FR2908467B1 - Capot de turboreacteur double flux. - Google Patents

Capot de turboreacteur double flux.

Info

Publication number: FR2908467B1
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.): Expired - Fee Related

Application number

FR0759000A

Other languages

English (en)

Other versions

FR2908467A1 (fr

Inventor

Ory Thomas Moniz

Jorge Francisco Seda

Robert Joseph Orlando

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

2016-03-04

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

2008-05-16 Publication of FR2908467A1 publication Critical patent/FR2908467A1/fr

2016-03-04 Application granted granted Critical

2016-03-04 Publication of FR2908467B1 publication Critical patent/FR2908467B1/fr

Status Expired - Fee Related 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
- 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
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
- 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)
Structures Of Non-Positive Displacement Pumps (AREA)
Turbine Rotor Nozzle Sealing (AREA)

FR0759000A 2006-11-14 2007-11-13 Capot de turboreacteur double flux. Expired - Fee Related FR2908467B1 (fr)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US11/559,747 US7886518B2 (en)	2006-11-14	2006-11-14	Turbofan engine cowl assembly and method of operating the same

Publications (2)

Publication Number	Publication Date
FR2908467A1 FR2908467A1 (fr)	2008-05-16
FR2908467B1 true FR2908467B1 (fr)	2016-03-04

Family

ID=38896307

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR0759000A Expired - Fee Related FR2908467B1 (fr)	2006-11-14	2007-11-13	Capot de turboreacteur double flux.

Country Status (5)

Country	Link
US (2)	US7886518B2 (fr)
JP (1)	JP5342130B2 (fr)
CA (1)	CA2609281C (fr)
FR (1)	FR2908467B1 (fr)
GB (1)	GB2443948B (fr)

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US7673458B2 (en) *	2006-11-14	2010-03-09	General Electric Company	Turbofan engine nozzle assembly and method for operating the same
US7726116B2 (en) *	2006-11-14	2010-06-01	General Electric Company	Turbofan engine nozzle assembly and method of operating same
US7681399B2 (en) *	2006-11-14	2010-03-23	General Electric Company	Turbofan engine cowl assembly and method of operating the same
US7886518B2 (en) *	2006-11-14	2011-02-15	General Electric Company	Turbofan engine cowl assembly and method of operating the same
EP2123884B1 (fr)	2008-05-13	2015-03-04	Rolls-Royce Corporation	Agencement d'embrayage double
US20090297339A1 (en) *	2008-05-29	2009-12-03	General Electric Company	Low noise ejector for a turbomachine
US8769924B2 (en) *	2008-05-30	2014-07-08	United Technologies Corporation	Gas turbine engine assembly including accessory components within the nacelle
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
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
US9188025B2 (en) *	2008-11-26	2015-11-17	Mra Systems, Inc.	Apparatus for facilitating access to a nacelle interior
US8220738B2 (en) *	2008-11-26	2012-07-17	Mra Systems, Inc.	Nacelle and method of assembling the same
US8021267B2 (en)	2008-12-11	2011-09-20	Rolls-Royce Corporation	Coupling assembly
US8075438B2 (en)	2008-12-11	2011-12-13	Rolls-Royce Corporation	Apparatus and method for transmitting a rotary input into counter-rotating outputs
CA2789438A1 (fr) *	2010-02-15	2011-11-17	General Electric Company	Glissiere a articulation
US8667802B2 (en) *	2010-05-06	2014-03-11	Spirit Aerosystems, Inc.	Variable fan duct nozzle translatable core/inner cowl including two overlapping portions made of different materials
US8615982B2 (en)	2011-07-05	2013-12-31	Hamilton Sundstrand Corporation	Integrated electric variable area fan nozzle thrust reversal actuation system
US20140161603A1 (en) *	2012-12-07	2014-06-12	General Electric Company	Exhaust diffuser
EP2982854B1 (fr)	2014-08-08	2023-03-01	Raytheon Technologies Corporation	Buse de sortie divergente convergente pour un moteur à turbine à gaz
DE102015100602A1 (de) *	2015-01-15	2016-07-21	Brandenburgische Technische Universität Cottbus-Senftenberg	Variable Kerntriebwerksverkleidung für Turbofan-Triebwerke mit hohem Nebenstromverhältnis
US20180355821A1 (en) *	2017-06-09	2018-12-13	United Technologies Corporation	Moveable exhaust plug
US10570852B2 (en)	2017-09-21	2020-02-25	United Technologies Corporation	Moveable exhaust plug liner
US11274630B2 (en)	2020-02-27	2022-03-15	Rolls-Royce North American Technologies Inc.	Exhaust nozzle with vane support structure for a gas turbine engine
US11313320B2 (en)	2020-02-27	2022-04-26	Rolls-Royce North American Technologies Inc.	Exhaust nozzle with centerbody support structure for a gas turbine engine
US11274631B2 (en)	2020-02-27	2022-03-15	Rolls-Royce North American Technologies Inc.	Methodology for minimizing aerodynamic buzz in an exhaust nozzle
US11319832B2 (en)	2020-02-27	2022-05-03	Rolls-Royce North American Technologies Inc.	Single movement convergent and convergent-divergent nozzle
US11326551B1 (en)	2020-02-27	2022-05-10	Rolls-Royce North American Technologies Inc.	Exhaust nozzle having a compliant shell for a gas turbine engine
US11408368B2 (en)	2020-03-31	2022-08-09	Rolls-Royce North American Technologies Inc.	Reconfigurable exhaust nozzle for a gas turbine engine
FR3125093A1 (fr) *	2021-07-12	2023-01-13	Safran Nacelles	Bielle pour nacelle de turbomachine
US11732673B2 (en) *	2021-07-27	2023-08-22	General Electric Company	Variable area exhaust nozzle system and method for control thereof

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US2570629A (en) *	1945-10-05	1951-10-09	Anxionnaz	Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles
US2938335A (en) *	1958-04-14	1960-05-31	Boeing Co	Noise suppressor and thrust reverser
GB1009776A (en) *	1964-08-25	1965-11-10	Rolls Royce	Supersonic jet propulsion nozzle
US3829020A (en) *	1973-06-13	1974-08-13	Boeing Co	Translating sleeve variable area nozzle and thrust reverser
US3897001A (en) *	1974-06-12	1975-07-29	Gen Electric	Nozzle and auxiliary inlet arrangement for gas turbine engine
US4043508A (en) *	1975-12-01	1977-08-23	General Electric Company	Articulated plug nozzle
US4039146A (en)	1975-12-01	1977-08-02	General Electric Company	Variable cycle plug nozzle and flap and method of operating same
US4228651A (en) *	1977-11-29	1980-10-21	Rolls-Royce Limited	Ducted fan gas turbine engine
GB2198999B (en) *	1986-12-17	1990-08-29	Rolls Royce Plc	Fluid propulsion engine with flow exit control device
US5261227A (en) *	1992-11-24	1993-11-16	General Electric Company	Variable specific thrust 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
WO1996012881A1 (fr)	1994-10-20	1996-05-02	United Technologies Corporation	Buse d'evacuation d'air de ventilation, a section de superficie variable
US5806302A (en) *	1996-09-24	1998-09-15	Rohr, Inc.	Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
JPH11159399A (ja)	1997-11-26	1999-06-15	Tech Res & Dev Inst Of Japan Def Agency	高バイパス比ターボファンエンジン
US6725542B1 (en) *	1999-09-17	2004-04-27	Alan R Maguire	Method of assembling a gas turbine engine and nacelle
DE60312817T2 (de) *	2002-01-09	2008-01-24	The Nordam Group, Inc., Tulsa	Turbofandüse und Geräuschminderungsverfahren in einer solchen Düse
WO2005085620A1 (fr)	2004-03-02	2005-09-15	Isamu Nemoto	Moteur a cycle variable pour propulser un aeronef subsonique
US7886518B2 (en) *	2006-11-14	2011-02-15	General Electric Company	Turbofan engine cowl assembly and method of operating the same

2006
- 2006-11-14 US US11/559,747 patent/US7886518B2/en active Active
2007
- 2007-11-01 CA CA 2609281 patent/CA2609281C/fr not_active Expired - Fee Related
- 2007-11-08 JP JP2007290252A patent/JP5342130B2/ja not_active Expired - Fee Related
- 2007-11-13 FR FR0759000A patent/FR2908467B1/fr not_active Expired - Fee Related
- 2007-11-14 GB GB0722371A patent/GB2443948B/en not_active Expired - Fee Related
2011
- 2011-01-26 US US13/014,168 patent/US8091334B2/en not_active Expired - Fee Related

Also Published As

Publication number	Publication date
CA2609281A1 (fr)	2008-05-14
GB2443948A (en)	2008-05-21
JP2008121681A (ja)	2008-05-29
US20080112801A1 (en)	2008-05-15
US7886518B2 (en)	2011-02-15
CA2609281C (fr)	2015-04-21
US20110120136A1 (en)	2011-05-26
JP5342130B2 (ja)	2013-11-13
GB0722371D0 (en)	2007-12-27
US8091334B2 (en)	2012-01-10
GB2443948B (en)	2011-09-07
FR2908467A1 (fr)	2008-05-16

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
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.
ITCE20060002A1 (it)	2007-09-11	Patok.
BRPI0718609A2 (pt)	2015-06-30	Anticorpos modificadores de doença cancerosa.
FR2898787B1 (fr)	2011-12-30	Equerre.
ES1061965Y (es)	2006-08-01	Tractocamion polivalente.
ES1064276Y (es)	2007-05-16	Triciclo.
ITTO20060824A1 (it)	2007-06-29	Motociclo.
ITTO20060657A1 (it)	2007-03-30	Motociclo.
ES1062074Y (es)	2006-08-01	Autorefrigerante solar-ecologico.
ES1061980Y (es)	2006-08-01	Contenedor-palet.
ITGE20060082A1 (it)	2008-02-04	Fattoria pet - therapyazienda agrituristica socioterapeutica e didattica.

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
2024-08-02	ST	Notification of lapse	Effective date: 20240706