气动

压力机液压、气动原理图的CAD

CAD of Hydraulic and Pneumatic Schematic Diagram of a Press

PLC在气动控制电极板剪切机中的应用

The Application of PLC in Pneumatic Control Electrode Board Cutting Machine

用气动吸引器将废水试样送入液体注射阀。

The wastewater samples is transmitted by an air-operated aspirator to the liquid injection valve .

离开液膜或射流的液滴，可能会受到高的相对速度气体的气动压力影响。

A liquid drop removed from a sheet or jet may be exposed to the aerodynamic pressure effect of a high relative gas velocity .

风动冲击器是气动冲击回转钻进的主要设备之一

Pneumatic DTH ( Down-The-Hole ) hammer is one of main pneumatic percussive-rotary drilling equipments .

下放单根进小鼠洞，摘掉气动绞车和提丝

Lower the drill pipe joint into the mouse hole , and remove air tugger and lifting cap .

简易啤酒桶装灌装机气动系统及其PLC控制

A Pneumatic System for the Barrelled Beer - filling Machine and its PLC Control

模糊PID控制在气动机械手中的应用

Application of Fuzzy PID Control for Pneumatic Manipulator

2D气动数字伺服阀静态特性分析

Analysis on static characteristics of 2 D pneumatic digital servo valve

气动柔性球关节的模糊PID控制

Fuzzy-PID Control for Flexible Pneumatic Spherical Joints

PWM气动高速开关阀描述函数的研究

On the Describing Functions of PWM Pneumatic High-Speed On-Off Valves

PWM线性化气动控制系统的研究

Linearized pulse-width-modulation ( pwm ) pneumatic control system

探讨了一种将CAD软件、CFD商用软件与代理模型相结合的飞机气动外形优化方法。

This paper discusses an approach of aerodynamic shape optimization combining CAD and CFD with surrogate models .

采用NURBS的某级透平叶片全三维气动最优化设计

Aerodynamic 3-Dimensional Optimal Design by NURBS of a Certain Stage Turbine Blades

SF6开关气动机构漏气原因分析与改造

Causes and Action for SF_6 Switch Pneumatic Mechanism

神经元自适应PSD控制在气动人工肌肉力控制中的应用

Study on the Force Control of Pneumatic Muscle Actuator with the Neural - PSD Adaptive Algorithm

CFD验证和确认是气动计算可信度分析的基本活动。

CFD verification and validation ( V & V ) are fundamental activities of credibility analysis for aerodynamic simulations .

开发了一个原形系统，该原形系统构造了一个完整的适用与三维虚拟设计的气动系统CAD软件框架，并实现了其中的主要模块。

A prototype system is developed , and a pneumatic system CAD software architecture that is applicable to 3D virtual design is constructed by the prototype system .

电压的变化反映了系统压差Δp的变化，根据Δp与s一一对应的关系，即可实现在线的气动检测。

The variation of voltage can reflect the variation of the system 's differential pressure Δ p , and according to the relation of Δ p and s , on-line pneumatic measurement become ture .

主机遥控气动装置FTA与FEA计算机分析软件开发

The development of analysis software for both FTA and FEA of pneumatic device in automatic remote control system for main diesel engine

将许多相同的MEMS器件组成阵列，构成自适应结构控制飞机气动性能已成为MEMS研究在航空领域的主要发展方向之一。

Self-adapting structure for the aerodynamic control , which arrayed by a lot of the same MEMS devices , became the important issue in the AERO-MEMS field .

根据压力机液压气动原理图的设计特点，开发了压力机液压、气动原理图的CAD软件，介绍了其程序框图及应用框图。

The CAD software , Which can be used for designing the hydraulic and pneumatic schematic diagram of a press , is developed according to the characteristics of the hydraulic and pneumatic schematic diagram of press .

用小型电弧加热器对筛形喷管CO2-N2超音速混合气动激光器进行了实验研究。

Experimental study on a CO_2-N_2 supersonic mixing GDL with a screen nozzle was performed on a small scale electric-ar (?) heater .

并将PMAC的标志控制口改作为通用I/O口，在此基础上进行了硅片传输机器人的气动控制回路的设计。

The flags of PMAC is used as the general I / O interface and the pneumatic control loop of the wafer robot is designed .

Zell浆纱机气动控制压浆原理分析

Working Principles of Pneumatic Squeezing Roller on Zell Size Machine

亚临界和超临界600MW机组高压调节阀组气动特性分析

Analysis on Aerodynamic Performance of HP Governing Valve Groups for Subcritical and Supercritical 600 MW Units

基于最优控制理论原理和Navier-Stokes方程，研究了气动/几何约束条件下多设计变量的翼型气动优化设计问题。

Based on the optimal control theory and Navier-Stokes equations , aerodynamic design of airfoil with multi-constraint conditions , such as aerodynamic and geometric constraint conditions , is studied .

采用模块化设计原理，应用现代气动元件、高精度差动电感传感器、PLC等组成自动分选仪，实现了对滑片几何参数进行高精度快速测量。

In order to realize measuring geometric parameter of slip accurately and quickly , the author adopts the module design principle , and uses modern pneumatic component , high-accuracy differential inductor sensor and PLC to make up the automatic sorting appearance .

以主动颤振抑制系统设计为代表的气动伺服弹性力学（ASE）是一门涉及柔性结构、飞行器运动引起的定常和非定常气动力以及飞行控制系统相互作用的多学科技术。

Aeroservoelasticity , including active flutter suppression technology , is a multidisciplinary optimization technology that studies the interaction of flexible structure , unsteady aerodynamics and flight control system .

进气道是飞机正前方三大强散射源中RCS值最大的一个，而在进气道中采用隐身技术又涉及到对气动特性和飞行安全性的影响。

Air intake is the RCS value among the three strong radiation sources in front of aircraft , and stealth technology adopted in air intake will have impact on aerodynamic characteristics and flight safety .