Read/Search this Article
Abstract
1) The evaluation and the improvement of each engine component were proceeded, and almost all components including ceramic components and engine housing relating components were qualified to be able to install in the engine assembly. 2) The assembly, including all of these components except regenerator and combustor, was operated up to the turbine inlet temperature of 1200℃ and the speed of 90000rpm.
Journal
- Bulletin of GTSJ [List of Volumes]
-
Bulletin of GTSJ 1994/1995, 28-33, 1995-03-01 [Table of Contents]
Gas Turbine Society of Japan
Share