Patent ID: 9212680
Filing Date: 2015-12-15
Classification: B64D,F16B

Abstract:
1. A tie bar for purposes of connecting an equipment fitting of an equipment module to a structure fitting of a fuselage cell structure of an aeronautical vehicle, comprising: a fork head at each end of the tie bar, each fork head having two fork head holes for purposes of accommodating a bolt, and a spacing between the fork heads that can be continuously adjusted, the fork head holes of at least one fork head having a captive bushing for purposes of sound and vibration decoupling, wherein each bushing has a hollow cylindrical base body having a shank with a peripheral annular bead in at least some sections disposed approximately on the central region of the shank height of the base body such that the peripheral bead causes a snapping into place of the bushing into the fork head holes, and a structure fitting disposed between the fork heads and retained between the bushings, the structure fitting having cooperating arcuate surfaces, wherein a relative movement between the arcuate surfaces allows an angular displacement between the structure fitting and the associated fork head.