BR112013006792A2 - conjunto para um motor de turboventilador, método e meio legível por computador não transitório - Google Patents

conjunto para um motor de turboventilador, método e meio legível por computador não transitório

Info

Publication number
BR112013006792A2
BR112013006792A2 BR112013006792A BR112013006792A BR112013006792A2 BR 112013006792 A2 BR112013006792 A2 BR 112013006792A2 BR 112013006792 A BR112013006792 A BR 112013006792A BR 112013006792 A BR112013006792 A BR 112013006792A BR 112013006792 A2 BR112013006792 A2 BR 112013006792A2
Authority
BR
Brazil
Prior art keywords
readable
assembly
transient computer
turbocharger engine
turbocharger
Prior art date
Application number
BR112013006792A
Other languages
English (en)
Inventor
Alan Roy Stuart
Kenneth Stephan Scheffel
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112013006792A2 publication Critical patent/BR112013006792A2/pt

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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F02K1/76—Control or regulation of thrust reversers
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BR112013006792A 2010-09-30 2011-09-29 conjunto para um motor de turboventilador, método e meio legível por computador não transitório BR112013006792A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US38834610P 2010-09-30 2010-09-30
US13/247,466 US20120079804A1 (en) 2010-09-30 2011-09-28 Cowl assembly
PCT/US2011/053993 WO2012044822A2 (en) 2010-09-30 2011-09-29 Cowl assembly

Publications (1)

Publication Number Publication Date
BR112013006792A2 true BR112013006792A2 (pt) 2016-07-12

Family

ID=44802388

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013006792A BR112013006792A2 (pt) 2010-09-30 2011-09-29 conjunto para um motor de turboventilador, método e meio legível por computador não transitório

Country Status (7)

Country Link
US (1) US20120079804A1 (pt)
EP (1) EP2622199A2 (pt)
JP (1) JP2013540940A (pt)
CN (1) CN103370522A (pt)
BR (1) BR112013006792A2 (pt)
CA (1) CA2812301A1 (pt)
WO (1) WO2012044822A2 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2957979B1 (fr) * 2010-03-25 2012-03-30 Aircelle Sa Dispositif d'inversion de poussee
US9347397B2 (en) * 2012-08-02 2016-05-24 United Technologies Corporation Reflex annular vent nozzle
WO2014051667A1 (en) * 2012-09-28 2014-04-03 United Technologies Corporation Divot for blocker doors of thrust reverser system
US10041443B2 (en) * 2015-06-09 2018-08-07 The Boeing Company Thrust reverser apparatus and method
US10378479B2 (en) 2015-10-19 2019-08-13 General Electric Company Variable effective area fan nozzle
US10605198B2 (en) * 2016-04-15 2020-03-31 Rohr, Inc. Nacelle thrust reverser

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1418905A (en) * 1972-05-09 1975-12-24 Rolls Royce Gas turbine engines
US5778659A (en) * 1994-10-20 1998-07-14 United Technologies Corporation Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems
JPH09195853A (ja) * 1995-12-14 1997-07-29 United Technol Corp <Utc> 可変面積ファンエキゾーストノズル
GB0025666D0 (en) * 2000-10-19 2000-12-06 Short Brothers Plc Aircraft propulsive power unit
FR2902839B1 (fr) * 2006-06-21 2011-09-30 Aircelle Sa Inverseur de poussee formant une tuyere adaptative
FR2904372B1 (fr) * 2006-07-26 2008-10-31 Snecma Sa Tuyere d'ejection des gaz pour turbomachine a double flux ayant une section d'ejection ou de col variable par deplacement du capot secondaire
US7673442B2 (en) * 2006-11-14 2010-03-09 General Electric Company Turbofan engine cowl assembly
US8074440B2 (en) * 2007-08-23 2011-12-13 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US20090226303A1 (en) * 2008-03-05 2009-09-10 Grabowski Zbigniew M Variable area fan nozzle fan flutter management system

Also Published As

Publication number Publication date
CA2812301A1 (en) 2012-04-05
WO2012044822A2 (en) 2012-04-05
US20120079804A1 (en) 2012-04-05
JP2013540940A (ja) 2013-11-07
WO2012044822A3 (en) 2013-07-18
EP2622199A2 (en) 2013-08-07
CN103370522A (zh) 2013-10-23

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]