机械工程学报
機械工程學報
궤계공정학보
CHINESE JOURNAL OF MECHANICAL ENGINEERING
2015年
6期
142-147
,共6页
设备舱支架%振动疲劳%气动压力%动应力%模态
設備艙支架%振動疲勞%氣動壓力%動應力%模態
설비창지가%진동피로%기동압력%동응력%모태
equipment cabin frame%vibration fatigue%aerodynamic pressure%dynamic stress%model
设备舱裙板支架作为连接设备舱底板和裙板的承载部件,在运用中承受来自裙板和底板的气动压力以及振动载荷,出现疲劳裂纹。开展支架裂纹断口的宏观分析,统计开裂支架的运用里程;基于高铁客运专线线路测试,得到明线运行、会车以及隧道运行、会车工况下设备舱裙板和底板的内、外侧气动压力以及压差值;对支架进行线路动应力测试,得到开裂部位的等效应力和一阶主频;采用脉冲激励法进行设备舱支架模块的模态试验,得到支架的垂向和横向一阶模态频率。研究结果表明,支架发生裂纹的主要成因是裙板、底板内外气动压力差产生的激励与支架自振频率具有交集,支架产生共振,共振现象使支架结构产生较高的应力幅值。该研究对确保高速列车运用安全以及为支架的新结构设计提供了参考。
設備艙裙闆支架作為連接設備艙底闆和裙闆的承載部件,在運用中承受來自裙闆和底闆的氣動壓力以及振動載荷,齣現疲勞裂紋。開展支架裂紋斷口的宏觀分析,統計開裂支架的運用裏程;基于高鐵客運專線線路測試,得到明線運行、會車以及隧道運行、會車工況下設備艙裙闆和底闆的內、外側氣動壓力以及壓差值;對支架進行線路動應力測試,得到開裂部位的等效應力和一階主頻;採用脈遲激勵法進行設備艙支架模塊的模態試驗,得到支架的垂嚮和橫嚮一階模態頻率。研究結果錶明,支架髮生裂紋的主要成因是裙闆、底闆內外氣動壓力差產生的激勵與支架自振頻率具有交集,支架產生共振,共振現象使支架結構產生較高的應力幅值。該研究對確保高速列車運用安全以及為支架的新結構設計提供瞭參攷。
설비창군판지가작위련접설비창저판화군판적승재부건,재운용중승수래자군판화저판적기동압력이급진동재하,출현피로렬문。개전지가렬문단구적굉관분석,통계개렬지가적운용리정;기우고철객운전선선로측시,득도명선운행、회차이급수도운행、회차공황하설비창군판화저판적내、외측기동압력이급압차치;대지가진행선로동응력측시,득도개렬부위적등효응력화일계주빈;채용맥충격려법진행설비창지가모괴적모태시험,득도지가적수향화횡향일계모태빈솔。연구결과표명,지가발생렬문적주요성인시군판、저판내외기동압력차산생적격려여지가자진빈솔구유교집,지가산생공진,공진현상사지가결구산생교고적응력폭치。해연구대학보고속열차운용안전이급위지가적신결구설계제공료삼고。
As the load bearing structure, the equipment cabin frames connecting the bottom plates and apron plates are acted on the aerodynamic load and vibration load, which appear the fatigue cracks in service. The crack macro analysis of the frame fracture section and the life mileage statistics of the frames are demonstrated. On the basis of the online pressure test of the equipment cabin on the passenger dedicated railway lines, the inside and outside aerodynamic pressure and differential pressure of the equipment cabin bottom plates and apron plates are executed and analyzed under the conditions of trains running or passing each other in the open air or in the tunnel. The equivalent stress and the first-order frequency of the crack position are gained by the on track dynamic stress test. The first-order modal frequency in the vertical and horizontal direction of the frames is tested using the pulse excitation method. The results show that the exciting frequency from the bottom plate or apron plate aerodynamic differential pressure is mixed with the frame natural frequency and the resonance of the frame happens, which induces the high dynamic stress amplitude. This idea is helpful to improve the equipment cabin frame design and ensure the high speed train running in safety.