Device for heating an aerofoil

• US 6,031,214 A
• Filed: 02/06/1997
• Issued: 02/29/2000
• Est. Priority Date: 02/08/1996
• Status: Expired due to Term

• Current Assignee: Airbus Helicopters
• Original Assignee: Eurocopter
• Inventors: Bost, Michel, Bauchet, Jean-Cyril
• Primary Examiner(s): PAIK, SANG YEOP
• Application Number:
  US08/796,588
• Time in Patent Office: 1,118 Days
• Field of Search: 219/201, 219/202, 219/528, 219/529, 219/535, 219/541, 219/545, 219/547, 219/548, 219/549, 244/134 R, 244/134 C, 244/134 D
• US Class Current: 219/545
• CPC Class Codes: B64D 15/12 by electric heating electric heating elements in general H05B
• CPC Class Codes: H05B 2203/005 using multiple resistive elements or resistive zones isolated from each other
• CPC Class Codes: H05B 2203/011 Heaters using laterally extending conductive material as connecting means
• CPC Class Codes: H05B 2203/015 Heater wherein the heating element is interwoven with the textile
• CPC Class Codes: H05B 2203/017 Manufacturing methods or apparatus for heaters
• CPC Class Codes: H05B 3/347 woven fabrics

Abstract

The heating device comprises electrically conducting longitudinal fibers extending substantially parallel to a leading edge of the aerofoil close to said leading edge, and means for electrically connecting the ends of the longitudinal conducting fibers to an electric power supply. The conducting fibers are grouped together in conducting rovings forming part of a hybrid fabric which furthermore includes a weft of electrically insulating fibers woven together and woven with the conducting rovings.

Claims

1. A device for heating an aerofoil, comprising electrically conducting longitudinal fibers extending substantially parallel to a leading edge of the aerofoil in a region of the aerofoil including said leading edge, and means for electrically connecting the ends of the longitudinal conducting fibers to an electric power supply, wherein the conducting fibers are grouped together in conducting rovings forming part of a hybrid fabric embedded in a set resin, said hybrid fabric further including a weft of electrically insulating fibers woven together and woven with the conducting rovings, and wherein the electrical connection means comprise, at each end of the hybrid fabric, a metallic conducting cable arranged along said end of the hybrid fabric and projecting from at least one lateral edge of the hybrid fabric, and a metallic mesh folded along said end of the hybrid fabric in such a way as to envelope said conducting cable and the hybrid fabric near said end.

2. The device for heating an aerofoil as claimed in claim 1, having several layers of hybrid fabric over at least part of said region of the aerofoil.

3. The device for heating an aerofoil as claimed in claim 1, wherein the hybrid fabric includes a portion where the density of rovings of longitudinal conducting fibers is a fraction of the density of rovings of longitudinal conducting fibers in other portions of the hybrid fabric.

4. The device for heating an aerofoil as claimed in claim 3, wherein said portion of the hybrid fabric where the density of rovings of longitudinal conducting fibers is a fraction of the density of rovings of longitudinal conducting fibers in other portions of the hybrid fabric is obtained by locally removing conducting rovings from a uniform hybrid fabric.

5. The device for heating an aerofoil as claimed in claim 1, wherein the hybrid fabric further includes rovings of transverse conducting fibers woven with the insulating fibers of said weft and with the rovings of longitudinal conducting fibers, and wherein the electrical connection means couple the ends of only the longitudinal conducting fibers to the electric power supply.