Title:
局部補強材を有するラミネートの結合構造体
Document Type and Number:
Japanese Patent JP4938455
Kind Code:
B2
Abstract:
A joining structure in a laminate includes metal layers as well as at least one adhesive layer which is enclosed by the metal layers, which metal layers each include separate metal-layer parts having a pair of overlapping edges, which pairs of edges are offset with respect to each other and together define a joining region. The laminate includes a section which is of standard construction and a section which contains an additional, internal reinforcing metal layer, the reinforcing metal layer including two reinforcing metal-layers parts with a pair of overlapping edges, the pair of edges being located outside the joining region.
Inventors:
Rajabali, Abduel Fazier
Tar Steeg, Willlem Jean Nicolas
Tar Steeg, Willlem Jean Nicolas
Application Number:
JP2006532145A
Publication Date:
May 23, 2012
Filing Date:
October 05, 2004
Export Citation:
Assignee:
Fokker Aerostructures B.V.
Airbus Operations GmbH
Airbus Operations GmbH
International Classes:
B32B15/08; B29C70/88; B32B3/08; B32B3/10; B32B15/14; B64C1/00
Domestic Patent References:
| JP2001526601A | 2001-12-18 | |||
| JP2007521164A | 2007-08-02 |
Foreign References:
| WO2002078950A1 | 2002-10-10 |
Attorney, Agent or Firm:
Satoshi Kono
Makoto Nakamura
Kurata Masatoshi
Takashi Mine
Yoshihiro Fukuhara
Toshio Shirane
Sadao Muramatsu
Nobuhisa Nogawa
Katsu Sunagawa
Ryo Hashimoto
Tetsuya Kazama
Makoto Nakamura
Kurata Masatoshi
Takashi Mine
Yoshihiro Fukuhara
Toshio Shirane
Sadao Muramatsu
Nobuhisa Nogawa
Katsu Sunagawa
Ryo Hashimoto
Tetsuya Kazama