FR2908468B1 - Capot de turboreacteur double flux. - Google Patents

Capot de turboreacteur double flux.

Info

Publication number: FR2908468B1
Authority: FR; France
Prior art keywords: hood; double flow; flow turboreactor; turboreactor; double
Prior art date: 2006-11-14
Legal status (The legal status 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 status listed.): Active

Application number

FR0758999A

Other languages

English (en)

Other versions

FR2908468A1 (fr

Inventor

Jorge Francisco Seda

Ory Thomas Moniz

Robert Joseph Orlando

Alan Roy Stuart

Kenneth S Scheffel

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

General Electric Co

Original Assignee

General Electric Co

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.)

2006-11-14

Filing date

2007-11-13

Publication date

2012-04-20

2007-11-13 Application filed by General Electric Co filed Critical General Electric Co

2008-05-16 Publication of FR2908468A1 publication Critical patent/FR2908468A1/fr

2012-04-20 Application granted granted Critical

2012-04-20 Publication of FR2908468B1 publication Critical patent/FR2908468B1/fr

Status Active legal-status Critical Current

2027-11-13 Anticipated expiration legal-status Critical

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
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing

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)

FR0758999A 2006-11-14 2007-11-13 Capot de turboreacteur double flux. Active FR2908468B1 (fr)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US11/559,761 US7673442B2 (en)	2006-11-14	2006-11-14	Turbofan engine cowl assembly

Publications (2)

Publication Number	Publication Date
FR2908468A1 FR2908468A1 (fr)	2008-05-16
FR2908468B1 true FR2908468B1 (fr)	2012-04-20

Family

ID=38858566

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR0758999A Active FR2908468B1 (fr)	2006-11-14	2007-11-13	Capot de turboreacteur double flux.

Country Status (5)

Country	Link
US (1)	US7673442B2 (fr)
JP (1)	JP5572285B2 (fr)
CA (1)	CA2609282C (fr)
FR (1)	FR2908468B1 (fr)
GB (1)	GB2443934B (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB0611963D0 (en) *	2006-06-16	2006-07-26	Rolls Royce Plc	A flow reverser
US8534074B2 (en)	2008-05-13	2013-09-17	Rolls-Royce Corporation	Dual clutch arrangement and method
US20100005810A1 (en) *	2008-07-11	2010-01-14	Rob Jarrell	Power transmission among shafts in a turbine engine
US8480527B2 (en)	2008-08-27	2013-07-09	Rolls-Royce Corporation	Gearing arrangement
GB2464960B (en) *	2008-10-31	2013-03-27	Gen Electric	Baffle seal for gas turbine engine thrust reverser
GB2496999B (en) *	2008-10-31	2013-10-02	Gen Electric	Transcowl assembly for gas turbine engine thrust reverser.
US8220738B2 (en) *	2008-11-26	2012-07-17	Mra Systems, Inc.	Nacelle and method of assembling the same
US9188025B2 (en) *	2008-11-26	2015-11-17	Mra Systems, Inc.	Apparatus for facilitating access to a nacelle interior
US9188026B2 (en) *	2008-11-26	2015-11-17	Mra Systems, Inc.	Apparatus for facilitating access to a nacelle interior and method of assembling the same
US8075438B2 (en)	2008-12-11	2011-12-13	Rolls-Royce Corporation	Apparatus and method for transmitting a rotary input into counter-rotating outputs
US8021267B2 (en)	2008-12-11	2011-09-20	Rolls-Royce Corporation	Coupling assembly
FR2944564B1 (fr) *	2009-04-16	2011-04-22	Aircelle Sa	Systeme de controle pour nacelle de turboreacteur
GB201002315D0 (en) *	2010-02-11	2010-03-31	Goodrich Actuation Systems Ltd	Control system
US20120079804A1 (en) *	2010-09-30	2012-04-05	Alan Roy Stuart	Cowl assembly
FR2978802B1 (fr) *	2011-08-05	2017-07-14	Aircelle Sa	Inverseur a grilles mobiles et tuyere variable par translation
GB201117824D0 (en) *	2011-10-17	2011-11-30	Rolls Royce Plc	Variable area nozzle for gas turbine engine
US9309835B2 (en)	2012-11-16	2016-04-12	Woodward Hrt, Inc.	Engine and thrust reverser actuation system
US10197007B2 (en)	2016-01-14	2019-02-05	General Electric Company	Method and system for controlling core cowl vent area
CN115217670B (zh) *	2022-05-24	2024-04-26	中国民用航空飞行学院	一种三涵道超声速喷管构型的设计方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3829020A (en)	1973-06-13	1974-08-13	Boeing Co	Translating sleeve variable area nozzle and thrust reverser
US4030291A (en)	1976-01-02	1977-06-21	General Electric Company	Thrust reverser for a gas turbofan engine
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
US5806302A (en)	1996-09-24	1998-09-15	Rohr, Inc.	Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
US6725542B1 (en)	1999-09-17	2004-04-27	Alan R Maguire	Method of assembling a gas turbine engine and nacelle
FR2812035B1 (fr) *	2000-07-24	2003-08-29	Hurel Dubois Avions	Perfectionnements aux inverseurs de poussee pour moteurs a reaction, du type a grilles
GB2395175B (en)	2000-10-19	2005-01-05	Short Brothers Plc	Aircraft propulsive power unit
GB0025666D0 (en)	2000-10-19	2000-12-06	Short Brothers Plc	Aircraft propulsive power unit
US6546715B1 (en) *	2001-01-25	2003-04-15	Rohr, Inc.	Cascade-type thrust reverser
JP4140049B2 (ja) *	2002-03-19	2008-08-27	株式会社Ｉｈｉ	可変ファンノズル装置
FR2887225B1 (fr)	2005-06-21	2008-09-19	Airbus France Sas	Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle
FR2900980B1 (fr)	2006-05-10	2011-08-19	Aircelle Sa	Nacelle pour turboreacteur double flux a grand taux de dilution

2006
- 2006-11-14 US US11/559,761 patent/US7673442B2/en active Active
2007
- 2007-11-01 CA CA 2609282 patent/CA2609282C/fr not_active Expired - Fee Related
- 2007-11-08 JP JP2007290253A patent/JP5572285B2/ja not_active Expired - Fee Related
- 2007-11-12 GB GB0722175A patent/GB2443934B/en active Active
- 2007-11-13 FR FR0758999A patent/FR2908468B1/fr active Active

Also Published As

Publication number	Publication date
GB2443934A (en)	2008-05-21
FR2908468A1 (fr)	2008-05-16
CA2609282C (fr)	2015-04-14
CA2609282A1 (fr)	2008-05-14
GB0722175D0 (en)	2007-12-19
JP2008121682A (ja)	2008-05-29
US7673442B2 (en)	2010-03-09
GB2443934B (en)	2011-09-07
JP5572285B2 (ja)	2014-08-13
US20080110153A1 (en)	2008-05-15

Publication	Publication Date	Title
FR2908467B1 (fr)	2016-03-04	Capot de turboreacteur double flux.
FR2908468B1 (fr)	2012-04-20	Capot de turboreacteur double flux.
FR2909857B1 (fr)	2009-03-06	Endovalve.
FR2897655B1 (fr)	2012-11-16	Turbopropulseur double flux
DE602007009284D1 (de)	2010-10-28	3-aza-bicycloä3.1.0ühexanderivate
EP2000245A4 (fr)	2009-11-04	Procede de soudage
DE602007003343D1 (de)	2009-12-31	Neue mikrobiozide
EP1907748A4 (fr)	2010-05-19	Raccord de tuyaux
EP1969592A4 (fr)	2012-03-28	Flux multimedia consultable
BRPI0716046A2 (pt)	2013-09-17	composiÇÕes de nanopartÍcula.
DE502006002257D1 (de)	2009-01-15	Durchflussmengenregler
DE102006032477A8 (de)	2008-04-30	Dunstabzugshaube
FR2917933B1 (fr)	2009-10-30	Decodeur de flux dvb.
NL2000066A1 (nl)	2006-11-14	Buisarmatuur.
FR2909834B1 (fr)	2011-04-01	Andaineuse transversale.
FR2903669B3 (fr)	2008-06-20	02isse demontable.
FR2898787B1 (fr)	2011-12-30	Equerre.
ITCE20060002A1 (it)	2007-09-11	Patok.
BRPI0718609A2 (pt)	2015-06-30	Anticorpos modificadores de doença cancerosa.
ES1061965Y (es)	2006-08-01	Tractocamion polivalente.
ES1064276Y (es)	2007-05-16	Triciclo.
ITTO20060657A1 (it)	2007-03-30	Motociclo.
ITTO20060824A1 (it)	2007-06-29	Motociclo.
ES1062074Y (es)	2006-08-01	Autorefrigerante solar-ecologico.
ES1061980Y (es)	2006-08-01	Contenedor-palet.

Legal Events

Date	Code	Title	Description
2015-11-17	PLFP	Fee payment	Year of fee payment: 9
2016-11-23	PLFP	Fee payment	Year of fee payment: 10
2017-11-27	PLFP	Fee payment	Year of fee payment: 11
2018-10-24	PLFP	Fee payment	Year of fee payment: 12
2019-10-22	PLFP	Fee payment	Year of fee payment: 13
2020-10-21	PLFP	Fee payment	Year of fee payment: 14
2021-10-20	PLFP	Fee payment	Year of fee payment: 15
2022-10-21	PLFP	Fee payment	Year of fee payment: 16
2023-10-19	PLFP	Fee payment	Year of fee payment: 17
2024-10-22	PLFP	Fee payment	Year of fee payment: 18