首页 | 本学科首页   官方微博 | 高级检索  
     检索      

国外航空发动机关键件定寿和延寿方法分析
引用本文:陈国栋,邢 雷,赵 明.国外航空发动机关键件定寿和延寿方法分析[J].航空发动机,2013,39(5):60-65.
作者姓名:陈国栋  邢 雷  赵 明
作者单位:1. 中航工业沈阳发动机设计研究所,沈阳 110015; 2. 驻沈阳黎明航空发动机(集团)有限责任公司军事代表室,沈阳 110043
摘    要:为获得航空发动机关键件的最大安全使用寿命,在国际航空领域开发了多种寿命评定方法。针对国外军、民用航空发动机通用规范对关键件的安全性要求,深入分析了5种定寿方法和基于裂纹扩展寿命、改进的统计方法、风险评估等方向研究发展起来的3种关键件延寿方法的原理、使用范围、使用条件以及安全性等问题。根据假设的轮盘试验结果,采用预定安全循环寿命法计算了轮盘的安全寿命,并分别运用改进的统计法和简化的风险模型进行了轮盘延寿的计算和分析

关 键 词:寿命评定  定寿  延寿  航空发动机  关键件  改进统计法  风险模型

Analysis of Life Deciding and Life Extending for Aeroengine Critical Parts
Authors:CHEN Guo-dong  XING Lei  ZHAO Ming
Institution:1.AVIC Shenyang Engine Design and Research Institute, Shenyang 110015, China;
Abstract:A variety of life assessment methods were investigated in international aviation field to obtain maximum safe service life of the aeroengine critical parts. Five life deciding methods and the principle, service area, service condition and safety of three life extending method based on crack extending life, improved statistical method and risk assessment were analyzed deeply against military and commercial aeroengine general specification for safety requirements of critical parts based on the assumed rig test results. The disk safe life was calculated by the method of the predicted cyclic life, and the life extending of the disk was predicted and analyzed by the improved statistical method and the simplified risk model.
Keywords:life assessment  life deciding  life extending  aeroengine  critical parts  improved statistical method  risk model
点击此处可从《航空发动机》浏览原始摘要信息
点击此处可从《航空发动机》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号