ATE552928T1 - Geformte strukturelle anordnung und zugehöriges herstellungsverfahren - Google Patents
Geformte strukturelle anordnung und zugehöriges herstellungsverfahrenInfo
- Publication number
- ATE552928T1 ATE552928T1 AT05808363T AT05808363T ATE552928T1 AT E552928 T1 ATE552928 T1 AT E552928T1 AT 05808363 T AT05808363 T AT 05808363T AT 05808363 T AT05808363 T AT 05808363T AT E552928 T1 ATE552928 T1 AT E552928T1
- Authority
- AT
- Austria
- Prior art keywords
- assembly
- support member
- skin member
- members
- skin
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title 1
- 239000012530 fluid Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
Classifications
-
- 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
- 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
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
- B21D26/055—Blanks having super-plastic properties
-
- 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
- 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
- B23K2103/14—Titanium or alloys thereof
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12361—All metal or with adjacent metals having aperture or cut
- Y10T428/12368—Struck-out portion type
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/970,151 US7210611B2 (en) | 2004-10-21 | 2004-10-21 | Formed structural assembly and associated preform and method |
| PCT/US2005/036198 WO2006047066A1 (en) | 2004-10-21 | 2005-10-06 | Formed structural assembly and associated preform and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE552928T1 true ATE552928T1 (de) | 2012-04-15 |
Family
ID=35810164
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05808363T ATE552928T1 (de) | 2004-10-21 | 2005-10-06 | Geformte strukturelle anordnung und zugehöriges herstellungsverfahren |
Country Status (4)
| Country | Link |
|---|---|
| US (3) | US7210611B2 (de) |
| EP (1) | EP1809431B1 (de) |
| AT (1) | ATE552928T1 (de) |
| WO (1) | WO2006047066A1 (de) |
Families Citing this family (39)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7416105B2 (en) * | 2005-05-06 | 2008-08-26 | The Boeing Company | Superplastically forming of friction welded structural assemblies |
| DE102006002248B4 (de) * | 2006-01-17 | 2008-01-03 | Airbus Deutschland Gmbh | Strukturgebende Konstruktion für einen Flugzeugrumpf |
| FR2904604B1 (fr) * | 2006-08-04 | 2009-02-27 | Airbus France Sas | Element de structure d'un aeronef |
| US20080308197A1 (en) * | 2007-06-15 | 2008-12-18 | United Technologies Corporation | Secondary processing of structures derived from AL-RE-TM alloys |
| US20080311421A1 (en) * | 2007-06-15 | 2008-12-18 | United Technologies Corporation | Friction stir welded structures derived from AL-RE-TM alloys |
| US20100068550A1 (en) * | 2007-06-15 | 2010-03-18 | United Technologies Corporation | Hollow structures formed with friction stir welding |
| US20080308610A1 (en) * | 2007-06-15 | 2008-12-18 | United Technologies Corporation | Hollow structures formed with friction stir welding |
| US8100361B2 (en) * | 2007-12-20 | 2012-01-24 | Airbus Deutschland Gmbh | Hull structure |
| US8757540B2 (en) * | 2008-06-30 | 2014-06-24 | Pratt & Whitney Canada Corp. | Nacelle inlet lip |
| US20100050726A1 (en) * | 2008-08-29 | 2010-03-04 | The Boeing Company | Superplastically Continuous Roll Forming Titanium |
| US10843291B2 (en) * | 2008-11-15 | 2020-11-24 | The Boeing Company | Welding in preparation for superplastic forming |
| FR2943317B1 (fr) * | 2009-03-20 | 2012-11-16 | Eads Europ Aeronautic Defence | Procede de fabrication d'une levre d'entree d'air pour nacelle d'aeronef |
| US9221120B2 (en) * | 2012-01-04 | 2015-12-29 | United Technologies Corporation | Aluminum fan blade construction with welded cover |
| US10215027B2 (en) | 2012-01-04 | 2019-02-26 | United Technologies Corporation | Aluminum fan blade construction with welded cover |
| US10315264B2 (en) | 2013-01-29 | 2019-06-11 | General Electric Company | Joining process and joined article |
| US20140212681A1 (en) * | 2013-01-29 | 2014-07-31 | General Electric Company | Joining process and joined article |
| US8844796B1 (en) * | 2013-03-05 | 2014-09-30 | The Boeing Company | Superplastically formed ultrasonically welded metallic structure |
| US9190094B2 (en) | 2013-04-04 | 2015-11-17 | Western Digital (Fremont) | Perpendicular recording media with grain isolation initiation layer and exchange breaking layer for signal-to-noise ratio enhancement |
| GB201312228D0 (en) * | 2013-07-08 | 2013-08-21 | Ludlow Michael | A lip skin and a method and apparatus for forming a lip skin |
| GB201318527D0 (en) * | 2013-10-21 | 2013-12-04 | Rolls Royce Plc | Hollow component manufacture |
| US9488067B2 (en) * | 2014-01-14 | 2016-11-08 | The Boeing Company | Aircraft anti-icing systems having deflector vanes |
| FR3020586B1 (fr) * | 2014-05-05 | 2017-01-06 | Acb | Procede de fabrication d'une piece de structure metallique |
| US9764849B2 (en) * | 2014-09-18 | 2017-09-19 | The Boeing Company | Method of attaching nacelle structure to minimize fatigue loading |
| FR3034690B1 (fr) * | 2015-04-09 | 2017-10-20 | Aurock | Procede de pilotage d'une machine de formage superplastique et machine correspondante |
| US9845728B2 (en) * | 2015-10-15 | 2017-12-19 | Rohr, Inc. | Forming a nacelle inlet for a turbine engine propulsion system |
| US10458275B2 (en) * | 2017-01-06 | 2019-10-29 | Rohr, Inc. | Nacelle inner lip skin with heat transfer augmentation features |
| DE102017102881A1 (de) | 2017-02-14 | 2018-08-16 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Verfahren für die Herstellung eines Mehrkomponentenbauteils eines Fahrzeugs |
| US10766626B2 (en) | 2017-05-24 | 2020-09-08 | The Boeing Company | Single-piece extended laminar flow inlet lipskin |
| US11020815B2 (en) | 2017-05-24 | 2021-06-01 | The Boeing Company | Single-piece extended laminar flow inlet lipskin |
| CA3072031A1 (en) * | 2017-08-22 | 2019-02-28 | Bae Systems Plc | Superplastic forming and diffusion bonding process |
| ES2947758T3 (es) * | 2017-08-22 | 2023-08-18 | Bae Systems Plc | Procedimiento de conformación superplástica y unión por difusión |
| FR3073206B1 (fr) * | 2017-11-08 | 2021-03-19 | Safran Nacelles | Procede de fabrication de panneau structural et/ou acoustique pour nacelle d'ensemble propulsif d'aeronef, et dispositif s'y rapportant |
| US10807143B2 (en) | 2018-04-02 | 2020-10-20 | Rohr, Inc | Tooling for forming nacelle components |
| US11433990B2 (en) | 2018-07-09 | 2022-09-06 | Rohr, Inc. | Active laminar flow control system with composite panel |
| CN109570738B (zh) * | 2019-02-12 | 2024-07-19 | 黄山学院 | 一种用于提高铜合金表层性能的搅拌头 |
| US11447228B2 (en) * | 2020-04-23 | 2022-09-20 | The Boeing Company | Methods of manufacture for aircraft substructure |
| US20220388090A1 (en) * | 2021-06-04 | 2022-12-08 | The Boeing Company | Fabrication of thick stock via diffusion bonding of titanium alloys |
| CN114309227B (zh) * | 2021-12-21 | 2024-04-05 | 北京星航机电装备有限公司 | 一种夹层部件的成形装置及成形方法 |
| EP4275835B1 (de) * | 2022-05-12 | 2024-12-04 | Creuzet Aeronautique | Verfahren zur herstellung einer einlasslippenhaut |
Family Cites Families (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3927817A (en) | 1974-10-03 | 1975-12-23 | Rockwell International Corp | Method for making metallic sandwich structures |
| US4087037A (en) * | 1976-07-09 | 1978-05-02 | Mcdonnell Douglas Corporation | Method of and tools for producing superplastically formed and diffusion bonded structures |
| US4117970A (en) | 1976-11-16 | 1978-10-03 | Rockwell International Corporation | Method for fabrication of honeycomb structures |
| US4181000A (en) | 1977-10-04 | 1980-01-01 | Rockwell International Corporation | Method for superplastic forming |
| US4217397A (en) | 1978-04-18 | 1980-08-12 | Mcdonnell Douglas Corporation | Metallic sandwich structure and method of fabrication |
| US4304821A (en) | 1978-04-18 | 1981-12-08 | Mcdonnell Douglas Corporation | Method of fabricating metallic sandwich structure |
| US4197978A (en) * | 1978-06-29 | 1980-04-15 | The Boeing Company | Method of making an integral structural member |
| US4294419A (en) * | 1979-01-22 | 1981-10-13 | Vought Corporation | Airframe assembly and process |
| US4811890A (en) | 1983-05-07 | 1989-03-14 | Rockwell International Corporation | Method of eliminating core distortion in diffusion bonded and uperplastically formed structures |
| US4603089A (en) | 1983-11-21 | 1986-07-29 | Rockwell International Corporation | Laser welding of sandwich structures |
| US4622445A (en) | 1984-09-28 | 1986-11-11 | The Boeing Company | Method of inductively brazing honeycomb panels |
| US4688745A (en) * | 1986-01-24 | 1987-08-25 | Rohr Industries, Inc. | Swirl anti-ice system |
| US5420400A (en) | 1991-10-15 | 1995-05-30 | The Boeing Company | Combined inductive heating cycle for sequential forming the brazing |
| US6211497B1 (en) | 1991-04-05 | 2001-04-03 | The Boeing Company | Induction consolidation system |
| US5410132A (en) | 1991-10-15 | 1995-04-25 | The Boeing Company | Superplastic forming using induction heating |
| US5118026A (en) | 1991-04-05 | 1992-06-02 | Rockwell International Corporation | Method for making titanium aluminide metallic sandwich structures |
| US5914064A (en) | 1991-10-15 | 1999-06-22 | The Boeing Company | Combined cycle for forming and annealing |
| US5705794A (en) | 1991-10-15 | 1998-01-06 | The Boeing Company | Combined heating cycles to improve efficiency in inductive heating operations |
| GB9125978D0 (en) | 1991-12-06 | 1992-02-05 | Welding Inst | Hot shear butt welding |
| JP3398246B2 (ja) * | 1995-02-24 | 2003-04-21 | 日本飛行機株式会社 | 金属サンドイッチ構造体およびその製造方法 |
| US5994666A (en) | 1996-01-12 | 1999-11-30 | The Boeing Company | Multisheet metal sandwich structures |
| US5866652A (en) * | 1996-02-27 | 1999-02-02 | The Boeing Company | Chromate-free protective coatings |
| US5946666A (en) * | 1996-05-21 | 1999-08-31 | Albert Einstein Healthcare Network | Monitoring device for financial securities |
| US5890285A (en) * | 1996-08-23 | 1999-04-06 | Mcdonnell Douglas Corporation | Method for superplastically forming a structural article |
| US6129261A (en) | 1996-09-26 | 2000-10-10 | The Boeing Company | Diffusion bonding of metals |
| JP3647612B2 (ja) * | 1997-07-24 | 2005-05-18 | 富士重工業株式会社 | 航空機の前縁構造及びその製造方法 |
| US6051325A (en) | 1997-12-23 | 2000-04-18 | Mcdonnell Douglas Corporation | Joining of machined sandwich assemblies by friction stir welding |
| US6180932B1 (en) | 1998-12-30 | 2001-01-30 | The Boeing Company | Brazing honeycomb panels with controlled net tooling pressure |
| US6337471B1 (en) | 1999-04-23 | 2002-01-08 | The Boeing Company | Combined superplastic forming and adhesive bonding |
| US6371411B1 (en) | 1999-11-23 | 2002-04-16 | The Boeing Company | Method and apparatus for aircraft inlet ice protection |
| JP4530495B2 (ja) | 2000-07-03 | 2010-08-25 | 富士重工業株式会社 | 超塑性材料の一体成形方法 |
| US6537682B2 (en) | 2001-03-27 | 2003-03-25 | The Boeing Company | Application of friction stir welding to superplastically formed structural assemblies |
| FR2834481B1 (fr) | 2002-01-10 | 2004-02-27 | Snecma Moteurs | Procede de fabrication de pieces par soudage par diffusion et par formage superplastique, et moule pour mettre en oeuvre un tel procede |
| US6528771B1 (en) | 2002-03-08 | 2003-03-04 | The Boeing Company | System and method for controlling an induction heating process |
| US6566635B1 (en) | 2002-03-08 | 2003-05-20 | The Boeing Company | Smart susceptor having a geometrically complex molding surface |
| US7533794B2 (en) * | 2004-03-31 | 2009-05-19 | The Boring Company | Superplastic forming and diffusion bonding of fine grain titanium |
| US7416105B2 (en) * | 2005-05-06 | 2008-08-26 | The Boeing Company | Superplastically forming of friction welded structural assemblies |
-
2004
- 2004-10-21 US US10/970,151 patent/US7210611B2/en not_active Expired - Lifetime
-
2005
- 2005-10-06 WO PCT/US2005/036198 patent/WO2006047066A1/en not_active Ceased
- 2005-10-06 AT AT05808363T patent/ATE552928T1/de active
- 2005-10-06 EP EP05808363A patent/EP1809431B1/de not_active Expired - Lifetime
-
2007
- 2007-03-16 US US11/687,244 patent/US7967240B2/en not_active Expired - Fee Related
-
2011
- 2011-06-27 US US13/169,632 patent/US8329312B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US20070175968A1 (en) | 2007-08-02 |
| US7210611B2 (en) | 2007-05-01 |
| US20110256343A1 (en) | 2011-10-20 |
| US7967240B2 (en) | 2011-06-28 |
| EP1809431A1 (de) | 2007-07-25 |
| WO2006047066A1 (en) | 2006-05-04 |
| US8329312B2 (en) | 2012-12-11 |
| US20060086774A1 (en) | 2006-04-27 |
| EP1809431B1 (de) | 2012-04-11 |
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