精密射出成型於微飛行器零組件成形之研究

機構典藏 > College of Engineering > Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering > Proceeding > Item 987654321/93273

Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/93273

Title:	精密射出成型於微飛行器零組件成形之研究
Other Titles:	Study on Fabrication of Micro Aerial Vehicle Parts by Precision Injection Molding
Authors:	沈永康;黃進光;楊龍杰;蕭富元;苗志銘;李建邦;鄧秉敦
Contributors:	淡江大學機械與機電工程學系;淡江大學航空太空工程學系
Keywords:	精密射出成型;MAV;模流分析;材料試驗;Precision Injection Molding;Micro Aerial Vehicle (MAV);Moldflow Analysis;Material Testing
Date:	2008-12
Issue Date:	2013-12-13 15:56:43 (UTC+8)
Publisher:	臺北市：中華民國航空太空學會
Abstract:	本文的目的是以精密射出成型製作微飛行器零件，針對不同材料進行機械性質之分析。由於微飛行器各部份零件之功能需求有所不同，利用ASTM 標準，對兩種材料(POM ; PA66)進行磨耗; 拉伸與衝擊試驗，以作為微飛行器各部份零件材料選用之參考。結果顯示POM 之抗拉強度優於PA66 ;衝擊試驗中， POM 之衝擊強度優於PA66 ;磨耗試驗中， POM 之耐磨耗性質略高於PA66 '因此連桿，基座及齒輪選用POM 材料進行製作。本文針對精密射出成型做成型性之探討，並利用成型視窗找出田口法之參數，以田口實驗計劃法，找出影響微飛行器零件收縮之重要參數，並找出最佳化的製程參數。結果顯示，影響收縮最重要之製程參數依序為模具溫度; 射出壓力; 保壓時間，最後是熔膠溫度。三個零件之最佳化製程參數相同，皆為AIBIC3D3 '分別為模其溫度的。c ; :熔膠溫度220 0C ; 射出壓力500b訂以及保壓時間2 秒。 This investigation fabricates the parts of MAV(Micro Aerial Vehicle) by using precision injection molding.The authors use different polymer materials to do the material testing. The authors base on ASTM standard, focus on two materials (POM, A66) to carry out the wearing testing, tensile testing and impact testing. In the tensile strength testing, the tensile strength ofPOM is better than PA66. In the impact testing, the impact strength of POM is better than PA66. In the wear testing, the wear resistance of POM is better than PA66 slightly. So the linking stickpart, base part and gear part are chosen POM as the injection material. This study uses precision injection molding to fabricate the MAV parts. The authors find out the processing window of POM material, and according to the processing window and then to determine the parameters of Taguchi method setting. The authors will find out the optimum processing parameter. The results show that the most important factor for shrinkage is followed by mold temperature, injection pressure, packing time, and the last one is the injection temperature. The optimal parameter is AIBIC3D3, it is mold temperature of 80�C, injection temperature of 200�C, injection pressure of 500bar and packing time of 2 second.
Relation:	中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集，頁155
Appears in Collections:	[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Proceeding [Graduate Institute & Department of Aerospace Engineering] Proceeding

Files in This Item:

There are no files associated with this item.

Loading...