Claims
- 1. A composition useful for lubricating aircraft turbines, comprising:
- (a) a lubricating fluid base stock and
- (b) a phosphorus-containing compound of Formula I: ##STR3## wherein a equals 1 or 2, b equals 1 or 2, X is oxygen or sulfur; Z1 and Z2 are independently in each occurrence a covalent bond or oxygen; Y is a covalent bond or is a diradical group of Formula II: ##STR4## wherein c equals 0 or 1; R1, R2, R3 and R4 are independently in each occurrence aryl of up to 12 carbons, alkyl of up to 6 carbons, alkoxy of up to 6 carbons, polyhaloalkyl of up to 6 carbons, polyhaloalkyoxy of up to 6 carbons, halo or aryloxy of up to 12 carbons wherein if R1, R2, R3 or R4 is aryloxy the aryloxy can be substituted by one or more R1, R2, R3 or R4; W is a covalent bond, O, SO.sub.2, C(CH.sub.3).sub.2, C(CF.sub.3).sub.2, or 9,9'-fluorene; n1 is 0 to 5; n2 is 0 to 5; n3 is 0 to 5; n4 is 0 to 5; with the provision that R1, R2, R3 and R4 are not hydroxy and with the provision that phosphorus is bonded to at least two oxygens and with the provision that a phosphorus atom is bonded to no more than three oxygens.
- 2. The composition of claim 1 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyhalomethyl, polyhalomethoxy, halo or aryloxy.
- 3. The composition of claim 1 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyfluoromethyl, polyfluoromethoxy, fluoro or phenyloxy.
- 4. The composition of claim 3 wherein a is 1; b is 2; n1 is 0, Z1 is a covalent bond, Z2 is oxygen, and Y is a covalent bond.
- 5. The composition of claim 4 wherein n2 is 1 and R2 is phenoxy or chlorophenoxy.
- 6. The composition of claim 5 wherein X is sulfur.
- 7. The composition of claim 1 wherein X is oxygen, a and b are 2, and Z1 and Z2 are covalent bonds.
- 8. The composition of claim 7 wherein c is 0.
- 9. The composition of claim 8 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyhalomethyl, polyhalomethoxy, halo or aryloxy.
- 10. The composition of claim 9 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyfluoromethyl, polyfluoromethoxy, fluoro or phenyloxy.
- 11. The composition of claim 8 wherein n1, n2, n3 and n4 are 0.
- 12. The composition of claim 1 wherein a and b are 2, X is oxygen and c is 1.
- 13. The composition of claim 12 wherein Z1 and Z2 are covalent bonds.
- 14. The composition of claim 13 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyhalomethyl, polyhalomethoxy, halo or aryloxy.
- 15. The composition of claim 14 wherein R1, R2, R3 and R4 are independently in each occurrence methyl, methoxy, polyfluoromethyl, polyfluoromethoxy, fluoro or phenyloxy.
- 16. The composition of claim 13 wherein n1, n2, n3 and n4 are 0.
- 17. The composition of any one of claims 1-16 wherein the lubricating fluid base stock is a polyphenyl ether.
- 18. The composition of claim 17 wherein the phosphorus-containing compound is present in an amount greater than about 0.5 weight percent and less than about 10 weight percent.
- 19. The composition of claim 18 wherein the phosphorus-containing compound is present in an amount less than about 5 weight percent.
Government Interests
The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided by the terms of contract no. F33615-89-C-2918 awarded by the U.S. Air Force.
US Referenced Citations (5)
Non-Patent Literature Citations (1)
Entry |
Gschwender, Lois J. et al. "Synthesis and Characterization of a High-Temperature, Low-Volatility Phosphate Additive for Aerospace Applications," Lubr. Eng., 41, pp. 935-938 (1991). |