Method of fusing thermoplastic composite structures

Patent metadata

Field	Value
Publication number	US-2020353702-A1
Application number	US-201916404794-A
Country	US
Kind code	A1
Filing date	May 7, 2019
Priority date	May 7, 2019
Publication date	Nov 12, 2020
Grant date	—

Abstract

A method for fusing thermoplastic composite structures includes placing a substructure on an inner surface of a skin that is laid up on a shaping surface of a tool configured to maintain the shape of an outer mold line. The method further includes applying at least one insulation layer over a flange of the substructure and over exposed portions of the inner surface of the skin not in contact with the substructure, and applying a vacuum bag to at least partly enclose the skin and the substructure. The method yet still further includes applying heat to the shaping surface to fuse the substructure to the skin such that the skin exceeds its melting point and at least a portion of a raised segment of the substructure does not exceed its melting point.

First claim

1 - 10 . (canceled)

11 . A method for fusing thermoplastic composite structures, the method comprising:
laying a skin comprising an outer surface and an inner surface on a shaping surface of a tool configured to maintain the outer surface in a shape of an outer mold line, the inner surface of the skin comprising a first faying surface; laying a substructure on the inner surface of the skin, the substructure comprising a flange and a raised segment, the flange comprising an outer surface and a second faying surface contacting the first faying surface of the skin and the raised segment comprising an outer surface; applying at least one insulation layer over the flange of the substructure and over exposed portions of the inner surface of the skin not in contact with the substructure, the insulation layer comprising an upper side opposite the shaping surface; applying a vacuum bag to cover the skin and the substructure such that the skin and the substructure are at least partly enclosed by the combination of the vacuum bag and the shaping surface of the tool, the vacuum bag comprising a first side adjacent the substructure and a second side opposite the first side; applying heat to the shaping surface to fuse the substructure to the skin such that the skin exceeds its melting point and at least a portion of the raised segment does not exceed its melting point and flowing a coolant fluid into contact with and over the second side of the vacuum bag during the fusing of the substructure to the skin, the coolant fluid being at a lower temperature than the skin,
wherein—
the vacuum bag comprises material having a melting point,
a first portion of the insulation layer covers the outer surface of the flange over the faying surfaces,
a second portion of the insulation layer covers at least one of the exposed portions of the inner surface of the skin,
the insulation layer is sized such that, during the fusing of the substructure to the skin, the upper side of the insulation layer and a portion of the first side of the vacuum bag covering the raised segment are each maintained below the melting point of the vacuum bag.

12 - 15 . (canceled)

16 . The method of claim 11 , further comprising applying a release layer between the inner surface of the skin and the second portion of the insulation layer.

17 . The method of claim 11 , wherein the skin comprises a plurality of composite layers and the insulation layer is sized such that the application of heat to the shaping surface also causes each of the plurality of composite layers to fuse with adjacent ones of the plurality of composite layers during the fusing of the substructure to the skin.

18 . The method of claim 17 , further comprising pressurizing the coolant fluid using an autoclave containing the substructure, the tool, and the vacuum bag, wherein the coolant fluid is pressurized above fourteen and seven-tenths pounds per square inch (14.7 psia) absolute pressure during the fusing of the substructure to the skin.

19 . The method of claim 18 , further comprising directing the flow of the coolant fluid across the second side of the vacuum bag via an impeller and a vane shaped and positioned to receive the flow of coolant fluid from the impeller and redirect the flow of the coolant fluid toward the vacuum bag.

20 . The method of claim 11 , wherein the tool comprises a sidewall covered by a tool insulation layer and at least one cooling portion, the at least one cooling portion each having an outer surface receiving perimeter portions of the vacuum bag and the at least one cooling portion being of a sufficient thinness to maintain each outer surface below the melting point of the vacuum bag during the fusing of the substructure to the skin.

Assignees

• Spirit Aerosys Inc

Inventors

• Wadsworth Mark Anthony

Classifications

• B29C70/342 Primary

  using isostatic pressure · CPC title

• B29D99/0014 Primary

  provided with ridges or ribs, e.g. joined ribs · CPC title

• B29L2031/3082

  Fuselages · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C70/44

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title