IL66912A - Method and apparatus for shaping metal panels - Google Patents

Method and apparatus for shaping metal panels

Info

Publication number
IL66912A
IL66912A IL66912A IL6691282A IL66912A IL 66912 A IL66912 A IL 66912A IL 66912 A IL66912 A IL 66912A IL 6691282 A IL6691282 A IL 6691282A IL 66912 A IL66912 A IL 66912A
Authority
IL
Israel
Prior art keywords
metal panels
shaping metal
shaping
panels
metal
Prior art date
Application number
IL66912A
Original Assignee
Dornier Gmbh
Eckold Vorrichtung
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=25796580&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=IL66912(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from DE19813139836 external-priority patent/DE3139836A1/en
Priority claimed from DE19818129965 external-priority patent/DE8129965U1/en
Application filed by Dornier Gmbh, Eckold Vorrichtung filed Critical Dornier Gmbh
Publication of IL66912A publication Critical patent/IL66912A/en

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
    • B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
    • 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
    • B21D11/00—Bending not restricted to forms of material mentioned in only one of groups B21D5/00, B21D7/00, B21D9/00; Bending not provided for in groups B21D5/00 - B21D9/00; Twisting
    • B21D11/20—Bending sheet metal, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Moulding By Coating Moulds (AREA)
IL66912A 1981-10-07 1982-09-30 Method and apparatus for shaping metal panels IL66912A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19813139836 DE3139836A1 (en) 1981-10-07 1981-10-07 Method and device for the bending of panels, in particular for the shell of the body of aircraft
DE19818129965 DE8129965U1 (en) 1981-10-14 1981-10-14 "DEVICE FOR CHIP-FREE SHAPING OF SHEETS WITH REINFORCING RIBS"

Publications (1)

Publication Number Publication Date
IL66912A true IL66912A (en) 1986-03-31

Family

ID=25796580

Family Applications (1)

Application Number Title Priority Date Filing Date
IL66912A IL66912A (en) 1981-10-07 1982-09-30 Method and apparatus for shaping metal panels

Country Status (4)

Country Link
EP (1) EP0078891B1 (en)
CA (1) CA1198322A (en)
DE (1) DE3268822D1 (en)
IL (1) IL66912A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10007995C2 (en) * 2000-02-22 2002-03-07 Airbus Gmbh Structural component, in particular for an aircraft and method for producing a structural component
GB0207239D0 (en) 2002-03-27 2002-05-08 Airbus Uk Ltd Wing skin and method of manufacture thereof
US7093470B2 (en) 2002-09-24 2006-08-22 The Boeing Company Methods of making integrally stiffened axial load carrying skin panels for primary aircraft structure and fuel tank structures
CN114799756B (en) * 2022-04-29 2023-10-31 沈阳飞机工业（集团）有限公司 Composite manufacturing device and method for high-rib thin-wall aluminum alloy wallboard part
CN115090750B (en) * 2022-07-14 2024-01-26 中国航空制造技术研究院 Shot-peening pre-bending tool for high-strength discontinuous wall plate and forming method using same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2980156A (en) * 1956-10-15 1961-04-18 Lockheed Aircraft Corp Method and apparatus for stretch shaping panels
DE1197841B (en) * 1963-02-14 1965-08-05 Ver Flugtechnische Werke Ges M Method and device for shaping honeycomb mats
FR2237435A5 (en) * 1973-07-10 1975-02-07 Aerospatiale
CH624318A5 (en) * 1977-06-16 1981-07-31 Naeslund G Korstraesk Mekanisk Method and apparatus for bending a corrugated sheet and a corrugated sheet bent by this method

Also Published As

Publication number Publication date
EP0078891B1 (en) 1986-01-29
EP0078891A1 (en) 1983-05-18
CA1198322A (en) 1985-12-24
DE3268822D1 (en) 1986-03-13

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