Presently in Japan 100 kW ceramic gas turbines (CGT) for automobiles are under development, parts of which include a turbine rotor, scrolls, a combustor, and other parts made of ceramics and ceramic matrix composites. The rotor is designed to rotate at 110,000 rpm, equal to the maximum stress of 300 MPa, and to be exposed to temperatures up to 1350°C. Initially, the strength of ceramic rotors was evaluated by a burst test using a cold spin tester. The burst picture was observed and compared with the 4pt bending strength of the ceramic test specimens. Next, the strength of the rotors was tested by a hot spin test and the burst result of the rotor was evaluated. A high-speed camera was used to observe the rotor at the instant of burst under a high-temperature condition. Applying the result of the cold and hot spin tests, ceramics for turbine rotor were selected and the shape of the rotor was designed.
Skip Nav Destination
Article navigation
January 1996
Research Papers
Evaluation of Ceramic Rotor Strength by Cold and Hot Spin Tests
M. Watanabe,
M. Watanabe
CGT Development Office, Petroleum Energy Center, Tokyo, Japan
Search for other works by this author on:
H. Ogita
H. Ogita
Ceramic Gas Turbine Research and Development Division, Japan Automobile Research Institute, Inc., Ibaraki, Japan
Search for other works by this author on:
M. Watanabe
CGT Development Office, Petroleum Energy Center, Tokyo, Japan
H. Ogita
Ceramic Gas Turbine Research and Development Division, Japan Automobile Research Institute, Inc., Ibaraki, Japan
J. Eng. Gas Turbines Power. Jan 1996, 118(1): 191-197 (7 pages)
Published Online: January 1, 1996
Article history
Received:
March 12, 1994
Online:
November 19, 2007
Citation
Watanabe, M., and Ogita, H. (January 1, 1996). "Evaluation of Ceramic Rotor Strength by Cold and Hot Spin Tests." ASME. J. Eng. Gas Turbines Power. January 1996; 118(1): 191–197. https://doi.org/10.1115/1.2816538
Download citation file:
13
Views
Get Email Alerts
Cited By
On Leakage Flows In A Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
J. Eng. Gas Turbines Power
A Computational Study of Temperature Driven Low Engine Order Forced Response In High Pressure Turbines
J. Eng. Gas Turbines Power
The Role of the Working Fluid and Non-Ideal Thermodynamic Effects on Performance of Gas Lubricated Bearings
J. Eng. Gas Turbines Power
Tool wear prediction in broaching based on tool geometry
J. Eng. Gas Turbines Power
Related Articles
Progress on the European Gas Turbine Program “AGATA”
J. Eng. Gas Turbines Power (January,1998)
Radial Turbine Development for the 100 kW Automotive Ceramic Gas Turbine
J. Eng. Gas Turbines Power (January,1998)
Research and Development of Ceramic Turbine Wheels
J. Eng. Gas Turbines Power (January,1993)
Hot Isostatic Pressing of Sintered Alpha Silicon Carbide Turbine Components
J. Eng. Gas Turbines Power (July,1987)
Related Proceedings Papers
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Verifying of a Network Cryptographic Protocol Using the Model Checking Tools
International Conference on Software Technology and Engineering (ICSTE 2012)
The Direct Contribution of Spin-Down Compression for Rotochemical Deviations in Stars Containing Mixed- Phase Matter
International Conference on Advanced Computer Theory and Engineering, 4th (ICACTE 2011)