Method for forming composite components and tool for use...

Plastic and nonmetallic article shaping or treating: processes – Mechanical shaping or molding to form or reform shaped article – Shaping against forming surface

Reexamination Certificate

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Details

C264S231000, C264S258000, C425S469000

Reexamination Certificate

active

07922957

ABSTRACT:
A method of making an aircraft component is provided, wherein the method comprises the steps of:providing a mould (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mould with said material providing an intensification tool (14) in spaced relationship to the mould and heating the material, tool and mould so that the tool expands and applies pressure to the material and so as to form the component andwherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.

REFERENCES:
patent: 4388263 (1983-06-01), Prunty
patent: 5073589 (1991-12-01), Milovich et al.
patent: 5387098 (1995-02-01), Willden
patent: 5817269 (1998-10-01), Younie et al.
patent: 2005/0116136 (2005-06-01), Artz et al.
patent: 2131934 (1984-11-01), None
patent: 2 316 036 (1998-02-01), None
patent: 62280027 (1987-12-01), None
patent: 03262607 (1991-11-01), None
Derwent abstract of JP62280027 and JP03262607.
Great Britain Search Report for GB Application No. 0712535.4, dated Aug. 17, 2007.

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