DE68908321D1 - Mantelgeblaese-turbinentriebwerk. - Google Patents
Mantelgeblaese-turbinentriebwerk.Info
- Publication number
- DE68908321D1 DE68908321D1 DE8989309846T DE68908321T DE68908321D1 DE 68908321 D1 DE68908321 D1 DE 68908321D1 DE 8989309846 T DE8989309846 T DE 8989309846T DE 68908321 T DE68908321 T DE 68908321T DE 68908321 D1 DE68908321 D1 DE 68908321D1
- Authority
- DE
- Germany
- Prior art keywords
- sheath
- turbine engine
- blower turbine
- blower
- engine
- Prior art date
- 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
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)
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)
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)
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 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |