FR2960856B1 - Cadre arriere d'une nacelle d'aeronef - Google Patents
Cadre arriere d'une nacelle d'aeronefInfo
- Publication number
- FR2960856B1 FR2960856B1 FR1054433A FR1054433A FR2960856B1 FR 2960856 B1 FR2960856 B1 FR 2960856B1 FR 1054433 A FR1054433 A FR 1054433A FR 1054433 A FR1054433 A FR 1054433A FR 2960856 B1 FR2960856 B1 FR 2960856B1
- Authority
- FR
- France
- Prior art keywords
- rear frame
- aircraft nacelle
- nacelle
- aircraft
- frame
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
-
- 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 (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054433A FR2960856B1 (fr) | 2010-06-07 | 2010-06-07 | Cadre arriere d'une nacelle d'aeronef |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054433A FR2960856B1 (fr) | 2010-06-07 | 2010-06-07 | Cadre arriere d'une nacelle d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2960856A1 FR2960856A1 (fr) | 2011-12-09 |
FR2960856B1 true FR2960856B1 (fr) | 2012-06-22 |
Family
ID=43464605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1054433A Active FR2960856B1 (fr) | 2010-06-07 | 2010-06-07 | Cadre arriere d'une nacelle d'aeronef |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2960856B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2998548B1 (fr) * | 2012-11-23 | 2015-01-30 | Airbus Operations Sas | Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation |
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 |
FR3087489B1 (fr) * | 2018-10-18 | 2022-12-09 | Airbus Operations Sas | Partie anterieure de nacelle de groupe propulsif d'aeronef comportant une voie principale de propagation d'efforts entre une levre d'entree d'air et une peau arriere d'un panneau acoustique |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2787509B1 (fr) * | 1998-12-21 | 2001-03-30 | Aerospatiale | Structure d'entree d'air pour moteur d'aeronef |
US6920958B2 (en) * | 2003-10-17 | 2005-07-26 | The Boeing Company | Annular acoustic panel |
FR2868124B1 (fr) * | 2004-03-29 | 2006-06-23 | Airbus France Sas | Structure d'entree d'air pour moteur d'aeronef |
FR2868123B1 (fr) * | 2004-03-29 | 2006-06-23 | Airbus France Sas | Structure d'entree d'air pour moteur d'aeronef |
-
2010
- 2010-06-07 FR FR1054433A patent/FR2960856B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2960856A1 (fr) | 2011-12-09 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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