航空发动机原理

根据航空发动机温度传感器的原理，提出一种基于数字信号处理器（DSP）与CAN的智能温度传感器。

According to the principle of aeroengine temperature sensor , aeroengine smart temperature sensor based on DSP and CAN is proposed .

给出了利用8个数字信号处理（DSP）微处理器（TMS320-C30）设计航空发动机数字仿真器的原理及结构，讨论了基于多口存贮器设计共享存贮器的性能特点。

By using 8 Digital Signal Processing ( DSP ) microprocessors , the principle and structure for designing an aeroengine digital simulator are presented . Based on a multi port memory , a common shared memory is designed and its characteristics are discussed .

对某型航空发动机排气温度测温原理进行了研究，为该型航空发动机排气温度的监测提供了理论依据。

The paper analyzes the temperature measuring principle of exhaust temperature of a certain type of engine and provides a theoretical basis for monitoring the exhaust temperature of the engine .