| Summary: | 碩士 === 國立虎尾科技大學 === 機械與電腦輔助工程系碩士班 === 103 === Research done on behalf of this paper, the internal flow field of the rotor type fluid machine to different design curves at different compression ratio of the engine to the design of the rotor, and the apex seal design immersive space bar on the left, with single-stage triangle rotary engine as a design fundamental, in order to extend the multi-rotor engine, multi-stage rotor engine must consider the position of the flow channel design, in terms of the flow channel design must be based on two rotor positions corresponding to each other to do the design, to avoid gas leakage problems, to explore changes in pressure, velocity of the internal flow field of multi-stage rotor triangle, and finally a single stage rotor engine with a multi-stage rotor engine to do a comprehensive comparison, and to explore the difference between the two.
According rotor to compressor design concept, the design of six different sets of compressor rotor eccentricity, the design of the rotor and end points of an arc-shaped tip like, and then by analyzing the results of its internal flow field to explore and leaks
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