Seat bottom assembly with self tensioning diaphragm and under seat access

Patent metadata

Field	Value
Publication number	US-12371168-B1
Application number	US-202418412874-A
Country	US
Kind code	B1
Filing date	Jan 15, 2024
Priority date	Jan 15, 2024
Publication date	Jul 29, 2025
Grant date	Jul 29, 2025

Abstract

A seat bottom assembly including a first frame subassembly and a second frame subassembly supported by and rotatably coupled to the first frame subassembly about a rotation axis, the second frame subassembly configured to rotate about the rotation axis between a first position and a second position. A fabric diaphragm has a fore end connected to the second frame subassembly and an aft end connected to the first frame subassembly. The rotation axis is positioned forward of the connection of the aft end of the fabric diaphragm to the first frame subassembly, such that when the second frame subassembly is in the first position the fabric diaphragm is stretched, and when the second frame subassembly is in the second position the fabric diaphragm is relaxed. In use, the first position may correspond to sitting and the second position may correspond to under seat access.

First claim

What is claimed is:

1. A seat bottom assembly, comprising:
a first frame subassembly;
a second frame subassembly rotatably coupled to the first frame subassembly about a rotation axis, wherein the second frame subassembly is configured to rotate about the rotation axis between a first position in which the first and second frame subassemblies are substantially coplanar, and a second position in which the second frame subassembly is rotated upward; and
a fabric diaphragm having a fore end connected to the second frame subassembly, and an aft end connected to the first frame subassembly;
wherein the rotation axis is positioned forward of the connection of the aft end of the fabric diaphragm to the first frame subassembly, such that when the second frame subassembly is in the first position the fabric diaphragm is stretched, and when the second frame subassembly is in the second position the fabric diaphragm is relaxed.

2. The seat bottom assembly according to claim 1 , wherein the rotation axis is positioned above a plane of the fabric diaphragm when the second frame subassembly is in the first position.

3. The seat bottom assembly according to claim 1 , wherein the first frame subassembly is stationary.

4. The seat bottom assembly according to claim 1 , wherein the first frame subassembly comprises:
left and right frame members; and
fore and aft frame tubes;
wherein the aft end of the fabric diaphragm is connected to the aft frame tube.

5. The seat bottom assembly according to claim 4 , wherein the second frame subassembly comprises:
left and right frame members; and
a fore frame tube;
wherein the fore end of the fabric diaphragm is connected to the fore frame tube of the second frame subassembly; and
wherein the left and right frame members of the second frame subassembly are rotatably coupled to the left and right frame members of the first frame subassembly, respectively.

6. The seat bottom assembly according to claim 5 , wherein the left and right frame members of the second frame subassembly are positioned inward of the left and right frame members of the first frame subassembly, respectively.

7. The seat bottom assembly according to claim 5 , wherein left and right lateral sides of the fabric diaphragm are connected to the left and right frame members of the second frame subassembly, respectively.

8. The seat bottom assembly according to claim 1 , wherein each of the fore end and the aft end of the fabric diaphragm includes a transverse sleeve configured to receive a frame member of its respective one of the first frame subassembly and the second frame subassembly to connect the fabric diaphragm to the first and second frame subassemblies.

9. The seat bottom assembly according to claim 1 , wherein, when the second frame subassembly is in the first position:
the fore frame tube of the second frame subassembly is positioned forward of the fore frame tube of the first frame subassembly; and
each of the left and right frame members of the second frame subassembly rests on the fore frame tube of the first frame subassembly.

10. The seat bottom assembly according to claim 1 , wherein:
the first position corresponds to sitting; and
the second position corresponds to under seat access.

11. A seat bottom assembly for an aircraft passenger seat, comprising:
a first frame subassembly configured to be connected to an aircraft passenger seat frame;
a second frame subassembly rotatably coupled to the first frame subassembly about a rotation axis, wherein the second frame subassembly is configured to rotate about the rotation axis between a first position in which the first and second frame subassemblies are substantially coplanar for sitting, and a second position in which the second frame subassembly is rotated upward for under seat access; and
a fabric diaphragm having a fore end connected to the second frame subassembly, and an aft end connected to the first frame subassembly;
wherein the rotation axis is positioned forward of the connection of the aft end of the fabric diaphragm to the first frame subassembly, such that when the second frame subassembly is in the first position the fabric diaphragm is stretched, and when the second frame subassembly is in the second position the fabric diaphragm is relaxed.

12. The seat bottom assembly according to claim 11 , wherein the rotation axis is positioned above a plane of the fabric diaphragm when the second frame subassembly is in the first position.

13. The seat bottom assembly according to claim 11 , wherein:
the first frame subassembly comprises:
left and right frame members; and
fore and aft frame tubes;
wherein the aft end of the fabric diaphragm is connected to the aft frame tube; and

the second frame subassembly comprises:
left and right frame members; and
a fore frame tube;
wherein the fore end of the fabric diaphragm is connected to the fore frame tube of the second frame subassembly; and
wherein the left and right frame members of the second frame subassembly are rotatably coupled to the left and right frame members of the first frame subassembly, respectively.

14. The seat bottom assembly according to claim 13 , wherein the left and right frame members of the second frame subassembly are positioned inward of the left and right frame members of the first frame subassembly, respectively.

15. The seat bottom assembly according to claim 13 , wherein left and right lateral sides of the fabric diaphragm are connected to the left and right frame members of the second frame subassembly, respectively.

16. The seat bottom assembly according to claim 13 , wherein:
each of the fore end and the aft end of the fabric diaphragm includes a transverse sleeve;
the transverse sleeve of the fore end of the fabric diaphragm is configured to receive the fore frame tube of the second frame subassembly; and
the transverse sleeve of the aft end of the fabric diaphragm is configured to receive the aft frame tube of the first frame subassembly.

17. The seat bottom assembly according to claim 11 , wherein, when the second frame subassembly is in the first position:
the fore frame tube of the second frame subassembly is positioned forward of the fore frame tube of the first frame subassembly; and
each of the left and right frame members of the second frame subassembly rests on the fore frame tube of the first frame subassembly.

Assignees

• Be Aerospace Inc

Inventors

• Suhre Ryan J
• Poole David J
• Valdes De La Garza Javier

Classifications

• A47C7/56

  Parts or details of tipping-up chairs, e.g. of theatre chairs · CPC title

• B64D11/064

  Adjustable inclination or position of seats · CPC title

• A47C7/282

  with mesh-like supports, e.g. elastomeric membranes · CPC title

• A47C4/28

  Folding chairs with flexible coverings for the seat or back elements · CPC title

• A47C4/42

  having a frame made of metal · CPC title