The Effect of Aircraft Gas Turbine Engine Lubricants on Rolling/Sliding Contact Fatigue.
Abstract
Contact fatigue testing under conditions of both pure rolling and rolling with sliding were conducted on various lubricants and additives. Principal findings were that: (a) perfluoroalkylpolyethers, C-ethers and a synthetic hydrocarbon traction fluid were all found to improve contact fatigue life over oils conforming to the MIL-L-23699B specification (i.e. polyol esters); (b) a phosphorous salt high gear loading additive was found to be detrimental to fatigue life; (c) micropitting is a precursor to fatigue spalling when sliding is present; (d) fatigue life decreases dramatically with increasing sliding velocity and increases with increasing rolling velocity, and (e) additives are most effective when sliding is present.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1976
- Accession Number
- ADA028295
Entities
People
- R. Valori