Gas pressure container and tube element for an airbag system, and method for producing same
A gas pressure container for an airbag system of a motor vehicle is disclosed having a tube element with a high bursting resistance when internal pressure is being applied. The tube element includes a steel alloy and a first longitudinal portion of the tube element has a tensile strength Rm, 11 higher than (>) 800 MPa, a transition temperature Tu, 11 of at least −40° C., and an outer circumference U1. The tube element also includes at least one second longitudinal portion and/or additional longitudinal portions, which extend axially from the first longitudinal portion. The second longitudinal portion or the additional longitudinal portions and the first longitudinal portion are formed from a seamless or welded single-piece tube made of a uniform material, and more specifically from a hot-rolled or cold-drawn tube.
1. A gas pressure container for an airbag system of a motor vehicle, the gas pressure container comprising:
a tube element with high bursting resistance when internal pressure is applied,
wherein the tube element is of a steel alloy,
wherein the tube element includes at least one first longitudinal portion which comprises
a tensile strength which is greater than 800 MPa,
a transition temperature of lower than −40° C., and
an outer circumference,
wherein the tube element further includes a second longitudinal portion which extends axially from the first longitudinal portion,
wherein the second longitudinal portion and the first longitudinal portion form a monolithic seamless or welded tube,
wherein the second longitudinal portion comprises an outer circumference which is reduced compared to the outer circumference of the first longitudinal portion,
wherein the second longitudinal portion comprises a transition temperature lower than −50° C. and lower than the transition temperature of the first longitudinal portion, and
wherein the second longitudinal portion is on an end of the tube element.
2. The gas pressure container as claimed in claim 1 ,
wherein the tube element further includes at least one third longitudinal portion which extends axially from the first longitudinal portion,
wherein the third longitudinal portion and the first longitudinal portion form a monolithic seamless or welded tube, and
wherein the third longitudinal portion comprises
an outer circumference which is reduced compared to the outer circumference of the first longitudinal portion, and
a transition temperature lower than −50° C. and lower than the transition temperature of the first longitudinal portion.
3. The gas pressure container as claimed in claim 2 ,
wherein the tube element includes two third longitudinal portions, and
wherein the following correlation applies:
U 12 =(0.6−0.9)× U 11 , and/or
U 13 =(0.6−0.9)× U 11 , and/or
U 16 =(0.65−0.95)× U 11 ,
where
U 11 is the outer circumference of the first longitudinal portion,
U 12 is the outer circumference of the second longitudinal portion,
U 13 is the outer circumference of one of the third longitudinal portions, and
U 16 is the outer circumference of another of the third longitudinal portions.
4. The gas pressure container as claimed in claim 2 ,
wherein a wall thickness of the first longitudinal portion is less than a wall thickness of the second longitudinal portion and/or a wall thickness of the third-longitudinal portion.
5. The gas pressure container as claimed in claim 4 ,
wherein the wall thickness of the second longitudinal portion and/or the wall thickness of the third longitudinal portion is at least 5% greater than the wall thickness in the first longitudinal portion.
6. The gas pressure container as claimed in claim 2 ,
wherein a wall thickness of the first longitudinal portion is greater than or equal to a wall thickness of the second longitudinal portion and/or a wall thickness of the third longitudinal portion.
7. The gas pressure container as claimed in claim 2 ,
wherein the tube element further includes a transition portion having an outer circumference that increases continuously in the direction of the first longitudinal portion, and
wherein the transition portion is arranged between the second longitudinal portion and the first longitudinal portion and/or between the third longitudinal portion and the first longitudinal portion.
8. The gas pressure container as claimed in claim 7 ,
wherein a transition region is located in the transition portion, and
wherein the transition portion comprises a width which is greater than a width of the transition region.
9. The gas pressure container as claimed in claim 2 ,
wherein the third longitudinal portion is a local predetermined breaking point arranged in a center of the gas pressure container when internal pressure is applied in the gas pressure container.
10. The gas pressure container as claimed in claim 1 ,
wherein the end of the tube element with the second longitudinal portion is a first end of the tube element,
wherein the tube element further includes a third longitudinal portion on a second end of the tube element, and
wherein the first longitudinal portion is a center portion between the second and third longitudinal portions.
11. The gas pressure container as claimed in claim 1 ,
wherein the tube element includes two first longitudinal portions between which the second longitudinal portion and/or a third longitudinal portion of the tube element extends, the third longitudinal portion having a reduced outer circumference compared to the outer circumference of the two first longitudinal portions.
12. The gas pressure container as claimed in claim 1 ,
wherein the following applies:
deformability, 12 >1.05×deformability, 11 ,
where
deformability, 11 is a plastic deformability of the first longitudinal portion in a circumferential direction of the tube element, and
deformability, 12 is a plastic deformability of the second longitudinal portion in the circumferential direction.
13. The gas pressure container as claimed in claim 1 ,
wherein the first longitudinal portion and/or the second longitudinal portion comprises/comprise a metallic microstructure with a surface portion of at least 70 percent tempered martensite.
14. The gas pressure container as claimed in claim 1 ,
wherein the following applies:
Rm, 12 <0.9 ×Rm, 11 ,
where
Rm, 11 is the tensile strength of the first longitudinal portion, and
Rm, 12 is a tensile strength of the second longitudinal portion.
15. The gas pressure container as claimed in claim 1 ,
wherein the tube element further includes a transition region having a tensile strength that continuously increases,
wherein the transition region is arranged between the second longitudinal portion and the first longitudinal portion, and
wherein the transition region comprises a width which is between 10 and 100 mm.
16. The gas pressure container as claimed in claim 1 ,
wherein the second longitudinal portion of the tube element comprises a mixed ferrite-perlite microstructure with a surface portion of at least 70 percent.
17. The gas pressure container as claimed in claim 1 ,
wherein the tube element includes a further longitudinal portion which comprises
a notch in a lateral surface of the tube element, and
an outer circumference with the notch being enlarged compared to the outer circumference of the first longitudinal portion.
18. The gas pressure container as claimed in claim 1 ,
wherein the tube element further includes a transition region having a tensile strength that continuously increases,
wherein the transition region is arranged between the second longitudinal portion and the first longitudinal portion, and
wherein the transition region comprises a width which is between 15 and 40 mm.