FR3055885B1 - Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride - Google Patents
Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride Download PDFInfo
- Publication number
- FR3055885B1 FR3055885B1 FR1658497A FR1658497A FR3055885B1 FR 3055885 B1 FR3055885 B1 FR 3055885B1 FR 1658497 A FR1658497 A FR 1658497A FR 1658497 A FR1658497 A FR 1658497A FR 3055885 B1 FR3055885 B1 FR 3055885B1
- Authority
- FR
- France
- Prior art keywords
- flange
- engine
- connection
- air intake
- aircraft nacelle
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
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- 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
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- 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
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- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1658497A FR3055885B1 (fr) | 2016-09-13 | 2016-09-13 | Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1658497 | 2016-09-13 | ||
FR1658497A FR3055885B1 (fr) | 2016-09-13 | 2016-09-13 | Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3055885A1 FR3055885A1 (fr) | 2018-03-16 |
FR3055885B1 true FR3055885B1 (fr) | 2022-06-03 |
Family
ID=57396628
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1658497A Active FR3055885B1 (fr) | 2016-09-13 | 2016-09-13 | Nacelle d'aeronef comprenant une liaison entre une entree d'air et une motorisation qui comporte une bride |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3055885B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3083214A1 (fr) * | 2018-06-28 | 2020-01-03 | Airbus Operations | Nacelle d'un ensemble propulsif d'aeronef comportant une pluralite d'elements amortisseurs entre une partie avant et une partie principale, et ensemble propulsif d'aeronef associe |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6920958B2 (en) * | 2003-10-17 | 2005-07-26 | The Boeing Company | Annular acoustic panel |
FR2903732B1 (fr) * | 2006-07-12 | 2008-09-12 | Airbus France Sas | Entree d'air pour turbomoteur d'aeronef. |
US7871486B2 (en) * | 2006-11-21 | 2011-01-18 | General Electric Company | Methods for making structures having mounting flanges |
FR2998547B1 (fr) * | 2012-11-23 | 2016-01-29 | Airbus Operations Sas | Nacelle d'aeronef comprenant une liaison deformable entre une entree d'air et une motorisation |
-
2016
- 2016-09-13 FR FR1658497A patent/FR3055885B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3055885A1 (fr) | 2018-03-16 |
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