DE602006008206D1 - Triebwerksgondel mit Zugangsöffnung zum Enteisungssystem - Google Patents
Triebwerksgondel mit Zugangsöffnung zum EnteisungssystemInfo
- Publication number
- DE602006008206D1 DE602006008206D1 DE602006008206T DE602006008206T DE602006008206D1 DE 602006008206 D1 DE602006008206 D1 DE 602006008206D1 DE 602006008206 T DE602006008206 T DE 602006008206T DE 602006008206 T DE602006008206 T DE 602006008206T DE 602006008206 D1 DE602006008206 D1 DE 602006008206D1
- Authority
- DE
- Germany
- Prior art keywords
- cowling
- inlet
- access opening
- access
- equipment
- 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.)
- Active
Links
- 238000010438 heat treatment Methods 0.000 abstract 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/08—Inspection panels for power plants
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- 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
- B64D2033/0273—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 jet engines
-
- 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
- B64D2241/00—NACA type air intakes
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pipe Accessories (AREA)
- Chairs Characterized By Structure (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/111,834 US7469862B2 (en) | 2005-04-22 | 2005-04-22 | Aircraft engine nacelle inlet having access opening for electrical ice protection system |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602006008206D1 true DE602006008206D1 (de) | 2009-09-17 |
Family
ID=36123363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602006008206T Active DE602006008206D1 (de) | 2005-04-22 | 2006-03-16 | Triebwerksgondel mit Zugangsöffnung zum Enteisungssystem |
Country Status (4)
Country | Link |
---|---|
US (3) | US7469862B2 (de) |
EP (2) | EP2112353B1 (de) |
AT (2) | ATE523674T1 (de) |
DE (1) | DE602006008206D1 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE602006013236D1 (de) * | 2005-08-25 | 2010-05-12 | Gkn Aerospace Services Ltd | Vorflügel für eine Flugzeugtragfläche |
FR2898869B1 (fr) * | 2006-03-24 | 2008-12-12 | Aircelle Sa | Levre d'entree d'air de nacelle a degivrage electrique |
FR2906568B1 (fr) * | 2006-10-02 | 2012-01-06 | Aircelle Sa | Structure d'entree d'air deposable pour nacelle de turboreacteur. |
US20090064684A1 (en) * | 2007-07-13 | 2009-03-12 | United Technologies Corp. | Systems Involving Inlet-Mounted Engine Controls |
US7922121B2 (en) | 2007-10-15 | 2011-04-12 | Rosemount Aerospace Inc. | Power distribution architecture for an ice protection system |
FR2922522B1 (fr) * | 2007-10-22 | 2010-04-16 | Aircelle Sa | Degivrage piezo-electrique d'une entree d'air |
FR2930234B1 (fr) * | 2008-04-21 | 2010-07-30 | Aircelle Sa | Systeme de degivrage et/ou d'antigivrage pour bord d'attaque de voilure d'aeronef. |
US8769924B2 (en) | 2008-05-30 | 2014-07-08 | United Technologies Corporation | Gas turbine engine assembly including accessory components within the nacelle |
FR2934566B1 (fr) | 2008-08-04 | 2011-03-11 | Aircelle Sa | Procede de fabrication d'un ensemble de degivrage sur un panneau d'une nacelle. |
FR2938236B1 (fr) * | 2008-11-13 | 2011-04-15 | Aircelle Sa | Nacelle pour turboreacteur |
US20100123044A1 (en) * | 2008-11-17 | 2010-05-20 | Botura Galdemir C | Aircraft Ice Protection System |
FR2943624B1 (fr) * | 2009-03-27 | 2011-04-15 | Airbus France | Nacelle d'aeronef comportant une paroi exterieure renforcee |
US20110179765A1 (en) * | 2010-01-22 | 2011-07-28 | Lalli Anthony S | Jet engine shield and deicer |
US20110233340A1 (en) * | 2010-03-29 | 2011-09-29 | Christy Daniel P | Aircraft ice protection system |
US8052484B1 (en) | 2010-10-15 | 2011-11-08 | United Technologies Corporation | Electrical connector with offset mating surfaces |
FR2980458B1 (fr) * | 2011-09-28 | 2013-08-30 | Aircelle Sa | Ensemble de levre pour nacelle de turboreacteur a degivrage electrique |
US9593628B2 (en) | 2012-01-31 | 2017-03-14 | United Technologies Corporation | Gas turbine engine variable area fan nozzle with ice management |
US8869508B2 (en) | 2012-01-31 | 2014-10-28 | United Technologies Corporation | Gas turbine engine variable area fan nozzle control |
US8998144B2 (en) * | 2012-02-06 | 2015-04-07 | Textron Innovations Inc. | Thermal insulation barrier for an aircraft de-icing heater |
FR2992291B1 (fr) * | 2012-06-25 | 2016-03-04 | Aircelle Sa | Ensemble electrique chauffant pour dispositif de degivrage |
CN103523235B (zh) * | 2012-07-06 | 2015-12-02 | 哈尔滨飞机工业集团有限责任公司 | 飞机发动机舱进气道整流罩 |
US9193466B2 (en) * | 2012-07-13 | 2015-11-24 | Mra Systems, Inc. | Aircraft ice protection system and method |
US8919494B2 (en) | 2012-07-31 | 2014-12-30 | Rohr, Inc. | Electric heater for integration into an aircraft acoustic panel |
US9297307B2 (en) * | 2012-09-28 | 2016-03-29 | United Technologies Corporation | Power cable and connector arrangement for a gas turbine engine |
FR3000724B1 (fr) * | 2013-01-07 | 2015-01-02 | Aircelle Sa | Architecture degivrage electrique a haute disponibilite d'entree d'air de nacelle a etages commutes |
WO2016064455A2 (en) * | 2014-07-23 | 2016-04-28 | Shield Aerodynamics Llc | Flow drag mitigation device |
US10662877B2 (en) * | 2016-10-03 | 2020-05-26 | Rohr, Inc. | Embedded aircraft heater repair |
CN106640378B (zh) * | 2016-11-24 | 2018-06-29 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种进气道主承载结构及进气道主承载结构变形控制方法 |
FR3060650B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Structure d'entree d'air pour une nacelle d'aeronef |
US10655539B2 (en) * | 2017-10-16 | 2020-05-19 | Rolls-Royce North America Technologies Inc. | Aircraft anti-icing system |
FR3079818A1 (fr) * | 2018-04-10 | 2019-10-11 | Airbus Operations (S.A.S.) | Nacelle de moteur d'aeronef munie d'un systeme de protection contre le givre et procede de protection associe |
FR3081837B1 (fr) * | 2018-06-05 | 2020-11-27 | Airbus Operations Sas | Ensemble turbomachine d'aeronef comportant un capot articule |
GB201809822D0 (en) * | 2018-06-15 | 2018-08-01 | Rolls Royce Plc | Gas turbine engine |
FR3085353A1 (fr) * | 2018-09-04 | 2020-03-06 | Airbus Operations | Ensemble turbomachine d'aeronef comportant un capot articule |
FR3086786B1 (fr) | 2018-10-01 | 2020-12-18 | Airbus Operations Sas | Procede de fabrication d'une peau acoustique degivrante pour panneau acoustique d'aeronef, utilisant un dispositif d'ecartement de fibres |
EP4305653A1 (de) | 2021-03-12 | 2024-01-17 | Essex Industries, Inc. | Wippschalter |
EP4309200A1 (de) | 2021-03-15 | 2024-01-24 | Essex Industries, Inc. | Fünfstellungsschalter |
US11807369B2 (en) * | 2021-03-23 | 2023-11-07 | Airbus Operations Gmbh | Heated leading edge structure for an aircraft |
US12077320B2 (en) | 2022-07-15 | 2024-09-03 | The Boeing Company | Method for producing a perforated nacelle inlet assembly |
US20240018883A1 (en) * | 2022-07-15 | 2024-01-18 | The Boeing Company | Nacelle inlet assembly with composite lipskin |
CN117699022B (zh) * | 2023-12-21 | 2024-07-12 | 中国科学院空天信息创新研究院 | 一种整流罩及飞行设备 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3397302A (en) | 1965-12-06 | 1968-08-13 | Harry W. Hosford | Flexible sheet-like electric heater |
GB1117843A (en) | 1966-02-25 | 1968-06-26 | Rolls Royce | Improvements relating to anti-icing heating apparatus |
GB1247071A (en) | 1969-01-24 | 1971-09-22 | Rolls Royce | An aircraft engine nose cowl |
GB1314162A (en) | 1969-05-08 | 1973-04-18 | Secr Defence | Intake anti-icing system for gas turbine engines |
DE2443224C3 (de) | 1974-09-10 | 1979-02-22 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Verfahren zum Enteisen von Triebwerks-, Flügel- und Leitwerksystemen an Flugkörpern |
AT383931B (de) | 1982-11-11 | 1987-09-10 | Hans Oppitz | Flaechenheizelement, insbesondere fuer verbaende oder heizdecken |
JPS60150682A (ja) | 1984-01-17 | 1985-08-08 | Sharp Corp | 半導体レ−ザ素子 |
US4826108A (en) | 1987-07-16 | 1989-05-02 | The B. F. Goodrich Company | De-icer |
US5098037A (en) | 1989-11-06 | 1992-03-24 | The B. F. Goodrich Company | Structural airfoil having integral expulsive system |
EP0459216A3 (en) | 1990-06-01 | 1993-03-17 | The Bfgoodrich Company | Electrical heater de-icer |
US5143325B1 (en) * | 1991-01-03 | 2000-09-05 | Electroimpact Inc | Electromagnetic repulsion system for removing contaminants such as ice from the surface of aircraft and other objects |
GB2259287B (en) | 1991-09-04 | 1994-08-10 | Rolls Royce Plc | Apparatus for de-icing a surface and method of using the same |
US5248116A (en) | 1992-02-07 | 1993-09-28 | The B. F. Goodrich Company | Airfoil with integral de-icer using overlapped tubes |
US5361183A (en) | 1993-06-30 | 1994-11-01 | Alliedsignal Inc. | Ground fault protection for electrothermal de-icing applications |
US5429327A (en) * | 1993-10-22 | 1995-07-04 | The B.F. Goodrich Company | Electro-impulse de-icer |
US5427332A (en) | 1993-11-10 | 1995-06-27 | The B. F. Goodrich Company | Modular ice protection assembly |
CA2147084A1 (en) | 1994-04-13 | 1995-10-14 | Tommy Maurice Wilson, Jr. | Electrothermal deicing system |
US5657951A (en) | 1995-06-23 | 1997-08-19 | The B.F. Goodrich Company | Electrothermal de-icing system |
US6027075A (en) | 1997-06-16 | 2000-02-22 | Trustees Of Dartmouth College | Systems and methods for modifying ice adhesion strength |
US6279856B1 (en) | 1997-09-22 | 2001-08-28 | Northcoast Technologies | Aircraft de-icing system |
US6237874B1 (en) | 1997-09-22 | 2001-05-29 | Northcoast Technologies | Zoned aircraft de-icing system and method |
FR2787509B1 (fr) | 1998-12-21 | 2001-03-30 | Aerospatiale | Structure d'entree d'air pour moteur d'aeronef |
US6227492B1 (en) | 1999-08-06 | 2001-05-08 | Bell Helicopter Textron Inc. | Redundant ice management system for aircraft |
US6725542B1 (en) | 1999-09-17 | 2004-04-27 | Alan R Maguire | Method of assembling a gas turbine engine and nacelle |
US7588212B2 (en) | 2003-07-08 | 2009-09-15 | Rohr Inc. | Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip |
-
2005
- 2005-04-22 US US11/111,834 patent/US7469862B2/en active Active
-
2006
- 2006-03-16 EP EP09007425A patent/EP2112353B1/de not_active Not-in-force
- 2006-03-16 AT AT09007425T patent/ATE523674T1/de not_active IP Right Cessation
- 2006-03-16 DE DE602006008206T patent/DE602006008206D1/de active Active
- 2006-03-16 EP EP06005409A patent/EP1715159B1/de not_active Not-in-force
- 2006-03-16 AT AT06005409T patent/ATE438794T1/de not_active IP Right Cessation
-
2008
- 2008-09-18 US US12/233,437 patent/US7681838B2/en active Active
- 2008-09-18 US US12/233,424 patent/US7631838B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2112353A1 (de) | 2009-10-28 |
US7681838B2 (en) | 2010-03-23 |
US20060237582A1 (en) | 2006-10-26 |
ATE438794T1 (de) | 2009-08-15 |
US20090014598A1 (en) | 2009-01-15 |
US20090008509A1 (en) | 2009-01-08 |
US7469862B2 (en) | 2008-12-30 |
EP1715159A1 (de) | 2006-10-25 |
ATE523674T1 (de) | 2011-09-15 |
US7631838B2 (en) | 2009-12-15 |
EP1715159B1 (de) | 2009-08-05 |
EP2112353B1 (de) | 2011-09-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |