Patent ID: 6884024

Claim:
An arrangement for fastening struts serving as bearing carriers for a bearing of a rotor of an aeronautical gas turbine to a casing structure of the aeronautical gas turbine, comprising: a first stop face arranged in a circumferential direction of the rotor and arranged at an end face facing away from the rotor bearing; a second stop face arranged in an axial direction of the rotor and arranged at the end face facing away from the rotor bearing; a third stop face arranged on the casing structure of the aeronautical gas turbine assigned to and matching the first stop face; a fourth stop face arranged on the casing structure of the aeronautical gas turbine assigned to and matching the second stop face; and at least one screw connection inclined at an angle to a parting plane between the casing structure and the end face and configured to hold at least two of the stop faces in bearing contact and to releasably fasten the strut to the casing structure.