公开(公告)号：US20160208738A1

公开(公告)日：2016-07-21

申请号：US14703144

申请日：2015-05-04

Applicant: AIRCELLE

Inventor： Vincent PEYRON ,  Laurent Georges VALLEROY ,  Bouziane BEHRAOUI

IPC: F02K1/54 ,  F01D25/24

CPC classification number: F02K1/54 ,  B64D29/06 ,  F01D25/24 ,  F05D2220/323 ,  F05D2260/50

Abstract: The present disclosure concerns an assembly including at least one unit assembly of a nacelle for a turbojet engine, and the assembly is movable relative to a fixed structure along at least one associated guide assembly. The guide assembly includes: at least one guiding element secured to the fixed structure; at least one guided element secured to the unit assembly, shaped so as to move along the guiding element; at least one contact surface common to said guiding and guided elements. In particular, the guided element and the guiding element present each at least one profile, and the profiles is non-complementary to each other at least at the contact surface, the profiles being shaped so as to achieve at least one plane abutment connection at least during circumferential forces of the unit assembly.

Abstract translation: 本公开涉及一种组件，其包括用于涡轮喷气发动机的机舱的至少一个单元组件，并且该组件可沿着至少一个相关联的引导组件相对于固定结构移动。 导向组件包括：固定到固定结构的至少一个引导元件; 固定到所述单元组件的至少一个被引导元件成形为沿着所述引导元件移动; 所述引导和引导元件共同的至少一个接触表面。 特别地，引导元件和引导元件至少呈现至少一个轮廓，并且轮廓至少在接触表面处彼此不互补，轮廓被成形为至少实现至少一个平面邻接连接 在单元组件的周向力期间。