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。
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.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1990年第4期321-324,共4页
Journal of Aerospace Power