DE60000813D1 - Gondel für einen Gasturbinentriebwerk - Google Patents
Gondel für einen GasturbinentriebwerkInfo
- Publication number
- DE60000813D1 DE60000813D1 DE60000813T DE60000813T DE60000813D1 DE 60000813 D1 DE60000813 D1 DE 60000813D1 DE 60000813 T DE60000813 T DE 60000813T DE 60000813 T DE60000813 T DE 60000813T DE 60000813 D1 DE60000813 D1 DE 60000813D1
- Authority
- DE
- Germany
- Prior art keywords
- gondola
- gas turbine
- turbine engine
- engine
- gas
- 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 - Lifetime
Links
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
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- 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
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB9921935.4A GB9921935D0 (en) | 1999-09-17 | 1999-09-17 | A nacelle assembly for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60000813D1 true DE60000813D1 (de) | 2003-01-02 |
DE60000813T2 DE60000813T2 (de) | 2003-03-27 |
Family
ID=10861051
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60000813T Expired - Lifetime DE60000813T2 (de) | 1999-09-17 | 2000-09-06 | Gondel für einen Gasturbinentriebwerk |
Country Status (4)
Country | Link |
---|---|
US (1) | US6360989B1 (de) |
EP (1) | EP1084951B1 (de) |
DE (1) | DE60000813T2 (de) |
GB (1) | GB9921935D0 (de) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2385382B (en) * | 2002-02-13 | 2006-02-15 | Rolls Royce Plc | A cowl structure for a gas turbine engine |
US7090165B2 (en) * | 2003-06-02 | 2006-08-15 | Rolls-Royce Plc | Aeroengine nacelle |
US20040244357A1 (en) * | 2003-06-05 | 2004-12-09 | Sloan Mark L. | Divergent chevron nozzle and method |
US6920958B2 (en) * | 2003-10-17 | 2005-07-26 | The Boeing Company | Annular acoustic panel |
FR2898870B1 (fr) * | 2006-03-24 | 2008-05-23 | Aircelle Sa | Structure de virole d'entree d'air |
US7866440B2 (en) * | 2006-07-21 | 2011-01-11 | Rohr, Inc. | System for joining acoustic cellular panel sections in edge-to-edge relation |
US7797944B2 (en) * | 2006-10-20 | 2010-09-21 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US7870721B2 (en) * | 2006-11-10 | 2011-01-18 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
GB0704879D0 (en) | 2007-03-14 | 2007-04-18 | Rolls Royce Plc | A Casing arrangement |
US8408491B2 (en) | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
US8205430B2 (en) * | 2007-05-16 | 2012-06-26 | United Technologies Corporation | Variable geometry nacelle assembly for a gas turbine engine |
US8727267B2 (en) * | 2007-05-18 | 2014-05-20 | United Technologies Corporation | Variable contraction ratio nacelle assembly for a gas turbine engine |
US8082726B2 (en) * | 2007-06-26 | 2011-12-27 | United Technologies Corporation | Tangential anti-swirl air supply |
US9091214B2 (en) * | 2007-06-28 | 2015-07-28 | United Technologies Corporation | Reduced gearbox size by separate electrically powered engine oil system |
US8402739B2 (en) * | 2007-06-28 | 2013-03-26 | United Technologies Corporation | Variable shape inlet section for a nacelle assembly of a gas turbine engine |
US9228534B2 (en) * | 2007-07-02 | 2016-01-05 | United Technologies Corporation | Variable contour nacelle assembly for a gas turbine engine |
US9004399B2 (en) | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
US9719428B2 (en) * | 2007-11-30 | 2017-08-01 | United Technologies Corporation | Gas turbine engine with pylon mounted accessory drive |
US8192147B2 (en) * | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8186942B2 (en) * | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
US8769924B2 (en) * | 2008-05-30 | 2014-07-08 | United Technologies Corporation | Gas turbine engine assembly including accessory components within the nacelle |
FR2932160B1 (fr) * | 2008-06-06 | 2010-11-26 | Airbus France | Support d'appareils de mesure intercale entre une motorisation et une entree d'air d'une nacelle d'aeronef |
GB0813483D0 (en) * | 2008-07-24 | 2008-08-27 | Rolls Royce Plc | Gas turbine engine nacelle |
FR2934247A1 (fr) * | 2008-07-25 | 2010-01-29 | Snecma | Nacelle de turboreacteur. |
FR2938236B1 (fr) * | 2008-11-13 | 2011-04-15 | Aircelle Sa | Nacelle pour turboreacteur |
US8152461B2 (en) * | 2008-11-19 | 2012-04-10 | Mra Systems, Inc. | Integrated inlet design |
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 |
GB0916823D0 (en) | 2009-09-25 | 2009-11-04 | Rolls Royce Plc | Containment casing for an aero engine |
GB201015437D0 (en) * | 2010-09-16 | 2010-10-27 | Rolls Royce Plc | Gas turbine engine bearing arrangement |
FR2990928B1 (fr) * | 2012-05-24 | 2014-06-27 | Snecma | Nacelle de moteur a turbine a gaz |
US20140352797A1 (en) * | 2013-06-04 | 2014-12-04 | Rohr, Inc. | Aircraft jet engine |
US9664113B2 (en) * | 2014-03-15 | 2017-05-30 | The Boeing Company | One piece inlet lip skin design |
US20180208297A1 (en) * | 2017-01-20 | 2018-07-26 | General Electric Company | Nacelle for an aircraft aft fan |
US10589869B2 (en) | 2018-07-25 | 2020-03-17 | General Electric Company | Nacelle inlet lip fuse structure |
CN110805496B (zh) * | 2018-08-06 | 2020-09-08 | 中国航发商用航空发动机有限责任公司 | 航空发动机风扇叶片脱落事件降载装置 |
US11085373B2 (en) | 2019-01-31 | 2021-08-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with mount for interchangeable inlets |
FR3097260B1 (fr) * | 2019-06-12 | 2021-06-11 | Safran Aircraft Engines | Carter de soufflante de turboréacteur |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4044973A (en) | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
US4500252A (en) * | 1981-12-21 | 1985-02-19 | United Technologies Corporation | Beam for a containment structure |
DE3277836D1 (en) * | 1982-03-26 | 1988-01-28 | Boeing Co | Collapsible cowl structure for gas-turbine engine strut |
GB2228639B (en) | 1989-02-17 | 1992-07-15 | Motorola Semiconducteurs | Protected darlington transistor arrangement |
GB9116986D0 (en) | 1991-08-07 | 1991-10-09 | Rolls Royce Plc | Gas turbine engine nacelle assembly |
US5205513A (en) * | 1991-09-26 | 1993-04-27 | General Electric Company | Method and system for the removal of large turbine engines |
GB2265418B (en) * | 1992-03-26 | 1995-03-08 | Rolls Royce Plc | Gas turbine engine casing |
US5259724A (en) * | 1992-05-01 | 1993-11-09 | General Electric Company | Inlet fan blade fragment containment shield |
GB9301457D0 (en) * | 1993-01-26 | 1993-03-17 | Short Brothers Plc | An aircraft propulsuve power unit |
US5447411A (en) * | 1993-06-10 | 1995-09-05 | Martin Marietta Corporation | Light weight fan blade containment system |
US5524847A (en) | 1993-09-07 | 1996-06-11 | United Technologies Corporation | Nacelle and mounting arrangement for an aircraft engine |
FR2757823B1 (fr) * | 1996-12-26 | 1999-03-12 | Aerospatiale | Nacelle de turboreacteur a ecoulement laminaire |
-
1999
- 1999-09-17 GB GBGB9921935.4A patent/GB9921935D0/en not_active Ceased
-
2000
- 2000-09-06 DE DE60000813T patent/DE60000813T2/de not_active Expired - Lifetime
- 2000-09-06 EP EP00307682A patent/EP1084951B1/de not_active Expired - Lifetime
- 2000-09-07 US US09/657,266 patent/US6360989B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1084951A2 (de) | 2001-03-21 |
EP1084951B1 (de) | 2002-11-20 |
US6360989B1 (en) | 2002-03-26 |
DE60000813T2 (de) | 2003-03-27 |
GB9921935D0 (en) | 1999-11-17 |
EP1084951A3 (de) | 2001-10-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |