非線性支撐基座之減振研究

淡江大學機構典藏 > 工學院 > 航空太空工程學系暨研究所 > 學位論文 > Item 987654321/35541

Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/35541

Title:	非線性支撐基座之減振研究
Other Titles:	A study of deck vibration with nonlinear supports
Authors:	張銘祥;Chang, Ming-hsiang
Contributors:	淡江大學航空太空工程學系碩士班王怡仁;Wang, Yi-ren
Keywords:	光碟機;振動;減振器;非線性;CD-ROM;vibration;Nonlinear
Date:	2008
Issue Date:	2010-01-11 06:45:33 (UTC+8)
Abstract:	過往減振設計，以改變減振器之質量或直接在基座支撐點使用減振材料使其具有減振效果。但如此之設計，所使用之減振器則需量身定做，來因應各種光碟機，不同的系統需要不同的減振器，這樣將大大增加成本。故在本研究中，我們將使用一種更符合經濟成本，且在不改變減振器材料及更動光碟機之大部分架構的方式之下，僅以改變減振器位置的方法來達到減振的效果。此外，本研究將基座四個角落的彈性係數作非線性化假設，並加入二個獨立之點質量減振器，運用Lagrangian Method導出其運動方程，再以複合時間比例法(Multiple Scales)求其穩態固定點(Foxed Point)的頻率愈響應和解析解，並以耦合模式之頻率響應數值解與解析解加以對照佐證此模式及結果的正確性。本研究除了使用雙質點減振系統之外，對於許多非線性的現象也有分析，其結果將是線性假設所無法發現的；而對於雙質點減振器擺放位置之於系統減振的效果，也詳加研究，相信可有效降低振動幅度，此數據期望能對相關產業作為測試、設計之參考。 In this research, an optimized position of a set of 2 mass-spring-damper vibration absorbers is proposed for a vibration mechanism device (such as optical disk drive or other mechanical vibration deck system). This vibration system is simulated by a rigid body deck with 4 corners supported by cubic springs. Only out-of-plane motions are considered in this research. 2 point-mass absorbers are attached under this deck. A nonlinear 3-D theoretical model for this system is established by Lagrange’s equation. The asymptotic analytical solution is obtained by the multiple time scale analysis. The IMSL © subroutine is employed for solving nonlinear system frequency response. The fixed points semi-analytic results in frequency domain are also acquired. Correlation is made in frequency domain to ensure the accuracy of our model. This research provides a theoretical background for the preliminary vibration reduction design for industries. It is found that the existing vibration deck amplitude and unsteady region can be reduced by simply adding the absorbers at the end corner of the deck, without changing the main configurations. This will not only save costs but also increase testing efficiency, achieving the most cost-effective vibration reduction result.
Appears in Collections:	[航空太空工程學系暨研究所] 學位論文

Files in This Item:

File	Size	Format
	0Kb	Unknown	240	View/Open

Loading...