Aircraft interior panels and methods of panel fabrication

Patent metadata

Field	Value
Publication number	US-10076895-B2
Application number	US-201514638952-A
Country	US
Kind code	B2
Filing date	Mar 4, 2015
Priority date	Nov 14, 2011
Publication date	Sep 18, 2018
Grant date	Sep 18, 2018

Abstract

A multifunctional fully integral panel system design, a unique material configuration, and a process for fabricating a net shape (or nearly net shape) panel in one production cycle. The panel may comprise a base facing with an outer perimeter, a decorative film applied to the exterior of the base facing, an aft facing having an outer perimeter fused to the base facing, and a reinforcement core disposed between the unfused portions of the base and aft facings, which reinforcement core also acts as acoustic insulation (i.e., a noise attenuator). Alternatively or additionally, a foam core or blanket having thermal and/or acoustic insulation properties is attached to the external surface of the aft facing. The fabrication process involves the application of different heat treatments to panel components having different forming temperature or rubbery/elastic plateaus.

First claim

The invention claimed is:

1. A method of making a panel:
bonding a plurality of polymer rods to one surface of a base facing;
heating the base facing to a softened state;
placing the softened base facing in a first tool having a shape defining one surface of a panel with the polymer rods being on a side of the base facing which faces away from the first tool;
heating an aft facing to a softened state;
placing a surface of the softened aft facing against a second tool having a shape defining another surface of the panel;
placing an insulation layer adjacent to the one surface of the base facing;
vacuum forming the base and aft facings to take the respective shapes of the first and second tools; and
pressing the base and aft facings together such that they contact each other and fuse along a perimeter to form a panel having an interior volume with the insulation layer and polymer rods inside.

2. The method as recited in claim 1 , further comprising applying a foaming film to the one surface of the base facing prior to vacuum forming and then applying heat to the film to cause the film to convert to foam that coats the one surface of the base facing to form the insulation layer.

3. The method as recited in claim 1 , wherein the polymer rods are hollow.

4. The method as recited in claim 3 , wherein the insulation layer comprises foam that encapsulates the hollow polymer rods.

5. The method as recited in claim 1 , wherein the base facing is a composite sheet having a fiber layer encapsulated in a polymer matrix.

6. The method as recited in claim 1 , further comprising attaching a decorative film to another surface of the base facing.

7. A method of making a panel:
placing a surface of a base facing against a first tool having a shape defining one surface of a panel;
placing a surface of an aft facing against a second tool having a shape defining another surface of the panel;
vacuum forming the base and aft facings to take the respective shapes of the first and second tools;
pressing the base and aft facings together such that they contact each other and fuse along a perimeter; and
attaching an insulation layer to an exterior surface of one of the base and aft facings,
wherein the insulation layer is attached to the exterior surface of the aft facing using an ultrasonic or laser welding technique.

8. The method as recited in claim 7 , wherein the base facing is a composite sheet having a fiber layer encapsulated in a polymer matrix.

9. A method of making a panel:
placing a surface of a base facing against a first tool having a shape defining one surface of a panel;
placing a surface of an aft facing against a second tool having a shape defining another surface of the panel;
vacuum forming the base and aft facings to take the respective shapes of the first and second tools;
pressing the base and aft facings together such that they contact each other and fuse along a perimeter; and
attaching an insulation layer to an exterior surface of one of the base and aft facings,
wherein the step of attaching the insulation comprises:
positioning a layer of batting material over the exterior surface of the aft facing;
positioning a thin film over the layer of batting material; and
fusing the thin film to the exterior surface of the aft facing.

10. The method as recited in claim 9 , wherein the base facing is a composite sheet having a fiber layer encapsulated in a polymer matrix.

Assignees

• Boeing Co

Inventors

• Patel Jayant Dahyabhai
• Harris John N
• Sanchez Sergio H
• Fullerton James A

Classifications

• Y10T428/31504

  Composite [nonstructural laminate] · CPC title

• B29C51/267

  Two sheets being thermoformed in separate mould parts and joined together while still in the mould (B29C49/0691 takes precedence) · CPC title

• B29C2043/561

  under vacuum conditions · CPC title

• Y10T428/249953

  Composite having voids in a component [e.g., porous, cellular, etc.] · CPC title

• B29C2791/006

  Using vacuum · CPC title