1) large aircraft
大飞机
1.
The development of aerodynamics & configuration technology for large aircraft
大飞机气动总体技术的发展
2.
Based on game theory,an improved "blocking monopoly model" was used to dynamically stimulate the decision-making process in China\'s large aircraft projects,and its equilibrium solution was analyzed with backward induction.
以博弈论的观点,利用改进过的阻截垄断模型对中国大飞机项目决策过程进行动态模拟,采用逆向归纳法分析该不完全信息动态博弈的均衡解。
2) large aircraft
大型飞机
1.
This paper aims at the large aircraft and its structure characteristics,and by comparing the man assembly system with the machine assembly system and analyzing relation curves of automatic assembly and assembly cost,points out the meaning of automatic assembly technology which ensures long life,high efficiency and low cost of large aircraft structure,both in research and in manufacture.
简述了大型飞机及其结构特点,通过比较人与机器两种装配系统的特性,及分析装配自动化水平与装配成本等诸因素的关系曲线,指出了自动化装配技术在保证大型飞机结构长寿命、高效率、低成本研制和生产等方面的意义;对国外大型飞机的装配自动化发展状况进行了综述,简要分析了国外发展的几种主要自动化装配系统,总结了国外大型飞机的自动化装配水平;对西方国家在大型飞机自动化装配中采用的先进的装配理念和方法,如决定性装配方法等进行了概述。
2.
The present development and tendency of new materials used in large aircraft are introduced.
介绍了用于大型飞机的新材料的发展现状和趋势。
3.
It is argued that while developing airborne equipment for China s large aircraft should mainly rely on our own research and development(R&D),attention should also be paid to possible international cooperation of various forms for win-win purposes.
阐述了大型飞机工程中飞机、发动机、机载设备协调发展的必要性;提出了中国大型飞机机载设备的研发必须把立足点放在自主研发上,同时也要注意不同形式的国际合作,争取双赢;建议重视大型飞机共用技术和共用研发平台的开发,以利于提高资金的有效利用率;特别强调找准市场定位发展有特色的机载设备以提高国产大型飞机的市场竞争力;最后建议了11项需提前启动的项目。
3) large airplane
大型飞机
1.
Through analyzing the necessity and feasibility of developing the avionics system of Chinese large airplane and the developing trend of avionics technology,this paper proposes the idea for developing the Integrated Modular Avionics(IMA)of Chinese large airplane,and gives some suggestions for the development plan.
在分析发展我国大型飞机航空电子系统的必要性和可行性,以及航空电子系统技术发展趋势的基础上,提出了未来发展我国大型飞机综合模块化航空电子系统的架构设想,并对我国发展大型飞机航空电子系统提出了几点建议。
4) flexible airplane
大柔性飞机
1.
For the case in which the rigid mode and the first n modes of a flexible airplane are considered,the body of the airplane is defined as a multi-mass equivalent system and the calculation formulas of the parameters of the system are derived,which presents a model for testing/verifying landing impact load,landing work etc.
还给出了大柔性飞机着陆功量、机翼位移、剪力、弯矩计算公式。
2.
Landing dynamic simulations are evaluated for a flexible airplane with the conventional type of oleo-pneumatic main landing gear.
为解决现行飞机起落架缓冲器设计不考虑机体柔性存在的问题,以大柔性飞机支柱型起落架油气式缓冲器为例,采用三质量块飞机着陆模型和功量预估分配法选择缓冲器参数,并对其进行着陆响应动力学分析。
5) large aircraft manufacturing
大飞机研制
6) large capacity aircraft
大容量飞机
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条