Patent ID: 8561266
Filing Date: 2013-10-22
Classification: F16B,Y10T

Abstract:
1. A holder arrangement of an aircraft or spacecraft, comprising: a structural member of an aircraft or spacecraft having a fastening portion, wherein the structural member is made of carbon fiber reinforced plastics material (CFRP); a holder comprising at least one lower part and at least one upper part which, for the purposes of attachment with a respectively non-positive fit to the fastening portion of the CFRP structural member, are formed so that the fastening portion can be clamped between them; and at least one fixing strip for connection to the fastening portion of the CFRP structural member in a longitudinal direction thereof, wherein the fixing strip has a fixing profile for fixing the holder to the CFRP structural member in the longitudinal direction of the CFRP structural member with a positive fit, and wherein the fixing strip, together with the fixing profile, is connected to the fastening portion of the CFRP structural member with a suitable adhesive or a casting material or is integrally formed in a casting process.