飞机座舱

本文主要阐述了飞机座舱仪表显示器的发展现状、术特点和未来的发展趋势。

In this paper several development actuality of cockpit display are introduced ; their technology property is discussed and future development of cockpit display is analyzed .

在这里，探索性草图位置的控制面板和处理是必需的，为了检查布局飞机座舱本身。

Here , exploratory sketches of the position of the control panel and handles were necessary in order to examine the layout of the cockpit itself .

基于DirectX的飞机座舱模拟

Simulation of interactive cockpit based on directX

本文应用雷诺平均Navier-Stokes方程和Launder-Sharma低雷诺数模型计算了飞机座舱内的流场和温度场。

The Reynolds averaged Navier Stokes equations and Launder Sharma low Reynolds number model are used to simulate the airflow in the cabin .

在基于PC机的网络环境中，通过VAPS开发工具作为平台，利用C语言和网络通信技术，设计了一套民用飞机座舱主要电子显示仪表的仿真系统。

Using C language and network communication , an electronic instrument simulation system of civil aircraft is developed with VAPS in PC network platform .

在飞机座舱电子飞行仪表系统中，电子式全姿态指示器（Electronicattitudedirectorindicator，EADI）的天地区域的重新填充是个非常费时的工作。

The filling of sky and ground region on the electronic attitude director indicator ( EADI ) in an aircraft electronic flight instrument system ( EFIS ) is a time-consuming work .

利用NASA最大关节力矩计算公式和飞机座舱操纵杆的实际安装尺寸，对驾驶员的操作活动进行模拟仿真。

Using the maximal joint torque expressions derived from NASA experimental data and the actual installation dimension of cockpit , the operation movement of the pilot is simulated .

以某飞机座舱模型为研究对象，利用压电智能结构，并结合振动主动控制方法和LMS自适应滤波算法，实现了一套完整的飞机座舱模型振动、噪声主动控制系统。

We used piezoelectric smart structures ; active vibration control technology and LMS adaptive filter algorithm to control the vibration and noise of the cockpit model and had realized a control system .

飞机座舱EADI画面高速填充的一种新方法

New High Speed Filling Method for EADI Graphics in Aircraft Cockpit

实验模拟飞机座舱环境，采用计算机生成的数字化言语信号，在90dB（A）的飞机噪声环境下，通过耳机传递给被试。

Digitized speech signals generated by computer were presented to subjects in 90 dB ( A ) cockpit noise condition .

介绍了第二代B737飞机座舱增压系统后外流活门和加温垫的工作及控制原理，对实际维护中的一种典型故障进行了分析和研究。

The paper summarizes the working process of outflow valve and heater gasket of second generation B737 , analyses a routine malfunction and provides a train of analysis .

飞机座舱压力控制系统性能分析

Analysis of the Capability of the Plane Cabin Pressure Control System

飞机座舱软连接用胶黏剂的研制

Study on the Adhesive Used for Flexible Bonding of Aircraft Cabin

飞机座舱模拟台控制系统的设计及实现

Design and Realization of Control System for Aircraft Cabin Simulation Table

飞机座舱显示/控制系统的综合评价方法

Method for comprehensive evaluation of the cockpit display and control system

采用压电陶瓷的飞机座舱辐射噪声主动控制

Active Radiation Noise Control of Airplane 's Cabin Using Piezoelectric Elements

设计了一套民用飞机座舱电子显示仪表的仿真系统。

An electronic instrument simulation system of civil aircraft is developed .

飞机座舱盖热疲劳试验台设计研究

Study of the Design for Canopy Thermal Fatigue Test - Bed

飞机座舱显示与显示器件的最新发展

Recent Development of the Aircraft Cockpit Display and its Display Devices

飞机座舱玻璃划痕深度的测量

Research on measurement of scratched mark depth on aero cabin glass

飞机座舱透明件设计理论及应用

Design Theory and Application for Transparency of Aircraft Canopy and Windshield

飞机座舱显控系统工效学评价技术与方法

Evaluation Technique & Method of Aircraft Cockpit Display and Control System

飞机座舱全姿态指示器的填充算法研究

One new filling algorithm of attitude indicator in aircraft cockpit

飞机座舱视听告警方式的工效学研究

An Ergonomic Study of Visual and Auditory Alerting Modes in Aircraft Cockpits

飞机座舱减振降噪优化设计方法

Structural Optimal Design to Reduce Vibration and Interior Noise of Aircraft Cabin

飞机座舱显示/控制系统设计与研究

Design and Research of Aircraft Cockpit Display and Control System

液晶显示器在飞机座舱的应用及发展

The Application and Development of LCD in Aircraft Cockpit System

飞机座舱热力特性的数值模拟研究

The numerical simulation on the thermal behaviour of aircraft cabin

目的综述飞机座舱毒理学研究进展情况。

Objective Researching advances in toxicological studies on aircraft cabin were reviewed .

飞机座舱风挡层合玻璃弹穿有限元分析

Finite Element Analysis of Bullet Perforating Multi Layer Composite Class