SE0402720L - Framdrivningssystem för en farkost - Google Patents

Framdrivningssystem för en farkost

Info

Publication number
SE0402720L
SE0402720L SE0402720A SE0402720A SE0402720L SE 0402720 L SE0402720 L SE 0402720L SE 0402720 A SE0402720 A SE 0402720A SE 0402720 A SE0402720 A SE 0402720A SE 0402720 L SE0402720 L SE 0402720L
Authority
SE
Sweden
Prior art keywords
craft
propulsion system
propulsion
Prior art date
Application number
SE0402720A
Other languages
English (en)
Other versions
SE0402720D0 (sv
SE527828C2 (sv
Inventor
Bernhard Gustafsson
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 SE0402720A priority Critical patent/SE527828C2/sv
Publication of SE0402720D0 publication Critical patent/SE0402720D0/sv
Priority to EP05797611A priority patent/EP1809891A1/en
Priority to PCT/SE2005/001580 priority patent/WO2006049555A1/en
Priority to US11/718,430 priority patent/US7753311B2/en
Publication of SE0402720L publication Critical patent/SE0402720L/sv
Publication of SE527828C2 publication Critical patent/SE527828C2/sv

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; 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
    • 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; 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
    • F02K3/12—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; 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
    • 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)
  • Jet Pumps And Other Pumps (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
SE0402720A 2004-11-05 2004-11-05 Framdrivningssystem för en farkost SE527828C2 (sv)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SE0402720A SE527828C2 (sv) 2004-11-05 2004-11-05 Framdrivningssystem för en farkost
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
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

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 SE0402720D0 (sv) 2004-11-05
SE0402720L true 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)

* Cited by examiner, † Cited by third party
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
US8322655B1 (en) 2009-03-25 2012-12-04 The Boeing Company Twin-boom empennage
US8317129B1 (en) * 2009-03-25 2012-11-27 The Boeing Company Universal convergent nozzle and distinct nozzle aperture
US8167249B1 (en) 2009-03-25 2012-05-01 The Boeing Company Controllable upper surface blown nozzle
US8403256B1 (en) 2009-03-25 2013-03-26 The Boeing Company Swept-wing powered-lift aircraft
US8353478B1 (en) 2009-03-25 2013-01-15 The Boeing Company Blended wing aircraft
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
US20070295860A1 (en) 2007-12-27
EP1809891A1 (en) 2007-07-25
SE0402720D0 (sv) 2004-11-05
SE527828C2 (sv) 2006-06-13
WO2006049555A1 (en) 2006-05-11
US7753311B2 (en) 2010-07-13

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