飞机座舱
- 网络Cockpit
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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 .
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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 .
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基于DirectX的飞机座舱模拟
Simulation of interactive cockpit based on directX
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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 .
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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 .
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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 .
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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 .
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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 .
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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
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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 .
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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 .
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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
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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
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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
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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
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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
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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 .
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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
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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
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飞机座舱玻璃划痕深度的测量
Research on measurement of scratched mark depth on aero cabin glass
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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
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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
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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
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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
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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
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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
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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
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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
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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 .
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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