Force level control for an energy absorber for aircraft

1. An energy absorber for an aircraft having a force level control, the energy absorber comprising:

a housing;

an adjustment element;

a first cover plate; and

an energy absorber element for absorption of an acceleration energy by plastic deformation,

wherein the energy absorber element comprises a sheet attached to the housing or to the first cover plate and bent by an angle of approximately 180 degrees within the housing, such that the plastic deformation of the energy absorber element takes place within the housing when the energy absorber element is pulled out of the housing,

wherein via the adjustment element, a bending radius of the energy absorber element is continuously adjustable in the housing, and

wherein a displacement of the first cover plate by actuation of the adjustment element results in an adjustment of the bending radius of the energy absorber element.

2. An energy absorber of for an aircraft having a force level control, the energy absorber comprising:

a housing;

a first adjustment element;

a first cover plate;

a second adjustment element for displacing the first cover plate,

wherein the second adjustment element is actuatable independently from the first adjustment element; and

an energy absorber element for absorption of an acceleration energy by plastic deformation, the energy absorber element comprising a sheet attached to the housing or to the first cover plate and bent by an angle of approximately 180 degrees within the housing such that the plastic deformation of the energy absorber element takes place within the housing when the energy absorber element is pulled out of the housing,

wherein via the first adjustment or the second adjustment element, a bending radius of the energy absorber element is continuously adjustable in the housing.

3. The energy absorber of claim 1 ,

wherein the cover plate has a contact surface formed such that the energy absorber element bends at or near the contact surface upon actuation of the adjustment element.

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

a second energy absorber element;

wherein the housing comprises 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;

a second attachment region;

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

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

6. The energy absorber of claim 5 ,

wherein the energy absorber is configured to be attached to the primary structure or to the inboard device by one or more screws, rivets, or self-locking locking pins.

7. The energy absorber of claim 1 ,

wherein the energy absorber has an energy absorption direction; and

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

8. The energy absorber of claim 2 , wherein a displacement of the first cover plate by actuation of the adjustment element results in an adjustment of the bending radius of the energy absorber element.