SE0402719L - Utloppsanordning för styrning av ett gasflöde från en jetmotor - Google Patents

Utloppsanordning för styrning av ett gasflöde från en jetmotor

Info

Publication number
SE0402719L
SE0402719L SE0402719A SE0402719A SE0402719L SE 0402719 L SE0402719 L SE 0402719L SE 0402719 A SE0402719 A SE 0402719A SE 0402719 A SE0402719 A SE 0402719A SE 0402719 L SE0402719 L SE 0402719L
Authority
SE
Sweden
Prior art keywords
controlling
gas flow
outlet device
jet engine
jet
Prior art date
Application number
SE0402719A
Other languages
English (en)
Other versions
SE527789C2 (sv
SE0402719D0 (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 SE0402719A priority Critical patent/SE527789C2/sv
Publication of SE0402719D0 publication Critical patent/SE0402719D0/sv
Priority to US11/718,433 priority patent/US20080104940A1/en
Priority to EP05796816A priority patent/EP1809887A1/en
Priority to PCT/SE2005/001589 priority patent/WO2006049556A1/en
Publication of SE0402719L publication Critical patent/SE0402719L/sv
Publication of SE527789C2 publication Critical patent/SE527789C2/sv

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/08Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/024Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising cooling means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Nozzles (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
SE0402719A 2004-11-05 2004-11-05 Utloppsanordning för styrning av ett gasflöde från en jetmotor SE527789C2 (sv)

Priority Applications (4)

Application Number Priority Date Filing Date Title
SE0402719A SE527789C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning för styrning av ett gasflöde från en jetmotor
US11/718,433 US20080104940A1 (en) 2004-11-05 2005-10-21 Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the Device
EP05796816A EP1809887A1 (en) 2004-11-05 2005-10-21 A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device
PCT/SE2005/001589 WO2006049556A1 (en) 2004-11-05 2005-10-21 A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0402719A SE527789C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning för styrning av ett gasflöde från en jetmotor

Publications (3)

Publication Number Publication Date
SE0402719D0 SE0402719D0 (sv) 2004-11-05
SE0402719L true SE0402719L (sv) 2006-05-06
SE527789C2 SE527789C2 (sv) 2006-06-07

Family

ID=33488189

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0402719A SE527789C2 (sv) 2004-11-05 2004-11-05 Utloppsanordning för styrning av ett gasflöde från en jetmotor

Country Status (4)

Country Link
US (1) US20080104940A1 (sv)
EP (1) EP1809887A1 (sv)
SE (1) SE527789C2 (sv)
WO (1) WO2006049556A1 (sv)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9097199B2 (en) 2012-06-21 2015-08-04 United Technologies Corporation Engine signature assessment system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB750616A (en) * 1952-05-21 1956-06-20 Snecma Improvements in jet propulsion nozzles
CH357923A (fr) * 1952-06-05 1961-10-31 Snecma Propulseur à réaction pourvu d'un dispositif de réglage de la section du jet propulsif
FR1072523A (fr) * 1952-12-12 1954-09-14 Snecma Dispositif de contrôle d'un écoulement de fluide par un éeoulement auxiliaire
US4004416A (en) * 1970-03-16 1977-01-25 United Technologies Corporation Infra-red suppressor for use with turbo-shaft engine
US4295332A (en) * 1978-11-13 1981-10-20 General Electric Company Infrared suppressor system
US4537026A (en) * 1982-04-07 1985-08-27 Rolls-Royce Inc. Variable area nozzles for turbomachines
US5205119A (en) * 1991-06-14 1993-04-27 Aerojet-General Corporation Ejector ramjet

Also Published As

Publication number Publication date
SE527789C2 (sv) 2006-06-07
WO2006049556A1 (en) 2006-05-11
EP1809887A1 (en) 2007-07-25
US20080104940A1 (en) 2008-05-08
SE0402719D0 (sv) 2004-11-05

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