首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到18条相似文献,搜索用时 109 毫秒
1.
分析总结了国内外小直径深孔加工技术后,介绍了小直径深孔加工技术在航空机载行业中的应用,及其小直径深孔加工时设备选型需注意的问题。  相似文献   

2.
张辉  杨继平  王君平 《推进技术》2001,22(6):526-528
为解决铸铝薄壁件进气机匣的深孔加工,针对麻花钻加工深孔的难点,在加工中心上研究了用枪钻和GT深孔麻花钻高速加工深孔的方案和工艺参数,并探讨了雾化高压气体强制排屑加工深孔的技术,获得了典型薄壁箱体零件的高速钻深孔的经验。  相似文献   

3.
深孔加工在航空制造业中具有广泛需求,是加工难度最大的工序之一。复杂壳体零件是航空发动机的关键部件,其深孔加工质量直接影响航空发动机的服役性能和使用寿命。以航空复杂壳体零件为对象,针对航空复杂壳体零件深孔加工的工艺特点及难点,就目前现有深孔加工方法、深孔钻削力学、深孔钻削切屑形态与排屑方法、深孔加工在线监控及深孔加工设备等方面关键技术进行综述,并探讨了深孔加工未来的发展趋势。  相似文献   

4.
通过分析某铝合金薄壁深孔零件在加工过程中存在的问题基础上,采用了拉镗拉铰加工内孔,再以轴向定位夹紧的方式加工外形的思路,该方法保证了零件加工精度,解决了该铝合金薄壁深孔零件的加工问题,完全满足生产实际需要,质量稳定可靠,可为类似零件加工提供参考。  相似文献   

5.
本文主要阐述深孔加工中断屑问题,从理论上分析出解决断屑问题关键所在,并通过实践设计出“齿轮-连杆式”断屑机构,该机构较好地解决了深孔加工中断屑问题。  相似文献   

6.
当孔深超过10倍孔径时,加工出的孔一般很深。孔深达300倍径时就需要专门的技术,并采用单管钻头或双管钻头进行钻削。在加工至这些孔底部的漫长过程中,需要使用正确的运动机构、刀具配置以及合适的切削刃才能完成内腔、凹槽、螺纹和型腔的加工。支撑板技术是另一重要领域,在深孔钻削中也至关重要,现在它作为深孔加工技术的一部分也发展很快,其中就包括在该领域能实现更高性能的高质刀具的开发。  相似文献   

7.
针对某类复杂壳体深小孔数量多、孔径小、长径比大、精度要求高的特点,在优化设计枪钻切削刃及冷却孔结构的基础上,将枪钻、直槽内冷钻等新型孔加工刀具与加工技术应用到卧式加工中心上,研究开发孔径Φ2~Φ10、长径比20~60深小孔的高效加工方法和加工工艺,优化得到符合要求的最佳切削参数,并建立深小孔高效加工切削参数数据库。实践表明,这一技术将深小孔加工效率提高30%以上,加工质量显著改善,有效解决了深小孔的高效精密加工问题。  相似文献   

8.
本文从刀具的受力分析、刀具材料的选择等实验数据出发,论述了运用外排屑深孔推镗刀加工热轧管料坯深孔、改进其加工工艺的过程。实践结果表明,运用外排屑深孔推镗刀加工热轧管料坯深孔可保证粗糙度3.2↓A,直线度0.0/100mm,提高工效5倍。  相似文献   

9.
空心长轴深孔加工工艺研究   总被引:1,自引:0,他引:1  
以某发动机空心长轴零件深孔加工为研究对象,设计了长径比为15,长度超过1米的整体硬质合金刀杆,在某加工项目试验中,应用这种超长整体硬质合金刀杆,在细长比大于10的空心长轴的深孔镗削加工中,改变了传统的深孔加工工艺,满足了空心长轴深孔加工中严格的壁厚差要求,取得了明显的效果.  相似文献   

10.
通过分析某30CrMnSiNi2A深孔薄壁零件在加工过程中存在的问题基础上,采用了带涂层的深孔加工刀具拉镗拉铰加工内孔后,再进行珩磨,最后以轴向定位夹紧的方式加工外形的思路,该方法保证了零件加工精度,解决了该薄壁深孔零件的加工问题,完全满足生产实际需要.  相似文献   

11.
分别采用机械钻削制孔与激光制孔两种工艺对SiC_f/SiC陶瓷基复合材料进行制孔,对其质量以及工艺特点进行评价分析。结果表明,机械钻削制孔孔径精度较好但存在刀具磨损严重、出现毛刺崩边现象等问题;激光制孔效率较高,但孔存在锥度且因热影响区的存在导致孔的内壁表面出现分层、裂纹等缺陷。  相似文献   

12.
Electrochemical drilling(ECD) provides an alternative technique for drilling multiple small holes in difficult-to-machine materials in numerous industrial applications such as for aeroengines. The value and fluctuation of electrolyte flowrate can seriously affect the machining stability and hole quality in ECD. In particular, when drilling multiple holes, the distribution and fluctuations of the electrolyte flowrate in each channel could influence the uniformity of the electrolyte flowrate among...  相似文献   

13.
李云花  张丽红 《洪都科技》2007,(4):31-36,43
就某轻型公务机上舱门框体零件所采用的高速数控加工工艺、工装的订制、加工刀具、编程、变形控制技术等方面进行研究分析,同时论述了如何解决这类零件加工难点及提高生产效率问题。  相似文献   

14.
MBD模型作为制造过程中唯一依据逐步成为航空制造业的发展趋势,并已应用到CAD/CAM中。但MBD技术尚未在CAPP中展开应用,导致MBD数据集在CAD/CAPP/CAM的集成设计制造过程中无法连续传递。针对航空数控加工需求,建立了基于图层的数控加工MBD工艺模型,提出了基于MBD的数控工艺设计流程,并设计开发了基于MBD的数控加工CAPP系统,实现了UG平台上集成设计制造的MBD应用。  相似文献   

15.
《中国航空学报》2020,33(12):3447-3459
In the machining of complicated surfaces, the cutters with large length/diameter ratios are used widely and the deformation of the machining system is one of the principal error sources. During the process planning stage, the cutting direction angle, the cutter lead and tilt angles are usually optimized to minimize the force induced error. It may lead to a low machining efficiency for bullnose end mills, as the material removal rates are different largely for different machining angles. In this paper, the influence mechanism of the machining angles on the force induced error is studied based on the models of the instantaneous cutting force when the cutter flute traveling through the cutting contact point and the stiffness of the machining system. In order to evaluate the machining angles, the force induced error/efficiency indicator (FEI) is defined as the division of the force induced error and the equal volume sphere of the removed material. FEI is dimensionless, with the lower FEI, the lower force induced error and the higher machining efficiency. For optimal selection of the machining angles, the critical FEI is calculated with the constraint of force induced error and the desired material removal rate, and the critical FEI separate the set of the machining angles into two subsets. After the feed rate scheduling process, the machining angles in the optimal subset would have higher machining accuracy and efficiency, while the machining angles in the other subset have lower machining accuracy and efficiency. Through the machining experiment of five axis machining and freeform surface machining, the effectiveness and superiority of the proposed FEI method is verified with a bullnose end mill, which can improve the machining efficiency with the constraint of force induced error.  相似文献   

16.
《中国航空学报》2016,(2):560-570
Single-crystal superalloys are typical advanced materials used for manufacturing aeroengine turbine blades. Their unique characteristics of high hardness and strength make them exceedingly difficult to machine. However, a key structure of a turbine blade, the film-cooling hole,needs to be machined in a single-crystal superalloy; such machining is challenging, especially considering the increasing levels of machining efficiency and quality demanded by the aeroengine industry. Tube electrode high-speed electrochemical discharge drilling(TSECDD), a hybrid technique of high-speed electrical discharge drilling and electrochemical machining, provides high machining efficiency and accuracy, as well as eliminating the recast layer. In this study, TSECDD is used to machine a film-cooling hole in a nickel-based single-crystal superalloy(DD6). The Taguchi methods of experiment are used to optimise the machining parameters. Experimental results show that TSECDD can effectively drill the film-cooling hole; the optimum parameters that give the best performance are as follows: pulse duration: 12 ls, pulse interval: 30 ls, peak current:6 A, and salt solution conductivity: 3 m S/cm. Finally, a hole is machined by TSECDD, and the results are compared with those obtained by electrical discharge machining. TSECDD is found to be promising for improving the surface quality and eliminating the recast layer.  相似文献   

17.
超精密机械加工技术在微光学元件制造中的应用   总被引:1,自引:0,他引:1  
超精密机械加工技术作为微光学元件的一种制造方法,具有很多其他传统方法所不具有的优点。本文回顾了超精密机械加工技术的发展,展望了其在微光学元件加工中的应用潜力。  相似文献   

18.
通过优化方案自主设计了一套用于深孔加工的刀具方案,用于某发动机主机匣内部关键件凸轮轴的安装孔的加工,为系列化研制该类机型积累了加工经验.  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号