公开(公告)号：US20150210400A1

公开(公告)日：2015-07-30

申请号：US14678200

申请日：2015-04-03

Applicant: AIRCELLE

Inventor： Patrick Gonidec ,  Bertrand Desjoyeaux ,  Caroline Coat-Lenzotti

IPC: B64D15/16 ,  F01D25/00 ,  B64D29/06

CPC classification number: B64D15/16 ,  B64D15/04 ,  B64D15/12 ,  B64D29/06 ,  B64D33/02 ,  B64D2033/0233 ,  F01D25/005

Abstract: The present disclosure concerns a component of an aircraft nacelle formed from at least one composite structure and one heating element. The nacelle includes frost protector, and the composite structure has a matrix reinforced by at least a material of which the heat conductivity at ambient temperature that is greater than or equal to 800 W·m−1·K−1, so as to provide transverse heat conductivity within the nacelle.

Abstract translation: 本公开涉及由至少一个复合结构和一个加热元件形成的飞机机舱的部件。 机舱包括防霜保护器，复合结构具有通过至少一种在环境温度下的导热率大于或等于800W·m-1·K-1的材料来增强的基体，从而提供横向 机舱内的导热系数。

公开(公告)号：US10214293B2

公开(公告)日：2019-02-26

申请号：US14877098

申请日：2015-10-07

Applicant: AIRCELLE

Inventor： Audrey Riquet ,  Caroline Coat-Lenzotti

IPC: B64D15/00 ,  F02C7/04 ,  B64D33/02

Abstract: The present disclosure provides an aircraft element including a leading edge section and a trailing edge section, and the leading edge section includes an anti-frost treatment device. This aircraft element is remarkable in that the trailing edge section includes a superhydrophobic surface.