CN201493529U - Radial Offset Mechanism of Helical Milling Device - Google Patents
Radial Offset Mechanism of Helical Milling Device Download PDFInfo
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- CN201493529U CN201493529U CN2009200963668U CN200920096366U CN201493529U CN 201493529 U CN201493529 U CN 201493529U CN 2009200963668 U CN2009200963668 U CN 2009200963668U CN 200920096366 U CN200920096366 U CN 200920096366U CN 201493529 U CN201493529 U CN 201493529U
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- sleeve
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- 238000003801 milling Methods 0.000 title claims abstract description 10
- 238000005516 engineering process Methods 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 10
- 238000005520 cutting process Methods 0.000 description 7
- 238000005553 drilling Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 229910001069 Ti alloy Inorganic materials 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
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Abstract
本实用新型公开了螺旋铣孔装置的径向偏移机构,它包括内外轮廓都为圆的外套筒、套在所述的外套筒内的内轮廓为圆、外轮廓为椭圆的内套筒,所述的内套筒上设置有蜗轮,在所述的内外套筒之间设置有其一端安装在外套筒上的调节丝杠,所述的调节丝杠与所述的蜗轮彼此之间相啮合配合,在所述的外套筒上设置有锁紧螺丝,所述的锁紧螺丝的一端能够压紧在所述的内套筒的端面上。本装置巧妙的利用了内、外套筒的内外轮廓的特点,通过调整内、外套筒之间的相对转动,从而调整径向偏移量,该机构不仅保证了加工的精度,而且大大节约了空间。
The utility model discloses a radial offset mechanism of a helical milling hole device, which comprises an outer sleeve with circular inner and outer contours, an inner sleeve with a circular inner contour and an elliptical outer contour sheathed in the outer sleeve. Sleeve, the inner sleeve is provided with a worm gear, and an adjusting lead screw whose one end is installed on the outer sleeve is arranged between the inner and outer sleeves, and the adjustment lead screw and the worm wheel are connected to each other Engaged with each other, a locking screw is provided on the outer sleeve, and one end of the locking screw can be pressed against the end surface of the inner sleeve. This device cleverly utilizes the characteristics of the inner and outer contours of the inner and outer sleeves, and adjusts the radial offset by adjusting the relative rotation between the inner and outer sleeves. This mechanism not only ensures the processing accuracy, but also greatly saves space.
Description
技术领域technical field
本实用新型涉及一种螺旋铣孔装置,特别是涉及一种螺旋铣孔装置的径向偏移机构。The utility model relates to a helical hole milling device, in particular to a radial offset mechanism of the helical hole milling device.
背景技术Background technique
现在我国正处于制造技术快速发展的时期,切削加工作为制造技术的主要基础工艺,随着制造技术的发展,取得了很大进步,进入了以发展高速切削、开发新的切削工艺和加工方法、提供成套技术为特征的发展新阶段。航空航天是制造业最为重要的组成部分之一,是高新技术最为富集的产业。在航空制造中,大量零部件都需要进行装配,需要加工成千上万的孔,对此类航空装配孔要实现高效、高精度、高质量加工,需要一种新型技术来代替传统钻孔技术。Now our country is in a period of rapid development of manufacturing technology. As the main basic technology of manufacturing technology, cutting processing has made great progress with the development of manufacturing technology. It has entered the stage of developing high-speed cutting, developing new cutting technology and processing methods, A new stage of development characterized by the provision of a complete set of technologies. Aerospace is one of the most important components of the manufacturing industry and the industry with the most high-tech enrichment. In aviation manufacturing, a large number of parts need to be assembled, and thousands of holes need to be processed. To achieve efficient, high-precision, and high-quality processing of such aviation assembly holes, a new technology is needed to replace the traditional drilling technology. .
航空制造装备设计、制造技术和高强度复合材料制造加工,铝钛合金广泛被应用在航空领域中,在航空装配中需要大量的铆接。因此在制造工程中,会有大量的不同规格的孔需要加工。孔的直径一般为6~15mm,在传统的钻孔过程中,主轴中心的线速度为零,即其钻头的中心不参与切削,而这一中心区域工件材料的去除完全是依靠钻机向下的推力将其挤出的,因而钻孔加工时的钻头所承受的Z向力非常大,在加工钛合金等高硬度材料时,刀具的快速磨损失效是很普遍的现象。另外,传统钻孔加工过程是一个连续的切削过程,刀刃与工件始终接触,切削时刀刃与工件接触面温度很高,钛合金的导热性又比较差,切削过程导致温度的累积,这也将加速刀具的磨损失效导致加工表面质量下降。目前已有的航天加工制造装配中,钻孔工艺一般都是先预钻孔,进行粗加工,而后再进行精加工,去除毛刺和提高孔的加工质量的工艺。由于航空工件的尺寸一般都比较大,这就要求该加工需要的机床的加工范围必须很大。因为螺旋铣是针对航空加工而新型的机械加工工艺,所以此种完成径向偏移的机构目前还没有。Aviation manufacturing equipment design, manufacturing technology and high-strength composite material manufacturing and processing, aluminum-titanium alloys are widely used in the aviation field, and a large number of riveting is required in aviation assembly. Therefore, in the manufacturing process, there will be a large number of holes with different specifications to be processed. The diameter of the hole is generally 6-15mm. In the traditional drilling process, the linear speed of the spindle center is zero, that is, the center of the drill bit does not participate in cutting, and the removal of workpiece material in this central area depends entirely on the downward movement of the drill. It is extruded by the thrust, so the Z-direction force that the drill bit bears during drilling is very large. When processing high-hardness materials such as titanium alloys, rapid wear and failure of the tool is a common phenomenon. In addition, the traditional drilling process is a continuous cutting process, the blade is always in contact with the workpiece, the temperature of the contact surface between the blade and the workpiece is very high during cutting, and the thermal conductivity of titanium alloy is relatively poor. The cutting process leads to the accumulation of temperature, which will also Accelerated tool wear failure leads to a decrease in the quality of the machined surface. In the existing aerospace processing and manufacturing assembly, the drilling process is generally a process of pre-drilling, roughing, and then finishing, removing burrs and improving the processing quality of the holes. Since the size of aerospace workpieces is generally relatively large, this requires that the processing range of the machine tools required for this processing must be large. Because helical milling is a new type of mechanical processing technology for aerospace processing, there is no such mechanism for radial offset.
发明内容Contents of the invention
本实用新型的目的在于克服已有技术的缺点,提供一种能够保证加工精度、节约空间的螺旋铣孔装置的径向偏移机构。The purpose of the utility model is to overcome the shortcomings of the prior art, and provide a radial offset mechanism of a helical milling device capable of ensuring machining accuracy and saving space.
本实用新型的螺旋铣孔装置的径向偏移机构,它包括内外轮廓都为圆的外套筒、套在所述的外套筒内的内轮廓为圆、外轮廓为椭圆的内套筒,所述的内套筒上设置有蜗轮,在所述的内外套筒之间设置有其一端安装在外套筒上的调节丝杠,所述的调节丝杠与所述的蜗轮彼此之间相啮合配合,在所述的外套筒上设置有锁紧螺丝,所述的锁紧螺丝的一端能够压紧在所述的内套筒的端面上。The radial offset mechanism of the spiral milling device of the present utility model comprises an outer sleeve whose inner and outer contours are both circular, and an inner sleeve whose inner contour is round and whose outer contour is elliptical, which is sleeved in the outer sleeve. , the inner sleeve is provided with a worm gear, and an adjusting lead screw whose one end is installed on the outer sleeve is arranged between the inner and outer sleeves, and the adjustment lead screw and the worm gear are connected to each other. Engagement fit, a locking screw is arranged on the outer sleeve, and one end of the locking screw can be pressed against the end surface of the inner sleeve.
本实用新型装置优点:针对航空领域的铆接孔的尺寸6~15mm,这样最大的径向偏移距离为4mm,一般机构无法满足保证加工精度,而该机构巧妙的利用了内、外套筒的内外轮廓的特点,通过调整内、外套筒之间的相对转动,从而调整径向偏移量,该机构不仅保证了加工的精度,而且大大节约了空间。The advantages of the utility model device: the size of the riveting hole in the aviation field is 6-15mm, so the maximum radial offset distance is 4mm, and the general mechanism cannot meet the guarantee of processing accuracy, but this mechanism cleverly uses the inner and outer sleeves. The characteristics of the inner and outer contours, by adjusting the relative rotation between the inner and outer sleeves, thereby adjusting the radial offset, this mechanism not only ensures the machining accuracy, but also greatly saves space.
附图说明Description of drawings
图1是本实用新型的螺旋铣孔装置的径向偏移机构结构示意图;Fig. 1 is a structural schematic diagram of the radial offset mechanism of the helical milling device of the present invention;
图2是图1所示装置的内、外套筒之间的锁紧结构示意图。Fig. 2 is a schematic diagram of the locking structure between the inner and outer sleeves of the device shown in Fig. 1 .
具体实施方式Detailed ways
下面结合附图和具体实施例对本实用新型作以详细描述。Below in conjunction with accompanying drawing and specific embodiment the utility model is described in detail.
如附图所示的本实用新型螺旋铣孔装置的径向偏移机构包括内外轮廓都为圆的外套筒7、套在所述的外套筒7内的内轮廓为圆、外轮廓为椭圆的内套筒6,所述的内套筒上设置有蜗轮8,在所述的内外套筒6、7之间设置有其一端安装在外套筒上的调节丝杠5,所述的调节丝杠5与所述的蜗轮8彼此之间相啮合配合,在所述的外套筒上设置有锁紧螺丝4,所述的锁紧螺丝4的一端能够压紧在所述的内套筒6的端面上。As shown in the accompanying drawings, the radial offset mechanism of the utility model helical milling device includes an
工作原理如下:当该系统工作时,外套筒和内套筒同时围绕着中心转动,两者之间通过锁紧螺丝被缩紧,两者之间没有相对转动。这样刀具的偏心距没有变化,这把刀具能加工比刀具直径大的同等尺寸的孔。当所要加工的孔的尺寸变化时,就需要调整刀具中心线的偏离机架中心线的距离。径向偏移距离的调整是通过内套筒和外套筒的相对转动来实现的。外套筒的外部轮廓是一个圆,内部轮廓也是一个圆,但是内套筒的外部轮廓一个椭圆,内部是一个圆,并与轴承相配合。内套筒和外套筒的转动是通过调整内外套筒之间的丝杠来实现的,内外套筒的配合是通过锁紧螺钉实现的。具体的原理如图1所示,图1中的d指径向偏移距离,加工孔9的半径为刀具半径与d之和。当内套筒6相对于外套筒7转动时,d就会变化,从而改变了所能加工孔的直径,达到了径向调整的目的。The working principle is as follows: when the system is working, the outer sleeve and the inner sleeve rotate around the center at the same time, and the two are tightened by locking screws, and there is no relative rotation between the two. In this way, the eccentricity of the tool does not change, and this tool can process holes of the same size that are larger than the tool diameter. When the size of the hole to be processed changes, it is necessary to adjust the distance from the tool centerline to the frame centerline. The adjustment of the radial offset distance is realized by the relative rotation of the inner sleeve and the outer sleeve. The external contour of the outer sleeve is a circle, and the internal contour is also a circle, but the external contour of the inner sleeve is an ellipse, and the interior is a circle, and is matched with the bearing. The rotation of the inner sleeve and the outer sleeve is realized by adjusting the lead screw between the inner and outer sleeves, and the cooperation of the inner and outer sleeves is realized by locking screws. The specific principle is shown in Figure 1, where d in Figure 1 refers to the radial offset distance, and the radius of the
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| Application Number | Priority Date | Filing Date | Title |
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| CN2009200963668U CN201493529U (en) | 2009-04-17 | 2009-04-17 | Radial Offset Mechanism of Helical Milling Device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN2009200963668U CN201493529U (en) | 2009-04-17 | 2009-04-17 | Radial Offset Mechanism of Helical Milling Device |
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| CN201493529U true CN201493529U (en) | 2010-06-02 |
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| CN2009200963668U Expired - Fee Related CN201493529U (en) | 2009-04-17 | 2009-04-17 | Radial Offset Mechanism of Helical Milling Device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102689040A (en) * | 2012-05-15 | 2012-09-26 | 上海飞机制造有限公司 | Hole helical milling device |
| CN103128354A (en) * | 2013-01-31 | 2013-06-05 | 南京航空航天大学 | Eccentricity adjustment mechanism and handheld helical hole milling device thereof and helical hole milling method |
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2009
- 2009-04-17 CN CN2009200963668U patent/CN201493529U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102689040A (en) * | 2012-05-15 | 2012-09-26 | 上海飞机制造有限公司 | Hole helical milling device |
| CN102689040B (en) * | 2012-05-15 | 2015-02-11 | 上海飞机制造有限公司 | Hole helical milling device |
| CN103128354A (en) * | 2013-01-31 | 2013-06-05 | 南京航空航天大学 | Eccentricity adjustment mechanism and handheld helical hole milling device thereof and helical hole milling method |
| CN103128354B (en) * | 2013-01-31 | 2015-03-11 | 南京航空航天大学 | Hand-held helical milling device and helical milling method using eccentric adjustment mechanism |
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Granted publication date: 20100602 Termination date: 20140417 |
