ATE523682T1 - Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk - Google Patents

Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk

Info

Publication number
ATE523682T1
ATE523682T1 AT05804138T AT05804138T ATE523682T1 AT E523682 T1 ATE523682 T1 AT E523682T1 AT 05804138 T AT05804138 T AT 05804138T AT 05804138 T AT05804138 T AT 05804138T AT E523682 T1 ATE523682 T1 AT E523682T1
Authority
AT
Austria
Prior art keywords
aircraft
jet engine
arrangement
driving
exhaust nozzle
Prior art date
Application number
AT05804138T
Other languages
English (en)
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
Application granted granted Critical
Publication of ATE523682T1 publication Critical patent/ATE523682T1/de

Links

Classifications

    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement 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
    • F02K1/40—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
    • F02K1/78—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
    • 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
    • F05D2250/10—Two-dimensional
    • F05D2250/14—Two-dimensional elliptical
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
AT05804138T 2005-09-27 2005-09-27 Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk ATE523682T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE2005/001430 WO2007037725A1 (en) 2005-09-27 2005-09-27 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine

Publications (1)

Publication Number Publication Date
ATE523682T1 true ATE523682T1 (de) 2011-09-15

Family

ID=37900041

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05804138T ATE523682T1 (de) 2005-09-27 2005-09-27 Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk

Country Status (4)

Country Link
US (1) US8061145B2 (de)
EP (1) EP1931870B1 (de)
AT (1) ATE523682T1 (de)
WO (1) WO2007037725A1 (de)

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US8353478B1 (en) 2009-03-25 2013-01-15 The Boeing Company Blended wing aircraft
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
US8317129B1 (en) * 2009-03-25 2012-11-27 The Boeing Company Universal convergent nozzle and distinct nozzle aperture
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
RU2478529C2 (ru) * 2009-07-24 2013-04-10 Открытое акционерное общество "ОКБ Сухого" Способ снижения демаскирующих признаков (заметности) реактивного двигателя (варианты)
US9291123B2 (en) * 2012-07-26 2016-03-22 United Technologies Corporation Gas turbine engine exhaust duct
EP2719621A3 (de) * 2012-10-10 2017-10-25 Sikorsky Aircraft Corporation Nachabgassystem für Drehflügelflugzeug
FR3014845B1 (fr) 2013-12-16 2017-09-01 Snecma Systeme de prelevement de fluide
US10040560B2 (en) * 2015-09-30 2018-08-07 The Boeing Company Trailing edge core compartment vent for an aircraft engine
US20170121032A1 (en) * 2015-10-30 2017-05-04 Sikorsky Aircraft Corporation Exhaust infrared signature reduction arrangement and method of reducing temperature of at least a portion of an exhaust duct
US10730636B2 (en) * 2016-07-18 2020-08-04 Rolls-Royce North American Technologies Inc. Integrated aircraft cooling system
US11333103B2 (en) * 2019-05-17 2022-05-17 The Boeing Company Method to re-loft a redesigned jet engine primary exhaust nozzle for an existing airplane to provide clearance to aircraft heat shield structure to prevent contact, fracture, and liberation of portions of the nozzle which might cause hazard to continued safe flight
DE102019210007A1 (de) * 2019-07-08 2021-01-14 Volkswagen Aktiengesellschaft Vertikal start- und landefähiges Flugobjekt und Mantelkörper
CN112412655A (zh) * 2020-11-05 2021-02-26 中国航发四川燃气涡轮研究院 一种多流道小偏心短距s弯喷管结构
CN114673605B (zh) * 2022-04-14 2023-10-10 中国航发沈阳发动机研究所 一种轻质高隐身能力单边膨胀喷管

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Also Published As

Publication number Publication date
EP1931870B1 (de) 2011-09-07
WO2007037725A1 (en) 2007-04-05
EP1931870A1 (de) 2008-06-18
US20080236138A1 (en) 2008-10-02
US8061145B2 (en) 2011-11-22

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