IP Library Granted Patent US 7,900,412
Granted Patent B2
US 7,900,412 · App. 11/020,873 · Granted Mar 8, 2011

Sealing material

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Quick Facts
Patent No.
US 7,900,412
App. No.
11/020,873
Granted
Mar 8, 2011
Kind
B2
Abstract

A sealing material comprises a partially or fully cured polysulphide sealant and a reinforcing element, especially glass fibre. The sealing material is a flexible solid and is preferably in sheet form. The sealing material is cut to shape like a gasket and is assembled between components to be fastened, for example, in airframe manufacture.

Claims (26)

1. A joint for joining two components in an aircraft, the joint including

a fastener, and

a sealing material in the form of a sheet comprising a cured polysulphide sealant and a reinforcing element which restricts the movement of the sealing material under pressure induced by the tightening of a fastener, the sealing material disposed so that the fastener passes through the sheet such that a significant thickness of the sealing material remains between the two components, after the fastener has been tightened, said reinforcing element selected from the group consisting of fibre materials and mesh materials.

2. A joint as claimed in claim 1 in which the reinforcing element is a fibre material selected from glass fibre, carbon fibre, aramid fibre, metal wool or mesh or polyamide fibre or mesh.

3. A joint as claimed in claim 1 in which the reinforcing element is glass fibre.

4. A joint as claimed in claim 1 which is a joint in an aircraft wing.

5. An aircraft including a joint as claimed in claim 1 .

6. A joint as claimed in claim 1 in which the cured polysulphide sealant penetrates into and contacts the fibre or mesh reinforcing element.

7. An aircraft comprising a joint as claimed in claim 1 .

8. An aircraft as claimed claim 7 in which the joint is between wing spars, ribs and stringers and the skin which is part of an integral fuel tank.

9. A sealing material for use in sealing joints in aircraft, the sealing material being in the form of a sheet comprising

an at least partially-cured polysulphide sealant, and

a reinforcing element which restricts the movement of the sealing material under pressure induced by the tightening of a fastener wherein said fastener passes through the sealing material, such that a significant thickness of the sheet sealing material remains between two components, after the fastener has been tightened, said reinforcing element selected from the group consisting of fibre materials and mesh materials.

10. A sealing material as claimed in claim 9 in which the sheet is less than 4 mm thick.

11. A sealing material as claimed in claim 9 in which the polysulphide sealant is essentially fully cured.

12. A sealing material as claimed in claim 9 in which the polysulphide sealant is a two-component polysulphide sealant.

13. A sealing material as claimed in claim 9 which also includes a release film.

14. A sealing material as claimed in claim 9 in which the reinforcing element is of glass fibre, carbon fibre, aramid fibre, metal wool or mesh or polyamide fibre or mesh.

15. A sealing material as claimed in claim 14 in which the reinforcing element is glass fibre fabric.

16. A sealing material as claimed in claim 15 which comprises a single layer of glass fibre fabric.

17. A joint for joining two components in an aircraft, the joint including

a fastener, and

a sealing material comprising an essentially fully cured polysulphide sealant such that it has a Shore A hardness of at least 35° A, and a woven fibre reinforcing element which restricts the movement of the sealing material under pressure induced by the tightening of a fastener, said fastener passing through the sealing material such that a significant thickness of the sealing material remains between the two components, after the fastener has been tightened.

18. A sealing material for use in sealing joints in an aircraft, the sealing material comprising:

an essentially fully cured polysulphide sealant such that it has a Shore A hardness of at least 35° A, and

a woven fibre reinforcing element which restricts the movement of the sealing material under pressure induced by the tightening of a fastener, said fastener passing through the sealing material such that a significant thickness of the sealing material remains between two components, after the fastener has been tightened.

Assignments (2)
CHANGE OF NAME Recorded Apr 18, 2011
From: AIRBUS UK LIMITED
To: AIRBUS OPERATIONS LIMITED
Reel/Frame 026141/0311 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 2, 2005
From: WEST, COLIN JOHN; CLARK, LESLIE JOHN
To: AIRBUS UK LIMITED
Reel/Frame 015721/0178 →