【摘要】：中介軸承作為航空發(fā)動(dòng)機(jī)的關(guān)鍵零部件,工作在高溫、高速、重載、強(qiáng)振動(dòng)的惡劣環(huán)境下,其性能的可靠性直接制約著飛行安全與飛機(jī)性能。因此深入研究中介軸承的運(yùn)行規(guī)律,對其進(jìn)行實(shí)時(shí)的狀態(tài)監(jiān)測,實(shí)現(xiàn)對中介軸承的故障診斷和壽命預(yù)測,對于視情維修,降低維修成本,提高航空發(fā)動(dòng)機(jī)健康管理水平有著重要的現(xiàn)實(shí)意義。本文以中介軸承為主要研究對象,研究基于Cox比例故障模型的壽命預(yù)測理論,并設(shè)計(jì)中介軸承試驗(yàn)臺,進(jìn)行壽命試驗(yàn),開發(fā)了相應(yīng)的中介軸承狀態(tài)監(jiān)測和壽命預(yù)測系統(tǒng),論文主要研究內(nèi)容如下：首先,本文論述了選題背景以及壽命預(yù)測理論和軸承試驗(yàn)臺的國內(nèi)外研究現(xiàn)狀；介紹了中介軸承的概況；剖析了中介軸承的常見失效形式；研究了軸承的振動(dòng)機(jī)理及時(shí)域、頻域、時(shí)頻域內(nèi)的振動(dòng)信號特征提取分析方法。其次,介紹了可靠性與壽命等相關(guān)指標(biāo)；研究了基于威布爾分布的比例故障率模型的壽命預(yù)測方法,選擇了最佳的壽命基準(zhǔn)函數(shù)；研究了基于極大似然估計(jì)模型的參數(shù)估計(jì)方法,基于相關(guān)性分析的協(xié)變量選取方法以及基于AR模型的協(xié)變量趨勢預(yù)測方法；根據(jù)FEMTO-ST研究所提供軸承全壽命周期的試驗(yàn)數(shù)據(jù),選取了三個(gè)協(xié)變量,建立了基于威布爾分布的比例故障率模型,并做出了可靠性函數(shù)圖,得到了可靠性壽命,驗(yàn)證了模型的有效性和可靠性。然后,以中介軸承為主要研究對象,模擬航空發(fā)動(dòng)機(jī)的實(shí)際支撐結(jié)構(gòu)和工作環(huán)境,設(shè)計(jì)了中介軸承雙轉(zhuǎn)子試驗(yàn)臺；進(jìn)行了中介軸承加速度壽命試驗(yàn),分析并選擇了合適的加速應(yīng)力,對停機(jī)閾值的選擇做了深入研究；設(shè)計(jì)了中介軸承加速壽命試驗(yàn)的監(jiān)測方案,對傳感器的選擇和布置做了詳細(xì)描述；進(jìn)行了壽命過程中的典型試驗(yàn),做了中介軸承不同損傷程度的壽命試驗(yàn)分析。最后,開發(fā)了中介軸承狀態(tài)監(jiān)測與壽命預(yù)測系統(tǒng)。介紹了系統(tǒng)的軟件和硬件開發(fā)環(huán)境；根據(jù)監(jiān)測方案要求,狀態(tài)監(jiān)測部分實(shí)現(xiàn)了溫度監(jiān)測、轉(zhuǎn)速監(jiān)測、位移監(jiān)測和振動(dòng)監(jiān)測,壽命預(yù)測系統(tǒng)部分實(shí)現(xiàn)了振動(dòng)信號特征提取,模型的協(xié)變量選取與趨勢分析,模型的參數(shù)估計(jì)和可靠性壽命估計(jì),系統(tǒng)還實(shí)現(xiàn)用戶登陸、報(bào)警設(shè)置、數(shù)據(jù)保存,擁有良好的人機(jī)關(guān)系。
[Abstract]:As the key parts of aero-engine, intermediate bearings work in the harsh environment of high temperature, high speed, heavy load and strong vibration. The reliability of their performance directly restricts flight safety and aircraft performance. Therefore, the running law of intermediary bearing is deeply studied, the real-time condition monitoring is carried out, the fault diagnosis and life prediction of intermediary bearing are realized, and the maintenance cost is reduced according to the situation. It is of great practical significance to improve the level of aero-engine health management. In this paper, the life prediction theory based on Cox proportional fault model is studied, and the life test bench is designed to carry out the life test, and the corresponding intermediate bearing condition monitoring and life prediction system is developed. The main contents of this paper are as follows: first, this paper discusses the background of the topic, the life prediction theory and the domestic and foreign research status of the bearing test bed, introduces the general situation of the intermediate bearing, analyzes the common failure forms of the intermediate bearing. The vibration mechanism of bearing and the extraction and analysis methods of vibration signals in time domain, frequency domain and time frequency domain are studied. Secondly, the reliability and service life are introduced, the life prediction method of proportional failure rate model based on Weibull distribution is studied, and the best life reference function is selected. Parameter estimation method based on maximum likelihood estimation model, covariable selection method based on correlation analysis and covariable trend prediction method based on AR model are studied. The proportional failure rate model based on Weibull distribution is established and the reliability function diagram is given. The reliability life is obtained and the validity and reliability of the model are verified. Then, taking the intermediate bearing as the main research object, simulates the actual supporting structure and working environment of the aeroengine, designs the double rotor test bench of the intermediate bearing, carries out the acceleration life test of the intermediate bearing, The suitable acceleration stress is analyzed and selected, the selection of stop threshold is studied deeply, the monitoring scheme of intermediate bearing accelerated life test is designed, and the selection and arrangement of sensor are described in detail. The typical life test was carried out, and the life test of intermediate bearing with different damage degree was made. Finally, an intermediate bearing condition monitoring and life prediction system is developed. This paper introduces the software and hardware development environment of the system, according to the requirements of the monitoring scheme, the state monitoring part realizes temperature monitoring, rotational speed monitoring, displacement monitoring and vibration monitoring, and the life prediction system realizes the feature extraction of vibration signal. Covariable selection and trend analysis of the model, parameter estimation and reliability life estimation of the model. The system also realizes user login, alarm setting, data saving and good man-machine relationship.
【學(xué)位授予單位】：大連理工大學(xué)
【學(xué)位級別】：碩士
【學(xué)位授予年份】：2016
【分類號】：V263.6

【參考文獻(xiàn)】

相關(guān)期刊論文 前10條

1 楊淑惠;;COX風(fēng)險(xiǎn)模型在企業(yè)經(jīng)營風(fēng)險(xiǎn)預(yù)警中的應(yīng)用[J];市場論壇;2014年10期

2 廖明夫;馬振國;劉永泉;王德友;;航空發(fā)動(dòng)機(jī)中介軸承的故障特征與診斷方法[J];航空動(dòng)力學(xué)報(bào);2013年12期

3 朱永明;邵庚云;;基于Cox生存模型的上市公司財(cái)務(wù)困境預(yù)測研究[J];商業(yè)研究;2013年11期

4 何正嘉;曹宏瑞;訾艷陽;李兵;;機(jī)械設(shè)備運(yùn)行可靠性評估的發(fā)展與思考[J];機(jī)械工程學(xué)報(bào);2014年02期

5 廖明夫;劉永泉;王四季;王儼剴;呂品;;中介軸承對雙轉(zhuǎn)子振動(dòng)的影響[J];機(jī)械科學(xué)與技術(shù);2013年05期

6 王英;呂文元;王奕嬌;王麗麗;王金武;;基于隨機(jī)濾波法的滾動(dòng)軸承剩余壽命預(yù)測[J];數(shù)學(xué)的實(shí)踐與認(rèn)識;2013年08期

7 孫闖;何正嘉;張周鎖;陳雪峰;曹宏瑞;寧喜鈺;鄒利民;;基于狀態(tài)信息的航空發(fā)動(dòng)機(jī)運(yùn)行可靠性評估[J];機(jī)械工程學(xué)報(bào);2013年06期

8 申中杰;陳雪峰;何正嘉;孫闖;張小麗;劉治汶;;基于相對特征和多變量支持向量機(jī)的滾動(dòng)軸承剩余壽命預(yù)測[J];機(jī)械工程學(xué)報(bào);2013年02期

9 王華偉;吳海橋;;基于信息融合的航空發(fā)動(dòng)機(jī)剩余壽命預(yù)測[J];航空動(dòng)力學(xué)報(bào);2012年12期

10 李云飛;周鐳;任靜思;;基于Cox模型的商業(yè)銀行顧客資產(chǎn)風(fēng)險(xiǎn)影響因素[J];武漢理工大學(xué)學(xué)報(bào)(信息與管理工程版);2012年03期

相關(guān)碩士學(xué)位論文 前3條

1 張博;直驅(qū)式風(fēng)電機(jī)組軸承振動(dòng)監(jiān)測與故障診斷[D];太原理工大學(xué);2014年

2 劉恩龍;基于WPHM模型的滾動(dòng)軸承壽命預(yù)測方法研究[D];大連理工大學(xué);2014年

3 陳鶴梅;某型航空軸承試驗(yàn)臺液壓加載系統(tǒng)研究[D];中南大學(xué);2010年

，

本文編號：2277467