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Patent Searching and Data


Title:
JOINT, AND AIRCRAFT STRUCTURE
Document Type and Number:
WIPO Patent Application WO/2015/049895
Kind Code:
A1
Abstract:
Provided is a joint and an aircraft structure wherein it is possible to position a member relative to a preform with high accuracy. A groove part, into which a plate material (30) is inserted, is formed on a π-shaped joint (20) provided to a preform (21), and the preform (21) and the plate material (30) are joined by being bonded. Moreover, a fitting shape (32A-1), into which the plate material (30) fits, is formed on the π-shaped joint (20) on the entire bottom surface of the groove part. Additionally, a fitting shape (32A-2), into which the plate material (30) fits, is formed on a portion of the bottom surface of the groove part. Furthermore, fitting shapes (32B-1, 32B-2), into which the bottom surface of the groove part that is formed on the π-shaped joint (20) fits, are formed on the surface of the plate material (30) that fits into the π-shaped joint (20).

Inventors:
ABE TOSHIO (JP)
TAKAGI KIYOKA (JP)
KOYAMA TAKAYUKI (JP)
KISHIMOTO KAZUAKI (JP)
SAITO KOUICHI (JP)
ISHIDA TAKASHI (JP)
Application Number:
PCT/JP2014/063384
Publication Date:
April 09, 2015
Filing Date:
May 20, 2014
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
F16B11/00; B29C65/48; B64C1/06
Foreign References:
US7205066B12007-04-17
JP2012528994A2012-11-15
US8393871B22013-03-12
US8403586B22013-03-26
Other References:
See also references of EP 3015721A4
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (JP)
Takaharu Fujita (JP)
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