Claims
- 1. A method of producing a mass of heat and aircraft fuel resistant elastomeric material in the form of a coating bonding layer or sealant mass adherent to one or more substrates of titanium or aluminium alloy characterised by the steps of forming a substantially solvent free primer coating on one or more substrates of titanium or aluminium alloy by application of a primer composition comprising organic material having isocyanate groups and hydrolysable silane groups available for reaction and organic solvent, and providing in contact with the primer coating a room temperature curable composition which comprises a fluorocarbon copolymer and a metallic oxide, characterised in that the composition is at least substanially free of thiol and comprises a compound having epoxy groups, and as crosslinking agent a diamino silane according to the general formula (i) namely ##STR5## in which R.sub.1 is an aliphatic hydrocarbon residue having 1 to 10 carbon atoms,
- R.sub.2 is an aliphatic hydrocarbon residue having 1 to 10 carbon atoms, and
- R.sub.3, R.sub.4 and R.sub.5 are the same or different monovalent aliphatic hydrocarbon residues having 1 to 5 carbon atoms.
- 2. A method according to claim 1 characterised in that the primer composition is prepared by admixture of an organic polyisocyanate and a silane according to the general formula (ii) namely ##STR6## in which R.sub.6 is a divalent aliphatic hydrocarbon residue having 1 to 10 carbon atoms,
- R.sub.7, R.sub.8 and R.sub.9 are the same or different monovalent aliphatic hydrocarbon residues having 1 to 5 carbon atoms, and,
- X is a grouping capable of a chemical reaction by condensation which comprises an epoxy, mercapto, amino or hydroxy group,
- the polyisocyanate and silane being used in amounts to provide a ratio of isocyanate groups to groups X of about 10:1 to 15;1.
- 3. A method according to claim 2 characterised in that the organic polyisocyanate comprises a 4.4' diphenyl methane diisocyanate partially reacted to include a minor amount of carbodiimide groups and in that the silane of general formula (ii) comprises gamma-glycidoxypropyl-trimethoxy-silane.
- 4. A method according to any one of claims 1 to 3 characterised in that the primer composition comprises a solution of from about 5 to 10% total solids, the organic solvent comprising N-methyl-2-pyrrolidone and toluene.
- 5. A method according to any one of claims 1 to 4 wherein the room temperature curable composition is provided in the form of a tacky, curable tape, or in the form of a layer deposited on the substrate from a solution.
- 6. A room temperature curable composition which is at least substantially free of thiol comprising three components (A), (B) and (C) in which the component (A) comprises a fluorocarbon copolymer, a metallic oxide, a liquid epoxy resin, and organic solvent; the component (B) comprises a silane according to the general formula (i) namely ##STR7## in which R.sub.1 is an aliphatic hydrocarbon residue having 1 to 10 carbon atoms,
- R.sub.2 is an aliphatic hydrocarbon residue having 1 to 10 carbon atoms, and
- R.sub.3, R.sub.4 and R.sub.5 are the same or different monovalent aliphatic hydrocarbon residues having 1 to 5 carbon atoms; and the component (C) comprises a primer composition comprising organic material having isocyanate groups and hydrolysable silane groups available for reaction and organic solvent, the composition being such that when the component (C) is applied to titanium substrate as a primer composition and the components (A) and (B) are mixed (in proportions to initiate at room temperature reticulation of the fluorocarbon copolymer) and applied to the primed substrate, the composition cures to provide a heat resistant, fuel resistant layer adhesively bonded to the substrate.
Priority Claims (1)
Number |
Date |
Country |
Kind |
8037487 |
Nov 1980 |
GBX |
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Parent Case Info
This is a division of application Ser. No. 403,626, filed as PCT GB81/00248, Nov. 19, 1981, published as WO82/01713, May 27, 1982, now U.S. Pat. No. 4,548,989, issued Oct. 22, 1985.
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
4338376 |
Kritzler |
Jul 1982 |
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4369279 |
Emerick |
Jan 1983 |
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Foreign Referenced Citations (2)
Number |
Date |
Country |
2413426 |
Dec 1978 |
FRX |
1037672 |
Aug 1966 |
GBX |
Non-Patent Literature Citations (1)
Entry |
Lee and Neville; "Handbook of Epoxy Resins", pp. 13-15 and 17-22; McGraw-Hill, 1967, New York, N.Y., TP1180E6, L4. |
Divisions (1)
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Number |
Date |
Country |
Parent |
403626 |
Jul 1982 |
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