| 摘要 |
PROBLEM TO BE SOLVED: To improve a conventional device in a mechanical aspect and a manufacturing cost aspect. SOLUTION: The present invention relates to a suspension of a turbo fan engine to an air craft pylon. The suspension includes a fitting 12 arranged to be attached to the pylon, a lever 15 fastened in its central portion 150 to the fitting via a linking means with a pivot pin 150P, and two thrust rods 20 and 22 each of which is connected by an end to the lever and includes the fastening means to the engine at the other end. The linking means is composed on the central portion 150 of the lever, of two parallel branches 151 and 152 apart from one another, and on the fitting, of a central fastening tab 133, whereas the fastening tab and both branches are held together by dint of the pivot pin 150P. COPYRIGHT: (C)2005,JPO&NCIPI
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