座舱盖

座舱盖系统三维数字化设计流程研究

Research of Three-Dimensional Digitalization Design Flow for Canopy Systems

近年来由于飞机座舱盖定向有机玻璃部件断裂破坏事故屡次发生，以及新型高性能飞机对其力学性能提出了更高要求，使得定向有机玻璃材料的力学性能逐渐得到研究人员的重视。

The mechanical properties of directional PMMA have received considerable attentions due to the fracture of aircraft canopy and requirements of high-performance aircraft .

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

活动座舱盖结构设计中连接形式分析

The Joint Mode Analysis for Structure Design of Movable Cabin

36号飞机座舱盖空中爆破故障分析

Failure Analysis of Canopy for 36 ￣ # Aircraft

座舱盖抛放过程中的非定常气动特性研究

Unsteady Aerodynamics Characteristic Study of a Jettisoned Aircraft Canopy

座舱盖跨声速阻力特性的试验研究、理论计算及工程应用

Experiment investigation of transonic drag characteristics theoretic calculation and engineering application for close cabin

弹射过程座舱盖抛放轨迹的预测

Prediction of the aircraft canopy trajectory

某型飞机座舱盖上位锁摇臂断裂故障分析

The Analysis of the Failures of the Rupturing of the Rocker in the Canopy Uplock of Some Model Fighter

介绍了某型飞机座舱盖系统的三维数字化设计特点和设计流程。

This paper focuses on three dimension digitalization design features and flow for the cockpit canopy system of a airplane .

有机玻璃材料由于具有较好的透光性和足够的结构强度而广泛应用于飞机座舱盖、风挡等结构中。

Polymethyl Methacrylate ( PMMA ) has been widely used in the wind shield of aircraft because of its excellent transparency and strength .

脱离连接时也是一点也不轻松，那一刹那从前置受油口飞溅出来的燃油喷射在座舱盖上，飞行员跟失明差不多。

Any relaxation vanishes at disconnect , when the pilot is momentarily blinded by fuel spray on the canopy from the forward-mounted receptacle .

飞机座舱盖玻璃成型残余应力测定&双折射主切片图解法

Determination of residual stress caused by forming in transparent airplane canopies & a graphic method by means of the birefringence in the first slice

利用其透明性和高抗冲击强度，可制作防弹玻璃、飞机的挡风罩、座舱盖等。

With the high transparence and impact strength , it could be applied in bulletproof glass , windshield , cockpit of airplane and so on .

驾驶舱盖，座舱盖飞机驾驶室顶部的透明覆盖物被盖顶盖被盖的联系只与上丘中、深层有关。

The transparent enclosure over the cockpit of an aircraft . The tegmentum tectum tegmentum connections are only concerned with the mid-dle and deep layers of the superior colliculus .

通过故障实例，综合分析某型现役主力战机座舱盖升降系统上位锁的工作原理及该系统中摇臂断裂故障产生的原因，提出修理及维护对策。

Based on a few failures of the canopy elevator system of some main force Fighter , this paper analyzes the working principle of the uplock and the causes of the rupturing of the rocker , proposes some repairing and maintaining solutions .