SE0402720D0 - Utloppsanordning till en jetmotor och ett framdrivningssystem - Google Patents
Utloppsanordning till en jetmotor och ett framdrivningssystemInfo
- Publication number
- SE0402720D0 SE0402720D0 SE0402720A SE0402720A SE0402720D0 SE 0402720 D0 SE0402720 D0 SE 0402720D0 SE 0402720 A SE0402720 A SE 0402720A SE 0402720 A SE0402720 A SE 0402720A SE 0402720 D0 SE0402720 D0 SE 0402720D0
- Authority
- SE
- Sweden
- Prior art keywords
- jet engine
- propulsion system
- outlet device
- gas
- duct
- 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
- F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- 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
- F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
-
- 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
-
- 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; Infra-red radiation suppressors
- F02K1/825—Infra-red 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
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D2033/045—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes comprising infrared suppressors
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/25—Three-dimensional helical
-
- 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
- F05D2250/312—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
-
- 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
- F05D2250/33—Arrangement of components symmetrical
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)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Jet Pumps And Other Pumps (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0402720A SE527828C2 (sv) | 2004-11-05 | 2004-11-05 | Framdrivningssystem för en farkost |
US11/718,430 US7753311B2 (en) | 2004-11-05 | 2005-10-20 | Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
EP05797611A EP1809891A1 (en) | 2004-11-05 | 2005-10-20 | Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
PCT/SE2005/001580 WO2006049555A1 (en) | 2004-11-05 | 2005-10-20 | Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0402720A SE527828C2 (sv) | 2004-11-05 | 2004-11-05 | Framdrivningssystem för en farkost |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0402720D0 true SE0402720D0 (sv) | 2004-11-05 |
SE0402720L SE0402720L (sv) | 2006-05-06 |
SE527828C2 SE527828C2 (sv) | 2006-06-13 |
Family
ID=33488190
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0402720A SE527828C2 (sv) | 2004-11-05 | 2004-11-05 | Framdrivningssystem för en farkost |
Country Status (4)
Country | Link |
---|---|
US (1) | US7753311B2 (sv) |
EP (1) | EP1809891A1 (sv) |
SE (1) | SE527828C2 (sv) |
WO (1) | WO2006049555A1 (sv) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US8317129B1 (en) * | 2009-03-25 | 2012-11-27 | The Boeing Company | Universal convergent nozzle and distinct nozzle aperture |
US8403256B1 (en) | 2009-03-25 | 2013-03-26 | The Boeing Company | Swept-wing powered-lift aircraft |
US8167249B1 (en) | 2009-03-25 | 2012-05-01 | The Boeing Company | Controllable upper surface blown nozzle |
US8353478B1 (en) | 2009-03-25 | 2013-01-15 | The Boeing Company | Blended wing aircraft |
US8322655B1 (en) | 2009-03-25 | 2012-12-04 | The Boeing Company | Twin-boom empennage |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
DE102010023938A1 (de) | 2010-06-16 | 2011-12-22 | Eads Deutschland Gmbh | Angetriebenes Fluggerät, insbesondere als Nurflügler und/oder mit geringer Radarsignatur ausgebildetes Fluggerät |
CN102926888B (zh) * | 2012-11-16 | 2014-10-22 | 中国航空工业集团公司西安飞机设计研究所 | 一种隐身排气系统 |
US9845159B2 (en) * | 2013-03-07 | 2017-12-19 | United Technologies Corporation | Conjoined reverse core flow engine arrangement |
WO2015065587A1 (en) * | 2013-11-04 | 2015-05-07 | United Technologies Corporation | Coated cooling passage |
CN104875898A (zh) * | 2015-06-23 | 2015-09-02 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机用尾部喷管组件及具有其的飞机 |
US10267263B2 (en) | 2016-08-08 | 2019-04-23 | United Technologies Corporation | Exhaust duct for turbine forward of fan |
US11149639B2 (en) * | 2016-11-29 | 2021-10-19 | Rolls-Royce North American Technologies Inc. | Systems and methods of reducing distortions of the inlet airflow to a turbomachine |
CN115196024B (zh) * | 2022-09-16 | 2022-12-09 | 中国航空工业集团公司西安飞机设计研究所 | 一种用于飞行器的动力设备 |
CN115571351A (zh) * | 2022-11-21 | 2023-01-06 | 中国空气动力研究与发展中心空天技术研究所 | 一种兼顾高低速性能和隐身性能的飞翼布局背负式进气道 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3056258A (en) * | 1960-01-26 | 1962-10-02 | Bristol Siddeley Engines Ltd | Aircraft propulsion power units |
GB1069431A (en) * | 1963-01-02 | 1967-05-17 | Bristol Siddeley Engines Ltd | Improvements in aircraft propulsion power plants |
US3631678A (en) * | 1970-11-02 | 1972-01-04 | Us Navy | Exhaust system |
GB2254589B (en) * | 1983-12-20 | 1993-04-14 | British Aerospace | Jet propulsion powerplants |
DE3909347A1 (de) * | 1989-03-22 | 1990-09-27 | Mtu Muenchen Gmbh | Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete |
US5699662A (en) * | 1996-05-28 | 1997-12-23 | Lockheed Martin Corporation | Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft |
-
2004
- 2004-11-05 SE SE0402720A patent/SE527828C2/sv unknown
-
2005
- 2005-10-20 WO PCT/SE2005/001580 patent/WO2006049555A1/en active Application Filing
- 2005-10-20 EP EP05797611A patent/EP1809891A1/en not_active Withdrawn
- 2005-10-20 US US11/718,430 patent/US7753311B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
SE0402720L (sv) | 2006-05-06 |
SE527828C2 (sv) | 2006-06-13 |
WO2006049555A1 (en) | 2006-05-11 |
EP1809891A1 (en) | 2007-07-25 |
US20070295860A1 (en) | 2007-12-27 |
US7753311B2 (en) | 2010-07-13 |
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