Accession Number : AD0744844
Title : Evaluation of Gas Lubricated Hydrodynamic Bearings in a Gas Turbine Environment.
Descriptive Note : Final rept. Mar 71-Apr 72,
Corporate Author : AIRESEARCH MFG CO OF ARIZONA PHOENIX
Personal Author(s) : Swenson,Kendall R. ; Hughes,Nick M. ; Heuer,Don F.
Report Date : JUN 1972
Pagination or Media Count : 58
Abstract : The report contains a summary of the design analysis, development testing, and demonstration testing performed to demonstrate the feasibility of using gas lubricated hydrodynamic bearings in a gas turbine environment. The gas generator portion of the jet fuel starter used on the A7D aircraft was modified to incorporate compliant-foil gas bearings and subjected to varied demonstration test. In addition, engine starts were made under conditions which simulated normal starting gear loads. Results of the testing were very satisfactory. It is concluded that gas lubricated bearings can be used in a gas turbine application and further testing is encouraged. (Author)
Descriptors : (*GAS BEARINGS, GAS GENERATING SYSTEMS), (*GAS TURBINES, GAS BEARINGS), AUXILIARY POWER PLANTS, AIRCRAFT ENGINES, FEASIBILITY STUDIES
Subject Categories : Machinery and Tools
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE