FR3032369B1 - Procede de realisation de panneau a raidissement croise, en particulier pour architecture d'avion, et structure d'avion formee a partir d'un tel panneau - Google Patents
Procede de realisation de panneau a raidissement croise, en particulier pour architecture d'avion, et structure d'avion formee a partir d'un tel panneauInfo
- Publication number
- FR3032369B1 FR3032369B1 FR1550944A FR1550944A FR3032369B1 FR 3032369 B1 FR3032369 B1 FR 3032369B1 FR 1550944 A FR1550944 A FR 1550944A FR 1550944 A FR1550944 A FR 1550944A FR 3032369 B1 FR3032369 B1 FR 3032369B1
- Authority
- FR
- France
- Prior art keywords
- panel
- aircraft
- making
- cross
- structure formed
- 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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- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/006—Vehicles
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1550944A FR3032369B1 (fr) | 2015-02-06 | 2015-02-06 | Procede de realisation de panneau a raidissement croise, en particulier pour architecture d'avion, et structure d'avion formee a partir d'un tel panneau |
PCT/EP2016/052483 WO2016124730A1 (fr) | 2015-02-06 | 2016-02-05 | Procede de realisation de panneau a raidissement croise par soudage par friction malaxage et structure d'avion formee a partir d'un tel panneau |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1550944A FR3032369B1 (fr) | 2015-02-06 | 2015-02-06 | Procede de realisation de panneau a raidissement croise, en particulier pour architecture d'avion, et structure d'avion formee a partir d'un tel panneau |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3032369A1 FR3032369A1 (fr) | 2016-08-12 |
FR3032369B1 true FR3032369B1 (fr) | 2017-08-11 |
Family
ID=52824494
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1550944A Active FR3032369B1 (fr) | 2015-02-06 | 2015-02-06 | Procede de realisation de panneau a raidissement croise, en particulier pour architecture d'avion, et structure d'avion formee a partir d'un tel panneau |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3032369B1 (fr) |
WO (1) | WO2016124730A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3124101A1 (fr) * | 2021-06-17 | 2022-12-23 | Latecoere | Procédés de production d’un panneau structural raidi d’aéronef par soudage FSW |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4056587B2 (ja) * | 1997-07-07 | 2008-03-05 | 昭和電工株式会社 | 摩擦撹拌接合による継手の形成方法 |
JP2001047260A (ja) * | 1999-08-06 | 2001-02-20 | Mitsubishi Heavy Ind Ltd | 長手方向に断面形状が変化している部材の製造方法、その製造方法により製造された部材およびその部材を用いた航空機 |
DE10007995C2 (de) | 2000-02-22 | 2002-03-07 | Airbus Gmbh | Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils |
JP4227886B2 (ja) * | 2003-11-27 | 2009-02-18 | 三菱重工業株式会社 | 摩擦攪拌接合用の金属板材の表面処理方法、表面処理金属板材、及び摩擦攪拌接合方法 |
US7159822B2 (en) | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
US20100006622A1 (en) * | 2008-07-10 | 2010-01-14 | Smith Christopher B | Self-clamping friction stir welding device |
-
2015
- 2015-02-06 FR FR1550944A patent/FR3032369B1/fr active Active
-
2016
- 2016-02-05 WO PCT/EP2016/052483 patent/WO2016124730A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2016124730A1 (fr) | 2016-08-11 |
FR3032369A1 (fr) | 2016-08-12 |
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