SE0402718L - Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning - Google Patents
Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordningInfo
- 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
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
- F02K1/006—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 within one plane only
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- 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
- F02K1/06—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
- F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
-
- 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
- F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified 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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
- F02K1/825—Infrared radiation suppressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants 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
- F02K3/025—Plants 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)
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) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3087303A (en) * | 1960-03-29 | 1963-04-30 | Northrop Corp | Jet propelled aircraft with jet deflecting means |
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 |
GB2155552B (en) * | 1981-02-24 | 1986-02-26 | Rolls Royce | Adjustable jet propulsion nozzle |
FR2608680B1 (fr) * | 1986-12-17 | 1989-03-17 | Snecma | Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion |
US4763840A (en) * | 1987-04-09 | 1988-08-16 | United Technologies Corporation | Thrust vectoring exhaust nozzle arrangement |
US4836451A (en) * | 1987-09-10 | 1989-06-06 | United Technologies Corporation | Yaw and pitch convergent-divergent thrust vectoring nozzle |
US4922711A (en) * | 1988-06-10 | 1990-05-08 | The Boeing Company | Thrust reversing system for high bypass fan engines |
US4948072A (en) * | 1989-02-08 | 1990-08-14 | Boeing Of Canada Ltd. | Segmented vectoring cruise nozzles |
DE3909347A1 (de) * | 1989-03-22 | 1990-09-27 | Mtu Muenchen Gmbh | Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete |
US4978071A (en) * | 1989-04-11 | 1990-12-18 | General Electric Company | Nozzle with thrust vectoring in the yaw direction |
EP0442899B1 (en) * | 1989-08-21 | 1994-04-27 | Moog Inc. | Vane-type thrust vectoring nozzle |
US5050803A (en) * | 1989-10-12 | 1991-09-24 | General Electric Company | Actuation system for positioning a vectoring exhaust nozzle |
US5092524A (en) * | 1990-02-12 | 1992-03-03 | Mcdonnell Douglas Corporation | Nozzle throat disc for thrust vectoring |
US5388765A (en) * | 1990-04-18 | 1995-02-14 | United Technologies Corporation | Gas turbine nozzle construction |
US5690280A (en) * | 1990-08-24 | 1997-11-25 | General Electric Company | Multifunction exhaust system for gas turbine engines |
US5261604A (en) * | 1992-05-11 | 1993-11-16 | General Electric Company | Yaw vectoring blade |
US5294055A (en) * | 1992-09-08 | 1994-03-15 | Mcdonnell Douglas Corporation | Rotatable arms for thrust vectoring and changing the area of a nozzle throat |
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. |
DE4426195C2 (de) | 1994-07-23 | 1998-02-05 | Daimler Benz Aerospace Ag | Schubdüse in Rechteckbauweise für Strahltriebwerke |
US6357672B1 (en) * | 1995-07-06 | 2002-03-19 | United Technologies Corporation | Sealing means for a multi-axis nozzle |
US5717172A (en) * | 1996-10-18 | 1998-02-10 | Northrop Grumman Corporation | Sound suppressor exhaust structure |
US6360528B1 (en) * | 1997-10-31 | 2002-03-26 | General Electric Company | Chevron exhaust nozzle for a gas turbine engine |
US6487848B2 (en) * | 1998-11-06 | 2002-12-03 | United Technologies Corporation | Gas turbine engine jet noise suppressor |
FR2792367B1 (fr) * | 1999-04-15 | 2002-04-26 | Snecma | Tuyere d'ejection axisymetrique, convergente divergente a orientation par un anneau guide |
US6382559B1 (en) * | 1999-08-13 | 2002-05-07 | Rolls-Royce Corporation | Thrust vectoring mechanism |
SE515379C2 (sv) * | 1999-12-22 | 2001-07-23 | Saab Ab | Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning |
US7578132B2 (en) * | 2001-03-03 | 2009-08-25 | Rolls-Royce Plc | Gas turbine engine exhaust nozzle |
FR2888211B1 (fr) * | 2005-07-06 | 2008-11-14 | Snecma Propulsion Solide Sa | Dispositif et procede de pilotage en lacets pour tuyere a section de sortie rectangulaire |
US7607306B2 (en) * | 2005-08-03 | 2009-10-27 | General Electric Company | Infrared suppressor apparatus and method |
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 |
-
2004
- 2004-11-05 SE SE0402718A patent/SE527787C2/sv unknown
-
2005
- 2005-10-20 EP EP05797617A patent/EP1809892A4/en not_active Withdrawn
- 2005-10-20 US US11/718,431 patent/US7900460B2/en not_active Expired - Fee Related
- 2005-10-20 WO PCT/SE2005/001574 patent/WO2006049553A1/en active Application Filing
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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