摘要
简要介绍了对某型航空发动机在外场使用过程中,实施战斗与训练状态控制的方法及其相应的控制装置。加装该装置的目的是对发动机在平时训练时,实行降负荷使用,以提高飞行安全性,而在作战需要时,可恢复发动机原有状态,以发挥发动机最大潜能。控制装置由单片微机组成,具有自检和故障检查能力。通过试飞和试用证明,控制装置改装简单、工作可靠,取得了满意的效果。
The fight and train state control method as well as the control device for the engine in airport using is briefly introduced.The control device is made of INTEL 8051 series single chip microcomputer which has eight analogy and seven I/O channels.It has selfcheck and fault diagnoses ability.Through flight test and application in aircraft,it has been proved that the control device is simple to install and works reliablly.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2003年第2期295-298,共4页
Journal of Aerospace Power
关键词
状态控制
战斗与训练
控制装置
航空发动机
aerospace propulsion
engine
state control
fight and train
control devices