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武器工业与军事技术
航空航天科学与工程
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aircraft gun
相关语句
  航炮
     Study on the Principle of Launching and Control of ГШ-301 Aircraft Gun
     ГШ-301航炮发射控制原理研究
短句来源
     Analysis on Failure of Link Jam for JL8 Aircraft Gun Pod
     JL8飞机航炮吊舱卡链故障分析
短句来源
     Designing of Safety Device for an 23mm Aircraft Gun
     某型23mm航炮防走火保险装置的设计
短句来源
     Analysis of Design Concepts and Technical Methods for ΓⅢ -301 Aircraft Gun
     ΓⅢ-301航炮的设计思想及技术措施分析
短句来源
     This paper introduce design method and work principle on the application of SCM to aircraft gun projecting control, and provide hardware circuit and software design process.
     本文主要介绍了单片机在航炮射弹控制中的设计方法和工作原理,给 出了硬件电路和软件设计过程。
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  机载航炮
     Expert system for aircraft gun fault diagnosis based on neural network
     基于神经网络的机载航炮故障诊断专家系统
短句来源
     On the basis of analyzing the advantages and disadvantage when expert system or neural network is applied to equipment fault diagnosis separately, an expert system based on neural network for aircraft gun fault diagnosis is set up.
     在分析专家系统和神经网络单独应用于设备故障诊断的优缺点基础上 ,建立了基于神经网络的机载航炮故障诊断专家系统。
短句来源
  “aircraft gun”译为未确定词的双语例句
     The Application of SCM to Aircraft Gun Firing Shell Number Control
     单片机在炮弹射击发数控制中的应用
短句来源
     Study on Fire control Model of Anti aircraft Gun Missile System
     弹炮结合防空武器系统射击指挥模型研究
短句来源
     Method of research for reducing the recoil force of aircraft gun and its tendency to advance
     减小航炮后座力研究的发展趋势与方法
短句来源
     The fire control process of anti aircraft gun missile system is analysed,primary models of fire control including models of target search,fire feasibility examine,menace assess,fire assignment,kill feasibility evaluation are summarized.
     分析了弹炮结合防空武器系统射击指挥过程 ,概述了主要射击指挥模型 ,包括目标搜索模型、拦截适宜性检查模型、威胁判断模型、火力分配模型、杀伤效果评估模型 .
短句来源
     This paper simply introduces the composing of the distributed interactive simulation system of anti aircraft gun, analyses the technology of the supporting software in the simulation of warning radar, command system and anti aircraft gun including system software of the computers and some self designed software.
     简单介绍了高炮分布交互仿真系统体系结构 ,分析了警戒雷达仿真、指挥系统仿真和高炮仿真所需要的软件支撑技术 ,包括计算机系统软件和自己开发的一些通用软件。
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In this paper, the method and principle of reducing the recoil force of theaircraft gun are systematically described. The method of the approximateestimate of the maximum recoil force is also described which considers theturret as a elastic body. Finally, the tendency for research of reducing therecoil force of the aircraft gun to advance is discussed and the applicationof the hydraulic control system to reducing the recoil force of the aircraftgun is also introduced.

本文较系统地叙述了各种减小航炮后座力的方法和原理以及考虑炮架为弹性体时,最大后座力的近似估算方法。最后讨论了减小航炮后座力研究的发展趋势,兹介绍了液压后座控制系统在减小航炮后座力方面的应用。

In this paper, the principle of a new device-high-energh absorbingbuffer, which can reduces the recoil force of an aircraft gun, is introduced.The equations of motion of each stage of the gun for this amortisseur andphase-plan which describes the state of motion are also derived. Finally,the condition of constraints used to select tie structure parameters of thebuffer is provided.

本文介绍了减小航炮后座力的一种新型装置-高吸能缓冲器的工作原理。导出了武器在此种缓冲器上各阶段的运动方程以及描述其运动状态的相平面图。最后提出了高吸能缓冲器结构参数选择的约束条件。

In this paper, the standardized general dynamic equations and imp-aet for mulas are derived which are suitable for the system of automatical weap-on with two degrees of freedom, and they are extended to the system with thr-ee degrees of freedom considering the elasticity of turret. Based on these egu-ations and formulas, the certain general mathematical analogye program is writ-ten which serve versat and man-machine dialogue functinos. When the programis applied to a certain aircraft gun, the influence...

In this paper, the standardized general dynamic equations and imp-aet for mulas are derived which are suitable for the system of automatical weap-on with two degrees of freedom, and they are extended to the system with thr-ee degrees of freedom considering the elasticity of turret. Based on these egu-ations and formulas, the certain general mathematical analogye program is writ-ten which serve versat and man-machine dialogue functinos. When the programis applied to a certain aircraft gun, the influence laws of its strueture param-eters and initial conditions on the motion, fire frequency and recoil force areobtained, and the feasible best matching of the structure paramaters of a certainaircraft gun buffer is also obtained when the recoil force has its minimum. Th-is paper has first applied the work-diagram to the dynamic analysis of autom-atic weapon.

本文导出了规范化的二自由度自动武器系统动力学普遍方程和撞击公式,并将其推广到考虑炮架弹性的三自由度系统。在此基础上,编制了具有一定通用性和人机对话功能的数学模拟程序,应用该程序对××航炮进行了数学模拟,得出了武器系统结构参数和初始条件对运动、射频和后座力的影响规律,以及使后座力最小时可行的××航炮缓冲器结构参数的最佳匹配。本文还首次将功图应用于自动武器动力分析。

 
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