FR2940377B1 - Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces - Google Patents
Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des piecesInfo
- Publication number
- FR2940377B1 FR2940377B1 FR0807350A FR0807350A FR2940377B1 FR 2940377 B1 FR2940377 B1 FR 2940377B1 FR 0807350 A FR0807350 A FR 0807350A FR 0807350 A FR0807350 A FR 0807350A FR 2940377 B1 FR2940377 B1 FR 2940377B1
- Authority
- FR
- France
- Prior art keywords
- preserving
- integrity
- assembly
- parts
- workpieces connected
- 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
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
- 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
-
- 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
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/14—Casings or housings protecting or supporting assemblies within
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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)
- Laminated Bodies (AREA)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0807350A FR2940377B1 (fr) | 2008-12-22 | 2008-12-22 | Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces |
RU2011106595/06A RU2521824C2 (ru) | 2008-07-30 | 2009-07-28 | Узел из элементов, соединенных посредством устройства, обеспечивающего целостность поверхности одного из элементов |
BRPI0914134A BRPI0914134A2 (pt) | 2008-07-30 | 2009-07-28 | conjunto de componentes e estrutura de entrada de ar |
ES09784308T ES2425078T3 (es) | 2008-07-30 | 2009-07-28 | Estructura de entrada de aire de góndola de turborreactor con desescarchado neumático |
US13/056,727 US8840059B2 (en) | 2008-07-30 | 2009-07-28 | Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
EP20090784308 EP2321510B1 (fr) | 2008-07-30 | 2009-07-28 | Structure d'entrée d'air de nacelle de turboréacteur à dégivrage pneumatique |
CA 2732351 CA2732351A1 (fr) | 2008-07-30 | 2009-07-28 | Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces |
PCT/FR2009/000934 WO2010012899A2 (fr) | 2008-07-30 | 2009-07-28 | Ensemble de pièces reliées entre elles par un dispositif permettant de conserver l'intégrité de la surface de l'une des pièces |
CN200980127934.9A CN102099556B (zh) | 2008-07-30 | 2009-07-28 | 具有气动除冰功能的用于涡轮喷气发动机舱的进气口结构 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0807350A FR2940377B1 (fr) | 2008-12-22 | 2008-12-22 | Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2940377A1 FR2940377A1 (fr) | 2010-06-25 |
FR2940377B1 true FR2940377B1 (fr) | 2012-12-28 |
Family
ID=40995645
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0807350A Expired - Fee Related FR2940377B1 (fr) | 2008-07-30 | 2008-12-22 | Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2940377B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966127B1 (fr) | 2010-10-15 | 2013-06-14 | Airbus Operations Sas | Nacelle d'aeronef incorporant au moins une cloison radiale entre deux conduits |
US9764847B2 (en) * | 2013-10-18 | 2017-09-19 | The Boeing Company | Anti-icing system for aircraft |
US20160084108A1 (en) * | 2014-09-24 | 2016-03-24 | Honeywell International Inc. | Nacelle inlet and engine fan housing assembly and method for making same |
FR3039509B1 (fr) | 2015-07-28 | 2017-12-22 | Thales Sa | Rechauffage pour equipement aeronautique pour un aeronef |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3481427A (en) * | 1968-11-29 | 1969-12-02 | Mc Donnell Douglas Corp | Acoustical panel structure |
US4240250A (en) * | 1977-12-27 | 1980-12-23 | The Boeing Company | Noise reducing air inlet for gas turbine engines |
US4235303A (en) * | 1978-11-20 | 1980-11-25 | The Boeing Company | Combination bulk absorber-honeycomb acoustic panels |
GB2112339B (en) * | 1981-11-13 | 1985-07-03 | T K S | Porous panel |
US7318499B2 (en) * | 2004-02-20 | 2008-01-15 | Honeywell International, Inc. | Noise suppression structure and method of making the same |
FR2869360B1 (fr) * | 2004-04-27 | 2006-07-14 | Airbus France Sas | Ensemble reducteur de bruit pour turboreacteur d'aeronef |
FR2906568B1 (fr) * | 2006-10-02 | 2012-01-06 | Aircelle Sa | Structure d'entree d'air deposable pour nacelle de turboreacteur. |
-
2008
- 2008-12-22 FR FR0807350A patent/FR2940377B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2940377A1 (fr) | 2010-06-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20150831 |