| 摘要 |
<p>Rear frame (1) for a deflection cascade-type thrust reverser structure for a turbo jet engine nacelle, said rear frame (1) being intended to support a downstream edge of one or more cascade(s) of deflection vanes and comprising at least an arcuate body (10) made of composite material and having two free ends (11) secured to two respective articulation pieces (13) for a pivoting connection of said rear frame (1) to at least one bearing structure, notable in that the articulation pieces (13) are made as one piece with the arcuate body (10) from composite material. The present invention finds an application in the field of nacelles for aircraft jet engines.</p> |
