ATE263917T1 - Schubdüsenanordnung für ein luftfahrzeug - Google Patents

Schubdüsenanordnung für ein luftfahrzeug

Info

Publication number
ATE263917T1
ATE263917T1 AT00942272T AT00942272T ATE263917T1 AT E263917 T1 ATE263917 T1 AT E263917T1 AT 00942272 T AT00942272 T AT 00942272T AT 00942272 T AT00942272 T AT 00942272T AT E263917 T1 ATE263917 T1 AT E263917T1
Authority
AT
Austria
Prior art keywords
aircraft
nozzle arrangement
thrust nozzle
exhaust gases
nozzle
Prior art date
Application number
AT00942272T
Other languages
English (en)
Inventor
Colin Whaites
Peter Richard House
Robert Brown
Original Assignee
Bae Systems Plc
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 Bae Systems Plc filed Critical Bae Systems Plc
Application granted granted Critical
Publication of ATE263917T1 publication Critical patent/ATE263917T1/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
    • 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
    • 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
    • F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids
    • 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
    • F02K1/38—Introducing air inside the jet
    • F02K1/383—Introducing air inside the jet with retractable elements
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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)
  • Exhaust Silencers (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
AT00942272T 1999-07-07 2000-07-05 Schubdüsenanordnung für ein luftfahrzeug ATE263917T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9915949.3A GB9915949D0 (en) 1999-07-07 1999-07-07 Engine nozzle arrangement for an aircraft
PCT/GB2000/002572 WO2001004485A1 (en) 1999-07-07 2000-07-05 Engine nozzle arrangement for an aircraft

Publications (1)

Publication Number Publication Date
ATE263917T1 true ATE263917T1 (de) 2004-04-15

Family

ID=10856845

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00942272T ATE263917T1 (de) 1999-07-07 2000-07-05 Schubdüsenanordnung für ein luftfahrzeug

Country Status (9)

Country Link
US (1) US6381950B1 (de)
EP (1) EP1192348B1 (de)
JP (1) JP3429294B2 (de)
AT (1) ATE263917T1 (de)
AU (1) AU5697300A (de)
DE (1) DE60009701T2 (de)
ES (1) ES2216906T3 (de)
GB (1) GB9915949D0 (de)
WO (1) WO2001004485A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE515379C2 (sv) * 1999-12-22 2001-07-23 Saab Ab Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning
FR2891008B1 (fr) * 2005-09-21 2010-06-25 Giat Ind Sa Dispositif de discretion infrarouge pour un conduit d'echappement d'un moteur de vehicule
US8065868B2 (en) * 2006-12-22 2011-11-29 Lockheed Martin Corporation System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft
FR2946019B1 (fr) * 2009-05-29 2013-03-29 Airbus France Systeme propulsif multifonctions pour avion
US20160122005A1 (en) * 2013-03-11 2016-05-05 United Technologies Corporation Embedded engines in hybrid blended wing body
EP2971728B1 (de) * 2013-03-14 2020-09-02 United Technologies Corporation Doppelziel-schubumkehrermodul
CN111237083B (zh) * 2018-11-28 2022-01-11 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机
CN114776466B (zh) * 2022-04-14 2024-01-30 中国航发沈阳发动机研究所 一种复合材料外调节片结构
US12559227B1 (en) * 2024-05-31 2026-02-24 Whisper Aero Inc. Uniform exhaust sheet and flow turning control

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1100385B (de) 1958-12-10 1961-02-23 Entwicklungsbau Pirna Veb Vorrichtung zur Laermbekaempfung des Abgasstrahles eines Strahltriebwerkes durch Zumischen von Frischluft und zur AEnderung der Ausstroemrichtung des Abgasstrahles mittels stellbarer Umlenkplatten
GB1141051A (en) 1966-02-18 1969-01-22 United Aircraft Corp Ejector type exhaust nozzle
US3601340A (en) 1969-05-28 1971-08-24 Rohr Corp Method and apparatus for augmenting and reversing thrust and reducing nozzle base drag and noise of an aircraft jet engine
US3647141A (en) * 1970-06-01 1972-03-07 Rohr Corp Thrust controlling apparatus
FR2189642B1 (de) * 1972-06-19 1976-08-06 Snecma
US4295332A (en) 1978-11-13 1981-10-20 General Electric Company Infrared suppressor system
GB2114229B (en) 1981-11-03 1984-11-21 Rolls Royce Gas turbine engine infra-red radiation suppressor
US4463903A (en) * 1982-05-10 1984-08-07 Nightingale Douglas J Turbomachine ejector nozzle
US4502637A (en) 1982-06-07 1985-03-05 Rolls-Royce Inc. Turbomachine ejector nozzle with thrust reverser
US4835961A (en) 1986-04-30 1989-06-06 United Technologies Corporation Fluid dynamic pump
DE3619652C1 (en) * 1986-06-11 1990-10-11 Messerschmitt Boelkow Blohm Jet aircraft manoeuvring aid - has three movable flaps each suspended from four point linkage
US5016818A (en) * 1989-08-21 1991-05-21 General Electric Company Integral transition and convergent section exhaust nozzle
US5216879A (en) 1991-08-30 1993-06-08 United Technologies Corporation Propulsion system assembly
US6164059A (en) * 1995-11-17 2000-12-26 United Technologies Corporation Multi-expansion ejector nozzle with diverging walls
US6016651A (en) 1997-06-24 2000-01-25 Sikorsky Aircraft Corporation Multi-stage mixer/ejector for suppressing infrared radiation
FR2781254B1 (fr) * 1998-07-17 2000-08-18 Snecma Tuyere d'ejection de turboreacteur a masquage du jet de gaz
FR2781253B1 (fr) * 1998-07-17 2000-08-18 Snecma Tuyere bidimensionnelle, convergente a volets froids, translatables

Also Published As

Publication number Publication date
EP1192348A1 (de) 2002-04-03
AU5697300A (en) 2001-01-30
JP3429294B2 (ja) 2003-07-22
DE60009701T2 (de) 2004-08-12
US6381950B1 (en) 2002-05-07
EP1192348B1 (de) 2004-04-07
WO2001004485A1 (en) 2001-01-18
ES2216906T3 (es) 2004-11-01
DE60009701D1 (de) 2004-05-13
JP2003504549A (ja) 2003-02-04
GB9915949D0 (en) 2000-06-21

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Legal Events

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