| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a balancing suspension for installing a front fan turbojet engine in a pylon, by using a means capable of reducing local strain of a frame. <P>SOLUTION: The suspension has a front attachment 10 on an intermediate casing, a rear attachment 11 having at least two rear attachment links 114, 115 connected to an outer shell 83 of an exhaust casing 8, and a pair of thrust bars 12, 12' being fixed at their upstream ends to a hub 35 of the intermediate casing 3, and is characterized in that a plane formed by the two links 114, 115 of the rear attachment 11 is inclined with respect to a plane of the exhaust casing 8. <P>COPYRIGHT: (C)2009,JPO&INPIT</p> |
