FR2888562B1 - Levre d'entree de nacelle pour moteur d'avion - Google Patents
Levre d'entree de nacelle pour moteur d'avionInfo
- Publication number
- FR2888562B1 FR2888562B1 FR0606366A FR0606366A FR2888562B1 FR 2888562 B1 FR2888562 B1 FR 2888562B1 FR 0606366 A FR0606366 A FR 0606366A FR 0606366 A FR0606366 A FR 0606366A FR 2888562 B1 FR2888562 B1 FR 2888562B1
- Authority
- FR
- France
- Prior art keywords
- input light
- aircraft engine
- platform input
- platform
- aircraft
- 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
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
- 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
-
- 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
- B64D15/14—De-icing or preventing icing on exterior surfaces of aircraft by electric heating controlled cyclically along length of surface
-
- 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
-
- 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
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Conditioning For Vehicles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US69921405P | 2005-07-14 | 2005-07-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2888562A1 FR2888562A1 (fr) | 2007-01-19 |
FR2888562B1 true FR2888562B1 (fr) | 2010-02-19 |
Family
ID=36926710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0606366A Active FR2888562B1 (fr) | 2005-07-14 | 2006-07-12 | Levre d'entree de nacelle pour moteur d'avion |
Country Status (4)
Country | Link |
---|---|
US (1) | US7780117B2 (fr) |
DE (1) | DE102006031330B4 (fr) |
FR (1) | FR2888562B1 (fr) |
GB (1) | GB2428275B (fr) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1866202B1 (fr) | 2005-04-04 | 2012-11-21 | Goodrich Corporation | Degivreur electrothermique et conducteur de resistance double fonction a utiliser dans cet appareil |
US8550402B2 (en) * | 2005-04-06 | 2013-10-08 | Sikorsky Aircraft Corporation | Dual-channel deicing system for a rotary wing aircraft |
US7940513B2 (en) * | 2005-07-18 | 2011-05-10 | Freescale Semiconductor, Inc. | Switch arrangement, integrated circuit, activation system |
US7633450B2 (en) * | 2005-11-18 | 2009-12-15 | Goodrich Corporation | Radar altering structure using specular patterns of conductive material |
FR2903074B1 (fr) * | 2006-06-28 | 2010-08-20 | Goodrich Corp | Procede de degivrage pour aeronef |
EP2066565B1 (fr) * | 2006-09-25 | 2010-11-24 | Rosemount Aerospace Inc. | Detection de particules de glace |
GB2450503A (en) * | 2007-06-26 | 2008-12-31 | Ultra Electronics Ltd | Ice protection system with plural heating elements |
FR2928625B1 (fr) * | 2008-03-14 | 2012-11-30 | Aircelle Sa | Dispositif de degivrage electrique |
US8006934B2 (en) * | 2008-03-31 | 2011-08-30 | United Technologies Corporation | Heating architecture for a composite fairing |
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. |
FR2935356B1 (fr) * | 2008-09-03 | 2010-08-27 | Aircelle Sa | Procede de fabrication d'un panneau acoustique d'une levre d'entree d'air d'une nacelle |
US20100123044A1 (en) * | 2008-11-17 | 2010-05-20 | Botura Galdemir C | Aircraft Ice Protection System |
US9004407B2 (en) * | 2008-12-24 | 2015-04-14 | Middle River Aircraft Systems | Anti-icing system and method for preventing ice accumulation |
FR2943038B1 (fr) * | 2009-03-13 | 2012-07-27 | Aircelle Sa | Dispositif de degivrage,notamment pour nacelle d'aeronef |
US9469408B1 (en) * | 2009-09-03 | 2016-10-18 | The Boeing Company | Ice protection system and method |
US8777163B2 (en) * | 2009-09-03 | 2014-07-15 | The Boeing Company | Ice protection system and method |
US20110233340A1 (en) * | 2010-03-29 | 2011-09-29 | Christy Daniel P | Aircraft ice protection system |
FR2966801B1 (fr) * | 2010-10-29 | 2012-11-02 | Aircelle Sa | Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef |
FR2976556B1 (fr) * | 2011-06-17 | 2013-12-27 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule |
US8869508B2 (en) | 2012-01-31 | 2014-10-28 | United Technologies Corporation | Gas turbine engine variable area fan nozzle control |
US9593628B2 (en) | 2012-01-31 | 2017-03-14 | United Technologies Corporation | Gas turbine engine variable area fan nozzle with ice management |
US20140014776A1 (en) * | 2012-07-13 | 2014-01-16 | Kelly Aerospace Thermal Systems Llc | System containing an electric heating element and method for installation and use thereof |
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 |
US9708072B2 (en) | 2014-04-30 | 2017-07-18 | The Boeing Company | Aircraft engine nacelle bulkheads and methods of assembling the same |
US9604438B2 (en) | 2014-04-30 | 2017-03-28 | The Boeing Company | Methods and apparatus for noise attenuation in an engine nacelle |
US9656761B2 (en) | 2014-04-30 | 2017-05-23 | The Boeing Company | Lipskin for a nacelle and methods of making the same |
US9938852B2 (en) * | 2014-04-30 | 2018-04-10 | The Boeing Company | Noise attenuating lipskin assembly and methods of assembling the same |
US10486821B2 (en) * | 2015-07-07 | 2019-11-26 | The Boeing Company | Jet engine anti-icing and noise-attenuating air inlets |
US10017262B2 (en) | 2015-09-22 | 2018-07-10 | Rohr, Inc. | Pulsed deicing system |
FR3041937B1 (fr) * | 2015-10-05 | 2017-10-20 | Airbus Operations Sas | Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure |
FR3045567B1 (fr) | 2015-12-21 | 2018-01-19 | Ratier Figeac | Dispositif de degivrage d'une pale d'helice, pale d'helice munie d'un tel dispositif, helice, turbomachine et aeronef |
US10384786B2 (en) | 2016-02-05 | 2019-08-20 | United Technologies Corporation | Thermally biased valve and anti-icing system |
US10189572B2 (en) * | 2016-05-02 | 2019-01-29 | The Boeing Company | Systems and methods for preventing ice formation on portions of an aircraft |
US9849992B2 (en) | 2016-05-23 | 2017-12-26 | United Technologies Corporation | Inline pressure regulating valve assembly with inlet pressure bias |
US10273884B2 (en) | 2016-06-09 | 2019-04-30 | Hamilton Sundstrand Corporation | Altitude compensating bleed valve |
US10450955B2 (en) | 2016-07-06 | 2019-10-22 | United Technologies Corporation | Nacelle anti ice system |
US20190360399A1 (en) * | 2018-05-25 | 2019-11-28 | Rolls-Royce Corporation | System and method to promote early and differential ice shedding |
EP3998212A1 (fr) * | 2021-02-19 | 2022-05-18 | Lilium eAircraft GmbH | Aéronef doté d'un système antigivre et procédé de dégivrage d'un aéronef avec un système antigivre |
FR3123049A1 (fr) * | 2021-12-20 | 2022-11-25 | Airbus Operations | Système de protection électrique contre le givre d’une nacelle d’aéronef. |
CN115370482B (zh) * | 2022-10-24 | 2023-03-07 | 成都纵横大鹏无人机科技有限公司 | 一种飞行器进气装置及进气方法 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1117843A (en) * | 1966-02-25 | 1968-06-26 | Rolls Royce | Improvements relating to anti-icing heating apparatus |
US4540143A (en) * | 1983-08-04 | 1985-09-10 | The Boeing Company | Nacelle/wing assembly with wake control device |
US5000399A (en) * | 1990-02-23 | 1991-03-19 | General Electric Company | Variable contour annular air inlet for an aircraft engine nacelle |
GB9502905D0 (en) * | 1995-02-15 | 1995-04-05 | Dunlop Ltd | Ice protection device |
US5921502A (en) * | 1996-06-19 | 1999-07-13 | Cox & Company, Inc. | Hybrid ice-protection system for use on roughness-sensitive airfoils |
EP0872417A1 (fr) * | 1997-04-16 | 1998-10-21 | The B.F. Goodrich Company | Dégivreur hybride |
US6027075A (en) * | 1997-06-16 | 2000-02-22 | Trustees Of Dartmouth College | Systems and methods for modifying ice adhesion strength |
US6027078A (en) * | 1998-02-27 | 2000-02-22 | The Boeing Company | Method and apparatus using localized heating for laminar flow |
FR2779314B1 (fr) * | 1998-05-27 | 2000-08-04 | Eurocopter France | Dispositif de chauffage a elements resistifs d'un profil aerodynamique |
US6576115B2 (en) * | 1998-06-15 | 2003-06-10 | The Trustees Of Dartmouth College | Reduction of ice adhesion to land surfaces by electrolysis |
US6427946B1 (en) * | 1998-10-27 | 2002-08-06 | Trustees Of Dartmouth College | Systems and methods for modifying ice adhesion strength |
FR2837409B1 (fr) * | 2002-03-20 | 2004-06-04 | Airbus France | Procede de formage d'un secteur de levre d'entree d'air, dispositif pour sa mise en oeuvre et secteur ainsi obtenu |
GB0211800D0 (en) * | 2002-05-22 | 2002-07-03 | Short Brothers Plc | An ice protection system for aircraft structures |
US6845943B2 (en) * | 2002-10-22 | 2005-01-25 | The Boeing Company | Apparatuses and methods for preventing foreign object damage to aircraft engines |
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 |
US6910327B2 (en) * | 2003-07-28 | 2005-06-28 | The Boeing Company | Apparatus and methods for varying inlet lip geometry of a jet engine inlet |
US7131612B2 (en) * | 2003-07-29 | 2006-11-07 | Pratt & Whitney Canada Corp. | Nacelle inlet lip anti-icing with engine oil |
JP2008546945A (ja) * | 2005-06-22 | 2008-12-25 | エアバス・フランス | 抵抗マットを有する航空機エンジン室用の防氷および除氷システム |
-
2006
- 2006-07-06 DE DE102006031330.5A patent/DE102006031330B4/de active Active
- 2006-07-10 GB GB0613616A patent/GB2428275B/en active Active
- 2006-07-11 US US11/456,629 patent/US7780117B2/en active Active
- 2006-07-12 FR FR0606366A patent/FR2888562B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
GB2428275A (en) | 2007-01-24 |
FR2888562A1 (fr) | 2007-01-19 |
GB0613616D0 (en) | 2006-08-16 |
DE102006031330A1 (de) | 2007-02-22 |
US20070102582A1 (en) | 2007-05-10 |
GB2428275B (en) | 2011-04-06 |
US7780117B2 (en) | 2010-08-24 |
DE102006031330B4 (de) | 2014-03-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2888562B1 (fr) | Levre d'entree de nacelle pour moteur d'avion | |
FR2906568B1 (fr) | Structure d'entree d'air deposable pour nacelle de turboreacteur. | |
FR2891244B1 (fr) | Mat d'accrochage de moteur pour aeronef | |
FR2891251B1 (fr) | Mat d'accrochage de moteur pour aeronef | |
FR2887852B1 (fr) | Mat d'accrochage de moteur pour aeronef | |
FR2905932B1 (fr) | Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef | |
FR2868041B1 (fr) | Suspension d'un moteur d'avion | |
FR2855495B1 (fr) | Dispositif d'accrochage avant de moteur d'avion | |
FR2874370B1 (fr) | Aile d'avion | |
FR2925607B1 (fr) | Nacelle pour moteur d'aeronef a tuyere de section variable | |
FR2941673B1 (fr) | Ensemble de suspension pour turboreacteur d'aeronef | |
DE602005011089D1 (de) | Motorhaube | |
FR2943331B1 (fr) | Atelier de preparation de moteurs d'avion pour leur expedition | |
BRPI0814498A2 (pt) | "dispositivo de acoplamento, nacele de motor turbojato e aeronave" | |
FR2908827B1 (fr) | Cone d'entree pour turbomachine | |
FR2900906B1 (fr) | Systeme de fixation tolerant aux dommages pour moteur d'aeronef | |
FR2869874B1 (fr) | Moteur d'avion avec des moyens de suspension a la structure d'un avion | |
FR2913061B1 (fr) | Systeme de deshuilage pour moteur d'aeronef. | |
FR2915460B1 (fr) | Architecture d'avion autonome pour le transport et le remplacement des moteurs de propulsion | |
FR2889505B1 (fr) | Structure primaire de mat de moteur d'aeronef perfectionnee | |
FR2885878B1 (fr) | Ensemble moteur pour aeronef | |
FR2936778B1 (fr) | Agencement d'entree d'air pour aeronef | |
FR2875971B1 (fr) | Convertisseur alternatif-continu pour l'aeronautique | |
FR2923263B1 (fr) | Turbomoteur comportant des moyens pour chauffer l'air entrant dans la turbine libre | |
FR2927609B1 (fr) | Entree d'air pour nacelle d'aeronef, et nacelle equipee d'une telle entree d'air |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
PLFP | Fee payment |
Year of fee payment: 18 |