发明名称 |
Method for making a nacelle de-icing element |
摘要 |
The invention relates to a method for making a nacelle element (2) that includes the steps of: (A) forming an array of heating resistors on a substrate using a photolithographic method; (B) applying a web (50, 52) of composite materials onto the array obtained in step (A); (C) applying an inner skin (12) onto the de-icing assembly (13) thus obtained. The invention also relates to a nacelle including such an element (2). |
申请公布号 |
US9027884(B2) |
申请公布日期 |
2015.05.12 |
申请号 |
US200913062000 |
申请日期 |
2009.08.14 |
申请人 |
Aircelle |
发明人 |
Valleroy Laurent Georges;Gerome Marc |
分类号 |
B64D15/12;B64D33/02;F02C7/047;H05B3/26;H05B3/28 |
主分类号 |
B64D15/12 |
代理机构 |
Brinks Gilson & Lione |
代理人 |
Brinks Gilson & Lione |
主权项 |
1. A method for making an aircraft nacelle element, comprising:
A. forming a single layer of an array of heating resistors comprising a metal or alloy with a resistivity between 0.00024 Ω-mm and 0.002 Ω-mm using a photolithographic method; B. encapsulating the array between webs of composite materials to form a de-icing assembly for a leading edge of the aircraft nacelle; and C. applying an inner skin onto an inner side of the de-icing assembly. |
地址 |
Gonfreville l'Orcher FR |