DESIGN AND EVALUATION OF A HIGH TEMPERATURE RADIAL TURBINE.
Quarterly technical summary rept. no. 5, 1 Aug-31 Oct 68,
PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FLA FLORIDA RESEARCH AND DEVELOPMENT CENTER
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The detailed designs of the turbine rotor, nozzles, and backplate were completed and checking of the drawings was started. Mechanical designs of the turbine-test and burner-test configurations were finalized. A contract modification to add a casting development effort to the program was proposed, and the casting vendor to perform the work was selected. Approximately 85 of the contractor-furnished tests parts were received, and installation of the contractor-furnished test facility was started. Author
- Jet and Gas Turbine Engines