Holder arrangement for air or spacecraft, has structural element of air or spacecraft which has fastening section, where holder has lower portion and upper portion, and lower and upper portions are formed to clamp each other

摘要

The holder arrangement has a structural element (22) of an air or spacecraft which has a fastening section (23). A holder has a lower portion (2) and an upper portion (8). The lower and upper portions are formed to clamp each other for the force-fit attaching to the fastening section of the structural element. A fixing bar (20) is connected with the fastening section of the structural element, where a fixing profile (21) is provided for a form-fit fixing of the holder to the structural element in the longitudinal direction.