FR2887518B1 - Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee - Google Patents
Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimiseeInfo
- Publication number
- FR2887518B1 FR2887518B1 FR0551711A FR0551711A FR2887518B1 FR 2887518 B1 FR2887518 B1 FR 2887518B1 FR 0551711 A FR0551711 A FR 0551711A FR 0551711 A FR0551711 A FR 0551711A FR 2887518 B1 FR2887518 B1 FR 2887518B1
- Authority
- FR
- France
- Prior art keywords
- aircraft engine
- engine nacelle
- defrosting device
- acoustical attenuation
- improved defrosting
- 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
- 238000010257 thawing Methods 0.000 title 1
Classifications
-
- 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
- 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
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- 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
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0551711A FR2887518B1 (fr) | 2005-06-22 | 2005-06-22 | Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee |
CA2611656A CA2611656C (fr) | 2005-06-22 | 2006-06-19 | Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
CN2006800225329A CN101203424B (zh) | 2005-06-22 | 2006-06-19 | 飞行器发动机舱及其解冻系统以及该系统的操控方法 |
PCT/FR2006/050608 WO2006136748A2 (fr) | 2005-06-22 | 2006-06-19 | Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
DE602006018005T DE602006018005D1 (de) | 2005-06-22 | 2006-06-19 | Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte |
EP06778954A EP1893484B1 (fr) | 2005-06-22 | 2006-06-19 | Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
RU2008102234/11A RU2411161C2 (ru) | 2005-06-22 | 2006-06-19 | Система защиты от обледенения и борьбы с обледенением гондолы двигателя летательного аппарата, содержащая резистивный слой |
BRPI0612110-1A BRPI0612110A2 (pt) | 2005-06-22 | 2006-06-19 | sistema de remoção de gelo e de anti-formação de gelo de nacela de motor de aeronave, nacela de motor de aeronave, e, processo de comando de um sistema de remoção de gelo e de anti-formação de gelo |
JP2008517556A JP2008546945A (ja) | 2005-06-22 | 2006-06-19 | 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 |
US11/993,693 US20100199629A1 (en) | 2005-06-22 | 2006-06-19 | Systeme d'anti givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
AT06778954T ATE486779T1 (de) | 2005-06-22 | 2006-06-19 | Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0551711A FR2887518B1 (fr) | 2005-06-22 | 2005-06-22 | Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2887518A1 FR2887518A1 (fr) | 2006-12-29 |
FR2887518B1 true FR2887518B1 (fr) | 2008-10-10 |
Family
ID=35614197
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0551711A Expired - Fee Related FR2887518B1 (fr) | 2005-06-22 | 2005-06-22 | Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2887518B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2912781B1 (fr) * | 2007-02-20 | 2009-04-10 | Airbus France Sas | Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud |
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 |
FR3060651B1 (fr) * | 2016-12-20 | 2020-11-06 | Airbus Operations Sas | Structure d'entree d'air pour une nacelle d'aeronef |
FR3085437B1 (fr) | 2018-09-05 | 2020-11-20 | Airbus Operations Sas | Structure d’entree d’air d’une nacelle d’aeronef |
CN113955124B (zh) * | 2021-11-05 | 2024-02-13 | 天津航空机电有限公司 | 一种嵌入式进气道唇口防冰加热组件及制作方法 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2259287B (en) * | 1991-09-04 | 1994-08-10 | Rolls Royce Plc | Apparatus for de-icing a surface and method of using the same |
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
- 2005-06-22 FR FR0551711A patent/FR2887518B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2887518A1 (fr) | 2006-12-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
ST | Notification of lapse |
Effective date: 20220205 |