Device for heating an aerofoil

• US 5,947,418 A
• Filed: 11/25/1997
• Issued: 09/07/1999
• Est. Priority Date: 11/27/1996
• Status: Expired due to Term

• Current Assignee: Airbus Helicopters
• Original Assignee: Eurocopter
• Inventors: Bessiere, Robert, Bauchet, Jean-Cyril
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): Zuniga, Patricia L.
• Application Number:
  US08/978,045
• Time in Patent Office: 651 Days
• Field of Search: 244/134 D, 244/134 R, 244/134 F, 219/202, 219/548, 219/535, 219/520, 219/542, 219/552, 219/545
• US Class Current: 244/134.00D
• CPC Class Codes: B64D 15/14 controlled cyclically along length of surface

Abstract

A number of resistive elements are incorporated into the aerofoil in the vicinity of its leading edge. Each of the resistive elements is electrically connected to the other resistive elements at its distal end and is fitted at its proximal end with means of connection to an electrical power supply. The resistive elements are split between a first set that includes at least two resistive elements and a second set that includes at least one resistive element. In service, the resistive of the first set are powered in turn, while each resistive element of the second set acts as a return path for the electricity and is powered continuously or almost continuously.

Claims

1. A device for heating an aerofoil comprising, incorporated into the aerofoil in the vicinity of a leading edge of the aerofoil, a number of resistive elements which are more or less parallel to the leading edge, each of said resistive elements being fitted at its proximal end with means of connection to an electrical power supply, and the distal ends of the resistive elements being connected electrically to one another, wherein said resistive elements are split between a first set including at least two resistive elements and a second set including at least one resistive element, wherein the device also comprises control means for the cyclic application of power to at least some of the resistive elements of the first set one after another in a determined sequence, and wherein the electric current flowing through any one of the resistive elements of the first set flows in the opposite direction through the resistive element of the second set, or flows in parallel through the resistive elements of the second set.

2. The device as claimed in claim 1, wherein the resistive elements are arranged one beside the other in a heating mat that covers the vicinity of the leading edge, at least one resistive element of the second set lying along a lateral edge of the heating mat.

3. The device as claimed in claim 2, wherein the second set contains at least one resistive element lying along a lateral edge of the heating mat and at least one resistive element lying along the opposite lateral edge of the heating mat.

4. The device as claimed in claim 1, wherein the resistive elements are arranged one beside the other in a heating mat covering the vicinity of the leading edge, at least one element of the second set lying closer to the leading edge than the elements of the first set.

5. The device as claimed in claim 1, wherein the resistive elements of the first set are arranged one beside the other in a heating mat covering the vicinity of the leading edge, and wherein at least one resistive element of the second set is arranged as an increase in thickness with respect to the elements in the first set in the heating mat.

6. The device as claimed in claim 5, wherein said second set is composed of the resistive element that more or less covers the entire width of the heating mat.

7. The device as claimed in claim 5, wherein at least one resistive element of the second set lies over part of the width of the heating mat which is at the leading edge.

8. The device as claimed in claim 5, wherein at least one resistive element of the second set is placed in such a way that it covers a gap between two adjacent resistive elements of the first set.

9. The device as claimed in claim 1, wherein the resistive elements each consist of layers of electrically conducting fibers more or less parallel to the leading edge of the aerofoil.

10. The device as claimed in claim 9, wherein the resistive elements are in contact at their distal ends with at least one layer of conducting fibers running transversely to the leading edge.