Vehicle seat tubing having variable wall thickness

Patent metadata

Field	Value
Publication number	US-10392115-B2
Application number	US-201816100547-A
Country	US
Kind code	B2
Filing date	Aug 10, 2018
Priority date	Apr 8, 2009
Publication date	Aug 27, 2019
Grant date	Aug 27, 2019

Abstract

Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

First claim

What is claimed is:

1. A seat for an aircraft, the seat comprising:
a base frame; and
a base frame tube, the base frame tube comprising:
a first portion having a first wall thickness;
a second portion having a second wall thickness that is greater than the first wall thickness, wherein the first portion defines an inner diameter that is greater than an inner diameter defined by the second portion; and
a third portion having an outer diameter that is greater than an outer diameter of at least one of the first portion or the second portion,

wherein the base frame tube is supported at a first location on the base frame, and wherein the base frame is configured to connect with a back frame for a seat back of the seat at a second location such that the base frame tube is not directly connected to the back frame.

2. The seat of claim 1 , wherein the third portion is the same thickness as the second wall thickness.

3. The seat of claim 1 , wherein the base frame tube is made from at least one of aluminum or steel.

4. The seat of claim 1 , wherein the base frame tube is made from a cold form drawing process.

5. The seat of claim 1 , wherein the third portion is capable of preventing the base frame tube from decoupling from another component of the base frame.

6. A seat for an aircraft, the seat comprising a seat base, the seat base comprising:
a base frame; and
a base frame tube supported by the base frame, wherein the base frame tube comprises a wall, the wall comprising a first portion having a first wall thickness and a second portion having a second wall thickness that is greater than the first wall thickness, wherein the first portion defines an inner diameter that is greater than an inner diameter defined by the second portion, and
wherein the base frame tube is supported at a first location on the base frame, and wherein the base frame is configured to connect with a back frame for a seat back of the seat at a second location that is different from the first location.

7. The seat of claim 6 , wherein the base frame tube further comprises a third portion having an outer diameter that is greater than an outer diameter of at least one of the first portion or the second portion.

8. The seat of claim 7 , wherein the third portion is the same thickness as the second wall thickness.

9. The seat of claim 7 , wherein the third portion is capable of preventing the base frame tube from decoupling from the base frame.

10. The seat of claim 6 , wherein the base frame tube is made from at least one of aluminum or steel.

11. The seat of claim 6 , wherein the base frame tube is made from a cold form drawing process.

12. A seat for an aircraft, the seat comprising a seat base, the seat base comprising:
a base frame; and
a base frame tube supported by the base frame, wherein the base frame tube comprises:
a first portion having a first thickness;
a second portion having a second thickness; and
a middle portion between the first portion and the second portion, the middle portion having a third thickness that is less than the first thickness and the second thickness,

wherein the base frame tube is supported at a first location on the base frame, and wherein the base frame is configured to connect with a back frame for a seat back of the seat at a second location that is different from the first location.

13. The seat of claim 12 , wherein the second thickness is greater than the first thickness.

14. The seat of claim 13 , wherein the first portion defines an inner diameter that is greater than an inner diameter defined by the second portion.

15. The seat of claim 12 , wherein the middle portion defines an outer diameter that is greater than an outer diameter of at least one of the first portion or the second portion.

16. The seat of claim 12 , wherein the middle portion is capable of preventing the base frame tube from decoupling from the base frame.

17. The seat of claim 12 , wherein the base frame tube is made from at least one of aluminum or steel.

18. The seat of claim 12 , wherein the base frame tube is made from a cold form drawing process.

Assignees

• C&D Zodiac Inc

Inventors

• Le Gary Tien
• Krikorian Aram Aris

Classifications

• B64D11/0649

  Seats characterised by special features for reducing weight · CPC title

• B60N2/68

  Seat frames · CPC title

• B60R21/026

  Rigid partitions inside vehicles, e.g. between passengers and load compartments (B60R21/12 takes precedence) · CPC title

• B64D11/0648 Primary

  Lower frame constructions · CPC title

• B64D11/06

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