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Evaluation of Gas Lubricated Hydrodynamic Bearings in a Gas Turbine Environment.


AD744844

Publication Date 1972
Personal Author Swenson, K. R.; Hughes, N. M.; Heuer, D. F.
Page 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)
Keywords
  • Gas bearings
  • Gas turbines
  • Gas generating systems
  • Auxiliary power plants
  • Aircraft engines
  • Feasibility studies
  • A-7D aircraft
  • Jet fuel starters
Source Agency
  • Invalid Source Agency Code
NTIS Subject Category
  • 41J - Tooling, Machinery, & Tools
  • 81D - Jet & Gas Turbine Engines
Corporate Authors AiResearch Mfg Co of Arizona Phoenix
Document Type Technical Report
Title Note Final rept. Mar 71-Apr 72.
NTIS Issue Number 197216
Contract Number
  • F33615-71-C-1376
Evaluation of Gas Lubricated Hydrodynamic Bearings in a Gas Turbine Environment.
Evaluation of Gas Lubricated Hydrodynamic Bearings in a Gas Turbine Environment.
AD744844

  • Gas bearings
  • Gas turbines
  • Gas generating systems
  • Auxiliary power plants
  • Aircraft engines
  • Feasibility studies
  • A-7D aircraft
  • Jet fuel starters
  • Invalid Source Agency Code
  • 41J - Tooling, Machinery, & Tools
  • 81D - Jet & Gas Turbine Engines
  • F33615-71-C-1376
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