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aircraft section相关的网络例句

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与 aircraft section 相关的网络例句 [注:此内容来源于网络,仅供参考]

1605 Antiaircraft Artillery Regiment, 4 Bomber Aircraft Corps (202, 219, 321 Bomber Aircraft Division), 5 Ground Attack Aircraft Corps (4 Guards, 264 Ground Attack Aircraft Division), 8 Ground Attack Aircraft Corps (224, 227 Ground Attack Aircraft Division), 5 Fighter Aircraft Corps (8 Guards, 256 Fighter Aircraft Division), 10 Fighter Aircraft Corps (10 Guards, 235 Fighter Aircraft Division), 10 Guards Ground Attack Aircraft Division, 331 Fighter Aircraft Division, 208 Night Bomber Aircraft Division, 98 Guards, 50 Recon Aircraft Regiment, 372, 1002 Separate Artillery Regiment

第1254﹑1554﹑1555﹑1605防空炮团,第4轰炸机军(第202﹑219﹑321轰炸机师),第5强击机军(第4近卫强击机师,第264强击机师),第8强击机军(第224﹑227强击机师),第5歼击机军(第8近卫歼击机师,第256歼击机师),第10歼击机军(第10近卫歼击机师,第235歼击机师),第10近卫强击机师,第331歼击机师,第208夜间轰炸机师,第98近卫侦察机团,第50侦察机团,第372﹑1002独立炮兵团

The main jobs of this paper are as followed: 1 The reuse of the frame design technology for aircraft assembly fixtures is researched. a frame line part library is built with the templet driven technology, the reuse of the frame line part come true by the tools for instantiation and instance modification. The design resources are effectively used, some repeating work is cut. 2 Two methods to obtain the assembly feature are proposed: the straight way by the Enumeration method and the indirect way by project features to the assembly plane. All of the assembly features of the frame and the adjustable bearings are obtained by these two methods which makes the frame automatic assembly technology for aircraft assembly fixtures come true. 3 The frame automatic assembly technology aircraft assembly fixtures based on assembly features is researched. A binary tree assembly model is used to express the assembly information of the frame for aircraft assembly fixtures, the automatic assembly between the frame, the aircraft and the adjustable bearing is completed within the three steps: distribute, obtain and evaluate assembly feature. Finally, the efficiency of the frame assembly design is proved. 4The frame interpart modeling technology for aircraft assembly fixtures is researched, the intersection methods are concluded and the arithmetic of the single-cut, double-cut and inter-cut intersection is proposed, the interpart fast modeling of the frame design for aircraft assembly fixture come true. 5Based on the researches mentioned before, a sub-system of frame fast design for aircraft assembly fixture is developed on CATIA. The sub-system is used to design the aircraft assembly fixtures in a large aeronautics corporation and make a good- effect.

论文的主要工作如下: 1研究了飞机装配型架骨架设计重用技术,在总结归纳骨架线框结构类型的基础上,应用模板驱动的方法建立了骨架线框库,通过骨架线框零件的实例化和离线编辑实现骨架线框的重用,有效利用设计资源,减少重复劳动; 2提出穷举几何对象的装配特征直接获取方法,遍历零件模型的几何对象,从中捕捉所需装配特征,该方法简捷、高效;提出向装配面投影的装配特征间接获取方法,该方法在现有特征基础上生成装配特征,解决了部分装配特征难以直接获取的问题; 3研究了基于装配特征的飞机装配型架骨架自动装配技术,采用一种二叉树装配模型表达骨架的装配关系,并通过装配特征的分配、获取和赋值三个步骤,实现了骨架分别与飞机产品和可调支承的自动装配,避免了繁琐的人工交互操作,提高了骨架设计的效率和规范化程度; 4研究了飞机装配型架骨架零件间建模技术,在总结归纳骨架元件相贯处理方式的基础上,提出了骨架元件单剪切相贯、双剪切相贯和互剪切相贯的实现算法,简化了骨架相贯处理的过程; 5基于以上研究,在CATIA平台上开发了飞机装配型架骨架快速设计子系统,并应用于某大型航空企业的装配型架设计,提高了设计效率和设计质量。

The paper chooses the assembly of aircraft digital assembly location as a research object, chooses the assembly of aircraft section as a research example, aims to study the method of aircraft digital assembly location, focuses on the research of the structure of digital assemble control prototype system for aircraft section based on laser measurement, develops the servo control device and related software based on LM629, ATmega128 and LMD18200, completes the construction of the system based on the assembly of aircraft section.

以飞机的数字化装配定位为研究对象,以飞机舱段的装配为例,以探索飞机数字化装配的方法为目的,通过对基于激光测量的飞机舱段数字化装配定位控制原型系统结构的研究,采用运动控制芯片LM629、单片机ATmega128和功率放大芯片LMD18200构成了伺服系统控制随动装置,并开发了相关软件系统,完成了基于舱段大部件装配的数字化装配定位控制原型系统的设计开发。

U.S. general aviation as a result of continued growth, the United States already have a complete general aviation industry, whose members include the following: United States aircraft manufacturers, parts manufacturers to the United States, the United States instrument avionics manufacturers, flight schools in the United States, the United States Flying Club, the United States Flight Simulator manufacturers, the United States maintenance base fixed, the United States airport development and management company, sales of U.S. aircraft, the U.S. aircraft leasing companies, aircraft broker the United States, the United States valued the company aircraft, the U.S. aircraft renovation company, the U.S. aircraft loans and insurance companies, property management companies to share the United States, the U.S. investment management business, the United States aviation fuel suppliers, the United States, such as security consultants.

由於美国通用航空的持续成长,美国已具备完整的通用航空工业,其成员包括:美国飞机制造商、美国零配件制造商、美国航空电子仪表制造商、美国飞行学校、美国飞行俱乐部、美国飞行模拟器制造商、美国固定维修基地、美国机场开发管理公司、美国飞机销售商、美国飞机租赁公司、美国飞机中介公司、美国飞机估价公司、美国飞机装修公司、美国飞机贷款和保险公司、美国产权分享管理公司、美国投资管理商、美国航油供应商、美国安全保障顾问公司等。

276 Bomber Aircraft Division, 277, 281 Ground Attack Aircraft Division, 275 Fighter Aircraft Division, 13 Recon Aircraft Regiment, 203 Spotter-Recon Aircraft Regiment, 283 Fighter Aircraft Regiment, 212 Sanitary Aircraft Regiment, 199 Separate Artillery Regimentс.

第113﹑276轰炸机师,第277﹑281近卫攻击机师,第275歼击机师,第13侦察机团,第203侦察-校射航空团,第283歼击机团,第212卫勤飞行团,第199独立炮兵团

Design and manufacture of aircraft tooling are key part in aircraft manufacture process. Aircraft tooling supports the whole manufacture and assemblage course of aircraft components. Aircraft tooling plays an important status in manufacture, and design and manufacture of aircraft tooling is always manufacture bottle-neck, so research on aircraft toolings fast design has important meaning.

飞机工艺装备简称飞机工装,飞机工装的设计与制造是飞机产品制造中的关键环节,飞机工装支撑着飞机零部件制造和装配的全过程,飞机工装在航空主机厂所生产中有着极其重要的地位,一直是飞机产品研制过程中的瓶颈环节,进行飞机工装的快速设计技术研究具有重要意义。

The paper is structured as follows: section 1 provides an introduction of practical background, research issues, related notion, research framework, research method and innovation points. Section 2 presents related literature review and comments. Section 3 focuses on the research on the factors of industrial environment and networking backgrounds which influencing dualistic-innovation of clustered firms, and puts forward the hypothesizes; Section 4 is the empirical research that inspect and verify the authenticity of hypothesis proposed in section 3; section 5 concentrates on research on coordination mechanism of dualistic-innovation for clustered firms; section 6 is another empirical research that exam the theoretical derivation of section 4; followed by section 7, the conclusion and suggestion for government policy and further research.

论文的主要内容如下:第一章是绪论,介绍研究的现实背景、研究问题、x相关概念、研究框架、研究方法和创新点等;第二章是对文章所涉及的创新领域研究文献的回顾与评述;第三章是网络视角的集群企业二元式创新的影响因素研究,分析影响集群企业二元式创新活动的产业环境和网络环境的关键因素及其作用机制,并提出相应的命题假设;第四章是对应的实证分析,检验上一章提出的二元式创新影响因素的命题假设成立与否;第五章是网络视角的集群企业二元式创新的协调方式研究,提出相应的协调模型和具体的运行机制;第六章同样是对应性的实证分析,检验集群企业二元式创新协调方式的理论推导;第七章是结论、建议与未来的研究展望。

There are three sections in this dissertation, Section Ⅰ, Section Ⅱ and Section Ⅲ. Section Ⅰ is the core of the whole paper, the main content of this section is "Characteristics and conversion behavior of Dongsheng-shenfu coal". Section Ⅱ(Appendix1) is"Petrographical Characteristics of Chinese Steam Coal". Section Ⅲ(Chapter6) is the summary and perspective of the whole paper. Section Ⅰ and Section Ⅱ has some relationship in context.

全文共分三大部分,第一部分是本研究的核心内容---&东胜-神府煤的煤质特征与转化特性&,第二部分(附录1)为&中国动力煤的岩相特征&,这部分内容与第一部分的内容既是相互独立的,又有一定的关联,是第一部分的重要补充与说明。

The seed embryoes were penetrated by 〓 ion beams of 75 MeV/u and the seed endosperms were implanted by the proper degraded 〓 ions, and soluble protein of the seedling in M1 generation was divided into 5 sections to analyze their changes at different molecular weight. 1 In comparison with control, the relative content of the second section (molecular weight is heavier in all sections) of all irradiated materials got down, while the relative content of the fifth section (molecular weight is the lightest) of those went up. 2 The penetrating seeds made the relative content of the first section (molecular weight is the heaviest) and the third section (mid-molecular weight) drop, while the fourth section went up. Moreover, the changes of the third section and the fourth section of the penetrated materials were clearly different from those of the implanted materials. 3 The difference between implanted embryo and implanted endosperm existed in deeper dropping of the first section and higher rising of the fifth section on relative content of soluble protein of the latter. 4 On irradiated materials at lower doses, there were exceptional changes of soluble protein, it may be thought that there was excited effect of low dose.

1.75MeV/u 〓O〓离子经过适当降能后注入小麦种子的不同部位和贯穿整个种子,对其M1代幼苗的可溶性蛋白质组分以及电泳中不同区段蛋白质组分相对含量加以分析,结果表明:1)同对照相比,随着辐照剂量的增加,所有辐照材料第二区段蛋白质组分的相对含量下降;而第五区段蛋白质组分的相对含量升高。2)种子的贯穿处理,同时也引起第一区段和第三区段蛋白质组分相对含量的下降以及第四区段的升高;其中第三、四区段的变化明显区别于注入效应。3)注入胚和胚乳的区别在于后者第一区段蛋白质组分相对含量的较大下降和第五区段的较大提高。4)小剂量辐照的材料,可溶性蛋白质组分的变化异常,可能与低剂量辐射兴奋效应有关。

Additional to the progress in combat aircraft, the PLA Air Force is quickly developing its capabilities in new areas such as the aerial refuelling tanker aircraft, airborne warning and control system aircraft, airborne electronic warfare/countermeasures aircraft, long-range transport aircraft, advanced training aircraft, and unmanned aerial vehicles.

除了在战斗机方面取得的进步以外,中国空军还加紧了在新领域的研发能力,如空中加油机,机载报警与控制系统( A irborne Warning and Control System , WACS )飞机,电子对抗/干扰飞机,远程运输机,先进教练机和无人驾驶航空器。

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