FR2943317B1 - METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLE - Google Patents
METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLEInfo
- Publication number
- FR2943317B1 FR2943317B1 FR0951808A FR0951808A FR2943317B1 FR 2943317 B1 FR2943317 B1 FR 2943317B1 FR 0951808 A FR0951808 A FR 0951808A FR 0951808 A FR0951808 A FR 0951808A FR 2943317 B1 FR2943317 B1 FR 2943317B1
- Authority
- FR
- France
- Prior art keywords
- launcher
- air inlet
- aircraft nacelle
- manufacturing air
- manufacturing
- 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
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/84—Making other particular articles other parts for engines, e.g. connecting-rods
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/92—Making other particular articles other parts for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/122—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding using a non-consumable tool, e.g. friction stir welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/08—Non-ferrous metals or alloys
- B23K2103/10—Aluminium or alloys thereof
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0951808A FR2943317B1 (en) | 2009-03-20 | 2009-03-20 | METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0951808A FR2943317B1 (en) | 2009-03-20 | 2009-03-20 | METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2943317A1 FR2943317A1 (en) | 2010-09-24 |
FR2943317B1 true FR2943317B1 (en) | 2012-11-16 |
Family
ID=41278406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0951808A Expired - Fee Related FR2943317B1 (en) | 2009-03-20 | 2009-03-20 | METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2943317B1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012098810A1 (en) * | 2011-01-19 | 2012-07-26 | 日本軽金属株式会社 | Rotary tool unit, friction stir welding method, double-skin panel assembly, and friction stir welding method for double-skin panel assembly |
US9845728B2 (en) * | 2015-10-15 | 2017-12-19 | Rohr, Inc. | Forming a nacelle inlet for a turbine engine propulsion system |
US11433990B2 (en) | 2018-07-09 | 2022-09-06 | Rohr, Inc. | Active laminar flow control system with composite panel |
FR3089442B1 (en) * | 2018-12-05 | 2020-12-18 | Airbus Operations Sas | A method of assembling at least two parts by transparency welding, a method of assembling a primary structure of an aircraft mast by transparency welding, the primary structure of an aircraft mast thus obtained and an aircraft comprising said primary structure |
FR3115222B1 (en) * | 2020-10-21 | 2023-05-12 | Safran Nacelles | Manufacture of annular sectors for the production of an air inlet lip |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9125978D0 (en) * | 1991-12-06 | 1992-02-05 | Welding Inst | Hot shear butt welding |
US6955283B2 (en) * | 2003-09-08 | 2005-10-18 | The Boeing Company | Adaptable mandrel for spin forming |
US7210611B2 (en) * | 2004-10-21 | 2007-05-01 | The Boeing Company | Formed structural assembly and associated preform and method |
US7416105B2 (en) * | 2005-05-06 | 2008-08-26 | The Boeing Company | Superplastically forming of friction welded structural assemblies |
-
2009
- 2009-03-20 FR FR0951808A patent/FR2943317B1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2943317A1 (en) | 2010-09-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2935356B1 (en) | METHOD FOR MANUFACTURING AN ACOUSTIC PANEL OF AN AIR INLET LAUNCHER OF A NACELLE | |
BRPI0821807A2 (en) | aircraft cooling system | |
BRPI1012630A2 (en) | supersonic cooling system | |
FR2953812B1 (en) | PROCESS FOR REPAIRING AN AIRCRAFT FUSELAGE | |
BR112012005978A2 (en) | "air particle filtration method" | |
SG10201401265XA (en) | Integrated Building Based Air Handler For Server Farm Cooling System | |
BRPI1014791A2 (en) | "high speed electrical system" | |
FR2942566B1 (en) | METHOD FOR MANAGING THE FLIGHT OF AN AIRCRAFT | |
BR112012000954A2 (en) | turbocharger set with a cooling system | |
BRPI0916416A2 (en) | floating turbine system | |
BRPI1015981A2 (en) | pressure controlled wind turbine boost system | |
IT1394227B1 (en) | AIR ROBOTIC SYSTEM | |
FR2960216B1 (en) | AERODYNAMIC ELEMENT FOR AN AIRCRAFT NACELLE | |
FR2941743B1 (en) | AIR STARTER FOR TURBOMACHINE. | |
FR2941648B1 (en) | METHOD FOR MANUFACTURING ALVEOLAR STRUCTURE FOR A TURBOJET NACELLE | |
FR2944125B1 (en) | METHOD FOR IDENTIFYING AERODYNAMIC MODELS FOR AIRCRAFT SIMULATION METHOD | |
FR2933375B1 (en) | AIR FUSELAGE ARRANGEMENT | |
BRPI0809967A2 (en) | GAS PUMP METHOD BY SUPERSONIC CENTRIFUGAL PUMP | |
FR2936778B1 (en) | AIR INTAKE ARRANGEMENT FOR AIRCRAFT | |
FR2980836B1 (en) | HEAT EXCHANGER FORMING AIRCRAFTS PRE-COOLANT | |
FR2943317B1 (en) | METHOD FOR MANUFACTURING AIR INLET LAUNCHER FOR AN AIRCRAFT NACELLE | |
BR112012001083A2 (en) | gas turbine exhaust gas cooling system | |
FR2981733B1 (en) | AIRCRAFT TURBOMACHINE COMBUSTION CHAMBER MODULE AND METHOD FOR DESIGNING THE SAME | |
FR2957339B1 (en) | METHOD FOR MANUFACTURING AN ELECTROMECHANICAL MICROSYSTEM | |
FR2966531B1 (en) | METHOD FOR CONTROLLING A TURBOMACHINE |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
ST | Notification of lapse |
Effective date: 20231105 |