本研究主要目的為利用TD-04渦輪增壓器作為氣體產生器，配合自行設計的液態燃料燃燒室，使用航空燃油JET A-1為主要燃料，利用氣體產生器所產生的氣體推動TD-08動力渦輪帶動發電機發電，形成高轉速微型渦輪發電系統，並利用動力渦輪所排放尾氣的廢熱加熱甲醇重組器產生富氫氣體導回燃燒室內摻燒，藉此降低汙染性廢氣的排放。
本研究成功將發電機拉轉至40,000 rpm，可得到最高發電量為1,290 W，且於氣體產生器達150,000 rpm以上的高轉速時，CO排放量為0 %，HC排放量為2 ppm；透過導入甲醇重組器產生的富氫氣體進入燃燒室摻燒，於120,000 rpm的低轉速時，HC的降幅達到50 %，CO排放量為0 %，NOx的排放量維持於60 ppm，符合氣渦輪機電力設施的空氣污染物排放法規標準。

The aim of this research is to establish a low emission micro gas turbine generator system. In this research, the smaller turbo charger, TD-04, is combined with the self-design combustion chamber as a gas generator. The larger turbo charger, TD-08, which combined with the high speed generator is placed behind the gas generator as a power turbine to slow down the rotating speed. The exhaust gas from the power turbine is used to heat the methanol reformer. The methanol, a liquid fuel, can be reformed easily with resultant hydrogen rich syngas and few byproducts. The hydrogen rich syngas is fed back to the combustion chamber of the gas generator to improve the exhaust gas composition.
In this research, the low emission micro gas turbine generator system is built successfully. The maximum rotating speed of generator can be reached 40,000 rpm with 1,290 Watt electricity output. With the hydrogen rich syngas injected into combustion chamber of gas generator with 150,000 rpm, the HC emission is 4 ppm (with 50 % reduction), while CO emission is down to 0 %. The NOx emission holds on about 60 ppm. The emission of the system conforms to the air pollution laws of gas generator system.

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