SE0402718L - Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning - Google Patents

Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning

Info

Publication number
SE0402718L
SE0402718L SE0402718A SE0402718A SE0402718L SE 0402718 L SE0402718 L SE 0402718L SE 0402718 A SE0402718 A SE 0402718A SE 0402718 A SE0402718 A SE 0402718A SE 0402718 L SE0402718 L SE 0402718L
Authority
SE
Sweden
Prior art keywords
outlet device
jet engine
jet
engine
outlet
Prior art date
Application number
SE0402718A
Other languages
English (en)
Other versions
SE527787C2 (sv
SE0402718D0 (sv
Inventor
Melker Haerefors
Original Assignee
Volvo Aero 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 Volvo Aero Corp filed Critical Volvo Aero Corp
Priority to SE0402718A priority Critical patent/SE527787C2/sv
Publication of SE0402718D0 publication Critical patent/SE0402718D0/sv
Priority to PCT/SE2005/001574 priority patent/WO2006049553A1/en
Priority to US11/718,431 priority patent/US7900460B2/en
Priority to EP05797617A priority patent/EP1809892A4/en
Publication of SE0402718L publication Critical patent/SE0402718L/sv
Publication of SE527787C2 publication Critical patent/SE527787C2/sv

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
    • F02K1/006Plants 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 within one plane only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C15/00Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • 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
    • F02K1/40Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
    • 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
    • F02K1/44Nozzles having means, e.g. a shield, reducing sound radiation in a specified 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
    • F02K1/78Other construction of jet pipes
    • F02K1/82Jet pipe walls, e.g. liners
    • F02K1/822Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F02K1/825Infrared radiation suppressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/025Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
SE0402718A 2004-11-05 2004-11-05 Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning SE527787C2 (sv)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SE0402718A SE527787C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning
PCT/SE2005/001574 WO2006049553A1 (en) 2004-11-05 2005-10-20 An outlet device for a jet engine and a jet engine comprising such an outlet device
US11/718,431 US7900460B2 (en) 2004-11-05 2005-10-20 Outlet device for a jet engine and a jet engine comprising such an outlet device
EP05797617A EP1809892A4 (en) 2004-11-05 2005-10-20 DRAIN DEVICE FOR A REACTION ENGINE AND REACTION MOTOR EQUIPPED WITH SAID DRAIN DEVICE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0402718A SE527787C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning

Publications (3)

Publication Number Publication Date
SE0402718D0 SE0402718D0 (sv) 2004-11-05
SE0402718L true SE0402718L (sv) 2006-05-06
SE527787C2 SE527787C2 (sv) 2006-06-07

Family

ID=33488188

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0402718A SE527787C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning

Country Status (4)

Country Link
US (1) US7900460B2 (sv)
EP (1) EP1809892A4 (sv)
SE (1) SE527787C2 (sv)
WO (1) WO2006049553A1 (sv)

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US7730727B2 (en) * 2005-09-06 2010-06-08 American Air Liquide, Inc. Flexible flow control device for cogeneration ducting applications
WO2007037725A1 (en) * 2005-09-27 2007-04-05 Volvo Aero Corporation An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine
US8020367B2 (en) * 2007-03-16 2011-09-20 General Electric Company Nozzle with yaw vectoring vane
US20100146980A1 (en) * 2007-05-22 2010-06-17 Volvo Aero Corporation masking arrangement for a gas turbine engine
FR2919268B1 (fr) 2007-07-26 2009-10-02 Airbus France Sa Avion a decollage court
DE102010023938A1 (de) * 2010-06-16 2011-12-22 Eads Deutschland Gmbh Angetriebenes Fluggerät, insbesondere als Nurflügler und/oder mit geringer Radarsignatur ausgebildetes Fluggerät
US9038404B2 (en) 2011-04-19 2015-05-26 Liebert Corporation High efficiency cooling system
US10562641B2 (en) * 2012-10-10 2020-02-18 Sikorsky Aircraft Corporation AFT exhaust system for rotary wing aircraft
CN104554739B (zh) * 2014-12-16 2016-08-24 空气动力学国家重点实验室 一种可以增强和调整无尾布局飞机航向稳定性的进气道唇口
US11434822B2 (en) 2015-06-19 2022-09-06 Raytheon Technologies Corporation Inverse modulation of secondary bleed
US9964069B2 (en) 2015-06-29 2018-05-08 United Technologies Corporation Exhaust nozzle control for a gas turbine engine
US10464668B2 (en) * 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
EP3472518B1 (en) * 2016-09-27 2020-11-18 Siemens Aktiengesellschaft Fuel oil axial stage combustion for improved turbine combustor performance
US20180149114A1 (en) * 2016-11-30 2018-05-31 Sikorsky Aircraft Corporation Low infrared signature exhaust through active film cooling active mixing and acitve vane rotation
US11352978B2 (en) 2020-06-24 2022-06-07 Raytheon Company Deflectable distributed aerospike rocket nozzle
CN112937916B (zh) * 2021-01-27 2022-12-06 西北工业大学深圳研究院 一种降低姿态发动机尾流影响的空间机器人及其工作方法
US11485451B2 (en) * 2021-02-03 2022-11-01 Jetts, Llc Jet sled
CN114151226B (zh) * 2021-10-20 2023-05-05 中国航发四川燃气涡轮研究院 一种置于直二元收敛喷管流道内的多隔板综合隐身结构
US11434018B1 (en) * 2021-11-27 2022-09-06 Airbus Defence and Space GmbH Switchable air inlet device for engine air

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DE1993361U (de) * 1968-04-25 1968-09-05 Ver Flugtechnische Werke G M B Ablenkvorrichtung fuer insbesondere heisse abgasstrahlen an flugzeugtriebwerken.
US5699966A (en) * 1980-03-31 1997-12-23 General Electric Company Exhaust nozzle of a gas turbine engine
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FR2608680B1 (fr) * 1986-12-17 1989-03-17 Snecma Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion
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DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
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US7568348B2 (en) * 2005-11-28 2009-08-04 Aerojet-General Corporation Nozzle assembly for rocket and ramjet applications
US20100146980A1 (en) * 2007-05-22 2010-06-17 Volvo Aero Corporation masking arrangement for a gas turbine engine

Also Published As

Publication number Publication date
SE527787C2 (sv) 2006-06-07
US7900460B2 (en) 2011-03-08
EP1809892A1 (en) 2007-07-25
US20080016873A1 (en) 2008-01-24
WO2006049553A1 (en) 2006-05-11
EP1809892A4 (en) 2012-02-01
SE0402718D0 (sv) 2004-11-05

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