弹用涡扇发动机,missile turbofan engine
1)missile turbofan engine弹用涡扇发动机
1.Selection of reliability parameters and targets assessment for certainmissile turbofan engine弹用涡扇发动机可靠性参数选择及评定方法
英文短句/例句
putation and assessment of aerodynamic stability of turbofan engine for missile弹用涡扇发动机气动稳定性计算与评定
2.Selection of reliability parameters and targets assessment for certain missile turbofan engine弹用涡扇发动机可靠性参数选择及评定方法
3.Study and Characteristic Analysis of Start-up Process for Missile-borne Fanjet弹载涡扇发动机起动过程的研究及其特性分析
4.Performance Deterioration and Control of Military Turbofan Engine军用航空涡扇发动机性能衰减及控制
5.Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles高空长航时无人机用涡扇发动机技术分析
6.An airplane with such an engine.由涡轮风扇发动机提供动力的飞机
7.Aerodynamic Design and Analysis for Low Pressure Turbine of a Large Scale Turbofan Engine;某大型涡扇发动机低压涡轮气动设计与分析
8.Numerical Analysis on Matching between Internal and External Bypass and Fan of Aero-engine;涡扇发动机风扇及内外涵道匹配的数值分析
9.Field Repairing Technology of Fan Blades for a Turofan Engine某型涡扇发动机风扇叶片外场抢修技术研究
10.The mission section, the constrain conditions, the weight composition of the maneuverable missile, and the model of used in turbofan engine maneuverable missile were presented.简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
11.Cutaway of the PW 4000112-in(284.48cm) gas turbine engine ,showing fan bypass section.涡轮发动机剖面图，展示风扇旁路部分。
12.Study of design method for the zero-stage compressor in an expendable gas turbine engine弹用涡喷发动机加零级压气机设计方法研究
13.AMESim Simulation Analysis of the Leakage of a Turbine Engine Fuel Adjustor Shutting Solenoid Valve某型涡扇发动机用燃调产品停车电磁阀泄漏影响性的AMESim仿真分析
14.Application of Support Vector Machine in Fault Diagnosis of Aeroengine Test支持向量机的涡扇发动机试车故障诊断
15.Overview of Advanced Technology for Geared Turbofan Engine (GTF)齿轮传动涡轮风扇(GTF)发动机先进技术综述
16.Ideal Starting Procedure Analysis and Optimization Control Investigation for Turbofan Engine涡扇发动机理想起动过程分析与控制问题探讨
17.Dual-mode Optimization Asymmetry Fuzzy Logic Controller Design for X Aeroengine MFP某涡扇发动机主燃油通道模糊控制器设计
18.Reliability growth analysis and assessment for a type of turbofan engine;某型涡扇发动机的可靠性增长分析与评估
相关短句/例句
military turbofan engine军用涡扇发动机
3)missile turbojet弹用涡喷发动机
1.Full process circled simulation flat of somemissile turbojet and its oilsupplied regulating system based on MATLAB is proposed for factually describing component interaction of engine system.为真实反映实际发动机系统的各部分相互影响,提出和建立了基于MATLAB环境的某弹用涡喷发动机及其供油调节系统的全工况闭环仿真平台。
2.According to themissile turbojet FADEC system request,applying step motor subdividing control technic,a kind of intelligent fuel actuator formissile turbojet which is based on the ATMEL 89C51 MCU was designed.根据弹用涡喷发动机数控系统对燃油控制执行器的要求 ,采用步进电机细分控制技术 ,设计以AT MEL 89C51单片机为核心的智能步进电机驱动控制器 ,实现了与上位机并行或串行数据传输 ,细分数、运行频率键盘设定 ,自动升降频运行 ,电机全电流与半电流控制 ,2 4 0个运行记录 ,步数、细分数、运行频率LED显示等功能。
4)turbofan engine涡扇发动机
1.A decentralized multivariable PI controller forturbofan engine;涡扇发动机分路式多变量PI解耦控制
2.Design of a newturbofan engine preservation equipment;新型涡扇发动机油封设备的研制
3.Numerical simulation of the start-up process of augmentedturbofan engines;某型涡扇发动机起动过程数值模拟
5)turbofan engines涡扇发动机
6)turbofan[英]["t?:b?uf?n][美]["t?bo,f?n]涡扇发动机
1.Key turbomachinery technology of civil high-bypass-ratioturbofan engine;民用大涵道比涡扇发动机叶轮机某些关键技术
2.The key technologies and future trend for several novelturbofan engines are described.总结了多电发动机、智能发动机、双外涵变循环发动机、复合材料发动机、外骨架发动机、绿色发动机等未来涡扇发动机的研究进展、关键技术和发展趋势。
3.To simulate the starting characteristics ofturbofan engine in different atmospheric environments, particularly in plateau regions and at high or low temperature, a generalized description of engine starting mathematical model based on state space is given.针对不同大气条件尤其是高原和高、低温条件,及不同起动机和负载扭矩特性下涡扇发动机起动过程的数值模拟问题,给出了通用起动模型状态空间描述形式,研究了基于支持向量机的起动模型辨识和起动性能仿真方法。
延伸阅读
航空发动机推重比(见航空发动机推力)航空发动机推重比(见航空发动机推力)thrust to weight ratio of aeroenginehQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
