Device for detecting and preventing the formation of ice on contoured surfaces

• US 4,508,295 A
• Filed: 06/09/1983
• Issued: 04/02/1985
• Est. Priority Date: 06/09/1982
• Status: Expired due to Term

• Current Assignee: Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA (Safran SA)
• Original Assignee: Snecma (Safran SA)
• Inventors: Derouet, Patrick R. J., Laroche, Michel C. F., Cattaneo, Christian J.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Corl, Rodney
• Application Number:
  US06/502,701
• Time in Patent Office: 663 Days
• Field of Search: 244/134 R, 244/134 A, 244/134 B, 244/134 P, 244/207
• US Class Current: 244/134.00A
• CPC Class Codes: B64D 15/16 by mechanical means
• CPC Class Codes: B64D 2033/0233 comprising de-icing means

Abstract

In a device for breaking up ice formed on a contoured surface before it reaches a dangerous thickness, a flexible and porous membrane is fixed on the contoured surface along airtight lines of contact defining elementary chambers, each of which communicates with a main chamber inside the contoured surface. The main chamber is fed continuously by a source of hot gases. The closing up of the pores of the membrane by ice causes an inflation of the elementary chambers and a deformation of the membrane. Application is to the cowl of the air intake of a turbojet engine and to a detector used for the control of a de-icing device of any type.

Claims

1. A device for detecting and preventing the formation of ice on contoured surfaces, comprising:

a rigid hollow support structure including a contoured surface;

a deformable wall covering said contoured surface;

means for providing an airtight securement between said support structure and said deformable wall along a plurality of lines of contact, whereby a plurality of elementary chambers are defined by said support structure, said deformable wall and said means for providing an airtight securement;

at least one first opening between the interior of said support structure and each of said elementary chambers;

at least one opening in said deformable wall at each said elementary chamber; and

means for feeding hot gas to said interior of said support structure.

2. The device as in claim 1 wherein said means for providing an airtight securement comprises ribs projecting outward from said support structure.

3. The device as in claim 1, wherein said means for providing an airtight securement comprises ribs projecting inward belonging to the deformable wall.

4. The device as in claim 1, wherein said means for providing an airtight securement comprises an adhesive substance between said support structure and said deformable wall.

5. The device as in claim 1, wherein the lines of contact are distributed along parallel lines.

6. The device as in claim 1, wherein some of said lines of contact intersect one another so as to form a network of said lines.

7. The device for detecting the formation of ice as in claim 1 wherein said support structure and said deformable wall include electric movement detection means at each said elementary chamber.

8. The device for detecting the formation of ice as in claim 1, wherein at least one of said elementary chambers is equipped with an excess pressure sensor which produces an excess pressure signal.

9. The device of claim 1 wherein said deformable wall is formed of an elastomeric material.

10. The device as in claim 2 wherein the lines of contact are distributed along parallel lines.

11. The device of claim 3 wherein the lines of contact are distributed along parallel lines.

12. The device of claim 4 wherein the lines of contact are distributed along parallel lines.

13. The device of claim 2 wherein some of said lines of contact intersect one another so as to form a network of said lines.

14. The device as in claim 3 wherein some of said lines of contact intersect one another so as to form a network of said lines.

15. The device as in claim 4 wherein some of said lines of contact intersect one another so as to form a network of said lines.