公开(公告)号：WO2017162862A1

公开(公告)日：2017-09-28

申请号：PCT/EP2017/057100

申请日：2017-03-24

Applicant: AUXITROL S.A.

Inventor： GUILLOU, Sébastien ,  DIJON, Sébastien ,  VALLET, Isabelle

IPC: B64D15/00 ,  B64D43/00 ,  G01P5/16 ,  G01P13/02 ,  G01K13/02

CPC classification number: B64D15/00 ,  B23K26/355 ,  B64D43/00 ,  G01K13/028 ,  G01P5/16 ,  G01P13/025

Abstract: The invention concerns an aircraft probe for resisting formation and propagation of ice comprising: • a base that is intended to be attached to an aircraft; • a housing extending from the base, said housing comprising:  a body extending from a leading edge of the housing to a trailing edge of the housing, defining at least an airfoil portion extending at least partially from the base to the end of the housing;  an airflow inlet having a first surface facing to an incoming airflow;  a primary airflow passage from the airflow inlet to a primary airflow outlet; and  a sensor assembly disposed within a sensor flow passage; wherein the surface of said housing having functional properties, said functional properties comprising hydrophobic or superhydrophobic and or icephobic or omniphobic, or hydrophilic properties characterized in that said surface functional properties are induced partly or wholly by laser treatment of the surface and wherein surface functional properties are arranged in topographical patterns.

Abstract translation: 本发明涉及一种用于抵抗冰的形成和传播的飞机探测器，其包括：·用于附接到飞机上的基座; ·从基座延伸的壳体，所述壳体包括：·从壳体的前缘延伸到壳体的后缘的主体，限定至少部分地从基座延伸到壳体的端部的翼型部分 ; 具有面向进入气流的第一表面的气流入口; 从气流入口到主气流出口的主气流通道; 以及设置在传感器流道内的传感器组件; 其中所述外壳的表面具有功能性质，所述功能性质包括疏水性或超疏水性和/或疏冰性或疏水性或亲水性，其特征在于所述表面功能性部分地或全部地通过表面的激光处理来诱导，并且其中表面功能性 以地形图案排列。