CN207642322U - A kind of micro- texture lathe tool blade of high pressure cooling cutting - Google Patents
A kind of micro- texture lathe tool blade of high pressure cooling cutting Download PDFInfo
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- CN207642322U CN207642322U CN201721556264.0U CN201721556264U CN207642322U CN 207642322 U CN207642322 U CN 207642322U CN 201721556264 U CN201721556264 U CN 201721556264U CN 207642322 U CN207642322 U CN 207642322U
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- 238000005520 cutting process Methods 0.000 title claims abstract description 45
- 238000001816 cooling Methods 0.000 title claims abstract description 15
- 230000001154 acute effect Effects 0.000 claims description 3
- 229910003460 diamond Inorganic materials 0.000 claims 2
- 239000010432 diamond Substances 0.000 claims 2
- 235000003283 Pachira macrocarpa Nutrition 0.000 claims 1
- 241001083492 Trapa Species 0.000 claims 1
- 235000014364 Trapa natans Nutrition 0.000 claims 1
- 235000009165 saligot Nutrition 0.000 claims 1
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 239000000110 cooling liquid Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
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Abstract
一种高压冷却切削微织构车刀刀片,它涉及一种用于高压切削的车刀片。本实用新型是为了解决现有刀片在切削过程中切削力大、切削温度高、刀具磨损破损严重、断屑困难、换刀频繁以及工件已加工表面质量差等问题。本实用新型包括刀片主体,刀体是菱形,刀体上端面为前刀面,前刀面四周设有四条切削刃,相邻两条切削刃交汇处设有圆弧刃,刀体前刀面上设有断屑槽,断屑槽是由直线和锯齿形圆弧构成,在断屑槽内靠近刀尖处设有凹槽,靠近刀尖处设有半球状微织结构,刀体的中心位置有圆孔,刀体前刀面设有凸台,主切削刃、圆弧刃处均设有倒棱。本实用新型主要用于高压冷却切削的车削加工。
The utility model relates to a high-pressure cooling cutting micro-texture turning tool insert, which relates to a turning insert used for high-pressure cutting. The utility model aims to solve the problems of large cutting force, high cutting temperature, serious tool wear and damage, difficult chip breaking, frequent tool changing and poor machined surface quality of the existing blade during the cutting process. The utility model comprises a blade main body, the cutter body is diamond-shaped, the upper end surface of the cutter body is a rake face, four cutting edges are arranged around the rake face, an arc edge is arranged at the intersection of two adjacent cutting edges, and the rake face of the cutter body is There is a chip breaker on the top. The chip breaker is composed of a straight line and a zigzag arc. There is a groove in the chip breaker near the tip of the tool, and a hemispherical micro-weave structure near the tip of the tool. There is a round hole at the position, a boss is provided on the rake face of the cutter body, and chamfers are provided on the main cutting edge and the arc edge. The utility model is mainly used for turning processing of high-pressure cooling cutting.
Description
技术领域technical field
本实用新型涉及一种高压冷却切削微织构车刀刀片。The utility model relates to a high-pressure cooling cutting micro-texture turning tool blade.
背景技术Background technique
高温合金、钛合金等难加工材料具有较高的抗氧化、耐高温、耐腐蚀等性能同时具有良好的疲劳性能、断裂韧性和塑性等独特的综合性能,这些合金广泛应用于航空发动机零部件中。但是这些性能导致在加工过程中切削力大且集中、切削温度高、断屑困难,刀具磨损破损严重,加工零件表面质量差,换刀频繁等问题。高压切削加工技术是一种高效、高精的切削技术,它在加工上述材料过程中可以有效提高工件加工质量、减少刀具磨损、降低生产成本。在此背景下提出的本实用新型对高压冷却切削起到了积极促进作用。Difficult-to-machine materials such as superalloys and titanium alloys have high oxidation resistance, high temperature resistance, corrosion resistance and other unique comprehensive properties such as good fatigue performance, fracture toughness and plasticity. These alloys are widely used in aero-engine parts . However, these properties lead to problems such as large and concentrated cutting force, high cutting temperature, difficult chip breaking, severe tool wear and damage, poor surface quality of machined parts, and frequent tool changes during processing. High-pressure cutting technology is an efficient and high-precision cutting technology, which can effectively improve the processing quality of workpieces, reduce tool wear and reduce production costs in the process of processing the above materials. The utility model proposed under this background plays a positive role in promoting high-pressure cooling cutting.
发明内容Contents of the invention
本实用新型的目的是提供一种高压冷却切削微织构车刀刀片,以解决现存刀片在加工过程中切削温度高、切削力大、断屑困难、零件加工表面质量差等方面的问题。The purpose of the utility model is to provide a high-pressure cooling cutting micro-textured turning tool blade to solve the problems of high cutting temperature, high cutting force, difficult chip breaking, and poor surface quality of parts processed by existing blades during processing.
本实用新型为解决上述技术问题,所采取的技术方案是:一种高压冷却切削微织构车刀刀片,它包括刀片刀体,它的特征为:刀体是菱形,菱形锐角为80°,刀体的中心位置有圆孔,刀体的四个边上设有主切削刃,在夹角为80°的两条切削刃汇交点上设有刀尖圆弧刃,在切削刃口处均存在钝圆,刀体前刀面上设有断屑槽,断屑槽是由直线和锯齿形圆弧构成,断屑槽靠近刀尖处设有凹槽,靠近刀尖处设有半球状微织结构,刀体前刀面设有凸台,主切削刃、圆弧刃处均设有倒棱。In order to solve the above-mentioned technical problems, the utility model adopts the technical scheme as follows: a high-pressure cooling cutting micro-texture turning tool blade, which includes a blade body, and its characteristics are: the body is diamond-shaped, and the acute angle of the rhombus is 80°. There is a circular hole in the center of the cutter body, main cutting edges are provided on the four sides of the cutter body, and a circular arc edge is provided at the intersection point of the two cutting edges with an included angle of 80°. There is a blunt circle, and there is a chip breaker on the rake face of the cutter body. The chip breaker is composed of a straight line and a zigzag arc. Weaving structure, the rake face of the cutter body is provided with a boss, and the main cutting edge and the arc edge are provided with chamfers.
本实用新型具有以下有益效果:在断屑槽靠近刀尖处设有凹槽,在保证刀尖强度的情况下使刀尖区域存留更多的冷却液。靠近刀尖处设有半球状微织结构,这种半球状微织结构可以在有限的空间使刀尖切削区面积变大,增加散热,降低切削温度,同时半球间的间隙可以利用液体间的张力存留更多的冷却液,减小刀屑间的摩擦。断屑槽由直线和锯齿形圆弧构成的槽型,减小了切屑对刀具的磨损,提高切削加工效率和延长了刀具使用寿命。The utility model has the following beneficial effects: the chip breaker is provided with a groove close to the tip of the tool, so that more cooling liquid can be reserved in the tip of the tool under the condition of ensuring the strength of the tip of the tool. There is a hemispherical micro-weave structure near the tip of the knife. This hemispherical micro-weave structure can enlarge the cutting area of the tool tip in a limited space, increase heat dissipation, and reduce the cutting temperature. At the same time, the gap between the hemispheres can be used Tension retains more coolant, reducing friction between chips. The chip breaker is composed of a straight line and a zigzag arc, which reduces the wear of the chip on the tool, improves the cutting efficiency and prolongs the service life of the tool.
附图说明Description of drawings
图1是本实用新型的俯视图;图2实用新型的正视图;图3是实用新型的A-A剖视图;图4是实用新型的B-B剖视图;图5是实用新型的C-C剖视图;图6是图1中H处的局部放大视图;图7是图3中G处的局部放大视图。Fig. 1 is a top view of the utility model; Fig. 2 is a front view of the utility model; Fig. 3 is a sectional view of A-A of the utility model; Fig. 4 is a sectional view of B-B of the utility model; Fig. 5 is a sectional view of C-C of the utility model; Partial enlarged view at H; FIG. 7 is partial enlarged view at G in FIG. 3 .
具体实施方式Detailed ways
具体实施方式一:结合图1说明本实施方式,本实施方式的刀片包括刀体1、刀体为80°菱形,在刀体的中心位置处开有圆孔1-1,刀体1的四个边上设有主切削刃3,在夹角为80°的两条切削刃汇交点上设有刀尖圆弧刃5,刀片的特征为在刀体1的前刀面上设有断屑槽2,断屑槽2的端面是由直线和锯齿形圆弧构成,刀体1的前刀面上设有凸台8,其高于前刀面,低于断屑槽的高度,断屑槽靠近刀尖处设有凹槽7,靠近刀尖处设有半球状微织结构6,主切削刃、圆弧刃处均设有倒棱4。主切削刃3和圆弧刃5的刃口钝圆半径均为40μm。Specific embodiment one: this embodiment is described in conjunction with Fig. 1, the blade of this embodiment comprises cutter body 1, and cutter body is 80 ° rhombus, has circular hole 1-1 at the central position of cutter body, four sides of cutter body 1 There is a main cutting edge 3 on one side, and a knife-tip arc edge 5 is provided at the intersection point of the two cutting edges with an included angle of 80°. Groove 2, the end face of the chip breaker 2 is composed of a straight line and a zigzag arc. The rake face of the cutter body 1 is provided with a boss 8, which is higher than the rake face and lower than the height of the chip breaker. A groove 7 is provided near the tip of the groove, a hemispherical micro-weave structure 6 is provided near the tip of the knife, and chamfers 4 are provided at the main cutting edge and the arc edge. The blunt circle radii of the main cutting edge 3 and the arc edge 5 are both 40 μm.
具体实施方式二:结合图1说明本实施方式,本实施方式的凹槽7为长圆形,长度为0.9mm,宽度为0.3mm,深度为0.1mm,相邻2个凹槽间距为1mm。Specific Embodiment 2: This embodiment is described with reference to FIG. 1 . The groove 7 of this embodiment is oblong, with a length of 0.9 mm, a width of 0.3 mm, and a depth of 0.1 mm. The distance between two adjacent grooves is 1 mm.
具体实施方式三:结合图1说明本实施方式,本实施方式的断屑槽2的槽型宽度沿着主切削刃3的长度方向是变化的,变化范围是0.5-2mm。Specific Embodiment Three: This embodiment is described with reference to FIG. 1 . The groove width of the chip breaker 2 in this embodiment varies along the length direction of the main cutting edge 3 , and the variation range is 0.5-2mm.
具体实施方式四:结合图1说明本实施方式,本实施方式的微织结构6是由24个半球组成的菱形,菱形锐角为80°,半球直径为0.1mm,相邻半球间的间距0.15mm。Specific Embodiment 4: This embodiment is described in conjunction with FIG. 1. The micro-woven structure 6 of this embodiment is a rhombus composed of 24 hemispheres. The acute angle of the rhombus is 80°, the diameter of the hemisphere is 0.1 mm, and the distance between adjacent hemispheres is 0.15 mm. .
具体实施方式五:结合图1说明本实施方式,本实施方式的主切削刃的正前角γ0为18o,后角α为0o,倒棱4的前角γ01为8o,倒棱4的宽度为0.2mm,刀尖圆弧半径为0.6mm。此结构有效的解决了切削过程中切屑难以折断、切削温度高、切削力大,刀具磨损破损严重等问题,改善了工件的已加工表面质量,提高了刀具的使用寿命。其他实施方式与具体实施方式一相同。Embodiment 5: This embodiment is described in conjunction with FIG. 1 . The positive rake angle γ 0 of the main cutting edge in this embodiment is 18 o , the relief angle α is 0 o , the rake angle γ 01 of the chamfer 4 is 8 o , and the chamfer The width of the edge 4 is 0.2mm, and the radius of the arc of the tool tip is 0.6mm. This structure effectively solves the problems of hard chip breaking, high cutting temperature, high cutting force, serious tool wear and damage during the cutting process, improves the machined surface quality of the workpiece, and increases the service life of the tool. Other implementation manners are the same as the specific implementation manner 1.
Claims (8)
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109746470A (en) * | 2019-03-20 | 2019-05-14 | 哈尔滨理工大学 | A grinding-reducing compound insert for turning and milling |
CN110842231A (en) * | 2019-10-15 | 2020-02-28 | 江苏大学 | Lubricated even compound texture cutter |
CN112475340A (en) * | 2020-12-07 | 2021-03-12 | 哈尔滨理工大学 | High-efficient chip breaking antifriction two-sided rhombus lathe tool piece under high pressure cooling |
CN113145878A (en) * | 2021-05-10 | 2021-07-23 | 哈尔滨理工大学 | Novel bias inclined groove microtexture antifriction diamond turning tool blade |
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2017
- 2017-11-21 CN CN201721556264.0U patent/CN207642322U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109746470A (en) * | 2019-03-20 | 2019-05-14 | 哈尔滨理工大学 | A grinding-reducing compound insert for turning and milling |
CN110842231A (en) * | 2019-10-15 | 2020-02-28 | 江苏大学 | Lubricated even compound texture cutter |
CN112475340A (en) * | 2020-12-07 | 2021-03-12 | 哈尔滨理工大学 | High-efficient chip breaking antifriction two-sided rhombus lathe tool piece under high pressure cooling |
CN113145878A (en) * | 2021-05-10 | 2021-07-23 | 哈尔滨理工大学 | Novel bias inclined groove microtexture antifriction diamond turning tool blade |
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