| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide an intermediate casing for an aircraft jet engine which remedies at least partially problems relating to the prior art. <P>SOLUTION: This intermediate casing 21 for the aircraft jet engine, includes an outer shell 23 and front and rear flanges 25, 27 which are arranged radially inside with respect to the outer shell. The casing 21 also includes structural arms 17 which extend radially between the flanges as far as the shell 23. The rear flange is equipped with receiving means 34 for receiving a fixing bracket for fixing a rod for absorbing the thrust forces, and the first receiving means include bosses 36 coming from the rear flange, through which bosses through-orifices 38 are formed which are passed through by fixing screws of the bracket. Accordingly, at least one of the bosses 36 extends as far as making contact with one of the structural arms 17. <P>COPYRIGHT: (C)2009,JPO&INPIT</p> |
