| 摘要 |
The present invention relates to an axisymmetric nozzle with adjustable cross-section intended to equip a turbomachine and including at least one ring of flaps, said ring of flaps including a series of operated flaps (3) and a series of interposed follower flaps (5), each follower flap (5) straddling the internal surfaces of the two adjacent operated flaps (3) and being held on the said operated flaps by fastening means, characterised in that the means for fastening a follower flap (5) include a double pin (6) acting like a spring for holding the said follower flap (5) against the internal surfaces of the two adjacent operated flaps (3), the said pin (6) including, upstream, two end portions (11, 12) articulated respectively to the two adjacent operated flaps (3) and, downstream, a middle portion (15) fixed to the said follower flap (5) by fixing means (17). <IMAGE> |
