ATE530268T1 - Verfahren zum herstellen einer rillenstruktur - Google Patents

Verfahren zum herstellen einer rillenstruktur

Info

Publication number
ATE530268T1
ATE530268T1 AT03290048T AT03290048T ATE530268T1 AT E530268 T1 ATE530268 T1 AT E530268T1 AT 03290048 T AT03290048 T AT 03290048T AT 03290048 T AT03290048 T AT 03290048T AT E530268 T1 ATE530268 T1 AT E530268T1
Authority
AT
Austria
Prior art keywords
forming
smooth outer
producing
outer skin
groove structure
Prior art date
Application number
AT03290048T
Other languages
English (en)
Inventor
Stephane Debaisieux
Christian Overbergh
Sebastien Quets
Original Assignee
Sonaca Sa
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 Sonaca Sa filed Critical Sonaca Sa
Application granted granted Critical
Publication of ATE530268T1 publication Critical patent/ATE530268T1/de

Links

Classifications

    • 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
    • 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
    • B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49805—Shaping by direct application of fluent pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
AT03290048T 2002-01-11 2003-01-09 Verfahren zum herstellen einer rillenstruktur ATE530268T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE2002/0014A BE1014570A4 (fr) 2002-01-11 2002-01-11 Procede de fabrication d'une structure cannelee et structure obtenue par ce procede.

Publications (1)

Publication Number Publication Date
ATE530268T1 true ATE530268T1 (de) 2011-11-15

Family

ID=3897158

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03290048T ATE530268T1 (de) 2002-01-11 2003-01-09 Verfahren zum herstellen einer rillenstruktur

Country Status (5)

Country Link
US (1) US6739029B2 (de)
EP (1) EP1327489B1 (de)
AT (1) ATE530268T1 (de)
BE (1) BE1014570A4 (de)
ES (1) ES2375712T3 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2308779T3 (es) * 1995-07-26 2008-12-01 Astrazeneca Ab Receptores quimericos y metodos para identificar compuestos activos en los receptores de glutamato metabotropico y el uso de tales compuestos en el tratamiento de trastornos y enfermedades neurologicas.
BE1016117A3 (fr) * 2004-07-09 2006-03-07 Sonaca Sa Volet mobile de bord d'attaque d'une aile principale de la voilure d'un aeronef.
GB2450935B (en) * 2007-07-13 2009-06-03 Rolls Royce Plc Component with internal damping
GB2450934B (en) 2007-07-13 2009-10-07 Rolls Royce Plc A Component with a damping filler
DE102007054071B4 (de) * 2007-11-13 2010-06-10 Eisfink Max Maier Gmbh & Co. Kg Verbundmetallgegenstand und Verfahren zur Herstellung eines Verbundmetallgegenstands
GB0808840D0 (en) 2008-05-15 2008-06-18 Rolls Royce Plc A compound structure
GB2462102B (en) 2008-07-24 2010-06-16 Rolls Royce Plc An aerofoil sub-assembly, an aerofoil and a method of making an aerofoil
GB0901235D0 (en) 2009-01-27 2009-03-11 Rolls Royce Plc An article with a filler
GB0901318D0 (en) 2009-01-28 2009-03-11 Rolls Royce Plc A method of joining plates of material to form a structure
GB0911416D0 (en) * 2009-07-02 2009-08-12 Rolls Royce Plc A method of forming an internal structure within a hollow component
GB201009216D0 (en) 2010-06-02 2010-07-21 Rolls Royce Plc Rotationally balancing a rotating part
GB2485831B (en) 2010-11-26 2012-11-21 Rolls Royce Plc A method of manufacturing a component
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
BE1022531B1 (fr) 2014-10-20 2016-05-24 Sonaca S.A. Systeme ameliore pour la gestion duale de l'antigivrage et de l'aspiration de la couche limite sur une surface portante d'un aeronef
US10569504B2 (en) * 2017-02-27 2020-02-25 The Boeing Company Panel and method of forming a three-sheet panel
GB201715791D0 (en) * 2017-09-29 2017-11-15 Rolls Royce Plc Blade and vanes for gas turbine engines and manufacture thereof
EP3505441B1 (de) * 2017-12-28 2023-02-08 Airbus Operations GmbH Vorderkantenstruktur für ein strömungsleitsystem eines flugzeugs
US11453477B2 (en) * 2019-02-28 2022-09-27 Airbus Operations Gmbh Wing leading edge device and a wing having such a wing leading edge device
CN113001125A (zh) * 2021-03-19 2021-06-22 沈阳万事达机械有限公司 尾翼骨架工艺流程
CN113814655B (zh) * 2021-08-23 2023-12-08 成都飞机工业（集团）有限责任公司 一种复杂型面气动加载超塑成形扩散连接方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2690002A (en) 1949-11-18 1954-09-28 Olin Ind Inc Method of making hollow sheet metal fabrications having a plurality of interconnected passageways
US2859509A (en) * 1956-02-24 1958-11-11 Olin Mathieson Fabrication of hollow articles
US2999307A (en) * 1956-11-30 1961-09-12 Olin Mathieson Fabrication of hollow articles
US3933327A (en) 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
EP0206416A3 (de) * 1985-06-17 1987-09-02 Paul Mueller Company Plattenwärmetauscher und Verfahren zu dessen Herstellung
US5011098A (en) 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US5115963A (en) * 1991-06-10 1992-05-26 Mcdonnell Douglas Corporation Superplastic forming of panel structures
GB9114258D0 (en) * 1991-07-02 1991-08-21 Secr Defence Superplastic deformation of diffusion bonded aluminium structures
GB9117546D0 (en) * 1991-08-14 1992-02-19 British Aerospace Manufacture of structures by diffusion bonding and superplastic forming
US5330092A (en) * 1991-12-17 1994-07-19 The Boeing Company Multiple density sandwich structures and method of fabrication
US5687900A (en) * 1995-03-28 1997-11-18 Mcdonnell Douglas Corporation Structural panel having a predetermined shape and an associated method for superplastically forming and diffusion bonding the structural panel
FR2739832B1 (fr) * 1995-10-12 1997-12-26 Aerospatiale Structure metallique creuse monobloc et dissymetrique telle qu'un bord de fuite d'un bec d'attaque d'une voilure d'aeronef et son procede de fabrication
US5881459A (en) * 1996-09-27 1999-03-16 Mcdonnell Douglas Corporation Pressure communication for superplastically formed, diffusion bonded panels and method of manufacture
DE19649132C2 (de) 1996-11-27 1999-09-02 Daimler Chrysler Aerospace Nase für eine aerodynamische Fläche und Verfahren zu ihrer Herstellung
GB2324351A (en) 1997-04-18 1998-10-21 British Aerospace Reducing drag in aircraft wing assembly
US5941446A (en) * 1997-07-10 1999-08-24 Mcdonnell Douglas Corporation SPF/DB airfoil-shaped structure and method of fabrication thereof
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
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

Also Published As

Publication number Publication date
EP1327489B1 (de) 2011-10-26
BE1014570A4 (fr) 2004-01-13
ES2375712T3 (es) 2012-03-05
EP1327489A1 (de) 2003-07-16
US20030136815A1 (en) 2003-07-24
US6739029B2 (en) 2004-05-25

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