Energy absorber for aircraft

1. An energy absorber for an aircraft, the energy absorber comprising:

a first energy absorber element, a second energy absorber element, a third energy absorber element, and a fourth energy absorber element, wherein all four energy absorber elements are adapted for absorption of an acceleration energy by plastic deformation; and

a housing,

wherein the energy absorber elements are configured to undergo plastic deformation within the housing, and

wherein the first energy absorber element is disposed adjacent to the second energy absorber element, and wherein the third energy absorber element is disposed adjacent to the fourth energy absorber element such that the respective, adjacent energy absorber elements are braced against one another during rolling motion,

wherein the first energy absorber element has a longitudinal slit, and

wherein the housing further has an intermediate wall, which is mounted in the region of the slit.

2. The energy absorber of claim 1 , further comprising:

a fifth energy absorber element and a sixth energy absorber element, which are arranged adjacent to one another so that they are braced against one another with rolling motion.

3. The energy absorber of claim 1 , further comprising:

a fifth energy absorber element and a sixth energy absorber element;

wherein the fifth energy absorber element is inlaid in the first energy absorber element; and

wherein the sixth energy absorber element is inlaid in the second energy absorber element.

4. The energy absorber of claim 1 ,

wherein the housing includes a first cover plate, a second cover plate and a fixed support for the second energy absorber element and the first energy absorber element.

5. The energy absorber of claim 1 , further comprising:

a first attachment region; and

a second attachment region;

wherein the first attachment region is configured for attachment of the energy absorber to a primary structure; and

wherein the second attachment region is configured for attachment of the energy absorber to an interior device.

6. The energy absorber of claim 1 further comprising:

one or more of screws, rivets, or self-locking locking pins for attaching the energy absorber to a primary structure or to an interior device.

7. The energy absorber of claim 1 ,

wherein the energy absorber has an energy absorption direction; and

wherein upon exceeding of a minimal force, which acts in the direction of the energy absorption direction, an energy absorption occurs through the energy absorber.

8. A method for energy absorption in an aircraft, comprising:

pulling-out of a first energy absorber element, a second energy absorber element, a third energy absorber element and a fourth energy absorber element from a housing;

absorbing an acceleration energy by plastic deformation of the first energy absorber element and of the second energy absorber element within the housing during the pulling-out; and

continuously adjusting a bending radius of at least one of the energy absorber elements via an adjustable element,

wherein the first energy absorber element is disposed adjacent to the second energy absorber element, and wherein the third energy absorber element is disposed adjacent to the fourth energy absorber element, so that the respective, adjacent energy absorber elements are braced against one another during rolling motion.

9. An energy absorber for an aircraft, the energy absorber comprising:

a first energy absorber element, a second energy absorber element, a third energy absorber element, and a fourth energy absorber element, wherein all four energy absorber elements are adapted for absorption of an acceleration energy by plastic deformation;

an adjustment element; and

a housing,

wherein the energy absorber elements are configured to undergo plastic deformation within the housing,

wherein the first energy absorber element is disposed adjacent to the second energy absorber element, and wherein the third energy absorber element is disposed adjacent to the fourth energy absorber element such that the respective, adjacent energy absorber elements are braced against one another during rolling motion, and

wherein via the adjustment element a bending radius of the energy absorber element is continuously adjustable.

10. The energy absorber of claim 9 , further comprising:

a fifth energy absorber element and a sixth energy absorber element arranged adjacent to one another so that they are braced against one another with rolling motion.

11. The energy absorber of claim 9 , further comprising:

a fifth absorber element and a sixth energy absorber element;

wherein the fifth energy absorber element is inlaid in the first energy absorber element; and

wherein the sixth energy absorber element is inlaid in the second energy absorber element.

12. The energy absorber of claim 9 ,

wherein the housing includes a first cover plate, a second cover plate and a fixed support for the second energy absorber element and the first energy absorber element.

13. The energy absorber of claim 9 , further comprising:

a first attachment region; and

a second attachment region;

wherein the first attachment region is configured for attachment of the energy absorber to a primary structure; and

wherein the second attachment region is configured for attachment of the energy absorber to an interior device.

14. The energy absorber of claim 9 further comprising:

one or more screws, rivets, or self-locking pins for attaching the energy absorber to a primary structure or to an interior device.

15. The energy absorber of claim 9 ,

wherein the energy absorber has an energy absorption direction; and

wherein upon exceeding of a minimal force, which acts in the direction of the energy absorption direction, an energy absorption occurs through the energy absorber.