公开(公告)号：US20130230390A1

公开(公告)日：2013-09-05

申请号：US13872325

申请日：2013-04-29

Applicant: AIRCELLE

Inventor： Florent Bouillon ,  Caroline Coat

IPC: F01D25/02

CPC classification number: F01D25/02 ,  B29C70/24 ,  B29C70/88 ,  B29K2995/0013 ,  B64D33/02 ,  B64D2033/0233 ,  B64D2033/0286 ,  Y02T50/43

Abstract: A leading edge structure for an air inlet of an aircraft nacelle includes a leading edge and an inner partition defining a longitudinal compartment that is located inside the leading edge and accommodates a de-icing and/or anti-icing mat. The leading edge structure includes a multi-axial composite structure placed on top of a heating element for anti-icing and/or de-icing.

Abstract translation: 用于飞机机舱的空气入口的前缘结构包括前缘和内部分隔板，其限定位于前缘内部并容纳除冰和/或防冰垫的纵向隔室。 前缘结构包括放置在用于防冰和/或除冰的加热元件顶部的多轴复合结构。