Moldable fly-away tool structure system

Patent metadata

Field	Value
Publication number	US-9868233-B2
Application number	US-201113578059-A
Country	US
Kind code	B2
Filing date	Jul 15, 2011
Priority date	Nov 5, 2010
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

A composite structure includes a first face sheet, a second face sheet, and a foam member located between the first face sheet and the second face sheet. The foam member has a molded contour, the mold contour being configured to provide tooling surface for at least one of the first face sheet and the second face sheet prior to curing of the composite structure. A method of making the foam member includes creating a mold tool having an interior surface which resembles the desired outer contour of the foam member. A mixture is poured into a pour opening in the mold tool. The mixture is allowed to polymerize into a foam as the foam expands and distributes within the mold tool. Vent openings in the mold tool are selectively tailored to control the density of the foam member. The foam member is cured in the mold tool.

First claim

The invention claimed is:

1. A composite structure, comprising:
a first face sheet;
a second face sheet;
a foam member located between the first face sheet and the second face sheet, the foam member having a molded contour, the molded contour being configured to provide a tooling surface for at least one of both the first face sheet and the second face sheet prior to curing of the composite structure, the foam member being rigid by having a foam body of uninterrupted foam, the molded contour of the foam member being an outer surface of the foam body; and
a honeycomb core member located between the first face sheet and the second face sheet and the honeycomb member adjacently abutting the foam member, the honeycomb core member configured to provide structural stiffness in the composite structure;
wherein a release member is used to prevent the foam member from being in bonding contact with the first face sheet and the second face sheet, so as to substantially prevent a shear load between first face sheet and second face sheet from being carried through the foam member.

2. The composite structure according to claim 1 , wherein at least one of the first face sheet and the second face sheet is a composite material.

3. The composite structure according to claim 1 , wherein the foam member has a side portion left exposed such that the first face sheet and second face sheet does not fully envelop the foam member.

4. The composite structure according to claim 1 , wherein the foam member is adhesively bonded to at least one of the first face sheet and the second face sheet, so that the foam member is capable of carrying a shear load between the first face sheet and the second face sheet.

5. The composite structure according to claim 1 , wherein the foam member is cured prior to abutting.

Assignees

• Mishra Suvankar
• Mccullough John R
• Chris Mark
• Woychesin Stanley B
• Textron Innovations Inc

Inventors

• Mishra Suvankar
• Mccullough John R
• Chris Mark
• Woychesin Stanley B

Classifications

• B32B5/245

  another layer next to it being a foam layer · CPC title

• B32B5/18

  characterised by features of a layer {of} foamed material · CPC title

• B32B2262/101

  Glass fibres · CPC title

• B32B3/263

  characterised by a layer having non-uniform thickness · CPC title

• Y10T428/24149

  Honeycomb-like · CPC title