CN202845892U - High-temperature alloy rough machining integrated alloy end mill - Google Patents

High-temperature alloy rough machining integrated alloy end mill Download PDF

Info

Publication number
CN202845892U
CN202845892U CN 201220463410 CN201220463410U CN202845892U CN 202845892 U CN202845892 U CN 202845892U CN 201220463410 CN201220463410 CN 201220463410 CN 201220463410 U CN201220463410 U CN 201220463410U CN 202845892 U CN202845892 U CN 202845892U
Authority
CN
China
Prior art keywords
alloy
end mill
cutting
cutting edge
temperature alloy
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
CN 201220463410
Other languages
Chinese (zh)
Inventor
唐臣升
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.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang Aircraft Industry Group 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 Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN 201220463410 priority Critical patent/CN202845892U/en
Application granted granted Critical
Publication of CN202845892U publication Critical patent/CN202845892U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Milling Processes (AREA)

Abstract

The utility model provides a high-temperature alloy rough machining integrated alloy end mill which comprises a handle part and a blade part, wherein a side blade front angle on the blade part is 5-7 degrees, a helical angle is 34-36 degrees, and the circular arc radius of the cutting edge is 0.02-0.04mm; and preferably, the side blade front angle on the blade part is 6 degrees, the helical angle is 35 degrees, and the circular arc radius of the cutting edge is 0.03mm. According to the alloy rough machining integrated alloy end mill, the cutting removal rate is not less than 7cm<3> per minute, and the one-time cutting machining time is prolonged to 120 minutes. By adopting the structure, the strength of the cutting edge is increased, the cutting resistance is reduced, and the service life of the cutting edge is prolonged; and therefore, the cutting performance of the rough machining ZG35Cr24Ni7SiN high-temperature alloy integrated hard alloy numerical control end mill is improved, the machining removal rate is correspondingly improved, and the service life of the integrated hard alloy numerical control end mill is prolonged.

Description

High temperature alloy roughing Integral alloy slotting cutter
Technical field
The utility model relates to a kind of high temperature alloy roughing Integral alloy slotting cutter, is used for the roughing of ZG35Cr24Ni7SiN high temperature alloy.
Background technology
The ZG35Cr24Ni7SiN high temperature alloy has the advantages such as intensity height, high-temperature behavior be good, thereby, be used in more and more widely in the Aero-Space manufacturing industry.But the ZG35Cr24Ni7SiN high temperature alloy is a kind of material of difficult machining, and its main cause is that yield strength is high, poor thermal conductivity, so the cutting ability of material is poor, and is larger to the wearing and tearing of cutter, so that tool wear is more serious.
Existing roughing ZG35Cr24Ni7SiN high temperature alloy solid carbide numerical control end mill is because main structure parameters side spiral cutting angle of cutting edge and relief angle are larger, it is 8 °~10 ° such as anterior angle numerical value, cutting edge is Passivation Treatment not, rounded cutting edge radius is 0~0.01mm, so that cutting edge strength is relatively poor, the wearing and tearing of cutter have been aggravated; Helical angle is larger, is 38 °~40 ° such as helical angle numerical value, has increased cutting resistance.Finally caused existing processing ZG35Cr24Ni7SiN high temperature alloy solid carbide numerical control end mill, the roughing clearance is low, generally at 2~3cm3/min, cutting at one time is short process time, be generally 35~40min, therefore be difficult to satisfy the roughing requirement of ZG35Cr24Ni7SiN high temperature alloy part.
Summary of the invention,
The purpose of this utility model provides a kind of roughing ZG35Cr24Ni7SiN high temperature alloy solid carbide numerical control end mill that improves cutting ability and working (machining) efficiency.
The technical solution of the utility model: high temperature alloy roughing Integral alloy slotting cutter, comprise shank and blade, the side edge anterior angle on the blade is 5 °~7 °, and helical angle is 34 °~36 °, and rounded cutting edge radius is 0.02mm~0.04mm.
Preferably, the side edge anterior angle on the blade is 6 °, and helical angle is 35 °, and rounded cutting edge radius is 0.03mm.
The cutting clearance of high temperature alloy roughing Integral alloy slotting cutter is not less than 7cm3/min, and disposable machining time lengthening is to 120min.
The beneficial effects of the utility model: because side spiral cutting angle of cutting edge and side spiral cutting sword helical angle are reduced, and rounded cutting edge radius increased, can be so that the intensity increase of cutting edge, cutting resistance reduces, prolonged the cutting edge working durability, therefore improve the cutting ability of roughing ZG35Cr24Ni7SiN high temperature alloy solid carbide numerical control end mill, also improved accordingly the machining clearance, prolonged the service life of solid carbide numerical control end mill; The utility model is 6 ° with the side edge anterior angle that end mill structure is designed on the blade, and helical angle is 35 °, and rounded cutting edge radius is 0.03mm, so that the performance of whole cutter reaches optimization.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the A-A cutaway view of Fig. 1.
Fig. 3 is the local enlarged diagram of Fig. 2.
The specific embodiment
As shown in Figure 1 to Figure 3, this embodiment is that diameter is that 20mm, cutting edge length are the high temperature alloy roughing Integral alloy slotting cutter of 38mm, comprises shank 2 and blade 1, and the side edge anterior angle 4 on the blade 1 is 5 °~7 °, helical angle 3 is 34 °~36 °, and rounded cutting edge radius 5 is 0.02mm~0.04mm.Preferably, the side edge anterior angle 4 on the blade 1 is 6 °, and helical angle 3 is 35 °, and rounded cutting edge radius 5 is 0.03mm.
Adopt the above-mentioned parameter design so that the intensity of cutting edge increases, cutting resistance reduces, prolonged the cutting edge working durability, therefore improved the cutting ability of roughing ZG35Cr24Ni7SiN high temperature alloy solid carbide numerical control end mill, also improved accordingly the machining clearance, prolong the service life of solid carbide numerical control end mill, satisfied the rough machined requirement of the high-quality and efficient milling of ZG35Cr24Ni7SiN high temperature alloy.

Claims (2)

1. high temperature alloy roughing Integral alloy slotting cutter, comprise shank (2) and blade (1), it is characterized in that: the side edge anterior angle (4) on the blade (1) is 5 °~7 °, and helical angle (3) is 34 °~36 °, and rounded cutting edge radius (5) is 0.02mm~0.04mm.
2. high temperature alloy roughing Integral alloy slotting cutter as claimed in claim 1, it is characterized in that: the side edge anterior angle (4) on the blade (1) is 6 °, and helical angle (3) is 35 °, and rounded cutting edge radius (5) is 0.03mm.
CN 201220463410 2012-09-13 2012-09-13 High-temperature alloy rough machining integrated alloy end mill Expired - Fee Related CN202845892U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220463410 CN202845892U (en) 2012-09-13 2012-09-13 High-temperature alloy rough machining integrated alloy end mill

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220463410 CN202845892U (en) 2012-09-13 2012-09-13 High-temperature alloy rough machining integrated alloy end mill

Publications (1)

Publication Number Publication Date
CN202845892U true CN202845892U (en) 2013-04-03

Family

ID=47977128

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220463410 Expired - Fee Related CN202845892U (en) 2012-09-13 2012-09-13 High-temperature alloy rough machining integrated alloy end mill

Country Status (1)

Country Link
CN (1) CN202845892U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104708098A (en) * 2015-02-16 2015-06-17 天津大学 Special cutter for machining small-diameter pore helical milling of composite material
CN105631072A (en) * 2014-11-03 2016-06-01 南京中车浦镇城轨车辆有限责任公司 Design method of tool for rough machining of aluminum alloys
CN112514651A (en) * 2020-08-17 2021-03-19 石河子大学 Spindle with profile modeling structure hook tooth for cotton picker

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105631072A (en) * 2014-11-03 2016-06-01 南京中车浦镇城轨车辆有限责任公司 Design method of tool for rough machining of aluminum alloys
CN105631072B (en) * 2014-11-03 2019-01-15 南京中车浦镇城轨车辆有限责任公司 A kind of aluminium alloy roughing tool design method
CN104708098A (en) * 2015-02-16 2015-06-17 天津大学 Special cutter for machining small-diameter pore helical milling of composite material
CN112514651A (en) * 2020-08-17 2021-03-19 石河子大学 Spindle with profile modeling structure hook tooth for cotton picker
CN112514651B (en) * 2020-08-17 2021-10-08 石河子大学 Spindle with profile modeling structure hook tooth for cotton picker

Similar Documents

Publication Publication Date Title
CN204565247U (en) Runner of blisk efficient Flank machining integral annular milling cutter
CN202845892U (en) High-temperature alloy rough machining integrated alloy end mill
CN102950335A (en) Metal ceramic reamer
CN202845893U (en) High-temperature alloy fine machining integrated alloy end mill
CN202824796U (en) Solid carbide numerical control end mill for TC 4 titanium alloy rough machining
CN206263326U (en) One kind processing high temperature alloy solid carbide end mill
CN202028813U (en) Welding type hard alloy rear wave blade spiral end mill
CN102962520A (en) PCD (Poly Crystal Diamond) spiral reamer
CN203031024U (en) Groove milling tool for welding diamond
CN102328125A (en) End milling cutter
CN204799964U (en) But be used for high temperature alloy semifinishing with novel transposition cell type lathe tool piece
CN205834314U (en) There is the chip-breaking drill bit of S type blade based on Logistic curve
CN204108415U (en) A kind of fluted drill being used for machining titanium alloy
CN202224728U (en) End mill
CN104551169A (en) Novel milling cutter
CN204430304U (en) A kind of digital cuttings
CN204843014U (en) High pressure cooling cutting titanium alloy semifinishing blade that needs car
CN204308275U (en) Helicla flute groove milling cutter
CN102837087A (en) Double-edge internal thread milling cutter
CN209349626U (en) A kind of carbide rotary tool cutter for processing high-speed rail industry titanium alloy
CN208528168U (en) A kind of milling cutter for processing aero titanium alloy
CN203003178U (en) Double-groove-shaped indexable numerical control turning blade for semi-finishing of workpieces
CN201519790U (en) Dual lead end milling cutter
CN202151740U (en) Double-blade internal thread milling cutter
CN204397017U (en) A kind of hard alloy cutter

Legal Events

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

Granted publication date: 20130403

Termination date: 20150913

EXPY Termination of patent right or utility model