本研究室近年來致力於超輕鎂合金(如LAZ1110)的研究，歸納出其具有質量輕、比強度高及加工成型性佳等優點，適合被運用於航太工業中，因此，本論文選擇航太領域中金屬材料尚未被廣泛使用的無人駕駛飛行載具(Unmanned Aerial Vehicles, UAV)做為運用目標，將其部分結構以超輕鎂合金取代，並結合國外汽車工業已發展、國內尚未萌芽的快塑成型(Quick Plastic Forming, QPF)製程來製作機身幾何形狀較複雜的部位。
本論文部分章節將對超輕鎂合金的材料特性及快塑成型技術的學理做探討、嘗試設計與規劃取代之結構如何與其他零件做接合，並在設計與規劃完成後針對利用超輕鎂合金取代的成品做一些初步的評估，分析其可行性。

Super-Light magnesium alloy (ex:LAZ1110) have some advantages for aeronautics, for example, it’s lower specific weight, better formability, and high specific strength, but it is not used extensively now. Thus, we want to popularize its use in aerospace industry, we choose Unmanned Aerial Vehicles (UAV) to take as our applicable target, because metallic materials are poor using in this field. Our method is to replace the some original parts by Super-Light magnesium alloy, and combine with the technique that be successfully used in US automotive industry but not develop in domestic, called Quick Plastic Forming (QPF).
This thesis’s some chapters will be mention material characteristics of Super-Light magnesium alloy, and the theory of Quick Plastic Forming technique, and try to design how to join between the structure that made from Super-Light magnesium alloy and other parts. As accomplished the design, we will make some simple estimates to decide this proposal’s feasibility.

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