公开(公告)号：US20150367947A1

公开(公告)日：2015-12-24

申请号：US14762085

申请日：2014-01-20

Applicant: Airbus Operations SAS ,  AIRBUS SAS

Inventor： Virginie Audart-Noel ,  Benoit Letay ,  Loïc Dussol ,  Michael Galinier ,  Nicolas Viallet ,  Laurent Cazeaux ,  Benjamin Vignoboul

IPC: B64D27/26 ,  B64D29/02 ,  B64D45/00 ,  B64D27/18

CPC classification number: B64D27/26 ,  B64D27/18 ,  B64D29/02 ,  B64D29/06 ,  B64D33/04 ,  B64D45/00 ,  B64D2045/009

Abstract: A seal is interposed between two surfaces of an aircraft propulsion assembly. The seal includes at least two layers each comprising a plurality of strands made of a heat-resistant material, the strands of a first layer being oriented in a first orientation and the strands of a second layer being oriented in a second orientation different than the first orientation.

Abstract translation: 在飞行器推进组件的两个表面之间插入密封件。 密封件包括至少两层，每层包括由耐热材料制成的多根股线，第一层的股线以第一取向取向，而第二层的股线被定向成不同于第一取向的第二取向 方向。