Research and development of advanced high-temperature air force turbine engine oil©

Lubrication Engineering

Volumn 56, Issue 5, 2000, Pages 20-25

  Gschwender, Lois ^a   Snyder Jr , Carl E ^a   Nelson, Lynne ^a   Carswell, Lisa ^a   Fultz, George W ^b   Saba, Costandy ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

Author keywords

Aerospace; Aerospace Lubrication; Aviation Jet Engines; Deposition of Tribomaterials; Gas Turbine Oils; GasTurbine Engines; High Temperature Lubricants; Oxidation Lubr. Degradation; Vapor Pressure; Volatility

Indexed keywords

AIRCRAFT; ENGINE OIL; ESTER; GAS TURBINE; HIGH TEMPERATURE APPLICATION; LUBRICANT;

AIRCRAFT ENGINES; COKING; COMBUSTION; HIGH TEMPERATURE APPLICATIONS; RESEARCH AND DEVELOPMENT MANAGEMENT; THERMAL EFFECTS; THERMODYNAMIC STABILITY;

AIR FORCE TURBINE ENGINE OIL; JET AIRCRAFT ENGINES; OIL SYSTEM COKING; OXIDATIVE STABILITY; STRUCTURAL ENGINE;

GAS TURBINES;

EID: 0034178222     PISSN: 00247154     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (10)

1. Clark, F. S., Miller, D. R. and Reid, S. L., "Development of a Gas Turbine Engine Oil for Bulk Oil Temperatures of -40° to +464°F," AFML-TR-74-247, Part I (April 1975), Part II (December 1975) and Part III (May 1977), AD Nos.: A014808, A027068 and B025740.
2. Clark, F. S., Miller, D. R. and Reid, S. L., "Development of a Gas Turbine Engine Oil for Bulk Oil Temperatures of -40° to +464°F," AFML-TR-74-247, Part I (April 1975), Part II (December 1975) and Part III (May 1977), AD Nos.: A014808, A027068 and B025740.
3. Clark, F. S., Miller, D. R. and Reid, S. L., "Development of a Gas Turbine Engine Oil for Bulk Oil Temperatures of -40° to +464°F," AFML-TR-74-247, Part I (April 1975), Part II (December 1975) and Part III (May 1977), AD Nos.: A014808, A027068 and B025740.
4. Military Specification MW-L-27502, Lubricating Oil, Aircraft Turbine Engine, Ester Based, (1972), (Cancelled).
5. Schrand, J. B., "Turbine Engine Evaluation of an Experimental MIL-L-27502 Lubricant Code 0-77-20," AFWAL-TM-81-33 (POSL), (1981).
6. Military Specification, MIL-PRF-7808L, Performance Specification Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, (1997).
7. Beane, G. A., IV, Gschwender, L. J. and Snyder, C. E., Jr., "Advanced Lubricants for Aircraft Turbine Engines," Society of Automotive Engineers, Inc., SAE Technical Paper Series, 851834, (1985).
8. Military Specification, MIL-PRF-23699F, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Number 0-156, (1997).
9. Smith, H. A. and Saba, C. S., "Lubricant Deposition Studies Using a Small Test Volume, Low Cost Static Coker," Lubr. Eng., 44, 12, pp 983-992, (1988).
10. Harsacky, F. J. and Dolle, R. E., "A Chronological History of the Development of High Temperature Oxidative-Corrosion Evaluation Methods Including an Improved Micro Oxidation-Corrosion Procedure for the Investigation of Advanced Gas Turbine Engine Lubricants," Air Force Materials Laboratory AD 464417, AFML-TDR-64-291, (1965).