ATE552928T1 - Geformte strukturelle anordnung und zugehöriges herstellungsverfahren - Google Patents

Geformte strukturelle anordnung und zugehöriges herstellungsverfahren

Info

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
Application number
AT05808363T
Other languages
English (en)
Inventor
Daniel Sanders
Jeff Will
Luis Leon
David Foutch
Gregory Ramsey
Garry Booker
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE552928T1 publication Critical patent/ATE552928T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-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
    • B23K20/122Non-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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping 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
    • B21D26/053Shaping 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
    • B21D26/055Blanks having super-plastic properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/08Non-ferrous metals or alloys
    • B23K2103/10Aluminium or alloys thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/08Non-ferrous metals or alloys
    • B23K2103/14Titanium or alloys thereof
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12361All metal or with adjacent metals having aperture or cut
    • Y10T428/12368Struck-out portion type
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273Structurally 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)
AT05808363T 2004-10-21 2005-10-06 Geformte strukturelle anordnung und zugehöriges herstellungsverfahren ATE552928T1 (de)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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

Similar Documents

Publication Publication Date Title
ATE552928T1 (de) Geformte strukturelle anordnung und zugehöriges herstellungsverfahren
CA128432S (en) Cross brace for a table
MX2018006983A (es) Metodo para producir una parte interna estructural automotriz que comprende areas reforzadas localizadas.
CN105312470A (zh) 汽车曲轴锻造复合模具
GB0903614D0 (en) Method of manufacturing an aerofoil
RU2016111329A (ru) Способ изготовления усиливающего кромочного элемента лопатки газотурбинного двигателя
CN205383424U (zh) 双拼c型结构承载杆
CN205871928U (zh) 可热板焊接的注塑件
CN202893984U (zh) 卡箍压模
CN106180355A (zh) 一种汽车零部件切边整形模具
TW200619523A (en) Method for making fluid bearing
CN202239176U (zh) 用于列车左右支撑座合二为一锤上模锻成型的切边模
KR101530588B1 (ko) 락볼트 제조방법
CN202019261U (zh) 手机马达固定支架
CN203356386U (zh) 一种加工弯头的模架
WO2010020240A3 (de) Axialkolbenmaschine
RU2013119274A (ru) Способ изготовления многослойных металлических панелей
CN202683734U (zh) 四角切边模
CN204018539U (zh) 法兰复合加工一次成型模具
CN203793498U (zh) 摩托车链盒
CN202021526U (zh) 用于调整模具配模精度的承压板
MX2017012825A (es) Metodo para fabricar diferentes versiones de un refuerzo de pilar con un molde comun.
CN204261882U (zh) 一种手工艺用点胶辅助平台
CN204505152U (zh) 一种冲击片雷管组件加压固化装置
CN203362701U (zh) 一种三通挤压油缸的缸底压圈