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 comprising a frame, the seat being for an aircraft, the frame comprising 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; 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 third portion defines an inner diameter that is greater than an inner diameter defined by the second portion, and wherein the third portion comprises a third wall thickness that is greater than the first wall thickness.
2. The seat of claim 1 , wherein the third wall thickness of the third portion is the same 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 frame.
6. A seat for an aircraft, the seat comprising a seat base, the seat base comprising a base frame tube, wherein the base frame tube comprises a wall, the wall comprising:
a first portion having a first wall thickness;
a second portion, 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 third portion comprises a third wall thickness that is greater than the first wall thickness.
7. The seat of claim 6 , wherein the outer diameter of the third portion is greater than the outer diameter of both the first portion and 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 a 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 tube, wherein the base frame tube comprises:
a first portion having a first inner diameter and a first outer diameter;
a second portion having a second inner diameter and a second outer diameter; and
a third portion having a third inner diameter and a third outer diameter,
wherein the first inner diameter is different from the second inner diameter,
wherein the first outer diameter is the same as the second outer diameter,
wherein the first inner diameter is the same as the third inner diameter, and
wherein the first outer diameter is different from the third outer diameter.
13. The seat of claim 12 , wherein the seat base further comprises a base frame, 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.
14. The seat of claim 12 , wherein the third portion is capable of preventing the base frame tube from decoupling from a base frame.
15. The seat of claim 12 , wherein the base frame tube is made from at least one of aluminum or steel.
16. The seat of claim 12 , wherein the base frame tube is made from a cold form drawing process.