IP Library Granted Patent US 9,186,756
Granted Patent B2
US 9,186,756 · App. 14/361,478 · Granted Nov 17, 2015

Repair method and repair structure for honeycomb sandwich structural body

Inventor: Toshikazu Shigetomi (Tokyo, JP)
Assignee: MITSUBISHI AIRCRAFT CORPORATION
B23P6/00B29C73/06B29C73/10B32B3/08B32B3/12B32B5/24B32B7/12F02C7/045B32B2250/02B32B2260/023B32B2260/046B32B2262/101B32B2262/106B32B2307/51B32B2307/714B32B2605/00F02K1/827F05D2230/80F05D2250/283Y02T50/672Y10T29/49732Y10T428/20
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Quick Facts
Patent No.
US 9,186,756
App. No.
14/361,478
Granted
Nov 17, 2015
Kind
B2
Abstract

A repair method includes the steps of: (A) forming a repair cavity 14 by removing a honeycomb core 11 including a damaged portion with a front-side skin 12 ; (B) inserting, into the repair cavity 14 , a repair honeycomb core 21 whose end surface 30 on a side to which a repair patch 22 is bonded is subjected to flattening treatment; (C) disposing the repair patch on the flattened end surface 30 of the repair honeycomb core 21 via a film-like adhesive 24 ; and (D) bonding the repair honeycomb core 21 to an existing portion of the honeycomb sandwich structural body 10 and to the repair patch 22 , and curing the repair patch 22 under a reduced-pressure atmosphere associated with heating.

Claims (14)

1. A method for repairing a honeycomb sandwich structural body where a skin is disposed on both front and rear surfaces of a honeycomb core, comprising the steps of:

(A) forming a repair cavity by removing the honeycomb core including a damaged portion with the skin;

(B) inserting, into the repair cavity, a repair honeycomb core whose end surface on a side to which a repair patch is bonded is subjected to flattening treatment;

(C) disposing the repair patch on the flattened end surface of the repair honeycomb core via an adhesive; and

(D) bonding the repair honeycomb core to an existing portion of the honeycomb sandwich structural body and to the repair patch, and curing the repair patch under a reduced-pressure atmosphere associated with heating.

2. The method for repairing a honeycomb sandwich structural body according to claim 1 , wherein in the flattening treatment, an opening of the repair honeycomb core is closed by resin that is not softened by heating in the step (D).

3. The method for repairing a honeycomb sandwich structural body according to claim 2 , wherein the opening of the repair honeycomb core is closed by immersing, in resin in an uncured state, the end surface of the repair honeycomb core on the side on which the repair patch is disposed, and curing the resin.

4. A repair structure of a honeycomb sandwich structural body where a skin is disposed on both front and rear surfaces of a honeycomb core,

wherein in a repair cavity including a first region formed by removing the skin, and a second region formed by removing the honeycomb core,

a repair honeycomb core disposed in the second region and a repair patch disposed in the first region are bonded to each other, and

an end surface of the repair honeycomb core on a side to which the repair patch is bonded is made flat.

5. The repair structure of a honeycomb sandwich structural body according to claim 4 , wherein an adhesive is interposed between the repair honeycomb core and the repair patch.

6. The repair structure of a honeycomb sandwich structural body according to claim 4 , wherein the end surface of the repair honeycomb core has an opening, and

the opening is closed with resin.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 29, 2014
From: SHIGETOMI, TOSHIKAZU
To: MITSUBISHI AIRCRAFT CORPORATION
Reel/Frame 032988/0387 →
Priority Claims (1)
JP 2012-008562 · Jan 19, 2012 · national
Continuity (1)
Related Publication 20140329043A1 · Nov 6, 2014