FR2998548B1 - Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation - Google Patents
Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisationInfo
- Publication number
- FR2998548B1 FR2998548B1 FR1261170A FR1261170A FR2998548B1 FR 2998548 B1 FR2998548 B1 FR 2998548B1 FR 1261170 A FR1261170 A FR 1261170A FR 1261170 A FR1261170 A FR 1261170A FR 2998548 B1 FR2998548 B1 FR 2998548B1
- Authority
- FR
- France
- Prior art keywords
- motorization
- air inlet
- aircraft nacelle
- reinforced connection
- reinforced
- 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
- 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
-
- 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
-
- 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
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1261170A FR2998548B1 (fr) | 2012-11-23 | 2012-11-23 | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
US14/084,691 US20140147270A1 (en) | 2012-11-23 | 2013-11-20 | Aircraft Nacelle Comprising A Reinforced Connection Between An Air Intake And A Means Of Propulsion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1261170A FR2998548B1 (fr) | 2012-11-23 | 2012-11-23 | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2998548A1 FR2998548A1 (fr) | 2014-05-30 |
FR2998548B1 true FR2998548B1 (fr) | 2015-01-30 |
Family
ID=47599004
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1261170A Active FR2998548B1 (fr) | 2012-11-23 | 2012-11-23 | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
Country Status (2)
Country | Link |
---|---|
US (1) | US20140147270A1 (fr) |
FR (1) | FR2998548B1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3016159B1 (fr) * | 2014-01-03 | 2016-01-01 | Airbus Operations Sas | Nacelle de turboreacteur d'aeronef comprenant un ensemble d'entree d'air a rigidite augmentee |
FR3055922B1 (fr) * | 2016-09-13 | 2020-06-19 | Airbus Operations | Ensemble propulsif d'aeronef comprenant une liaison entre une entree d'air et une motorisation |
FR3075761A1 (fr) * | 2017-12-21 | 2019-06-28 | Airbus Operations | Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline |
FR3075759B1 (fr) * | 2017-12-21 | 2020-11-06 | Airbus Operations Sas | Partie anterieure de nacelle d'un ensemble propulsif d'aeronef comportant un element amortisseur |
FR3095418B1 (fr) | 2019-04-26 | 2021-09-24 | Safran Nacelles | Entrée d’air de nacelle et nacelle comportant une telle entrée d’air |
FR3095417B1 (fr) | 2019-04-26 | 2021-09-24 | Safran Nacelles | Entrée d’air de nacelle et nacelle comportant une telle entrée d’air |
BR102022003769A2 (pt) * | 2021-05-04 | 2022-11-16 | The Boeing Company | Estrutura de entrada de nacele de um conjunto de motor |
US11852022B2 (en) * | 2021-06-10 | 2023-12-26 | William Maxwell | Retaining ejected gas turbine blades |
US11346242B1 (en) * | 2021-06-10 | 2022-05-31 | William Maxwell | Retaining ejected gas turbine blades |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5114100A (en) * | 1989-12-29 | 1992-05-19 | The Boeing Company | Anti-icing system for aircraft |
US5000399A (en) * | 1990-02-23 | 1991-03-19 | General Electric Company | Variable contour annular air inlet for an aircraft engine nacelle |
US6706406B1 (en) * | 1996-11-13 | 2004-03-16 | Fern Investments Limited | Composite steel structural plastic sandwich plate systems |
US6945727B2 (en) * | 2002-07-19 | 2005-09-20 | The Boeing Company | Apparatuses and methods for joining structural members, such as composite structural members |
US7244487B2 (en) * | 2003-04-24 | 2007-07-17 | Lockheed Martin Corporation | Apparatus, system, and method of joining structural components with a tapered tension bond joint |
FR2856379B1 (fr) * | 2003-06-18 | 2006-11-24 | Airbus France | Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit |
US6920958B2 (en) * | 2003-10-17 | 2005-07-26 | The Boeing Company | Annular acoustic panel |
US20060145001A1 (en) * | 2004-12-30 | 2006-07-06 | Smith Matthew C | Fan cowl door elimination |
FR2903732B1 (fr) * | 2006-07-12 | 2008-09-12 | Airbus France Sas | Entree d'air pour turbomoteur d'aeronef. |
US7721525B2 (en) * | 2006-07-19 | 2010-05-25 | Rohr, Inc. | Aircraft engine inlet having zone of deformation |
FR2904604B1 (fr) * | 2006-08-04 | 2009-02-27 | Airbus France Sas | Element de structure d'un aeronef |
US8082667B2 (en) * | 2007-05-31 | 2011-12-27 | The Boeing Company | Apparatus and methods for securing a first structural member and a second structural member to one another |
DE102007044388B4 (de) * | 2007-09-18 | 2012-08-02 | Airbus Operations Gmbh | Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs |
US8197191B2 (en) * | 2009-04-14 | 2012-06-12 | Rohr, Inc. | Inlet section of an aircraft engine nacelle |
FR2960856B1 (fr) * | 2010-06-07 | 2012-06-22 | Airbus Operations Sas | Cadre arriere d'une nacelle d'aeronef |
FR2966126B1 (fr) * | 2010-10-15 | 2013-06-28 | Airbus Operations Sas | Nacelle d'aeronef incorporant un cadre arriere incline vers l'arriere |
CA2820004C (fr) * | 2010-12-28 | 2016-02-16 | Bell Helicopter Textron Inc. | Systeme d'assemblage a charge multidirectionnelle |
-
2012
- 2012-11-23 FR FR1261170A patent/FR2998548B1/fr active Active
-
2013
- 2013-11-20 US US14/084,691 patent/US20140147270A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
FR2998548A1 (fr) | 2014-05-30 |
US20140147270A1 (en) | 2014-05-29 |
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