形狀記憶合金連接分離裝置的若干研究
[Abstract]:In this paper, based on the separation of payloads between spacecraft and underwater vehicle by using the shape memory effect of shape memory alloy (Shape MemoryAlloy,SMA), a low impact, low noise, large load and fast response SMA connection separation device is designed. And through the theoretical, experimental, simulation and other research means to begin the work. The main contents are as follows: (1) the separation process of several typical SMA connection separators at home and abroad is analyzed and the driving principle of SMA in SMA connection separation device is summarized. Combined with the SMA constitutive model, the SMA driving model and the electrothermal model were established, and the SMA wire diameter was analyzed by using MATLAB to simulate the time-temperature curve of SMA electric heating. Effect of heating current and convection heat transfer coefficient of SMA wire on heating speed of SMA wire. (2) the recovery performance of SMA wire is tested, including phase transition temperature, recovery rate, maximum recovery force and load response. The influence of electric current and constant load on the recovery performance of SMA wire provides guidance for the design of SMA wire connection separation device. (3) the connection separation device is designed by the combination of SMA wire and separation nut. By optimizing the trigger mode of SMA wire and reducing the trigger force required by SMA wire, a kind of connection separation device which can be separated in 200ms under the preloading of 20kN is designed. Through the force analysis of the split nut and the locking assembly, the split nut, the drive spring and the safety spring are determined. Release the basic performance parameters of spring and SMA wire. (4) LS-DYNA finite element analysis software is used to simulate the SMA connection separation device, which verifies the feasibility of the design principle of the SMA connection separation device proposed in this paper. When the current is 8A and the preloading force is 20kN, the separation time obtained by numerical simulation is 87.12ms.
【學(xué)位授予單位】:北京理工大學(xué)
【學(xué)位級(jí)別】:碩士
【學(xué)位授予年份】:2015
【分類號(hào)】:V444
【參考文獻(xiàn)】
相關(guān)期刊論文 前10條
1 張廷華,鄭玉峰,蔡偉,趙連城;TiNi形狀記憶合金的相變行為及其影響因素[J];材料科學(xué)與工藝;1997年01期
2 白志富;果琳麗;陳岱松;;新型非火工星箭連接分離技術(shù)[J];導(dǎo)彈與航天運(yùn)載技術(shù);2009年01期
3 牛曉東;王利;呂昊暾;龔建華;;NiTi形狀記憶合金絲的加熱電流與相變時(shí)間關(guān)系的研究[J];彈箭與制導(dǎo)學(xué)報(bào);2008年04期
4 肖恩忠;;形狀記憶合金的應(yīng)用現(xiàn)狀與發(fā)展趨勢(shì)[J];工具技術(shù);2005年12期
5 錢輝;李宏男;宋鋼兵;陳淮;;超彈性NiTi合金絲動(dòng)力特性試驗(yàn)及本構(gòu)模型研究[J];固體力學(xué)學(xué)報(bào);2011年04期
6 陳斌;彭向和;王軍;王滬毅;;形狀記憶合金單晶細(xì)觀本構(gòu)關(guān)系的一種相變動(dòng)力學(xué)模型及算法[J];固體力學(xué)學(xué)報(bào);2012年01期
7 高濱,李忠剛,馬景;分離螺母的關(guān)鍵設(shè)計(jì)參數(shù)分析[J];航天返回與遙感;2001年02期
8 高濱;形狀記憶合金在航天器分離機(jī)構(gòu)上的應(yīng)用[J];航天返回與遙感;2005年01期
9 徐惠彬,蔣成保,宮聲凱;TiNiPd高溫形狀記憶合金相變溫度與相變滯后的研究[J];航空學(xué)報(bào);2000年S1期
10 李安生;王良文;杜文遼;郭志強(qiáng);;HCD110型振動(dòng)沖擊夯運(yùn)動(dòng)分析及工作彈簧的設(shè)計(jì)[J];機(jī)械設(shè)計(jì)與制造;2009年03期
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