CN103157834B - Drill bit with low chisel edge - Google Patents

Drill bit with low chisel edge Download PDF

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CN103157834B
CN103157834B CN201310104178.6A CN201310104178A CN103157834B CN 103157834 B CN103157834 B CN 103157834B CN 201310104178 A CN201310104178 A CN 201310104178A CN 103157834 B CN103157834 B CN 103157834B
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drill bit
knife
chisel edge
main cutting
edge
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CN103157834A (en
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刘伟
王弢
蒋长青
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Suzhou Ahno Precision Cutting Tool Technology Co Ltd
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Suzhou Ahno Precision Cutting Tool Technology Co Ltd
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Abstract

The invention relates to a drill bit with a low chisel edge. The drill bit comprises a handle portion and a head portion, wherein the handle portion is a cylinder, the head portion is a coaxial cylinder which shares the same axis with the handle portion, two chip discharge grooves are formed in the head portion, a solid portion forming the chip discharge grooves is a knife back, intersecting lines of the two chip discharge grooves and the knife back in the axis direction respectively form two main cutting edges, intersecting lines of the two chip discharge grooves and the knife back in the radial direction form seamed edges, the seamed edges and the main cutting edges intersect to form a knife point, the chisel edge with 140-degree convexity is arranged between the two main cutting edges, and a sharp point of the chisel edge is 0.5-1mm lower than the knife point in the axis direction. Due to the chisel edge with the 140-degree convexity, knife strength is guaranteed, and meanwhile prominent centring capacity is guaranteed; the powerful centring capacity can inhibit bouncing and thereby guarantees long service life of a knife; and the drill bit is suitable for drilling machining for carbon fiber composite materials used for aviation.

Description

低横刃钻头Low Chisel Drill

技术领域 technical field

本发明涉及高效高速精密刀具,尤其涉及一种用于航空碳纤维复合材料加工的低横刃钻头,属于光机电一体化加工技术领域。 The invention relates to high-efficiency, high-speed precision cutting tools, in particular to a low chisel drill bit used for processing aviation carbon fiber composite materials, and belongs to the technical field of optical-mechanical-electrical integration processing.

背景技术 Background technique

航空碳纤维复合材料加工仍是航空制造领域中的加工难点,尤其在孔加工中极易出现拱边、材料分层、出口毛刺等制造缺陷,严重时会导致零件报废。目前,由于硬质合金有着均衡的物理性能、较高的韧性和耐磨性,仍是航空碳纤维复合材料加工中的主要刀具材料。但如何通过改进刀具的几何角度,提高钻孔工艺刚性并减少切削阻力,继而避免类似的制造缺陷,是当前急需解决的问题。 The processing of aviation carbon fiber composite materials is still a difficult point in the field of aviation manufacturing. Especially in hole processing, manufacturing defects such as arching, material delamination, and export burrs are prone to occur, which will lead to parts scrapping in severe cases. At present, due to its balanced physical properties, high toughness and wear resistance, cemented carbide is still the main tool material in the processing of aviation carbon fiber composite materials. However, how to increase the rigidity of the drilling process and reduce the cutting resistance by improving the geometric angle of the tool, and then avoid similar manufacturing defects is an urgent problem to be solved at present.

发明内容 Contents of the invention

本发明的目的是克服现有技术存在的不足,提供一种低横刃钻头,旨在解决航空碳纤维复合材料孔加工出现的拱边、材料分层、出口毛刺等制造问题。 The purpose of the present invention is to overcome the deficiencies in the prior art and provide a low chisel drill bit, which aims to solve the manufacturing problems such as arching, material delamination, and exit burrs in the hole machining of aviation carbon fiber composite materials.

本发明的目的通过以下技术方案来实现: The purpose of the present invention is achieved through the following technical solutions:

低横刃钻头,包括柄部和头部,柄部为一圆柱体,头部为一与柄部同轴线的同轴圆柱体,头部上开有两个排屑槽,形成排屑槽的实体部分为刀背,两个排屑槽与刀背在轴线方向上的交线分别形成两个主切削刃,排屑槽与刀背在径向方向上的交线形成棱边,棱边与主切削刃相交形成刀尖;特点是:两个主切削刃之间设置中凸140°的横刃,在轴线方向横刃尖点低于刀尖0.5~1mm。 The low chisel drill bit includes a shank and a head. The shank is a cylinder, and the head is a coaxial cylinder coaxial with the shank. There are two chip removal grooves on the head to form a chip removal groove. The solid part of the tool back is the tool back, the intersection lines of the two chip flutes and the tool back in the axial direction form two main cutting edges respectively, the intersection lines of the chip flutes and the tool back in the radial direction form edges, and the edges and the main cutting The blades intersect to form a tool tip; the feature is: a chisel edge with a convex 140° is set between the two main cutting edges, and the point of the chisel edge is 0.5~1mm lower than the tool tip in the axial direction.

进一步地,上述的低横刃钻头,其中,主切削刃形成的夹角为120°内凹角。 Further, in the above-mentioned low chisel edge drill, the included angle formed by the main cutting edge is a concave angle of 120°.

更进一步地,上述的低横刃钻头,其中,刀尖形成的夹角为60°。 Further, in the low chisel edge drill mentioned above, the included angle formed by the cutting edge is 60°.

更进一步地,上述的低横刃钻头,其中,所述排屑槽中设置有保护刀槽。 Furthermore, in the above-mentioned low chisel edge drill bit, a protective flute is provided in the flute.

再进一步地,上述的低横刃钻头,其中,保护刀槽为负5~10°前角的保护刀槽;保护刀槽的宽度为0.8~1.0mm。 Still further, in the above-mentioned low chisel edge drill bit, the protective sipe is a protective sipe with a rake angle of negative 5-10°; the width of the protective sipe is 0.8-1.0 mm.

本发明技术方案突出的实质性特点和显著的进步主要体现在: The outstanding substantive features and remarkable progress of the technical solution of the present invention are mainly reflected in:

(1)中凸140°的横刃既兼顾刀具强度,又保证了较为突出的定心能力,适合采用风动工具的加工现场;较强的定心能力可抑制跳动,从而保证较长的刀具寿命; (1) The convex 140° chisel edge not only takes into account the strength of the tool, but also ensures a relatively prominent centering ability, which is suitable for the processing site where pneumatic tools are used; the strong centering ability can restrain the beating, thereby ensuring a longer tool life;

(2)钻头主切削刃采用120°内凹角设计,使得轴向力朝轴线,避免了朝向孔壁的轴向力,继而避免工件拱边现象; (2) The main cutting edge of the drill bit is designed with a 120° inner concave angle, so that the axial force is directed towards the axis, avoiding the axial force towards the hole wall, and then avoiding the phenomenon of workpiece arching;

(3)钻头的刀尖设计为60°极为锋利 ,从而可轻快地切削工件,继而减少材料分层与出口毛刺; (3) The tip of the drill bit is designed to be extremely sharp at 60°, so that the workpiece can be cut briskly, thereby reducing material delamination and export burrs;

(4)140°的横刃,在轴线方向低于刀尖0.5~1mm,一方面在切削工程中稳定地定心,另一方面由于增大了实际刃长,提高了钻头的散热能力,延长刀具的整体寿命; (4) The 140° chisel edge is 0.5~1mm lower than the tool tip in the axial direction. On the one hand, it can be stably centered in the cutting process. overall tool life;

(5)在排屑槽中设置有负前角的保护刀槽,使其不参与切削,提高其导向能力;避免在钻削过程中受跳动过大等工艺因素的影响而导致的“扎刀”现象。 (5) A protective sipe with a negative rake angle is set in the chip flute so that it does not participate in the cutting and improves its guiding ability; avoiding the "knife stabbing" caused by the influence of technological factors such as excessive jumping during the drilling process "Phenomenon.

附图说明 Description of drawings

下面结合附图对本发明技术方案作进一步说明: Below in conjunction with accompanying drawing, technical solution of the present invention will be further described:

图1:本发明低横刃钻头的结构示意图; Fig. 1: the structural representation of the low chisel drill bit of the present invention;

图2:主切削刃夹角的示意图; Figure 2: Schematic diagram of the included angle of the main cutting edge;

图3:刀尖夹角的示意图; Figure 3: Schematic diagram of the included angle of the tool tip;

图4:横刃的结构示意图; Figure 4: Schematic diagram of chisel blade structure;

图5:保护刀槽的示意图; Figure 5: Schematic diagram of the protective knife groove;

图6:图5的B-B剖视示意图。 Fig. 6: B-B sectional schematic diagram of Fig. 5 .

具体实施方式 Detailed ways

本发明低横刃钻头的设计思路是提高钻头的锋利度,改变传统钻头横刃先接触工件的加工方式,由传统设计的凸顶角改为120°内凹角,避免入钻时的径向力。在钻头后端采用负前角的保护刀槽,以提高导向的稳定性,减少钻头棱边对工件的二次切削,从而抑制工件产生拱边与毛刺的倾向。 The design concept of the low-chisel drill bit of the present invention is to improve the sharpness of the drill bit, change the traditional processing method in which the chisel edge of the drill bit touches the workpiece first, and change the traditionally designed convex angle into a 120° inner concave angle to avoid radial force when drilling. A protective sipe with a negative rake angle is used at the rear end of the drill to improve the stability of the guide and reduce the secondary cutting of the workpiece by the edge of the drill, thereby inhibiting the tendency of the workpiece to produce arches and burrs.

如图1所示,低横刃钻头,包括柄部1和头部2,柄部1为一圆柱体,头部2为一与柄部同轴线的同轴圆柱体,头部上开有两个排屑槽3,形成排屑槽的实体部分为刀背4,两个排屑槽3与刀背4在轴线方向上的交线形成有两个主切削刃5,排屑槽3与刀背4在径向方向上的交线形成棱边6,棱边6与主切削刃5相交形成刀尖7;两个主切削刃之间设置中凸140°的横刃8,如图4,在轴线方向横刃尖点低于刀尖0.5~1mm,一方面可以在切削工程中稳定地定心,另一方面由于增大了实际刃长,提高了钻头的散热能力,继而显著提高刀具的整体寿命。主切削刃承担主要的钻孔任务,内切削刃相交形成中凸140°的横刃8起到定心作用,减少加工中的径向跳动,棱边6用于导向,同时棱边形成的外圆直径就是钻孔直径。在钻削工程中,刀尖7首先接触工件,并且是工作时间最长、线速度最大的工作位置。 As shown in Figure 1, the low chisel drill bit includes a shank 1 and a head 2, the shank 1 is a cylinder, the head 2 is a coaxial cylinder coaxial with the shank, and the head has a Two chip flutes 3, the solid part forming the chip flute is the back 4, the intersection line of the two chip flutes 3 and the back 4 in the axial direction forms two main cutting edges 5, the chip flute 3 and the back 4 The intersection line in the radial direction forms an edge 6, and the edge 6 intersects with the main cutting edge 5 to form a tool tip 7; a chisel edge 8 with a convex 140° is set between the two main cutting edges, as shown in Figure 4, on the axis The directional chisel edge point is 0.5~1mm lower than the tool tip. On the one hand, it can be stably centered in the cutting process. On the other hand, due to the increase of the actual edge length, the heat dissipation capacity of the drill is improved, and the overall life of the tool is significantly improved. . The main cutting edge undertakes the main drilling task. The inner cutting edges intersect to form a convex 140° chisel edge 8, which plays a centering role and reduces the radial runout during processing. The edge 6 is used for guiding, and the outer edge formed by the edge The circle diameter is the drill diameter. In the drilling process, the tool tip 7 first touches the workpiece, and it is the working position with the longest working time and the highest linear speed.

如图2所示,主切削刃形成的夹角为120°内凹角,使得轴向力朝轴线,避免了朝向孔壁的轴向力,继而可以减少工件拱边现象。 As shown in Figure 2, the included angle formed by the main cutting edge is a concave angle of 120°, so that the axial force is directed toward the axis, avoiding the axial force toward the hole wall, and thus reducing the phenomenon of workpiece arching.

如图3所示,刀尖形成的夹角为60°,刀尖极为锋利 ,从而可轻快地切削工件继而减少材料分层与出口毛刺。 As shown in Figure 3, the angle formed by the tool tip is 60°, and the tool tip is extremely sharp, which can cut the workpiece lightly and reduce material delamination and exit burrs.

如图5所示,排屑槽中设置有保护刀槽9,如图6所示,保护刀槽为负10°前角的保护刀槽;保护刀槽的宽度为0.8~1.0mm。避免钻削过程中受跳动过大等工艺因素的影响而导致的“扎刀”现象,通过在排屑槽中设置负前角的保护刀槽,使其不参与切削,提高其导向能力。 As shown in Fig. 5, a protective sipe 9 is provided in the flute, and as shown in Fig. 6, the protective sipe is a protective sipe with a rake angle of negative 10°; the width of the protective sipe is 0.8~1.0mm. To avoid the phenomenon of "knife sticking" caused by the influence of technological factors such as excessive runout during the drilling process, a protective sipe with a negative rake angle is set in the chip removal flute so that it does not participate in cutting and improves its guiding ability.

低横刃钻头采用整体硬质合金材料,由于其具有较高的硬度和耐磨性,适合航空碳纤维复合材料的加工特点。通常选择ISO K05~K10 牌号,当孔较深或者加工系统刚性较差时可选用ISO K30~K40等韧性好的牌号。 The low chisel drill bit is made of solid carbide material, which is suitable for the processing characteristics of aviation carbon fiber composite materials due to its high hardness and wear resistance. Usually choose ISO K05~K10 grades, when the hole is deep or the rigidity of the processing system is poor, you can choose ISO K30~K40 grades with good toughness.

由于低横刃钻头属于高效高精密金属切削刀具,刀尖及切削刃极为锋利,在普通设备上容易产生微观崩口而影响刀具寿命,必须在五轴CNC工具磨床等高刚性设备上制造,并在200倍放大镜下观察刃口状态。关键控制尺寸通过公差来保证制造精度:主切削刃内凹120°±1.5°;刀尖夹角60±1.5°;横刃中凸140°~137°;横刃低于刀尖0.5~1mm。 Since the low chisel drill bit is a high-efficiency and high-precision metal cutting tool, the tip and cutting edge are extremely sharp, and it is easy to produce microscopic chipping on ordinary equipment and affect the life of the tool. It must be manufactured on high-rigidity equipment such as a five-axis CNC tool grinder. Observe the state of the cutting edge under a magnifying glass of 200 times. The key control dimensions ensure the manufacturing accuracy through tolerances: the main cutting edge is concave at 120°±1.5°; the included angle of the tool tip is 60±1.5°; the chisel edge is convex at 140°-137°;

综上所述,本发明低横刃钻头适用于航空用碳纤维复合材料的钻孔加工,通过几何结构的优化,可以避免拱边、材料分层、出口毛刺等制造缺陷,并且可以通过PVD涂层等多种辅助工艺手段达到较高的刀具耐用度,应用前景看好。 In summary, the low-chisel drill bit of the present invention is suitable for drilling of carbon fiber composite materials for aviation. Through the optimization of the geometric structure, manufacturing defects such as arched edges, material delamination, and exit burrs can be avoided, and PVD coating can be used. And other auxiliary process means to achieve high tool durability, the application prospect is promising.

需要理解到的是:以上所述仅是本发明的优选实施方式,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以作出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。 It should be understood that: the above is only a preferred embodiment of the present invention, for those of ordinary skill in the art, without departing from the principle of the present invention, some improvements and modifications can also be made, these improvements and Retouching should also be regarded as the protection scope of the present invention.

Claims (3)

1. low chisel edge drill bit, comprise shank and head, shank is a cylinder, head is the coaxial clyinder of one and shank coaxial line, head has two chip areas, the entity part forming chip area is the knife back, and two chip areas and the intersection of the knife back on the radial line direction of drill bit form two main cutting edges respectively, chip area and the intersection of the knife back on the axial direction of drill bit form seamed edge, and seamed edge is crossing with main cutting edge forms point of a knife; It is characterized in that: the chisel edge arranging convexity 140 ° between two main cutting edges, at axis direction chisel edge cusp lower than point of a knife 0.5 ~ 1mm, the angle that main cutting edge is formed is re-entrant angle in 120 °, and the angle that point of a knife is formed is 60 °.
2. low chisel edge drill bit according to claim 1, is characterized in that: be provided with protection cutter groove in described chip area.
3. low chisel edge drill bit according to claim 2, is characterized in that: the width of described protection cutter groove is 0.8 ~ 1.0mm.
CN201310104178.6A 2013-03-28 2013-03-28 Drill bit with low chisel edge Active CN103157834B (en)

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JP6395217B2 (en) 2014-12-12 2018-09-26 住友電工焼結合金株式会社 Method for manufacturing sintered parts
CN104999118B (en) * 2015-07-13 2017-05-03 大连理工大学 High-efficiency special drilling head for drilling holes in carbon fiber composite material
CN108608040B (en) * 2018-05-10 2020-04-07 大连理工大学 Vertical-edge double-step micro-tooth cutter for high-quality hole making of composite material and laminated structure of composite material
JP6573245B2 (en) * 2018-08-31 2019-09-11 住友電工焼結合金株式会社 Sintered part manufacturing method and sintered part
CN113909537A (en) * 2021-10-26 2022-01-11 蓝鲸科技(深圳)有限公司 Machining drill bit for carbon fiber reinforced resin matrix composite and aluminum alloy laminated member
CN119456812A (en) * 2024-10-31 2025-02-18 深圳市金洲精工科技股份有限公司 A cutting tool, use method and processing device

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Address after: Suzhou City, Jiangsu province 215021 Industrial Park Kuatang subarea Baoda Road No. 8

Patentee after: Suzhou Ahno Precision Cutting Technology Co., Ltd.

Address before: Suzhou City, Jiangsu province 215021 Park Kuatang subarea Baoda Road No. 8

Patentee before: Suzhou Ahno Cutting Tool Technology Co., Ltd.