Abstract: The invention relates to a method for producing glass fibers that laterally emit light and to glass fibers produced according to said method.

Abstract: The invention relates to a method for producing glass fibers that laterally emit light and to glass fibers produced according to said method.

Abstract: An energy absorber for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure and the respective inboard devices is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.

Abstract: An energy absorber for aircraft includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing.

Abstract: To allow a user to select a route to the destination himself, an exemplary embodiment relates to a method for assisting a user in arriving at a destination point within a time limit. The exemplary method comprises receiving a determined position and the destination point. The exemplary method also comprises estimating an accessible geographic area which can be traversed by the user with a predetermined speed before reaching the destination within the time limit, when starting from the determined position. The exemplary method additionally comprises providing information on the estimated accessible area for presentation to the user. Furthermore, exemplary embodiments of the invention relate to a computer program and a system for executing the method.

Abstract: An energy absorber for aircraft includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing.

Abstract: A force level control for an energy absorber is provided for aircraft, and includes an adjustment element and a housing, whereby via the adjustment element, a bending radius of the energy absorber element is continuously adjustable in the housing.

Abstract: An energy absorber for aircraft, which includes one or more energy absorber elements and a housing, whereby the energy absorber elements can absorb crash impulses by plastic deformation within the housing. Thus, the load on the primary structure and the respective inboard devices is limited, which can lead to an increased, passive safety of the passengers and a weight reduction.