DE68908321D1 - Mantelgeblaese-turbinentriebwerk. - Google Patents

Mantelgeblaese-turbinentriebwerk.

Info

Publication number: DE68908321D1
Authority: DE; Germany
Prior art keywords: sheath; turbine engine; blower turbine; blower; engine
Prior art date: 1988-09-28
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

DE8989309846T

Other languages

English (en)

Other versions

DE68908321T2 (de

Inventor

Norman Armstrong

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.)

Short Brothers PLC

Original Assignee

Short Brothers 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.)

1988-09-28

Filing date

1989-09-27

Publication date

1993-09-16

1989-09-27 Application filed by Short Brothers PLC filed Critical Short Brothers PLC

1993-09-16 Publication of DE68908321D1 publication Critical patent/DE68908321D1/de

1994-02-24 Application granted granted Critical

1994-02-24 Publication of DE68908321T2 publication Critical patent/DE68908321T2/de

2009-09-28 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

Links

RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1

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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Turbine Rotor Nozzle Sealing (AREA)
Catching Or Destruction (AREA)

DE89309846T 1988-09-28 1989-09-27 Mantelgebläse-Turbinentriebwerk. Expired - Fee Related DE68908321T2 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB888822798A GB8822798D0 (en)	1988-09-28	1988-09-28	Ducted fan turbine engine

Publications (2)

Publication Number	Publication Date
DE68908321D1 true DE68908321D1 (de)	1993-09-16
DE68908321T2 DE68908321T2 (de)	1994-02-24

Family

ID=10644413

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE89309846T Expired - Fee Related DE68908321T2 (de)	1988-09-28	1989-09-27	Mantelgebläse-Turbinentriebwerk.

Country Status (11)

Country	Link
US (1)	US5136839A (de)
EP (1)	EP0361901B1 (de)
JP (1)	JPH03501835A (de)
AU (1)	AU633518B2 (de)
BR (1)	BR8907100A (de)
CA (1)	CA1334723C (de)
DE (1)	DE68908321T2 (de)
ES (1)	ES2043032T3 (de)
GB (2)	GB8822798D0 (de)
IL (1)	IL91811A0 (de)
WO (1)	WO1990003309A1 (de)

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB9120658D0 (en) *	1991-09-27	1991-11-06	Short Brothers Plc	Ducted fan turbine engine
GB9123083D0 (en) *	1991-10-31	1991-12-18	Band David M	Ion-selective polymeric electrodes
GB9301457D0 (en) *	1993-01-26	1993-03-17	Short Brothers Plc	An aircraft propulsuve power unit
FR2755095B1 (fr) *	1996-10-24	1998-12-18	Conception Aeronautique Du Sud	Nacelle longue pour moteur a reaction double flux d'aeronef
FR2764644B1 (fr) *	1997-06-12	1999-07-16	Hispano Suiza Sa	Turboreacteur a double flux associe a un inverseur de poussee avec un carenage rapporte dans la veine fluide
FR2771330B1 (fr) *	1997-11-26	2004-02-27	Aerospatiale	Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
FR2811716B1 (fr) *	2000-07-17	2002-10-04	Hurel Dubois Avions	Perfectionnements aux arriere-corps de nacelle, a tuyere commune, de reacteur d'avion
US6887035B2 (en)	2002-10-23	2005-05-03	General Electric Company	Tribologically improved design for variable stator vanes
FR2856379B1 (fr) *	2003-06-18	2006-11-24	Airbus France	Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
US6971240B2 (en) *	2004-03-30	2005-12-06	General Electric Company	Methods and apparatus for exhausting gases from gas turbine engines
ES2264625B1 (es) *	2004-12-15	2007-12-01	GAMESA INNOVATION & TECHNOLOGY, S.L.	Procedimiento de retirada de la cubierta de un aerogenerador.
FR2896481B1 (fr) *	2006-01-23	2009-12-04	Aircelle Sa	Systeme de fixation pour element constitutif d'une nacelle de turboreacteur
ES2316257B1 (es) *	2006-10-31	2010-01-12	Airbus España, S.L.	Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos.
FR2912378B1 (fr) *	2007-02-14	2009-03-20	Aircelle Sa	Nacelle de moteur a reaction pour un avion
FR2916426B1 (fr) *	2007-05-22	2010-04-02	Aircelle Sa	Ensemble arriere de nacelle pour turboreacteur.
US8844265B2 (en)	2007-08-01	2014-09-30	United Technologies Corporation	Turbine section of high bypass turbofan
US20150377123A1 (en)	2007-08-01	2015-12-31	United Technologies Corporation	Turbine section of high bypass turbofan
US11346289B2 (en)	2007-08-01	2022-05-31	Raytheon Technologies Corporation	Turbine section of high bypass turbofan
US11149650B2 (en)	2007-08-01	2021-10-19	Raytheon Technologies Corporation	Turbine section of high bypass turbofan
US11242805B2 (en)	2007-08-01	2022-02-08	Raytheon Technologies Corporation	Turbine section of high bypass turbofan
US8256707B2 (en) *	2007-08-01	2012-09-04	United Technologies Corporation	Engine mounting configuration for a turbofan gas turbine engine
US11486311B2 (en)	2007-08-01	2022-11-01	Raytheon Technologies Corporation	Turbine section of high bypass turbofan
FR2920136B1 (fr) *	2007-08-20	2009-10-30	Aircelle Sa	Systeme de liaison entre une structure interne et un structure externe d'une nacelle
US8118251B2 (en) *	2008-01-18	2012-02-21	United Technologies Corporation	Mounting system for a gas turbine engine
US8167237B2 (en) *	2008-03-21	2012-05-01	United Technologies Corporation	Mounting system for a gas turbine engine
US8800914B2 (en)	2008-06-02	2014-08-12	United Technologies Corporation	Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en)	2008-06-02	2014-04-15	United Technologies Corporation	Gas turbine engine with low stage count low pressure turbine
US8128021B2 (en) *	2008-06-02	2012-03-06	United Technologies Corporation	Engine mount system for a turbofan gas turbine engine
US8511605B2 (en)	2008-06-02	2013-08-20	United Technologies Corporation	Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en)	2008-06-02	2014-08-19	United Technologies Corporation	Gas turbine engine compressor arrangement
US20140174056A1 (en)	2008-06-02	2014-06-26	United Technologies Corporation	Gas turbine engine with low stage count low pressure turbine
US8262050B2 (en)	2008-12-24	2012-09-11	General Electric Company	Method and apparatus for mounting and dismounting an aircraft engine
US8469309B2 (en) *	2008-12-24	2013-06-25	General Electric Company	Monolithic structure for mounting aircraft engine
ES2398861B1 (es) *	2010-10-08	2014-04-29	Airbus Operations, S.L.	Concepto de unión intercambiable para un cono de un fuselaje trasero de un avión.
CN103112595B (zh) *	2013-02-06	2016-01-27	中国商用飞机有限责任公司	推进***一体化的吊挂结构
WO2015054233A1 (en)	2013-10-07	2015-04-16	Rohr, Inc.	Hybrid inner fixed structure with metallic and composite construction
US10371047B2 (en)	2013-10-16	2019-08-06	United Technologies Corporation	Geared turbofan engine with targeted modular efficiency
US10161356B2 (en) *	2014-06-02	2018-12-25	Ge Aviation Systems Llc	Integrated thrust reverser actuation system
US10759541B2 (en)	2016-10-14	2020-09-01	Rohr, Inc.	Nacelle bifurcation with leading edge structure
US10611490B2 (en) *	2016-11-02	2020-04-07	Rohr, Inc.	Fan cowl fairing restraining system
US10543927B2 (en) *	2016-11-18	2020-01-28	Rohr, Inc.	Lockable track system for a translating nacelle structure
US10899463B2 (en)	2017-05-16	2021-01-26	Rohr, Inc.	Segmented pylon for an aircraft propulsion system
CN109502034B (zh) *	2018-12-11	2021-10-19	湖北航天飞行器研究所	一种小口径飞行器燃气舵挡火结构

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB758205A (en) *	1953-12-30	1956-10-03	Armstrong Siddeley Motors Ltd	Improvements relating to by-pass, turbo-jet engines
GB966522A (en) *	1960-02-02	1964-08-12	Bristol Siddeley Engines Ltd	Improvements relating to aerial vehicles having jet propulsion engines
US3542152A (en) *	1968-04-08	1970-11-24	Gen Electric	Sound suppression panel
US3508838A (en) *	1968-09-16	1970-04-28	Gen Electric	Sound suppression of compressors used in gas turbine engines
US3541794A (en) *	1969-04-23	1970-11-24	Gen Electric	Bifurcated fan duct thrust reverser
US3670964A (en) *	1971-01-18	1972-06-20	Gen Motors Corp	Jet nozzle
GB1375868A (de) *	1972-09-22	1974-11-27
GB1533551A (en) *	1974-11-08	1978-11-29	Gen Electric	Gas turbofan engines
FR2291091A1 (fr) *	1974-11-13	1976-06-11	Snecma	Dispositif de montage sur avion d'un turboreacteur
GB1522558A (en) *	1976-04-05	1978-08-23	Rolls Royce	Duct linings
GB1543312A (en) *	1976-07-21	1979-04-04	Rolls Royce	Honeycomb linings
CA1324999C (en) *	1986-04-30	1993-12-07	Walter M. Presz, Jr.	Bodies with reduced surface drag
US4696159A (en) *	1986-08-04	1987-09-29	United Technologies Corporation	Gas turbine outlet arrangement
US4790137A (en) *	1987-07-17	1988-12-13	The United States Of America As Represented By The Secretary Of The Air Force	Aircraft engine outer duct mounting device
GB2212859B (en) *	1987-12-02	1991-03-06	Rolls Royce Plc	Ducted fan gas turbine engine with surge controller

1988
- 1988-09-28 GB GB888822798A patent/GB8822798D0/en active Pending
1989
- 1989-09-25 CA CA000612774A patent/CA1334723C/en not_active Expired - Fee Related
- 1989-09-27 WO PCT/GB1989/001137 patent/WO1990003309A1/en unknown
- 1989-09-27 US US07/476,376 patent/US5136839A/en not_active Expired - Lifetime
- 1989-09-27 ES ES89309846T patent/ES2043032T3/es not_active Expired - Lifetime
- 1989-09-27 AU AU43277/89A patent/AU633518B2/en not_active Ceased
- 1989-09-27 GB GB8921744A patent/GB2225060B/en not_active Expired - Fee Related
- 1989-09-27 JP JP1510014A patent/JPH03501835A/ja active Pending
- 1989-09-27 EP EP89309846A patent/EP0361901B1/de not_active Expired - Lifetime
- 1989-09-27 BR BR898907100A patent/BR8907100A/pt not_active IP Right Cessation
- 1989-09-27 IL IL91811A patent/IL91811A0/xx not_active IP Right Cessation
- 1989-09-27 DE DE89309846T patent/DE68908321T2/de not_active Expired - Fee Related

Also Published As

Publication number	Publication date
BR8907100A (pt)	1991-02-05
US5136839A (en)	1992-08-11
WO1990003309A1 (en)	1990-04-05
IL91811A0 (en)	1990-06-10
GB2225060B (en)	1993-03-24
EP0361901A1 (de)	1990-04-04
CA1334723C (en)	1995-03-14
GB8921744D0 (en)	1989-11-08
GB2225060A (en)	1990-05-23
JPH03501835A (ja)	1991-04-25
DE68908321T2 (de)	1994-02-24
GB8822798D0 (en)	1988-11-02
AU633518B2 (en)	1993-02-04
AU4327789A (en)	1990-04-18
ES2043032T3 (es)	1993-12-16
EP0361901B1 (de)	1993-08-11

Legal Events

Date	Code	Title	Description
1994-09-08	8364	No opposition during term of opposition
1997-09-11	8339	Ceased/non-payment of the annual fee

Publication	Publication Date	Title
DE68908321D1 (de)	1993-09-16	Mantelgeblaese-turbinentriebwerk.
DE68912214D1 (de)	1994-02-24	Motorregler.
DE58900152D1 (de)	1991-08-01	Propfan-turbotriebwerk.
DE68908734D1 (de)	1993-10-07	Schalldämpfer.
AR240355A1 (es)	1990-03-30	Turbina de viento mejorada.
DE69008291D1 (de)	1994-05-26	Turboladermotor.
DE68912705D1 (de)	1994-03-10	Vogelabschreckungsanordnung.
DE3861665D1 (de)	1991-02-28	Windkraftmaschine.
DE68900273D1 (de)	1991-10-24	Zweistoffraketenmotor.
DE68911510D1 (de)	1994-01-27	Wärmegedämpfter motor.
DE3779460D1 (de)	1992-07-09	Abgasturbine.
DK374589A (da)	1990-01-31	Turbine
DE69002283D1 (de)	1993-08-26	Gasturbinen-triebwerkseinheit.
DE68921574D1 (de)	1995-04-13	Klebeband.
DE68901930D1 (de)	1992-08-06	Luefter.
FR2652459B1 (fr)	1993-03-12	Turbomachine magnetohydrodynamique.
DE58907776D1 (de)	1994-07-07	Brüstungskanalanordnung.
DE59000390D1 (de)	1992-12-03	Turbinen-staustrahltriebwerk.
DE68914051D1 (de)	1994-04-28	Gasturbine.
DE3864003D1 (de)	1991-09-05	Turbinenzwischenleitung.
DE58900303D1 (de)	1991-10-24	Axialluefter.
DE59000083D1 (de)	1992-05-21	Turbostrahltriebwerk.
DE3873728D1 (de)	1992-09-17	Luefter.
DE58904491D1 (de)	1993-07-01	Viertakt-brennkraftmaschine.
OA09101A (fr)	1991-10-31	Turbo-Eolienne.