天堂国产午夜亚洲专区-少妇人妻综合久久蜜臀-国产成人户外露出视频在线-国产91传媒一区二区三区

當(dāng)前位置:主頁 > 科技論文 > 航空航天論文 >

某型飛機(jī)主起落架交點(diǎn)孔機(jī)器人鏜孔加工系統(tǒng)穩(wěn)定性研究

發(fā)布時(shí)間:2018-04-19 16:51

  本文選題:壓腳 + 工業(yè)機(jī)器人; 參考:《浙江大學(xué)》2015年碩士論文


【摘要】:采用工業(yè)機(jī)器人與專用的末端執(zhí)行器組合在裝配現(xiàn)場(chǎng)解決大型飛機(jī)主起落架交點(diǎn)孔鏜孔精加工問題是一種新的技術(shù)思路。然而,由于六自由度工業(yè)機(jī)器人結(jié)構(gòu)剛度低引起的加工顫振現(xiàn)象限制了主軸轉(zhuǎn)速和鏜削深度等加工工藝參數(shù)的設(shè)定范圍,降低了機(jī)器人鏜孔系統(tǒng)的加工質(zhì)量與效率。在加工對(duì)象與末端執(zhí)行器之間引入壓腳裝置是抑制加工顫振的重要手段。本文以此為背景研究機(jī)器人鏜孔加工系統(tǒng)的穩(wěn)定性,重點(diǎn)針對(duì)壓腳機(jī)構(gòu)對(duì)提高機(jī)器人鏜孔系統(tǒng)穩(wěn)定性的影響規(guī)律進(jìn)行理論分析和實(shí)驗(yàn)研究。本文主要內(nèi)容如下:第一章綜述機(jī)器人制孔系統(tǒng)的國(guó)內(nèi)外研究應(yīng)用和切削加工顫振問題的研究現(xiàn)狀。第二章針對(duì)裝配現(xiàn)場(chǎng)主起落架交點(diǎn)孔加工要求,構(gòu)建一套工業(yè)機(jī)器人鏜孔加工系統(tǒng)。在描述系統(tǒng)總體結(jié)構(gòu)和控制系統(tǒng)結(jié)構(gòu)基礎(chǔ)上闡述各個(gè)組成部分的機(jī)械結(jié)構(gòu)和功能特點(diǎn),并根據(jù)加工對(duì)象特點(diǎn)建立機(jī)器人鏜孔加工工藝流程。第三章通過對(duì)加工系統(tǒng)合理簡(jiǎn)化分別建立工業(yè)機(jī)器人和氣動(dòng)壓腳系統(tǒng)的數(shù)學(xué)模型,進(jìn)而建立整體系統(tǒng)動(dòng)力學(xué)模型,分析壓腳作用對(duì)系統(tǒng)動(dòng)力學(xué)特性的影響。第四章建立機(jī)器人鏜孔系統(tǒng)的穩(wěn)定性分析模型。通過對(duì)鏜削過程鏜削厚度、動(dòng)態(tài)鏜削力的建模,結(jié)合機(jī)器人鏜孔系統(tǒng)動(dòng)力學(xué)模型,根據(jù)再生顫振原理得到加工系統(tǒng)穩(wěn)定性的解析條件,繪制穩(wěn)定性葉瓣圖研究加工參數(shù)的穩(wěn)定區(qū)間。第五章設(shè)計(jì)機(jī)器人鏜孔實(shí)驗(yàn)系統(tǒng),通過實(shí)際鏜孔加工實(shí)驗(yàn)驗(yàn)證機(jī)器人鏜孔系統(tǒng)在不同壓腳壓力下的加工穩(wěn)定性,表明合理的壓腳壓力可提高穩(wěn)定切深,拓展機(jī)器人鏜孔加工穩(wěn)定區(qū)域,有效避免加工顫振。第六章總結(jié),并對(duì)有待進(jìn)一步研究的內(nèi)容進(jìn)行展望。
[Abstract]:It is a new technical idea to use industrial robot and special end actuators to solve the problem of boring holes at the intersection point of the main landing gear of large aircraft in the assembly site.However, the machining flutter caused by low structural stiffness of six-DOF industrial robot limits the setting range of machining parameters such as spindle speed and boring depth, and reduces the machining quality and efficiency of the robot boring system.It is an important method to suppress machining chatter by introducing pin pressing device between the machining object and the end actuator.In this paper, the stability of the robot boring system is studied, and the influence of the pin pressing mechanism on the stability of the robot boring system is analyzed theoretically and experimentally.The main contents of this paper are as follows: the first chapter summarizes the research and application of robot hole making system at home and abroad and the research status of cutting chatter problem.In the second chapter, a boring machining system of industrial robot is built according to the requirements of the intersecting hole machining of the main landing gear on the assembly site.On the basis of describing the overall structure of the system and the structure of the control system, the mechanical structure and functional characteristics of each component are described, and the machining process of the robot boring is established according to the characteristics of the machining objects.In the third chapter, the mathematical models of industrial robot and pneumatic pin system are established by reasonably simplifying the machining system, and then the dynamic model of the whole system is established, and the influence of the pin pressing action on the dynamic characteristics of the system is analyzed.In chapter 4, the stability analysis model of robot boring system is established.By modeling the boring thickness and the dynamic boring force in the boring process and combining with the dynamic model of the robot boring system, the analytical conditions of the stability of the machining system are obtained according to the principle of regenerative chatter.The stable leaflet map was drawn to study the stable interval of machining parameters.In the fifth chapter, the robot boring experiment system is designed. The stability of the robot boring system under different pressure is verified by the actual boring experiment. It shows that the reasonable pressure can increase the stable cutting depth.Expand the stable area of robot boring machining, effectively avoid machining chatter.The sixth chapter summarizes and looks forward to the content to be further studied.
【學(xué)位授予單位】:浙江大學(xué)
【學(xué)位級(jí)別】:碩士
【學(xué)位授予年份】:2015
【分類號(hào)】:V262.4

【二級(jí)參考文獻(xiàn)】

相關(guān)期刊論文 前5條

1 王飛,楊湘龍,馮允成;虛擬現(xiàn)實(shí)仿真技術(shù)及在飛機(jī)裝配中的應(yīng)用[J];北京航空航天大學(xué)學(xué)報(bào);2001年02期

2 鄭國(guó)磊,朱心雄,許德,曾春玲;飛機(jī)裝配型架標(biāo)準(zhǔn)接頭定位器自動(dòng)選取算法[J];北京航空航天大學(xué)學(xué)報(bào);2002年04期

3 李廣云;LTD500激光跟蹤測(cè)量系統(tǒng)原理及應(yīng)用[J];測(cè)繪工程;2001年04期

4 徐紅爐;劉軍;章剛;岳珠峰;;制孔工藝對(duì)緊固孔疲勞性能的影響[J];飛機(jī)設(shè)計(jì);2008年03期

5 趙慶丹;鄭國(guó)磊;馮子明;杜寶瑞;;飛機(jī)裝配工序的可視化建模及仿真[J];工程圖學(xué)學(xué)報(bào);2008年01期

,

本文編號(hào):1773922

資料下載
論文發(fā)表

本文鏈接:http://www.sikaile.net/kejilunwen/hangkongsky/1773922.html


Copyright(c)文論論文網(wǎng)All Rights Reserved | 網(wǎng)站地圖 |

版權(quán)申明:資料由用戶c987c***提供,本站僅收錄摘要或目錄,作者需要?jiǎng)h除請(qǐng)E-mail郵箱bigeng88@qq.com