Foam stiffened structure and method of making the same

Patent metadata

Field	Value
Publication number	US-11097507-B2
Application number	US-201615195501-A
Country	US
Kind code	B2
Filing date	Jun 28, 2016
Priority date	Nov 5, 2010
Publication date	Aug 24, 2021
Grant date	Aug 24, 2021

Abstract

A structure includes a skin and a foam member. The foam member has a molded contour, the mold contour being configured to provide tooled surface for the skin. When the skin is a composite skin, the foam member provides support for the skin so that the skin can be cured under heat and pressure. A method of making the foam member for a foam stiffened structure includes creating a mold having an interior cavity which resembles a desired shape the foam member. A subsequent step involves introducing a foam mixture into the mold. Next, the foam mixture is allowed to polymerize so as to expand and distribute within the cavity of the mold. The method further includes selectively controlling a density of the foam member in the mold. The foam member is at least partially cured. The foam member is assembled with a skin to produce the foam stiffened structure.

First claim

The invention claimed is:

1. A foam stiffened composite structure, having a predetermined shape, for use in aviation, comprising:
an outer skin member, comprising a composite fiber material disposed in a polymeric matrix;
a foam member having multiple zones of varying density with each zone being formed of the same material, the foam member abutting the outer skin member, the foam member having a tooled surface; and
an inner skin member abutting the foam member, the foam member surrounding the inner skin member;
wherein the inner skin member is tubular, thereby defining a hollow void space in the interior of the foam member;
wherein the hollow void space is delimited by the predetermined shape; and
wherein the outer skin member has the same tooled surface as the tooled surface of the foam member.

2. The structure according to claim 1 , wherein the foam member is a cured foam mixture, the foam stiffened composite structure further comprising at least one of:
a rib attached to the cured foam mixture; and
a trailing edge member attached to the cured foam mixture.

3. The structure according to claim 1 , wherein the inner skin member is fully cured before the foam member abuts the outer skin member and abuts the inner skin member.

4. The structure according to claim 1 , wherein the foam member is at least partially cured before the foam member abuts the outer skin member.

Assignees

• Textron Innovations Inc

Inventors

• Thiagarajan Ramesh
• Mishra Suvankar
• Chris Mark
• Evans Iii William
• Mikel Mike

Classifications

• B64C1/068

  Fuselage sections · CPC title

• Y02T50/40

  Weight reduction · CPC title

• B32B2250/40

  Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA · CPC title

• B32B2603/00

  Vanes, blades, propellers, rotors with blades · CPC title

• B32B7/12

  using interposed adhesives or interposed materials with bonding properties · CPC title