SE515379C2 - Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning - Google Patents
Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordningInfo
- Publication number
- SE515379C2 SE515379C2 SE9904734A SE9904734A SE515379C2 SE 515379 C2 SE515379 C2 SE 515379C2 SE 9904734 A SE9904734 A SE 9904734A SE 9904734 A SE9904734 A SE 9904734A SE 515379 C2 SE515379 C2 SE 515379C2
- Authority
- SE
- Sweden
- Prior art keywords
- outlet
- aircraft
- flow
- portions
- outlet device
- 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
-
- 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
- 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
- F02K1/1207—Varying 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Massaging Devices (AREA)
- Fuel-Injection Apparatus (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (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)
Priority Applications (8)
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 |
ES00989152T ES2240227T3 (es) | 1999-12-22 | 2000-12-22 | Dispositivo de salida para motor a reaccion. |
EP00989152A EP1240420B1 (de) | 1999-12-22 | 2000-12-22 | Eine auslasseinrichtung für einen strahlmotor |
US10/149,368 US6681561B2 (en) | 1999-12-22 | 2000-12-22 | Outlet device for a jet engine |
PCT/SE2000/002661 WO2001046580A1 (en) | 1999-12-22 | 2000-12-22 | An outlet device for a jet engine |
DE60020161T DE60020161T2 (de) | 1999-12-22 | 2000-12-22 | Eine auslasseinrichtung für einen strahlmotor |
AU25695/01A AU2569501A (en) | 1999-12-22 | 2000-12-22 | An outlet device for a jet engine |
AT00989152T ATE295475T1 (de) | 1999-12-22 | 2000-12-22 | Eine auslasseinrichtung für einen strahlmotor |
Applications Claiming Priority (1)
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 |
Publications (3)
Publication Number | Publication Date |
---|---|
SE9904734D0 SE9904734D0 (sv) | 1999-12-22 |
SE9904734L SE9904734L (sv) | 2001-06-23 |
SE515379C2 true SE515379C2 (sv) | 2001-07-23 |
Family
ID=20418262
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE9904734A SE515379C2 (sv) | 1999-12-22 | 1999-12-22 | Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning |
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)
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 |
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 |
FR2900387B1 (fr) * | 2006-04-28 | 2009-01-16 | Snecma Sa | Ensemble d'echappement des gaz de propulsion dans un aeronef avec deux elements coudes |
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)
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 |
-
1999
- 1999-12-22 SE SE9904734A patent/SE515379C2/sv not_active IP Right Cessation
-
2000
- 2000-12-22 WO PCT/SE2000/002661 patent/WO2001046580A1/en active IP Right Grant
- 2000-12-22 EP EP00989152A patent/EP1240420B1/de not_active Expired - Lifetime
- 2000-12-22 AU AU25695/01A patent/AU2569501A/en not_active Abandoned
- 2000-12-22 US US10/149,368 patent/US6681561B2/en not_active Expired - Fee Related
- 2000-12-22 DE DE60020161T patent/DE60020161T2/de not_active Expired - Lifetime
- 2000-12-22 ES ES00989152T patent/ES2240227T3/es not_active Expired - Lifetime
- 2000-12-22 AT AT00989152T patent/ATE295475T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE60020161T2 (de) | 2006-01-26 |
SE9904734D0 (sv) | 1999-12-22 |
US20020189232A1 (en) | 2002-12-19 |
EP1240420B1 (de) | 2005-05-11 |
EP1240420A1 (de) | 2002-09-18 |
ATE295475T1 (de) | 2005-05-15 |
AU2569501A (en) | 2001-07-03 |
WO2001046580A1 (en) | 2001-06-28 |
SE9904734L (sv) | 2001-06-23 |
US6681561B2 (en) | 2004-01-27 |
ES2240227T3 (es) | 2005-10-16 |
DE60020161D1 (de) | 2005-06-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |