turbojet engine

turbojet engine

美 　英

• un.涡轮喷气发动机
• 网络涡轮喷射发动机；涡喷发动机；喷气涡轮机

英汉解释

un.	1. 涡轮喷气发动机

例句

A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust.

涡轮风扇喷气发动机一种涡轮喷气发动机带有一个风扇，通过将空气直接压入热的涡轮排气管而补充总推力

A diagnosis and signal analysis method with FFT signal processer is provided for on surge-detonation of a twin-spool turbojet engine.

本文着重介绍某双轴发动机喘振—爆燃故障用FFT信号处理机进行诊断和信号分析的方法。

Experiments were performed to investigate surge problem of a single shaft axial flow turbojet engine during throttling.

对某型单轴涡喷发动机节流过程中的喘振故障进行了试验研究。

The validation of the method is demonstrated by the identification examples of turbojet engine.

以涡喷发动机辨识算例证明了该方法的有效性。

It was powered by an Allison J33-A turbojet engine.

它由一阿利森J33座，阿涡喷发动机。

Among these superalloys, nickel-base superalloys are widely used as thermal components in the turbojet engine.

涡轮喷气发动机各种热部件使用的材料中镍基高温合金占有很大比重。

The process of loosing compressor aerodynamic stability in a turbojet engine was analyzed using the correlation integral method.

对某涡喷发动机压气机的气动失稳过程进行了相关积分分析。

A turbojet engine used to drive an external propeller.

一种用于推动外部螺旋桨的涡轮喷气式发动机

The validation of method is demonstrated by one-spool turbojet engine.

单轴涡喷发动机的算例证明了方法的有效性。

Structural design study of a micro-turbojet engine

微型涡喷发动机结构设计研究

A digital electronic control system design and test for a certain small turbojet engine

某型小涡喷发动机数控系统设计及试验

Study on the Method Establishing the Revolution Difference Map for a Two-Spool-Turbojet Engine

双轴式涡喷发动机的转差线图确定方法的研究

Experimental Study on the Inlet Total Pressure Distortion of a Turbojet Engine

某型涡喷发动机进气总压畸变的试验研究

Nonlinear Analysis of the Process of loosing Compressor Aerodynamic Stability in a Turbojet Engine

某涡喷发动机压气机气动失稳过程的非线性分析

Starting and acceleration control law design for a missile turbojet engine

某型弹用涡喷发动机启动加速控制规律设计

Field Instrumentation Design of Turbojet Engine Performance Monitoring

涡喷发动机外场监测分析仪的设计

Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade

某涡喷发动机涡轮导向器的热应力分析

Failure Mechanism and Improvement Measures of High-temperature and High-speed Ball Bearings for Turbojet Engine

涡喷发动机高温高速轴承失效机理及改进措施

Installation Evaluation and Adjustment of Turbojet Engine Parameters

涡轮喷气发动机参数的装机评价和调整

Reliability growth analysis of a turbojet engine

某涡喷发动机可靠性增长分析

Experimental research on the simulation of distortion flow field for turbojet engine distortion test

涡轮喷气发动机抗畸变流场模拟试验研究

Analysis of installation performance of the missile turbojet engine

某型弹用涡喷发动机安装性能分析

Multimedia real-time data simulation for a turbojet engine

涡喷发动机多媒体实时数字仿真

Structure of dynamic seal used in the lubricating system of a missile turbojet engine

弹用涡喷发动机润滑油系统动密封结构研究换

Experimental study on the tribological properties of missile turbojet engine seals

弹用涡喷发动机密封元件摩擦性能试验研究

Performance monitoring and diagnosis system for missile turbojet engine

弹用涡喷发动机性能监视与诊断系统软件研制

Reducing Turbojet Engine Vibration by Optimizing Blade Arrangement Order on Rotor

采用转子叶片优化排序技术降低涡喷发动机的振动

Numerical simulation of redesigned turbine matching in turbojet engine

涡喷发动机涡轮改型匹配的数值仿真

Hardware in the Loop Simulation of Minitype Turbojet Engine Digital Control Regulator

小型涡喷发动机数控调节器的半实物仿真

Research on characteristics of turbojet engine with simple control program

简单控制规律下涡喷发动机特性的研究

Neural network PID adaptive control in pilotless aircraft turbojet engine

无人机涡喷发动机的神经网络自适应PID控制

Analysis on Methods of Missile Turbojet Engine Condition Monitoring

弹用涡喷发动机的状态监控方法分析

Research on Self-adaptive Neural Network Control of Pilotless Turbojet Engine

无人机涡喷发动机的自适应神经网络控制研究

Effect of Inlet Pressure Distortion on Stability Margin of Missile Turbojet Engine

进口压力畸变对弹用涡喷发动机稳定性的影响

Starting and accelerating model of missile turbojet engine in flight test

弹用涡喷发动机飞行试验启动加速性能仿真

Application of simulation model of sensors to analysis fault of control system of turbojet engine

应用传感器仿真模型分析发动机控制系统故障

Design for scheme of reliability growth testing of turbojet engine

涡喷发动机可靠性增长试验方案的设计

Investigation of rocket sled test for missile turbojet engine

弹用涡轮喷气发动机火箭橇试验研究

Identification of Expansion Model Based on Equilibrium Manifold of Turbojet Engine

涡轮发动机平衡流形展开模型辨识方法研究

A Testing Instrument for the Box Against Pant of Some Turbojet Engine

某涡喷发动机防喘盒检测仪的研制