本研究主要目的是利用渦輪增壓器(TD-08)建立一套微型渦輪氣體產生器，使用JP-8為主要燃料，並利用渦輪氣體產生器出口高溫氣體特性，連結動力渦輪並帶動高轉速發電機，形成高轉速渦輪發電系統，藉由建立此套系統供後續研究所用。研究中以兩種不同架設方法進行發電機的架設，並探討發電機在不同負載測試下對渦輪增壓器溫度、壓力、油耗率等影響。
本研究之發電機為適合渦輪引擎高轉速特性的三相交流發電機，發電機測試不是經由主軸馬達輔以變速箱來製作一高速發電機測試平台，而是藉由渦輪氣體產生器出口氣體推動動力渦輪帶動發電機，並經由實驗點火成功且運轉至發電機所需之轉速(90,000 RPM)。利用3 kW級負載機進行發電機性能量測，在最高轉速時量測得發電機最大輸出功率為550 W。

The purpose of this research is to establish the micro gas generator by using turbocharger. The JP-8 is the major fuel used in the system. The system, combined power turbine with generator, was powered by the high exhaust gas temperature from the high speed turbine generator. In this study, there were two different ways to link generator and turbine engine. The parameters in the system with different generator output were investigated, including temperature, pressure, fuel consumption, etc.
The three-phase alternator used in this study is suitable for the high-speed turbine engine. Rather than using spindle motor, the power turbine was powered by the gas generator. The gas generator with separate power turbine was successfully set up; and after ignition process, it could reach the required high revolution speed, i.e. 90,000 RPM. The results showed that the generator could provide 550 W at the maximum speed.

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