| 摘要 |
Case structure of an aircraft, comprising: a shell ring surrounding the engine and comprising a plurality of sectors (12A, 12B), a number of radial arms (14), each mounted between two adjacent shell ring sectors and each having a base (14A), a number of means for fastening these shell ring sectors to the bases of the radial arms, these fastening means having a number of mounting plates (20) that are each mounted in a flush manner in grooves (22) with a shape corresponding to the shell ring sectors and a set of cap screws (26A-26D) that are held captive by the mounting plate as a result of a difference in diameter between the body and the thread of said screws, a set of captive nuts being fixed to the bases so as to ensure, by each receiving the thread of a captive screw of this set of cap screws, a secure connection between the shell ring sectors and the radial arms. |
