Patent ID: 9400066
Filing Date: 2016-07-26
CPC Classification: F16L

Claim Text:
1. A clamping ring for fastening piping in an aircraft, comprising: two jaws shaped and assembled to each other to prevent gliding arcs, the two jaws each including a baseplate with a ridge extending from the baseplate, and the two jaws each including at least one transverse support cut-out for receiving at least one tube, wherein the baseplate is wider than the ridge along a same plane, wherein the at least one transverse support cut-out is disposed on an upper surface of the ridge opposite of the baseplate, wherein the ridge includes a column that extends from the ridge on a first longitudinal side of the ridge relative to the at least one transverse support cut-out, wherein lateral flanks of the ridge include ribs that project from the lateral flanks in an axial direction of the at least one transverse support cut-out, and wherein the baseplate includes a first mounting hole penetrating through the baseplate, the ridge, and the column on the first longitudinal side.