Frame component with variable wall thickness

Patent metadata

Field	Value
Publication number	US-2022242576-A1
Application number	US-201917610667-A
Country	US
Kind code	A1
Filing date	May 30, 2019
Priority date	May 30, 2019
Publication date	Aug 4, 2022
Grant date	—

Abstract

Described is a frame component for a passenger seat assembly. The frame includes a tubular frame component having a first portion and a second portion. The bent portion bends the frame at a non-zero angle within a plane. The tubular frame component includes a variable inner diameter such that the first portion of the tubular frame component has a first wall thickness and the bent portion of the tubular frame component has a second wall thickness that is different from the first wall thickness.

First claim

That which is claimed is:

1 . A passenger seat assembly comprising:
a seat base; and a backrest connected to the seat base and comprising a frame, wherein the frame comprises a tubular frame component having a variable inner diameter such that a first portion of the tubular frame component comprises a first wall thickness and a second portion of the tubular frame component comprises a second wall thickness that is different from the first wall thickness.

2 . The passenger seat assembly of claim 1 , wherein the first portion of the tubular frame component is a bent portion bending the frame at a non-zero angle within a plane defined by the backrest.

3 . The passenger seat assembly of claim 2 , wherein the plane is a first plane, wherein the backrest defines a second plane, wherein the bent portion is a first bent portion, and wherein the second portion of the tubular frame component is a second bent portion bending the frame at a non-zero angle within a second plane defined by the backrest.

4 . The passenger seat assembly of claim 1 , wherein the backrest comprises an upper end and a lower end, wherein the first portion at least partially forms the lower end of the backrest, and wherein the second portion at least partially forms the upper end of the backrest.

5 . The passenger seat assembly of claim 1 , wherein the tubular frame component further comprises a third portion between the first portion and the second portion, and wherein the third portion of the tubular frame component comprises a third wall thickness that is greater than the first wall thickness and less than the second wall thickness.

6 . The passenger seat assembly of claim 1 , wherein the first wall thickness and the second wall thickness are between about 0.006 inches and about 0.25 inches.

7 . The passenger seat assembly of claim 1 , wherein the tubular frame component comprises at least one of aluminum, magnesium, titanium, or steel.

8 . A frame for a passenger seat assembly, the frame comprising a tubular frame component comprising:
an inner surface and an outer surface, wherein a distance from the inner surface to the outer surface is a thickness of the tubular frame component; a first portion; and a bent portion bending the frame at a non-zero angle within a plane, and wherein the thickness of the bent portion of the tubular frame component is different from the thickness of the first portion of the tubular frame component.

9 . The frame of claim 8 , wherein the thickness of the bent portion of the tubular frame component is greater than the thickness of the first portion of the tubular frame component.

10 . The frame of claim 9 , wherein the first portion is a non-bent portion of the tubular frame component.

11 . The frame of claim 8 , wherein the thickness of the tubular frame component is from about 0.006 inches to about 0.25 inches.

12 . The frame of claim 8 , wherein the bent portion is a first bent portion and the plane is a first plane, wherein the tubular frame component further comprises a second bent portion bending the frame at a non-zero angle within a second plane, and wherein the thickness of the second bent portion of the tubular frame component is different from the thickness of the first portion of the tubular frame component.

13 . The frame of claim 12 , wherein the first portion is between the first bent portion and the second bent portion.

14 . The frame of claim 12 , wherein the thickness of the second bent portion is greater than the thickness of the first portion and less than the thickness of the second bent portion.

15 . A frame for a passenger seat assembly the frame comprising a tubular frame component comprising:
a first portion; and a bent portion bending the frame at a non-zero angle within a plane, wherein the tubular frame component comprises a variable inner diameter such that the first portion of the tubular frame component comprises a first wall thickness and the bent portion of the tubular frame component comprises a second wall thickness that is different from the first wall thickness.

16 . The frame of claim 15 , wherein the bent portion is a first bent portion and the plane is a first plane, wherein the tubular frame component further comprises a second bent portion bending the frame at a non-zero angle within a second plane and comprising a third wall thickness.

17 . The frame of claim 16 , wherein the third wall thickness is less than at least one of the first wall thickness or the second wall thickness.

18 . The frame of claim 17 , wherein the first portion is between the first bent portion and the second bent portion and wherein the third wall thickness is less than both the first wall thickness and the second wall thickness.

19 . The frame of claim 18 , wherein the first wall thickness and the second wall thickness are less than or equal to about 0.25 inches.

20 . The frame of claim 15 , wherein the frame comprises at least one of a backrest frame or a luggage bar frame.

Assignees

• Safran Seats Usa Llc

Inventors

• Tranier Romain
• Mansouri Reza
• Parker Charles Michael

Classifications

• B60N2/68

  Seat frames · CPC title

• B60N2/22

  the back-rest being adjustable {(B60N2/2878 takes precedence)} · CPC title

• B64D11/0649 Primary

  Seats characterised by special features for reducing weight · CPC title

• B64D11/06 Primary

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title