| 摘要 |
<p>The invention relates to an assembly for an aircraft nacelle, characterized in that it includes: a flange (30) comprising at least one first portion (31) to be attached to another flange, and a second portion (32) which extends transversely relative to the first portion (31) and which is to be attached onto a panel of said assembly; and a reinforcing plate (330) attached directly, or optionally indirectly, onto the flange via an intermediate plate attached between the reinforcing plate and the flange, said reinforcing plate having a beveled portion opposite the second portion of the flange.</p> |
