Vehicle seat tubing having variable wall thickness
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.
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.