CN201632674U - Boring blade for processing camshaft hole - Google Patents

Boring blade for processing camshaft hole Download PDF

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Publication number
CN201632674U
CN201632674U CN2010200411063U CN201020041106U CN201632674U CN 201632674 U CN201632674 U CN 201632674U CN 2010200411063 U CN2010200411063 U CN 2010200411063U CN 201020041106 U CN201020041106 U CN 201020041106U CN 201632674 U CN201632674 U CN 201632674U
Authority
CN
China
Prior art keywords
boring cutter
boring blade
sections
utility
cutter sheet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN2010200411063U
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Chinese (zh)
Inventor
汪建海
刘俊江
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhengzhou Diamond Precision Manufacturing Co Ltd
Original Assignee
Zhengzhou Diamond Precision Manufacturing Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhengzhou Diamond Precision Manufacturing Co Ltd filed Critical Zhengzhou Diamond Precision Manufacturing Co Ltd
Priority to CN2010200411063U priority Critical patent/CN201632674U/en
Application granted granted Critical
Publication of CN201632674U publication Critical patent/CN201632674U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a boring blade for processing a camshaft hole. The section of a boring blade is trapezoidal; a cutting part is inlaid and welded on the upper side surface of the edge position at one end of the boring blade; one side of a knife point of the cutting part is provided with two sections of amelioration blades; and amelioration angles alpha and beta of the two sections of amelioration blades are respectively equal to 10-15 degrees and 70-80 degrees. The utility model has simple structure and practical function, is difficult to scratch a workpiece and improves the quality of products.

Description

A kind of boring cutter sheet of machining cam axis hole
Technical field
The utility model relates to the Machining Technology field, particularly a kind of boring cutter sheet of machining cam axis hole.
Background technology
Be used for the boring cutter that the machining cam axis hole is used, the boring cutter sheet that adopts is that the cross section is trapezoidal blade at present, the top of boring cutter sheet is provided with the two holddown grooves that are used for fixing, pass through solder flux welding-on cutting tip on the upper side of one end edges and corners of boring cutter sheet, cutting tip mainly is the composite sheet of polycrystalline diamond (or polycrystalline cubic boron nitride), its composite sheet is that polycrystalline diamond layer (or polycrystalline cubic boron nitride layer) and hard alloy layer form through the HTHP compacting, because side, cutting tip top is the right angle face, adding the man-hour impulsive force concentrates and bigger, scratch workpiece easily, the workpiece accuracy of processing is not high, influences the product quality of workpiece.
The utility model content
The utility model purpose is to provide a kind of boring cutter sheet of machining cam axis hole, can improve the precision of processing work, thereby improves the product quality of workpiece.
To achieve these goals, the utility model adopts following technical scheme: a kind of boring cutter sheet of machining cam axis hole, boring cutter sheet cross section is trapezoidal, welding-on cutting tip on the upper side of end edges and corners of boring cutter sheet, and cutting tip point of a knife one side is provided with two sections wiper edges that are connected mutually.
The smoothing angle of described two sections wiper edges is respectively α=10 °~15 ° and β=70 °~80 °.
The utility model is simple in structure, function is practical, is not easy to scratch workpiece, has improved the quality of product.Cutting tip has characteristics such as hardness height, compression strength height, thermal conductivity and wearability are good, but high-speed cutting obtains very high manufacturing accuracy working (machining) efficiency.Two sections wiper edges have effectively improved the precision of workpiece to be machined.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is a vertical view of the present utility model;
Fig. 3 is a left view of the present utility model.
The specific embodiment
Embodiment: as Fig. 1, Fig. 2, shown in Figure 3, a kind of boring cutter sheet of machining cam axis hole, boring cutter sheet cross section is trapezoidal, welding-on cutting tip 1 on the upper side of end edges and corners of boring cutter sheet, cutting tip 1 point of a knife one side is provided with two sections wiper edges that are connected mutually.The smoothing angle of two sections wiper edges is respectively α=10 °~15 ° and β=70 °~80 °.
Cutting tip mainly is the composite sheet of polycrystalline diamond (or polycrystalline cubic boron nitride), its composite sheet is that polycrystalline diamond layer (or polycrystalline cubic boron nitride layer) and hard alloy layer form through the HTHP compacting, PCD (polycrystalline diamond) material mainly contains following characteristics: 1. PCD hardness can reach 8000HV, is 80~120 times of carbide alloy; 2. the PCD thermal conductivity factor is 700W/mK, be 1.5~9 times of carbide alloy, even be higher than PCBN, copper, so the transmission of PCD cutter heat is rapid; 3. the PCD coefficient of friction generally only is 0.1~0.3 (the carbide alloy coefficient of friction is 0.4~1), so the PCD cutter can significantly reduce cutting force; 4. the PCD thermal coefficient of expansion only is 0.9 * 10-6~1.18 * 10-6, only is equivalent to carbide alloy 1/5, so the thermal deformation of PCD cutter is little, the machining accuracy height; 5. affinity is very little between PCD cutter and non-ferrous metal, nonmetallic materials, and the process smear metal is difficult for bonding and forms built-up edge.

Claims (2)

1. the boring cutter sheet of a machining cam axis hole, it is characterized in that: boring cutter sheet cross section is trapezoidal, welding-on cutting tip on the upper side of end edges and corners of boring cutter sheet, cutting tip point of a knife one side is provided with two sections wiper edges that are connected mutually.
2. the boring cutter sheet of machining cam axis hole according to claim 1 is characterized in that: the smoothing angle of described two sections wiper edges is respectively α=10 °~15 ° and β=70 °~80 °.
CN2010200411063U 2010-01-11 2010-01-11 Boring blade for processing camshaft hole Expired - Fee Related CN201632674U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010200411063U CN201632674U (en) 2010-01-11 2010-01-11 Boring blade for processing camshaft hole

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010200411063U CN201632674U (en) 2010-01-11 2010-01-11 Boring blade for processing camshaft hole

Publications (1)

Publication Number Publication Date
CN201632674U true CN201632674U (en) 2010-11-17

Family

ID=43077150

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010200411063U Expired - Fee Related CN201632674U (en) 2010-01-11 2010-01-11 Boring blade for processing camshaft hole

Country Status (1)

Country Link
CN (1) CN201632674U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103286337A (en) * 2012-02-29 2013-09-11 沈阳黎明航空发动机(集团)有限责任公司 Method for processing stepped hole in precise molded surface of titanium alloy casing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103286337A (en) * 2012-02-29 2013-09-11 沈阳黎明航空发动机(集团)有限责任公司 Method for processing stepped hole in precise molded surface of titanium alloy casing

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101117

Termination date: 20140111