IP Library › Granted Patent US 9,475,587
Granted Patent B2
US 9,475,587 · App. 14/165,734 · Granted Oct 25, 2016

Jig for forming sealant layer for lightning protection fastener, method for forming sealant layer for lightning protection fastener, and wing of aircraft

Inventors: Wataru Nishimura (Tokyo, JP); Hideo Yamakoshi (Aichi, JP); Yuji Asahara (Aichi, JP); Atsuhiro Iyomasa (Tokyo, JP); Takeyasu Tarumi (Tokyo, JP); Noritomo Takata (Tokyo, JP); Jun Kawaguchi (Tokyo, JP); Hiroshi Rikukawa (Tokyo, JP); Tomonori Okumura (Aichi, JP); Kengo Nomiya (Tokyo, JP); Tooru Hashigami (Aichi, JP)
Assignee: MITSUBISHI AIRCRAFT CORPORATION
B64D45/02F16B37/14
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Quick Facts
Patent No.
US 9,475,587
App. No.
14/165,734
Granted
Oct 25, 2016
Kind
B2
Abstract

To provide a jig for forming a sealant layer which enables to quickly and accurately form a sealant layer having a required film thickness. The jig includes: a sealant cup 13 that overlays a sealant 28 around a collar 26 ; a cup holder 12 that determines a position of the sealant cup 13 with respect to a fastener member 24 ; and a dummy cup 11 that determines a position of the cup holder 12 with respect to the fastener member 24 . The cup holder 12 is determined in position with respect to the fastener member 24 by being guided along the dummy cup 11 determined in position with respect to the fastener member 24 . The sealant cup 13 is guided along a guide of the cup holder 12 so as to overlay the sealant 28 around the collar 26 after removing the dummy cup 11 from the cup holder 12 determined in position with respect to the fastener member 24.

Claims (13)

1. A method for producing a lightning protection fastener with an insulating sealant layer, the lightning protection fastener comprising:

a fastener member that passes through and fastens a plurality of members constituting an airframe of an aircraft; and

an insulating sealant layer that is formed around the fastener member,

with a jig comprising:

a sealant cup that overlays a sealant to be stored in a cavity on the fastener member;

a cup holder that includes a guide for determining a position of the sealant cup with respect to the fastener member; and

a dummy cup that determines a position of the cup holder with respect to the fastener member,

performing the method comprising:

a first step of mounting the dummy cup to the fastener member;

a second step of mounting the cup holder to the dummy cup by moving the guide along the dummy cup; and

a third step of mounting the sealant cup to the fastener member so as to overlay the sealant on the fastener member while moving the sealant cup along the guide of the cup holder after removing the dummy cup with a relative position of the cup holder to the fastener member maintained.

2. The method according to claim 1 , wherein a sealant is fed into the cavity of the sealant cup in advance before the third step.

3. The method according to claim 1 , wherein before the first step, the fastener member is coated with another sealant having lower viscosity than the sealant to be fed into the sealant cup.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 10, 2015
From: NISHIMURA, WATARU; YAMAKOSHI, HIDEO; ASAHARA, YUJI; IYOMASA, ATSUHIRO
To: MITSUBISHI AIRCRAFT CORPORATION
Reel/Frame 036998/0262 →
Priority Claims (1)
JP 2013-14091 · Jan 29, 2013 · national
Continuity (1)
Related Publication 20140209736A1 · Jul 31, 2014