-16

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties