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DC Field | Value | Language |
---|---|---|
dc.contributor.author | 葉昶志 | en_US |
dc.contributor.author | Chang-Jhih Yeh | en_US |
dc.contributor.author | 徐文祥 | en_US |
dc.contributor.author | Wensyang Hsu | en_US |
dc.date.accessioned | 2014-12-12T01:15:21Z | - |
dc.date.available | 2014-12-12T01:15:21Z | - |
dc.date.issued | 2007 | en_US |
dc.identifier.uri | http://140.113.39.130/cdrfb3/record/nctu/#GT009514507 | en_US |
dc.identifier.uri | http://hdl.handle.net/11536/38496 | - |
dc.description.abstract | 本論文主要利用微機電製程技術及電鍍技術,製作電鍍鎳及電鍍鎳-鑽奈米複合材料之懸臂樑結構,並採用微力試驗機搭配微探針頂推懸臂樑自由端的方式,對懸臂樑進行彎曲及疲勞試驗,以探討電鍍鎳及電鍍鎳-鑽奈米複合材料之疲勞特性的差異。 在試片設計上,本論文於懸臂樑上增加一接觸孔設計,可方便微探針對位,及避免微探針與試片表面接觸時的滑動。此一接觸孔設計,為彎曲及疲勞試驗時因接觸滑動所引起的誤差,找到了一個簡易的解決方法。 在彎曲試驗中,以電鍍鎳及電鍍鎳-鑽奈米複合材料所製成的長130 μm、厚15 μm懸臂樑結構,於試驗所得的F-δ圖,可得材料的比例限對應的位移分別為18 μm及22 μm,以作為疲勞試驗的最大位移量,且由電鍍鎳-鑽奈米複合材料製作而成之懸臂樑的剛性及楊氏係數略高於電鍍鎳,與前人的研究結果相符。 在疲勞試驗中,由試驗所得的S-N曲線可知,當材料受到相同比例的週期性位移負載時,如約89% δmax時,電鍍鎳材料的疲勞壽命比電鍍鎳-鑽奈米複合材料高約5倍。而受相同位移負載時,例如16 μm時,電鍍鎳材料的疲勞壽命比電鍍鎳-鑽奈米複合材料高約3倍,利用奈米壓痕機量測得知的楊氏係數計算力量及應力,在受到相同的力量時,例如50 mN時,電鍍鎳材料的疲勞壽命比電鍍鎳-鑽奈米複合材料高約3倍,而受相同週期性應力也是。電鍍鎳及電鍍鎳-鑽奈米複合材料的疲勞比分別為0.69及0.46。 | zh_TW |
dc.description.abstract | In this study, cantilever beams are fabricated by electroplated Ni and Ni-diamond nanocomposite. A MTS micro-force testing machine (Tytron 250) with a probe is adopted for bending test and fatigue test. In the test beam design, a cantilever beam with a contact hole is included to improve the quality of the test data. In the bending test, a load-displacement curve is obtained and the Ni-diamond nanocomposite is about 1.2 times the proportional limit of the pure electroplated nickel. In addition, the stiffness, as well as the Young’s modulus, of Ni-diamond nanocomposite is higher than pure electroplated nickel, and this result is insistent with previously reported results. In the fatigue test, the S-N curve is obtained. The Young’s modulus of electroplated Ni and Ni-diamond nanocomposite are measured by the means of the nanoindentation test. In the same proportional loading of maximum displacement (ex. 89% δmax), the pure electroplated nickel is about 5 times the fatigue life of Ni-diamond nanocomposite. When the same displacement is applied (ex. 16 μm), the pure electroplated nickel is about 3 times the fatigue life of Ni-diamond nanocomposite. Similarly, when the same force is applied (ex. 50 mN), as well as the stress, the pure electroplated nickel is about 3 times the fatigue life of Ni-diamond nanocomposite. In addition, the endurance ratio of pure electroplated Ni and Ni-diamond nanocomposite are 0.69 and 0.46, respectively. | en_US |
dc.language.iso | zh_TW | en_US |
dc.subject | 疲勞 | zh_TW |
dc.subject | 複合材料 | zh_TW |
dc.subject | 電鍍鎳 | zh_TW |
dc.subject | fatigue | en_US |
dc.subject | Nanocomposite | en_US |
dc.subject | Electroplated Ni | en_US |
dc.title | 電鍍鎳及電鍍鎳-鑽奈米複合材料之疲勞特性研究 | zh_TW |
dc.title | Fatigue Property Investigation on Electroplated Ni and Ni-diamond Nanocomposite | en_US |
dc.type | Thesis | en_US |
dc.contributor.department | 機械工程學系 | zh_TW |
Appears in Collections: | Thesis |
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