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RISStudy on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An innovative internal cooling structure named multislot cooling has been invented for high-pressure turbine (HPT) nozzles and blades. This cooling structure has been designed to be simple and ...
Conceptual Design and Cooling Blade Development of 1700°C Class High-Temperature Gas Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this paper we describe the conceptual design and cooling blade development of a 1700°C-class high-temperature gas turbine in the ACRO-GT-2000 (Advanced Carbon Dioxide Recovery System of ...