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1.
介绍了四轴联动加工蒙皮削弱槽中涉及到的数控工艺方案,测量软件的开发和使用,计算机模拟仿真加工,刀具选用过程等关键技术。这些技术的开发,实现了蒙皮削弱槽的数控测量加工。该技术成为加工蒙皮削弱槽或薄壁类零件的关键工具。  相似文献   

2.
通过DLY-4A大壳体型腔的加工,简要论述了在数控加工中心上应用UG软件进行计算机自动编程加工的应用。  相似文献   

3.
文中讲述了数控加工技术在北京空间机电研究所承担的型号产品零件制造中的应用。主要涉及异形零件的编程和加工,使用参数编程的一些技巧和经验,以及使用自动编程软件在数控编程所取得的一些经验。  相似文献   

4.
阐述了数控加工软件的内容和形成过程。提出零件代码和装夹代码,直接建立计算机管理目录的方法,解决数控加工软件在管理中的问题。该方法在实际应用中已取得了良好的效果。  相似文献   

5.
文中讲述了数控加工技术在北京空间机电研究所承担的型号产品零件制造中的应用。主要涉及异步形零件的编程和加工,使用参数程的一些技巧和经验,以及使用自动编程软件在数控编程所取得的一些经验。  相似文献   

6.
《航天器工程》2009,(5):41-41
据中国航天新闻网2009年8月26日报道,中国空间技术研究院通过大量研究工作,于近日研制成功了新型原理薄壁壳体加工工装,突破了超薄钛合金壳体类零件制造的技术瓶颈,取得了阶段性成果。该原理薄壁壳体加工工装克服了由于超薄壁工件内壁与工装贴合不好,存在间隙的部位,从而造成在切削力等外力作用下变形而导致壁厚一致性差的问题,提升了半球零件壁厚一致性,实现了超薄工件的车削加工。  相似文献   

7.
以不锈钢薄壁件的型面加工为例,论述了数控加工过程中影响工件变形的几个主要因素,通过具体分析加工变形情况及其影响,针对加工中工艺安排、切削用量、装夹方式、刀具参数选择及切削液的选择等方面,分析了零件的加工变形情况,并提出了相应解决措施,为薄壁零件的数控加工提供了有益的方法。  相似文献   

8.
超高强度钢薄壁件车削变形控制   总被引:1,自引:0,他引:1  
结合固体火箭发动机超高强度钢薄壁壳体的特点,分析了其在切削加工过程中产生变形的影响因素;重点分析了工件的装夹、切削力、切削温度对加工精度的影响;介绍了应用有限元分析软件研究超高强度薄壁零件变形的基本方法;提出了控制薄壁零件加工变形的方法,即合理选择夹具及装夹方式、刀具的正确选择、减小切削热的影响、合理选择切削用量以及减小切削力等措施。  相似文献   

9.
对用Pro/NC软件在航天产品加工中的应用进行了研究。介绍了Pro/NC刀具轨迹的编程过程、方法、加工仿真、NC检测,以及生成G代码程序等。给出了一壳体零件的加工实例。结果表明:在产品加工中应用Pro/NC软件可提高加工和编程效率。  相似文献   

10.
徐之焜 《火箭推进》2006,32(2):41-45
通过对某型号火箭薄壁半球零件的加工,对该零件在数控加工时所需的工艺流程的安排、工装的设定、刀具的选用以及数控程序的编制作了阐述。介绍了以这个零件为基础库,加工其它类似半球类零件的情况。  相似文献   

11.
A string moving with geostationary angular velocity in its radial relative equilibrium configuration around the Earth, reaching from the surface of the Earth far beyond the geostationary height, could be used as track for an Earth to space elevator. This is an old dream of mankind, originating about 100 years ago in Russia. Besides the question of feasibility from a technological point of view also the question concerning the stability of such a configuration has not yet been completely solved. Under the assumption that a proper material (carbon nanotubes) is available, making the connection possible technologically, we address the question of existence and stability of the radial relative equilibrium of a tapered string on a circular geosynchronous trajectory around the Earth, reaching from the surface of the Earth far beyond the geostationary height.  相似文献   

12.
In this paper, we analyze the illumination conditions, the thermal regime, and the possibility of deposits of volatile compounds existing in the vicinity region (NSR S5 region) near the southern pole of the Moon. It has been found that there are no permanently shadowed zones near the Scott crater and the NSR S5 region, though the temperature conditions allow the of compounds such as CH3OH, SO2, NH3, CO2, H2S, C2H4, and water to remain stable relative to evaporation for a long time (≥1 Gyr). It has been also shown that compounds like CO and CH4 cannot stably exist in these regions.  相似文献   

13.
The results of an investigation of the distribution of plasma pressure, pressure gradients, and magnetic field near the equatorial plane in the plasma ring surrounding the Earth under magneto-quiet conditions are presented. Observational data obtained during the international THEMIS mission are used. The picture of the distribution of transverse-current density near the equatorial plane was obtained under assumption of observing the magnetostatic balance condition at geocentric distances from 6 to 12R E. In estimating the integral transverse current it was accepted that in daytime sector the magnetic-field minima on magnetic field lines are not localized in the equatorial plane. Estimates of the integral transverse current were obtained, which demonstrate the possibility of closing nighttime transverse currents at geocentric distances of up to ~12R E inside the magnetosphere, which form a high-latitudinal continuation of the ring current.  相似文献   

14.
对老年人体育锻炼负荷量监控方法的探讨   总被引:2,自引:0,他引:2  
通过对老年人体育锻炼活动的情况进行相关调查,发现目前老年人体育锻炼中存在一些误区。因此本文针对这些现实情况提出,应根据实际情况运用一些简单易行的方法来对老年人体育锻炼实施医务监督,达到提高老年人体育锻炼的科学性。  相似文献   

15.
The paper has studied the accuracy of the technique that allows the rotational motion of the Earth artificial satellites (AES) to be reconstructed based on the data of onboard measurements of angular velocity vectors and the strength of the Earth magnetic field (EMF). The technique is based on kinematic equations of the rotational motion of a rigid body. Both types of measurement data collected over some time interval have been processed jointly. The angular velocity measurements have been approximated using convenient formulas, which are substituted into the kinematic differential equations for the quaternion that specifies the transition from the body-fixed coordinate system of a satellite to the inertial coordinate system. Thus obtained equations represent a kinematic model of the rotational motion of a satellite. The solution of these equations, which approximate real motion, has been found by the least-square method from the condition of best fitting between the data of measurements of the EMF strength vector and its calculated values. The accuracy of the technique has been estimated by processing the data obtained from the board of the service module of the International Space Station (ISS). The reconstruction of station motion using the aforementioned technique has been compared with the telemetry data on the actual motion of the station. The technique has allowed us to reconstruct the station motion in the orbital orientation mode with a maximum error less than 0.6° and the turns with a maximal error of less than 1.2°.  相似文献   

16.
本文介绍了“三位一体”教育模式的内容,描述亍我们实施该模式所采取的措施及取得的成效。实践表明,“三位一体”教育模式能够提高学生的综合素质,为学生毕业后的发展打下坚实基础,对教育模式的改革具有一定的指导意义。  相似文献   

17.
电阻式传感器的核心部件——电阻应变计是目前最常用的应力分析的敏感元件。也常用于测量力、压力、扭矩和加速度等物理量。作者简要回顾了电阻应变计的发展历史,介绍了电阻应变计的结构、分类及现状,展望了电阻式传感器的前景。  相似文献   

18.
The results of modeling the dynamics of the Space Radiotelescope are presented. The results of ground-based vibration-dynamic tests are used to validate the calculation models and estimate the damping levels. The dynamic distortions of the reflecting surface caused by the operation of the pointing mechanism of the high-gain antenna are estimated.  相似文献   

19.
The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterized by a relatively small perihelion radius and relatively high inclination, which allows one to investigate the polar regions of the Sun. The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.  相似文献   

20.
火箭推进剂液体晃动关机响应的数值仿真   总被引:4,自引:0,他引:4  
本文采用VOF方法对火箭发动机关机阶段所引起的液体晃动进行了数值仿真,以氧化剂贮箱为例,得到了贮箱无阻尼环和带阻尼环时的晃动仿真图和液体质心变化曲线,检验了VOF方法处理碎波的能力。  相似文献   

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