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

计算轮盘破裂转速的大变形解析法
引用本文:洪其麟,王屏.计算轮盘破裂转速的大变形解析法[J].航空动力学报,1990,5(4):321-324,371-372.
作者姓名:洪其麟  王屏
作者单位:北京航空航天大学 (洪其麟),北京航空航天大学(王屏)
摘    要:本文为轮盘破裂转速研究课题组的研究报告之一。文中提出的大变形解析法是计算轮盘破裂转速的一种新方法 ,首先推导了基本方程 ,其次叙述了计算步骤 ,并对几个试验盘作了数值计算。最后将计算结果与试验结果作了对比 ,误差均在 4 %以内。作者认为 ,此法简便易行 ,准确度符合工程需要 ,适应范围较大 ,可以在发动机轮盘研制工作中应用。

收稿时间:5/1/1990 12:00:00 AM

A LARGE ANALYTICAL DEFORMATION METHOD FOR PREDICTION OF DISK BURST SPEED
Hong Qilin and Wang Ping.A LARGE ANALYTICAL DEFORMATION METHOD FOR PREDICTION OF DISK BURST SPEED[J].Journal of Aerospace Power,1990,5(4):321-324,371-372.
Authors:Hong Qilin and Wang Ping
Institution:Beijing University of Aeronautics and Astronautics;Beijing University of Aeronautics and Astronautics
Abstract:A new method has been elaborated to predict the burst speed of aeroengine disks.The disks should overspeed or even break due to malfunction of control system,shaft decoupling or afterburning failure.In order to avoid catastrophic failure of an engine,it is required to allow a margin of the disk burst speed.When the maximum rotor speed approaches to the disk burst speed,the plastic strain attains to large value in strain hardening range.So the concepts of material and geometrical nonlinearities are employed,but it is very difficult to obtain the solution of the double nonlinear problems.An approximate large deformation large analytical method is proposed firstly.The basic equations are derived according to the variable thickness and temperature of the disks.Secondly,the computational procedure is described and the burst speeds of four tested disks are obtained from the calculations.At last,the calculated results are compared with the test data,and the differences are less than four percent.Therefrom,it is proved that the new method is simple,convinent and accurate for engineering application as well as it is applicable to a wide variety of disks.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》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