SILICONE RUBBER COMPOSITIONS

• US 20120133079A1
• Filed: 06/07/2010
• Published: 05/31/2012
• Est. Priority Date: 06/05/2009
• Status: Abandoned Application

• Current Assignee: Meggitt Aerospace Ltd. (Meggitt PLC), Meggitt-Oregon, Inc. (Meggitt PLC)
• Original Assignee: Meggitt Aerospace Ltd. (Meggitt PLC), Meggitt-Oregon, Inc. (Meggitt PLC)
• Inventors: Sykes, David, Ly, Kim Loan Thi
• Application Number:
  US13/376,042
• Publication Number:
  US 20120133079A1
• Time in Patent Office: Days
• US Class Current: 264/299
• CPC Class Codes: C08K 5/14 Peroxides
• CPC Class Codes: C08L 83/04 Polysiloxanes

Abstract

The present invention relates to silicone rubber compositions, methods for their preparation and uses thereof. In particular, the invention relates a heat curable silicone rubber composition comprising: 100 parts by weight of a defined HCR silicone elastomer; 0.5 to 30 parts by weight of hollow filler; and 0.1 to 3.0 parts by weight of a curing agent.

Claims

1. A heat curable silicone rubber composition comprising:

100 parts by weight of a HCR silicone elastomer base which has, when determined in its cured state, a tensile strength of at least 8 MPa, a tear strength at least 18 N/mm, and a specific gravity of between 1.05 and 1.35 g/cc;

0.5 to 30 parts by weight of a hollow filler;

0.1 to 3.0 parts by weight of a curing agent.

2. A composition according to claim 1, wherein the HCR silicone elastomer base has, in its cured state, a hardness of between 30 and 80 IRHD, preferably not more than 70 IRHD, more preferably not more than 60 IRHD.

3. A composition according to claim 1 wherein the HCR silicone elastomer base has, in its cured state, an elongation at break of at least 500%.

4. A composition claim 1, wherein the HCR silicone elastomer base is a polydimethyl or polydimethylphenyl siloxane containing crosslinking groups having hydroxyl, vinyl or hexenyl groups.

5. A composition according to claim 1, wherein the hollow filler is hollow glass balls and wherein the hollow glass balls have a specific gravity of from 0.15 to 0.45.

6. A composition according to claim 1, wherein the curing agent is an organic peroxide curing agent selected from the group consisting of 2,5-dimethyl-2,5-di-(tert-butylperoxy)hexane, di-tert-butyl peroxide, 2,4-dichlorobenzoyl peroxide, benzoyl peroxide, dicumyl peroxide, tert-butyl perbenzoate, tert-butylperoxy and isopropyl carbonate or any combination thereof.

7. A composition according to claim 1, further comprising up to 1.5 parts by weight of an organosilane coupling agent.

8. A composition according to claim 1, further comprising up to 3 parts by weight of a tensile strength modifier.

9. A composition according to claim 1, further comprising up to 5 parts by weight of a heat stabilizing additive.

10. A composition according to claim 1, further comprising up to 10 parts by weight of one or more processing additives.

11. A method of preparing the curable silicone composition according to claim 1, said method comprising the steps of:

a) Adding the HCR silicone elastomer to a mixing chamber and mixing the elastomer until the elastomer is suitably homogenised;

b) Optionally adding and mixing one or more additives selected from the group consisting of heat stabilizing additives, organosilane coupling agents, pigment dispersions, tensile strength modifiers, and processing additives into the HCR silicone elastomer in the mixing chamber;

c) Adding and mixing the hollow filler into the HCR silicone elastomer in the mixing chamber;

d) Removing the mixture from the mixing chamber and blending the mixture to obtain a homogenous composition

wherein the curing agent is either added to the homogenised HCR silicone elastomer in step b) or is added to the mixture during the blending in step d).

12. A method according to claim 11, wherein step c) comprises adding and mixing from 30 to 70% of the volume of the hollow filler into the HCR silicone elastomer in the mixing chamber followed by adding and mixing the remaining volume of hollow fillers into the silicone elastomer in the mixing chamber.

13. Use of a composition according to claim 1 in the preparation of a cured silicone rubber having a hardness of from 40 to 80 IRHD, a minimum tensile strength of between 4.0 and 7.0 MPa, a minimum tear strength of between 10 to 12 kN/m², and a density of less than 1 g/cc.

14. Use of a composition according to claim 1 in the preparation of a cured silicone rubber having a Shore A hardness of between 48 and 58, a minimum tensile strength of 1050 psi, a minimum tear strength of 140 lbs/inch and a density of less than 1 g/cc.

15. A method of forming a silicone rubber based seal, which method comprises the steps of:

a) Moulding the curable silicone rubber composition according to claim 1 to provide the shape of the seal; and

b) Heating the composition in order to cure the composition to an elastomeric state for formation of the rubber seal.

16. A method according to claim 15 in which the seal is an airframe seal.

17. A method according to claim 16 in which the seal is a fabric-reinforced airframe seal.

18. Use of a composition according to claim 1 in the production of an aircraft seal.

19. Use according to claim 18 in the production of an airframe seal.

20. Use according to claim 19 in the production of a fabric-reinforced airframe seal.