SEAT CUSHION WITH INTEGRATED SEAT FRAME ATTACHMENT STRUCTURE

• US 20130247303A1
• Filed: 03/20/2012
• Published: 09/26/2013
• Est. Priority Date: 03/20/2012
• Status: Active Grant

• Current Assignee: B/E Aerospace Incorporated (Spirit Realty Capital, Inc.)
• Original Assignee: B/E Aerospace Incorporated (Spirit Realty Capital, Inc.)
• Inventors: Pozzi, Alexander N.
• Granted Patent: US 8,782,835 B2
• Time in Patent Office: Days
• US Class Current: 5/653
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/0647 Seats characterised by special upholstery or cushioning features

Abstract

A seat cushion, such as for use in an aircraft passenger seat, including a layer of open cell foam for passenger comfort, a closed cell foam core for flotation and structural support, and support structure positioned on the underside of the seat cushion for directly engaging underlying beams of a seat frame to attach the seat cushion to the seat frame without the need for additional fasteners.

Claims

1. A seat cushion, comprising:

a layer of open cell foam for passenger comfort;

a closed cell foam core for flotation and structural support; and

support structure positioned on the underside of the seat cushion for directly engaging underlying beams of a seat frame to attach the seat cushion to the seat frame.

2. The seat cushion according to claim 1, wherein the support structure comprises a platform that is sheet-like and substantially covers the underside of the seat cushion.

3. The seat cushion according to claim 2, wherein the platform comprises spaced semi-circular portions connected through a middle planar portion, the semi-circular portions shaped to directly engage spaced tubular beams of the seat frame.

4. The seat cushion according to claim 1, wherein the support structure comprises spaced, upwardly-extending curved flanges connected through a center portion, wherein the spaced, upwardly-extending curved flanges are shaped to complement tubular beams of the seat frame for engagement therewith.

5. The seat cushion according to claim 1, wherein the support structure is rigid and unitary.

6. The seat cushion according to claim 1, wherein the support structure comprises a plurality of spaced semi-circular clips.

7. The seat cushion according to claim 1, wherein the support structure has a nominal thickness as compared to the thickness of the top layer of open cell foam and the closed cell foam core.

8. The seat cushion according to claim 1, wherein the support structure snap fit engages the underlying beams of the seat frame.

9. The seat cushion according to claim 1, wherein the support structure is integrated into the seat cushion construction.

10. The seat cushion according to claim 1, wherein the support structure is at least partially encapsulated in one of the top layer of open cell foam and the closed cell foam core.

11. An aircraft passenger seat, comprising:

a seat frame including spaced lateral beams; and

a seat cushion including a top layer of open cell foam for passenger comfort, a closed cell foam core for flotation and structural support, and support structure positioned on the underside of the seat cushion for directly engaging the spaced lateral beams of the seat frame to attach the seat cushion to the seat frame without the need for additional fasteners.

12. The aircraft passenger seat according to claim 11, wherein the support structure is a platform integrated into the seat cushion construction.

13. The aircraft passenger seat according to claim 12, wherein the platform is a unitary sheet substantially covering the underside of the seat cushion.

14. The aircraft passenger seat according to claim 12, wherein the platform comprises spaced semi-circular portions connected through a middle planar portion, the semi-circular portions directly engaging the spaced lateral beams of the seat frame and the planar middle portion spanning the spaced lateral beams of the seat frame.

15. The aircraft passenger seat according to claim 11, wherein the support structure comprises a plurality of spaced semi-circular clips that directly engage the spaced lateral beams of the seat frame.

16. The aircraft passenger seat according to claim 11, wherein the support structure comprises spaced, upwardly-extending curved flanges connected through a center portion, wherein the spaced, upwardly-extending curved flanges are shaped to complement the spaced lateral beams of the seat frame for engagement therewith.

17. The aircraft passenger seat according to claim 11, wherein the support structure is a rigid, sheet-like platform having a nominal thickness as compared to the thickness of the top layer of open cell foam and the closed cell foam core.

18. The aircraft passenger seat according to claim 11, wherein the support structure snap fit engages directly with the spaced lateral beams of the seat frame.

19. The aircraft passenger seat according to claim 11, wherein the support structure is at least partially encapsulated in one of the top layer of open cell foam and the closed cell foam core.