CN205183873U - A cutter that is used for layered materials drilling of carbon -fibre composite aluminum alloy to process - Google Patents

A cutter that is used for layered materials drilling of carbon -fibre composite aluminum alloy to process Download PDF

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CN205183873U
CN205183873U CN201520881132.XU CN201520881132U CN205183873U CN 205183873 U CN205183873 U CN 205183873U CN 201520881132 U CN201520881132 U CN 201520881132U CN 205183873 U CN205183873 U CN 205183873U
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drilling
working part
aluminum alloy
carbon fiber
fiber composite
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刘剑鸣
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Abstract

本实用新型公开了一种用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,包括工作部和柄部,工作部包括设置于前端的钻孔工作部,钻孔工作部包括设置于前端的第一钻孔工作部及第二钻孔工作部,第一钻孔工作部的第一钻尖角为118°,第二钻孔工作部的第二钻尖角为15°,所述钻尖角为刀具该部切削刃的旋转锥面的顶角。本实用新型的钻孔加工的刀具既能有效减少碳纤维复合材料层出现材料烧伤、分层、毛刺、撕裂等缺陷,又能保证铝合金材料层良好的孔壁光洁度和孔径精度,是能够更好地适用于碳纤维复合材料-铝合金的叠层材料装配后整体钻孔加工的特种刀具。

The utility model discloses a cutting tool used for drilling of laminated materials of carbon fiber composite aluminum alloy, comprising a working part and a handle part, the working part includes a drilling working part arranged at the front end, and the drilling working part includes The first drilling working part and the second drilling working part of the front end, the first drilling point angle of the first drilling working part is 118 °, and the second drilling point angle of the second drilling working part is 15 °. The drill point angle is the vertex angle of the rotating cone surface of the cutting edge of the tool. The drilling tool of the utility model can not only effectively reduce defects such as material burns, delamination, burrs, and tears in the carbon fiber composite material layer, but also ensure good hole wall smoothness and hole diameter accuracy of the aluminum alloy material layer, which can be more It is a special tool suitable for overall drilling of carbon fiber composite material-aluminum alloy laminated materials after assembly.

Description

用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具Tools for drilling laminates in carbon fiber composite aluminum alloys

技术领域technical field

本实用新型涉及机加工设备,尤其涉及一种钻孔加工刀具。The utility model relates to machining equipment, in particular to a drilling tool.

背景技术Background technique

随着航空航天工业的不断发展,许多产品对材料提出了高强度轻量化的要求。碳纤维复合材料+铝合金的叠层就完全具有质量轻、强度大、耐磨性高、抗疲劳性能好、耐高温好等优点,因此碳纤维复合材料+铝合金的叠层正被广泛应用于航空航天,而航空航天技术中制孔是重要的一环,所以选择合适的刀具和工具才是保证制孔质量最重要的。With the continuous development of the aerospace industry, many products have put forward high-strength and lightweight requirements for materials. The laminate of carbon fiber composite material + aluminum alloy has the advantages of light weight, high strength, high wear resistance, good fatigue resistance, and high temperature resistance. Therefore, the laminate of carbon fiber composite material + aluminum alloy is being widely used in aviation Aerospace, and hole making is an important part of aerospace technology, so choosing the right cutting tools and tools is the most important thing to ensure the quality of hole making.

目前现有工艺是两层材料分开制初孔,然后再把两层材料合并起来,一点一点铰到终孔,工作效率效率低下。由于两层材料所适用的钻孔刀具的参数各不相同,如果使用任何一款对于某层材料适用的刀具统一制孔都会在钻削另一层材料时造成缺陷,刀具寿命短,钻出来的孔质量差。碳纤维复合材料极易出现材料烧伤、分层、毛刺、撕裂等缺陷等,而铝又会出现孔壁光洁度不好,孔径超差等造成产品不合格等,给客户带来较大成本压力;同时刀具上分刀步骤多、刀具磨损快、刀具数量导致成本高。At present, the existing technology is to separate the two layers of materials to make the initial hole, and then combine the two layers of materials, and hinge to the final hole bit by bit, which is inefficient. Since the parameters of the drilling tools applicable to the two layers of material are different, if any tool suitable for a certain layer of material is used to make holes uniformly, it will cause defects when drilling another layer of material, the tool life is short, and the drilled Poor hole quality. Carbon fiber composite materials are prone to defects such as material burns, delamination, burrs, tears, etc., while aluminum will have poor hole wall finish and out-of-tolerance hole diameters, resulting in unqualified products, etc., which will bring greater cost pressure to customers; At the same time, there are many cutting steps on the cutting tool, fast cutting tool wear, and high cost due to the number of cutting tools.

实用新型内容Utility model content

本实用新型所要解决的技术问题是要提供一种能够更好地适用于碳纤维复合材料-铝合金的叠层材料装配后整体钻孔加工的特种刀具,既能有效减少碳纤维复合材料层出现材料烧伤、分层、毛刺、撕裂等缺陷,又能保证铝合金材料层良好的孔壁光洁度和孔径精度。The technical problem to be solved by the utility model is to provide a special cutting tool that is better suitable for the overall drilling of the carbon fiber composite material-aluminum alloy laminated material after assembly, which can effectively reduce the occurrence of material burns on the carbon fiber composite material layer , delamination, burrs, tears and other defects, and can ensure good hole wall finish and hole diameter accuracy of the aluminum alloy material layer.

为解决上述技术问题,本实用新型的技术方案如下:For solving the problems of the technologies described above, the technical scheme of the utility model is as follows:

一种用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,包括工作部和柄部,所述的工作部包括设置于前端的钻孔工作部,所述刀具的材料选择整体硬质合金,所述的钻孔工作部包括设置于前端的第一钻孔工作部及所述第一钻孔工作部后端的第二钻孔工作部,所述的第一钻孔工作部的第一钻尖角为118°,所述的第二钻孔工作部的第二钻尖角为15°,所述钻尖角为刀具该部切削刃的旋转锥面的顶角。A cutting tool for drilling laminated materials of carbon fiber composite aluminum alloy, including a working part and a handle, the working part includes a drilling working part arranged at the front end, and the material of the cutting tool is selected as a whole hard alloy, the drilling working part includes a first drilling working part arranged at the front end and a second drilling working part at the rear end of the first drilling working part, and the first drilling working part of the first drilling working part The drill point angle is 118°, the second drill point angle of the second drilling part is 15°, and the drill point angle is the vertex angle of the rotating cone surface of the cutting edge of the tool.

所述刀具的后角角度最好设为18°。The relief angle of the cutter is preferably set to 18°.

所述的第一钻孔工作部的轴向长度最好为2.0mm。The axial length of the first drilling working portion is preferably 2.0 mm.

所述刀具的螺旋角最好为10°。The helix angle of the cutter is preferably 10°.

本实用新型的刀具首先材料选择整体硬质合金,整体硬质合金有很好的刚性和尺寸精度,确保钻孔的加工质量。在刀具尺寸设计中,很多因素对钻孔质量都有影响,为了减小推进力、避免纤维材料的撕裂现象而减小钻尖角度,但是为了刀具寿命和铝材料的钻孔质量又必需增大钻尖角度,这两者之间是矛盾的,所以选择合适的刀具钻型是非常困难的,因为这两种材料在切削过程中表现出完全不同的特性(铝合金有良好的导热性加工出来的孔一般会因为热膨胀原因孔径变大,排屑和断屑要求是非常高的;而碳纤维复合材料导热性差加工中会出现缩孔现象,排屑不用考虑;同时刀具的耐磨性又是一个问题角度越大耐磨性越好)。复合材料在钻孔加工时通常长切削刃,因为碳纤维应当沿着切削刃发生剪切作用,而长切削刃需通过小钻尖角实现。众所周知,钻尖角在低于90°或高于150°时,是可以帮助降低钻孔出口处的毛刺高度。所以设计双钻尖角,第一钻尖角118°,第二钻尖角15°。此外,复合材料的钻孔加工还应降低轴向力,以避免在退刀是发生加工材料层裂。这个特点可以用非常锋利的切削刃槽型,后角角度设为18°(标准钻头后角一般在8-14°,大后角能够使后刀面上热量降低,减少刀侧面因高温的磨损)。The cutting tool of the utility model is firstly made of integral hard alloy, which has good rigidity and dimensional accuracy, so as to ensure the processing quality of drilling. In the design of tool size, many factors have an impact on the drilling quality. In order to reduce the propulsion force and avoid the tearing of fiber materials, the drill point angle must be reduced, but for the tool life and the drilling quality of aluminum materials must be increased. Large drill point angle, there is a contradiction between the two, so it is very difficult to choose a suitable tool drill type, because the two materials show completely different characteristics in the cutting process (aluminum alloy has good thermal conductivity for machining The holes that come out will generally become larger due to thermal expansion, and the requirements for chip removal and chip breaking are very high; while carbon fiber composite materials have poor thermal conductivity, shrinkage cavities will appear during processing, and chip removal does not need to be considered; at the same time, the wear resistance of the tool is also very important. A larger angle of question the better the wear resistance). Composite materials are usually drilled with long cutting edges because the carbon fiber should be sheared along the cutting edge, and the long cutting edge needs to be achieved with a small drill point angle. It is well known that point angles lower than 90° or higher than 150° can help reduce the burr height at the exit of the drilled hole. Therefore, double drill tip angles are designed, the first drill tip angle is 118°, and the second drill tip angle is 15°. In addition, the drilling of composite materials should also reduce the axial force to avoid lamination of the processed material during tool retraction. This feature can be used with a very sharp cutting edge geometry, and the relief angle is set to 18° (the standard drill relief angle is generally 8-14°, and the large relief angle can reduce the heat on the flank surface and reduce the wear of the flank due to high temperature ).

后角角度为18°、螺旋角约为10°、第一钻孔工作部的轴向长度为2.0mm时刀具的综合切削性能和加工质量都是最好的。When the relief angle is 18°, the helix angle is about 10°, and the axial length of the first drilling working part is 2.0mm, the overall cutting performance and processing quality of the tool are the best.

附图说明Description of drawings

为了更清楚地说明本实用新型实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本实用新型的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description These are only some embodiments of the utility model, and those skilled in the art can also obtain other drawings based on these drawings without creative work.

图1是本实用新型用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具的结构示意图。Fig. 1 is a structural schematic diagram of a cutting tool of the utility model for drilling of laminated materials of carbon fiber composite aluminum alloy.

图中:In the picture:

工作部1柄部2钻孔工作部101Working part 1 Shank part 2 Drilling working part 101

第一钻孔工作部1011第二钻孔工作部1012The first drilling working part 1011 and the second drilling working part 1012

第一钻尖角α第二钻尖角βFirst drill point angle α Second drill point angle β

具体实施方式detailed description

下面将结合本实用新型实施例中的附图,对本实用新型实施例中的技术方案进行清楚、完整地描述。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention.

图1示出了一种用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,包括工作部1和柄部2,所述的工作部1包括设置于前端的钻孔工作部101,所述刀具的材料选择整体硬质合金,所述的钻孔工作部101包括设置于前端的第一钻孔工作部1011及所述第一钻孔工作部后端的第二钻孔工作部1012,所述的第一钻孔工作部1011的第一钻尖角α为118°,所述的第一钻孔工作部的轴向长度为2mm(当然出于加工孔径的差异该轴向长度也可以做适应性调整);所述的第二钻孔工作部1012的第二钻尖角β为15°,所述钻尖角为刀具该部切削刃的旋转锥面的顶角。Fig. 1 shows a kind of cutter for the laminated material drilling processing of carbon fiber composite material aluminum alloy, comprises working part 1 and handle part 2, and described working part 1 comprises the drilling working part 101 that is arranged on the front end, The material of the cutter is solid carbide, and the drilling working part 101 includes a first drilling working part 1011 arranged at the front end and a second drilling working part 1012 at the rear end of the first drilling working part, The first drill point angle α of the first drilling working part 1011 is 118 °, and the axial length of the first drilling working part is 2 mm (of course, the axial length can also be Adaptive adjustment); the second drill point angle β of the second drilling working part 1012 is 15°, and the drill point angle is the apex angle of the rotating cone surface of the cutting edge of the tool.

所述刀具的后角角度设为18°,所述的后角角度是指刀具后刀面与垂直平面的夹角。所述刀具的螺旋角为10°,所述的螺旋角又叫排屑槽螺旋角,是刀具圆柱螺旋线的切线与通过切点的圆柱面之间所夹的锐角。The relief angle of the tool is set to 18°, and the relief angle refers to the angle between the flank of the tool and the vertical plane. The helix angle of the tool is 10°, and the helix angle is also called the chip flute helix angle, which is the acute angle between the tangent of the tool cylindrical helix and the cylindrical surface passing the tangent point.

以上所述,仅为本实用新型的具体实施方式,但本实用新型的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本实用新型揭露的技术范围内,可轻易想到变化或替换,都应涵盖在本实用新型的保护范围之内。因此,本实用新型的保护范围应所述以权利要求的保护范围为准。The above is only a specific embodiment of the present utility model, but the scope of protection of the present utility model is not limited thereto. Anyone familiar with the technical field can easily think of changes or changes within the technical scope disclosed by the utility model Replacement should be covered within the protection scope of the present utility model. Therefore, the protection scope of the present utility model should be based on the protection scope of the claims.

Claims (5)

1.一种用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,包括工作部和柄部,所述的工作部包括设置于前端的钻孔工作部,其特征在于:所述刀具的材料选择整体硬质合金,所述的钻孔工作部包括设置于前端的第一钻孔工作部及所述第一钻孔工作部后端的第二钻孔工作部,所述的第一钻孔工作部的第一钻尖角为118°,所述的第二钻孔工作部的第二钻尖角为15°,所述钻尖角为刀具该部切削刃的旋转锥面的顶角。1. A cutting tool for drilling of laminated materials of carbon fiber composite aluminum alloy, comprising a working part and a handle, and the working part includes a drilling working part arranged at the front end, characterized in that: the cutting tool The material selection solid carbide, the drilling working part includes the first drilling working part arranged at the front end and the second drilling working part at the rear end of the first drilling working part, the first drilling working part The first drill point angle of the hole working part is 118°, the second drill point angle of the second drilling part is 15°, and the drill point angle is the apex angle of the rotating cone surface of the cutting edge of the tool . 2.如权利要求1所述的用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,其特征在于:所述刀具的后角角度设为18°。2 . The cutting tool for drilling carbon fiber composite aluminum alloy laminated materials according to claim 1 , wherein the relief angle of the cutting tool is set to 18°. 3 . 3.如权利要求1或2所述的用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,其特征在于:所述的第一钻孔工作部的轴向长度为2.0mm。3. The cutting tool for drilling carbon fiber composite aluminum alloy laminated materials according to claim 1 or 2, characterized in that: the axial length of the first drilling working part is 2.0mm. 4.如权利要求1或2所述的用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,其特征在于:所述刀具的螺旋角为10°。4. The cutting tool for drilling carbon fiber composite aluminum alloy laminated materials according to claim 1 or 2, characterized in that: the helix angle of the cutting tool is 10°. 5.如权利要求3所述的用于碳纤维复合材料铝合金的叠层材料钻孔加工的刀具,其特征在于:所述刀具的螺旋角为10°。5. The cutting tool for drilling carbon fiber composite aluminum alloy laminated materials according to claim 3, characterized in that: the helix angle of the cutting tool is 10°.
CN201520881132.XU 2015-11-06 2015-11-06 A cutter that is used for layered materials drilling of carbon -fibre composite aluminum alloy to process Expired - Fee Related CN205183873U (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106647632A (en) * 2016-12-27 2017-05-10 沈阳航空航天大学 CFRP and titanium alloy laminated structure reamer service life prediction method
US11278970B2 (en) 2018-10-09 2022-03-22 Milwaukee Electric Tool Corporation Drill bit
US11407039B2 (en) 2018-01-29 2022-08-09 Milwaukee Electric Tool Corporation Drill bit

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106647632A (en) * 2016-12-27 2017-05-10 沈阳航空航天大学 CFRP and titanium alloy laminated structure reamer service life prediction method
CN106647632B (en) * 2016-12-27 2018-10-19 沈阳航空航天大学 The prediction technique of CFRP and titanium alloy laminated construction reaming knife service life
US11407039B2 (en) 2018-01-29 2022-08-09 Milwaukee Electric Tool Corporation Drill bit
US11278970B2 (en) 2018-10-09 2022-03-22 Milwaukee Electric Tool Corporation Drill bit

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Granted publication date: 20160427