Aircraft cabin pressure regulating subfloor

Patent metadata

Field	Value
Publication number	US-10160533-B2
Application number	US-201414494131-A
Country	US
Kind code	B2
Filing date	Sep 23, 2014
Priority date	Sep 23, 2014
Publication date	Dec 25, 2018
Grant date	Dec 25, 2018

Abstract

An aircraft cabin subfloor construction has flow paths through the subfloor that vent air pockets trapped beneath an air impermeable floor mat on the subfloor where, due to a difference in pressure in the air pockets trapped beneath the floor mat and the air in the aircraft cabin above the floor mat, the air pockets would create bubbles or buckling in the floor mat. The venting of the air pockets beneath the floor mat by the flow paths eliminates the problem of bubbling or buckling in the floor mat.

First claim

The invention claimed is:

1. An aircraft cabin subfloor comprising:
a first rigid sheet having opposite top and bottom surfaces the first rigid sheet having a plurality of flow pat through the first rigid sheet;
an air impermeable mat having a top, surface that is a carpet surface of the aircraft cabin subfloor and an opposite bottom surface, the bottom surface of the impermeable mat opposes and is secured to the top surface of the first rigid sheet with an air filled void between the bottom surface of the air impermeable mat and the top surface of the first rigid sheet;
the plurality of flow paths through the first rigid sheet a configured to vent the air filled void to an exterior of the aircraft cabin subfloor;
a pattern of adhesive applied between the bottom surface of the air impermeable mat and the top surface of the first rigid sheet, the pattern of adhesive securing the bottom surface of the air impermeable mat to the top surface of the first rigid sheet and the pattern of adhesive surrounding the air filled void between the bottom surface of the air impermeable mat and the top surface of the first rigid sheet;
a plurality of perforations through the first rigid sheet, the plurality of perforations at least partially forming the plurality of flow paths;
an open cell core panel having a top surface and an opposite bottom surface, the top surface of the open cell core panel being secured to the bottom surface of the first rigid sheet; and,
the plurality of perforations through the first rigid sheet and open cells of the open cell core panel at least partially forming the plurality of flow paths.

2. The aircraft cabin subfloor of claim 1 , further comprising:
the pattern of adhesive further comprises a loop pattern of adhesive applied between the bottom surface of the air impermeable mat and the top surface of the first rigid sheet, the loop pattern of adhesive securing the bottom surface of the air impermeable mat to the top surface of the first rigid sheet and the loop pattern of adhesive surrounding the air filled void between the bottom surface of the air impermeable mat and the top surface of the first rigid sheet.

3. The aircraft cabin subfloor of claim 1 , further comprising:
the bottom surface of the air impermeable mat having a peripheral edge; and,
the pattern of adhesive is applied to the bottom surface of the air impermeable mat adjacent the peripheral edge.

4. The aircraft cabin subfloor of claim 1 , further comprising:
a second rigid sheet having opposite top and bottom surfaces and a plurality of perforations through the second rigid sheet, the top surface of the second rigid sheet being secured to the bottom surface of the open cell core panel; and,
the plurality of perforations through the first rigid sheet, the open cells of the open cell core panel, and the plurality of perforations through the second rigid sheet forming the plurality of flow paths.

5. The aircraft cabin subfloor of claim 4 , further comprising:
the first rigid sheet being a first facesheet of composite material;
the open cell core panel being an open cell core panel of composite material; and,
the second rigid sheet being a second facesheet of composite material.

6. An aircraft cabin subfloor comprising:
a first facesheet having a substantially flat top surface and an opposite bottom surface, and the first facesheet having a plurality of perforations through the first facesheet;
an open cell core panel having a top surface and an opposite bottom surface, the top surface of the open cell core panel being secured to the bottom surface of the first facesheet;
a second facesheet having a top surface and an opposite bottom surface, the top surface of the second facesheet being secured to the bottom surface of the open cell core panel, and the second facesheet having a plurality of perforations through the second facesheet;
an air impermeable mat having a top surface that is a carpet surface of the aircraft cabin subfloor and an opposite bottom surface, the bottom surface of the air impermeable mat opposes and lays over the top surface of the first facesheet;
a loop pattern of adhesive applied between the bottom surface of the air impermeable mat and the top surface of the first facesheet, the loop pattern of adhesive securing the bottom surface of the air impermeable mat to the top surface of the first facesheet, the loop pattern of adhesive surrounding an air filled void between the bottom surface of the air impermeable mat and the top surface of the first facesheet; and,
the plurality of perforations through the first facesheet, open cells of the open cell core panel, and the plurality of perforations through the second facesheet creating a plurality of flow paths from the air filled void, through the first facesheet, through the open cell core panel, and through the second facesheet, the plurality of flow paths configured to vent the air filled void to an exterior of the aircraft cabin subfloor.

7. The aircraft cabin subfloor of claim 6 , further comprising;
the aircraft cabin subfloor being an aircraft galley floor.

8. The aircraft cabin subfloor of claim 6 , further comprising:
the air impermeable mat having a peripheral edge; and,
the loop pattern of adhesive being applied to the peripheral edge of the air impermeable mat.

Assignees

• Boeing Co

Inventors

• Koreis Rocke R

Classifications

• B32B3/266

  characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12 · CPC title

• B32B2038/047

  Perforating · CPC title

• B32B7/05

  the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection (using interposed adhesives or bonding materials applied in spaced arrangements B32B7/14) · CPC title

• B32B7/12

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

• B32B2307/7242

  Non-permeable · CPC title