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AGT101 automotive gas turbine system developmentThe AGT101 automotive gas turbine system consisting of a 74.6 kw regenerated single-shaft gas turbine engine, is presented. The development and testing of the system is reviewed, and results for aerothermodynamic components indicate that compressor and turbine performance levels are within one percent of projected levels. Ceramic turbine rotor development is encouraging with successful cold spin testing of simulated rotors to speeds over 12,043 rad/sec. Spin test results demonstrate that ceramic materials having the required strength levels can be fabricated by net shape techniques to the thick hub cross section, which verifies the feasibility of the single-stage radial rotor in single-shaft engines.
Document ID
19820051504
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rackley, R. A.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Kidwell, J. R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 82-1166
Meeting Information
Meeting: Joint Propulsion Conference
Location: Cleveland, OH
Start Date: June 21, 1982
End Date: June 23, 1982
Sponsors: AIAA, SAE, and ASME
Accession Number
82A35039
Funding Number(s)
CONTRACT_GRANT: DEN3-167
Distribution Limits
Public
Copyright
Other

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