IP Library Granted Patent US 11,273,896
Granted Patent B2
US 11,273,896 · App. 16/074,206 · Granted Mar 15, 2022

Shape holding fixture and method for manufacturing aircraft panel

Inventors: Makoto Hirai (Tokyo, JP); Hiroki Azuma (Tokyo, JP); Takuya Goto (Tokyo, JP); Sachio Takeyama (Tokyo, JP)
Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
B64C1/12B25B11/005B64F5/10B21J15/142B64C1/061B64C1/064B64C2001/0054
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Quick Facts
Patent No.
US 11,273,896
App. No.
16/074,206
Granted
Mar 15, 2022
Kind
B2
Abstract

To simplify the structure of a holding fixture which holds the shape of the aircraft panel and conveys the aircraft panel, an object is to ensure shape accuracy required in the manufacturing process and hold an aircraft panel in an appropriate shape, in combination with a holding fixture. A shape holding fixture includes: a plurality of support units configured to be positioned on a lower surface side of an aircraft panel, and provided at intervals along a one-axis direction, the aircraft panel being held by a holding fixture configured to grip an edge portion of the aircraft panel; and a shape holding unit provided to each of the plurality of support units, including a rod which supports the aircraft panel from the lower surface side of the aircraft panel, and configured to adjust a position where the rod comes into contact with the aircraft panel to support the aircraft panel, corresponding to the shape of the aircraft panel.

Claims (8)

1. A method for manufacturing an aircraft panel including a plate-like member, the method comprising the steps of:

conveying a holding fixture to a position above a shape holding fixture;

setting the holding fixture on the shape holding fixture in an overlapping manner;

causing a plurality of gripping units provided to the holding fixture to grip an aircraft panel including the plate-like member, at edge portions on two opposite sides of the aircraft panel on the holding fixture such that the aircraft panel has a curved shape in cross section taken in a direction perpendicular to a one-axis direction;

adjusting positions of rods conforming to a shape of the aircraft panel, the rods being provided to a plurality of support units of the shape holding fixture which are arranged at intervals along the one-axis direction;

causing the rods to come into contact with the aircraft panel from a lower surface side of the aircraft panel so as to support the aircraft panel;

joining an overlapping portion of the aircraft panel by a rivet; and

conveying the holding fixture while maintaining a state where the holding fixture holds the edge portions of the aircraft panel.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 31, 2018
From: HIRAI, MAKOTO; AZUMA, HIROKI; GOTO, TAKUYA; TAKEYAMA, SACHIO
To: MITSUBISHI HEAVY INDUSTRIES, LTD.
Reel/Frame 046511/0326 →
Priority Claims (1)
JP JP2016-018426 · Feb 2, 2016 · national
Continuity (1)
Related Publication 20210171181A1 · Jun 10, 2021
Cited By (2)
US 12,304,659 US 12,337,996