The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 31, 2015

Filed:

Dec. 11, 2013
Applicant:

Mitsubishi Aircraft Corporation, Aichi, JP;

Inventors:

Koji Kawahara, Tokyo, JP;

Hideo Yamakoshi, Tokyo, JP;

Yuichiro Kamino, Tokyo, JP;

Atsuhiro Iyomasa, Tokyo, JP;

Toru Hashigami, Aichi, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H05H 3/02 (2006.01); H01R 4/06 (2006.01); B64C 3/34 (2006.01); B64D 45/02 (2006.01); F16B 37/14 (2006.01); F16B 15/02 (2006.01); F16B 5/02 (2006.01); F16B 1/00 (2006.01);
U.S. Cl.
CPC ...
H01R 4/06 (2013.01); F16B 15/02 (2013.01); H05H 3/02 (2013.01); B64C 3/34 (2013.01); B64D 45/02 (2013.01); F16B 5/02 (2013.01); F16B 37/14 (2013.01); F16B 2001/0064 (2013.01);
Abstract

Provided is a coupling structure for airframe components that is capable of ensuring sufficient lightning protection capability. A conductive pattern partmade of a conductive material is formed around each fastener memberbetween wing surface panelsA andB. The conductive pattern partis formed, for example, around each of holesandon the plane on which the wing surface panelA and the wing surface panelB abut against each other. Then, the conductive pattern partis pushed against both the wing surface panelA and the wing surface panelB by the fastening power of the fastener members, whereby electrical conduction between the wing surface panelA and the wing surface panelB can be achieved.


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