FORCE LEVEL CONTROL FOR AN ENERGY ABSORBER FOR AIRCRAFT

摘要

These days, typically strong holders for attachment of inboard devices to the primary structure of an aircraft are used, which may often only ineffectively manage dynamic loads . According to an exemplary embodiment of the present invention, a force level control for an energy absorber (100) is provided for aircraft, which includes an adjustment element (801) and a housing 101;102) , whereby via the adjustment element, a bending radius of the energy absorber element (102) is continuously adjustable in the housing.