CN206263329U - A kind of multiple-cutting-edge postwave blade milling cutter - Google Patents
A kind of multiple-cutting-edge postwave blade milling cutter Download PDFInfo
- Publication number
- CN206263329U CN206263329U CN201621306023.6U CN201621306023U CN206263329U CN 206263329 U CN206263329 U CN 206263329U CN 201621306023 U CN201621306023 U CN 201621306023U CN 206263329 U CN206263329 U CN 206263329U
- Authority
- CN
- China
- Prior art keywords
- blade
- cutting
- edge
- milling cutter
- postwave
- 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
Links
Landscapes
- Milling Processes (AREA)
Abstract
The utility model is related to aero-engine tool technical field, and in particular to a kind of multiple-cutting-edge postwave blade milling cutter.Including handle of a knife, spiral chip flute and rear knife face below handle of a knife have the rear wave-blade spiral cutting sword of waveform concaveconvex structure.The multiple-cutting-edge rear wave-blade milling cutter has 5~7 rear wave-blade spiral cutting swords, and every rear wave-blade spiral cutting sword surface attachment has nitrogen chromaking aluminized coating, and rear wave-blade spiral cutting sword is by rounding Passivation Treatment;The crest radius value of the waveform concaveconvex structure of rear wave-blade spiral cutting sword is 2~3 times of trough radius value.The milling cutter is applied to the roughing of aero-engine, have the advantages that it is wear-resistant, be difficult to collapse it is scarce.
Description
Technical field
The utility model is related to aero-engine tool technical field, and in particular to a kind of multiple-cutting-edge rear wave-blade milling
Knife.
Background technology
With the high speed development of domestic air mail enterprise, increasing sophisticated equipment comes into aviation large and medium-sized enterprise.With this
Meanwhile, aeronautical material is also continued to develop, continuous with high intensity, high tenacity, the titanium alloy of corrosion resistance and high-temperature nickel-base alloy
Use the performance in aero-engine, having greatly reinforced aero-engine.But, the manufacture difficulty brought therewith is also abnormal
Substantially, the machinability of these new materials is poor, only the 0.28 of 45# steel, and tool wear situation is extremely in process
Seriously.Titaniferous coated cutting tool conventional at present, because the two contains titanium elements during machining titanium alloy, therefore meeting in processing
Compatibility is produced, causes tool wear serious.In the present case, a domestic cutter can only often process an aeroplane engine
Machine blade, midway tool changing causes waste of time again, and many difficulties are brought to processing and manufacturing.Therefore, aviation hair at home
Motivation critical component manufacture field, High-speed Machining Technology and advanced manufacturing process cannot be applied fully, make Aviation Enterprise
Advanced process equipment cannot get due performance, and the processing of aero-engine is also in the state of depression, is especially embodied in and starts
In the processing of machine blade.
Blade of aviation engine in addition to the poor processability of material, also with a common drawback:Blade is thin, is adding
Man-hour easily produces vibration, deformation, causes blade to collapse scarce.So, the relatively common steel of machining status of blade of aviation engine
For it is relatively severe, the requirement to process tool is extremely strict, should consider its processing intensity, also to take the impact resistance of cutter into account
And wearability, so, the aspect such as the design of cutter, selection and coating is all worthy of careful study.
Utility model content
A purpose of the present utility model is to provide a kind of multiple-cutting-edge postwave blade milling cutter, to solve to process aviation in the prior art
During engine blade, the problem that cutter easily weares and teares.
The utility model is it is also an object that provide a kind of multiple-cutting-edge postwave blade milling cutter, processing is navigated in the prior art with solution
During empty engine blade, cutter easily collapses scarce problem.
The utility model embodiment provides a kind of multiple-cutting-edge postwave blade milling cutter, including handle of a knife, and the spiral below handle of a knife holds
Bits groove and rear knife face have the rear wave-blade spiral cutting sword of waveform concaveconvex structure, it is characterised in that:Including 5~7 it is described after
Ripple sword spiral cutting sword, every rear wave-blade spiral cutting sword surface attachment has nitrogen chromaking aluminized coating, the rear wave-blade spiral
Cutting edge is by rounding Passivation Treatment;The crest radius value of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword is trough
2~3 times of radius value.
As preferred embodiment of the present utility model, the rounding radii value of the rear wave-blade spiral cutting sword for R0.03~
0.05mm。
Used as preferred embodiment of the present utility model, the waveform concaveconvex structure of the rear wave-blade spiral cutting sword is in periodically weight
It is multiple.
As preferred embodiment of the present utility model, the repetition period of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword
It is 1.0mm.
As preferred embodiment of the present utility model, the crest and ripple of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword
The difference in height of paddy is 0.4mm.
As preferred embodiment of the present utility model, the crest radius of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword
It is R0.8mm.
As preferred embodiment of the present utility model, the trough radius of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword
It is R0.4mm.
Used as preferred embodiment of the present utility model, the waveform concaveconvex structure of rear wave-blade spiral cutting sword is at one described in each bar
Mutually stagger equal distance in wave period.
Used as preferred embodiment of the present utility model, the making material of the rear wave-blade spiral cutting sword is that amount containing cobalt is 12%
Ultrafine gain size.
Used as preferred embodiment of the present utility model, the thickness of the nitrogen chromaking aluminized coating is 0.002~0.003mm.
The multiple-cutting-edge postwave blade milling cutter that the utility model is provided, uses amount containing cobalt to be made for 12% ultrafine gain size
Form, the dense structure's property and uniformity of its alloy are better than the routinely material that amount containing cobalt is 10%, in the premise that hardness is constant
Under greatly strengthen the bending strength of Hardmetal materials, improve the impact resistance of cutter.Every surface of cutting edge is also
Nitrogen chromaking aluminized coating is attached with, without titanium elements in the coating composition, it is to avoid occur what compatibility was caused in titanium alloy blade processing
Tool wear.This coating is not under conditions of hardness is reduced, and red hardness and wearability are relatively good, and cutting edge portion maximum temperature is reachable
1100 DEG C, frictional surface coefficient is also below common at present nitrogen titanium aluminide and nitrogen titanizing aluminized coating.Rear wave-blade spiral cutting sword is passed through
Rounding Passivation Treatment is crossed, cutting edge is become fillet by wedge angle before, in the case where ensureing that cutting is sharp, be not
Cause vibration during processing thin-wall part and to cause cutting edge to collapse scarce, further extend cutter life.Additionally, the utility model is set
5~7 cutting edges, compared to existing technology in common 2 or 4 milling cutters of cutting edge, its amount of feeding per minute can phase
Should improve, so as to accelerate processing speed, save the quality time.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme in the utility model embodiment, below will be to needed for embodiment description
The accompanying drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some realities of the present utility model
Example is applied, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is the structural representation of the utility model embodiment;
Fig. 2 is the cross section structure schematic diagram of the utility model embodiment;
Fig. 3 is the partial enlarged drawing of the cross section structure of the utility model embodiment;
Fig. 4 is the schematic diagram of the waveform concaveconvex structure of the utility model embodiment.
Wherein, 1, handle of a knife, 2, spiral chip flute, 3, rear wave-blade spiral cutting sword, 4, fillet.
Specific embodiment
It is new to this practicality below in conjunction with accompanying drawing to make the purpose of this utility model, technical scheme and advantage clearer
Type implementation method is described in further detail.
Shown in reference picture 1, the utility model embodiment discloses a kind of multiple-cutting-edge postwave blade milling cutter, including handle of a knife 1, and is located at
The spiral chip flute 2 of the lower section of handle of a knife 1 and rear knife face have the rear wave-blade spiral cutting sword 3 of waveform concaveconvex structure.After the multiple-cutting-edge
Ripple blade milling cutter has 5~7 rear wave-blade spiral cutting swords 3, compared to common two-edged or four blade milling cutters, sets a plurality of cutting edge
Cutter overall structure can be made compacter, firm, cutter strength and stiffness in itself are favorably improved.
Additionally, in the case where single-blade cutting output is constant, the quantity for increasing cutting edge can correspondingly improve feeding per minute
Amount, so that processing efficiency is improved, it is time-consuming.Therefore, the milling cutter operating efficiency of 5 cutting edges is substantially better than common two-edged or four
Blade milling cutter.
However, as the increase of cutting edge quantity, the manufacture difficulty of cutter can also be increased therewith, being unfavorable for controlling cost.
On the other hand, with the increase of cutting edge quantity, the space of chip pocket can reduce on the contrary, be unfavorable for the discharge of chip.Cause
This, the quantity of cutting edge is not more many more is conducive to practical application.
Consider the factors such as processing efficiency, manufacturing cost, the chip removal of cutter, the quantity of cutting edge is limited in 5~7
In the range of can improve processing efficiency, cutter manufacture cost and chip removal can be taken into account again.
Waveform concaveconvex structure is set in the rear knife face of cutting edge, rear wave-blade, the waveform concaveconvex structure of postwave blade milling cutter is formed
Be conducive to point bits and a chip removal, the velocity of discharge of chip can be accelerated.The quick discharge of chip can take away the heat produced during cutting, drop
The heat build-up of low cutter, reduces the thermal wear of cutter.
Every the surface attachment of rear wave-blade spiral cutting sword 3 has nitrogen chromaking aluminized coating.The parts of aero-engine are closed for titanium
Golden material, and in the prior art, cutting tool coating material is generally nitrogen titanium aluminide or nitrogen titanizing aluminized coating, these cutters are in processing titanium
During alloy, because cutter and workpiece contain titanium elements, compatibility occurs in processing, the abrasion of cutter is extremely serious.
And metal titanium elements are free of in nitrogen chromated aluminum coating composition, it is to avoid in machining titanium alloy blade there is compatibility
The tool wear for causing.Under conditions of hardness is not reduced, red hardness and wearability are showed well nitrogen chromaking aluminized coating, cutting
, up to 1100 DEG C, frictional surface coefficient is also below nitrogen titanium aluminide and nitrogen titanizing aluminized coating for blade maximum temperature.
Preferably, the thickness of nitrogen chromaking aluminized coating is 0.002~0.003mm.
Shown in reference picture 1, the waveform concaveconvex structure of rear wave-blade spiral cutting sword 3 is covered with whole piece postwave in being repeated cyclically
Sword spiral cutting sword 3.
Preferably, the repetition period T=1.0mm of the waveform concaveconvex structure of rear wave-blade spiral cutting sword 3.Further, respectively
The waveform concaveconvex structure of bar rear wave-blade spiral cutting sword 3 mutually staggers equal distance in a wave period.Can so have
Effect ensures the continuity of machined surface, while the axial force that cutter is subject to can also be decomposed, reduces the axial vibration of cutter.
Shown in reference picture 2 and Fig. 3, rear wave-blade spiral cutting sword 3 by Passivation Treatment, in rear wave-blade spiral cutting sword 3
Fillet 4 is provided with cutting edge.Due to the cutting edge concaveconvex structure in wave shape of multiple-cutting-edge postwave blade milling cutter, can be formed with the cutting edge many
At individual cusp, the i.e. crest of waveform concaveconvex structure.Cutting force suffered by such cusp work in-process is very big and processed
Cutter can produce vibration in journey, easily cause cutting edge collapse it is scarce.Therefore, the utility model is especially carried out to multiple-cutting-edge postwave blade milling cutter
Passivation Treatment, makes the cutting edge of cutting edge show a fillet 4, in the case where cutting ability is not influenceed, enhances cutting
The intensity of sword.
Preferably, the rounding radii value of rear wave-blade spiral cutting sword 3 is R0.03~0.05mm, under this parameter, can
Ensure the sharpness of cutter, the intensity of cutter is can guarantee that again.
Postwave blade milling cutter is by the i.e. crest work of projection of waveform concaveconvex structure, in order to improve postwave blade milling cutter
Overall stock-removing efficiency, the crest radius value of the waveform concaveconvex structure of rear wave-blade spiral cutting sword 3 is greater than trough radius value.
Preferably, the crest radius value of the waveform concaveconvex structure of rear wave-blade spiral cutting sword 3 is the 2~3 of trough radius value
Times.Further, the crest radius R1=0.8mm of the waveform concaveconvex structure of rear wave-blade spiral cutting sword 3, trough radius R2=
The difference in height h=0.4mm of 0.4mm, crest and trough.
The making material of the multiple-cutting-edge postwave blade milling cutter that the utility model is provided is the ultra-fine grain hard that amount containing cobalt is 12%
Alloy.It is 10% versatility material compared to amount containing cobalt, amount containing cobalt is 12% ultra-fine cemented carbide materials microstructure densification
Property and uniformity better than amount containing cobalt for 10% versatility material, on the premise of hardness is constant, substantially increase the bending resistance of material
Intensity, so as to improve the impact resistance of cutter.
Preferred embodiment of the present utility model is the foregoing is only, is not used to limit the utility model, it is all in this practicality
Within new spirit and principle, any modification, equivalent substitution and improvements made etc. should be included in guarantor of the present utility model
Within the scope of shield.
Claims (10)
1. a kind of multiple-cutting-edge postwave blade milling cutter, including handle of a knife, spiral chip flute and rear knife face below handle of a knife have waveform
The rear wave-blade spiral cutting sword of concaveconvex structure, it is characterised in that:Including 5~7 rear wave-blade spiral cutting swords, described in every
Rear wave-blade spiral cutting sword surface attachment has a nitrogen chromaking aluminized coating, the rear wave-blade spiral cutting sword by rounding passivation at
Reason;The crest radius value of the waveform concaveconvex structure of the rear wave-blade spiral cutting sword is 2~3 times of trough radius value.
2. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the rounding of the rear wave-blade spiral cutting sword
Angular radius value is R0.03~0.05mm.
3. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the waveform of the rear wave-blade spiral cutting sword
Concaveconvex structure is in be repeated cyclically.
4. multiple-cutting-edge postwave blade milling cutter according to claim 3, it is characterised in that the waveform of the rear wave-blade spiral cutting sword
The repetition period of concaveconvex structure is 1.0mm.
5. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the waveform of the rear wave-blade spiral cutting sword
The crest of concaveconvex structure and the difference in height of trough are 0.4mm.
6. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the waveform of the rear wave-blade spiral cutting sword
The crest radius of concaveconvex structure are R0.8mm.
7. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the waveform of the rear wave-blade spiral cutting sword
The trough radius of concaveconvex structure is R0.4mm.
8. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that rear wave-blade spiral cutting sword described in each bar
Waveform concaveconvex structure mutually staggers equal distance in a wave period.
9. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the making of the rear wave-blade spiral cutting sword
Material is the ultrafine gain size that amount containing cobalt is 12%.
10. multiple-cutting-edge postwave blade milling cutter according to claim 1, it is characterised in that the thickness of the nitrogen chromaking aluminized coating is
0.002~0.003mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621306023.6U CN206263329U (en) | 2016-12-01 | 2016-12-01 | A kind of multiple-cutting-edge postwave blade milling cutter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621306023.6U CN206263329U (en) | 2016-12-01 | 2016-12-01 | A kind of multiple-cutting-edge postwave blade milling cutter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206263329U true CN206263329U (en) | 2017-06-20 |
Family
ID=59042162
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621306023.6U Expired - Fee Related CN206263329U (en) | 2016-12-01 | 2016-12-01 | A kind of multiple-cutting-edge postwave blade milling cutter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206263329U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111958029A (en) * | 2020-08-12 | 2020-11-20 | 内蒙古第一机械集团股份有限公司 | Titanium alloy material milling processing method |
-
2016
- 2016-12-01 CN CN201621306023.6U patent/CN206263329U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111958029A (en) * | 2020-08-12 | 2020-11-20 | 内蒙古第一机械集团股份有限公司 | Titanium alloy material milling processing method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2019047557A1 (en) | Micro-teeth arrangement designable end mill having tip blade for dedicated use with carbon fiber composite material | |
JPWO2009122937A1 (en) | End mill | |
JP5451831B2 (en) | Drilling tools and drilling methods for fiber reinforced composites | |
JPH08507724A (en) | End mill | |
CN103418822A (en) | Rough milling cutter for rotor and wheel groove of steam turbine and manufacturing technology of rough milling cutter | |
CN101716691A (en) | Active-type chip-breaking drill bit | |
CN103722227B (en) | The indexable rose cutter of mould | |
CN107755770A (en) | A kind of hard alloy processes rose cutter | |
CN111570878B (en) | High-speed rough milling method for impeller | |
CN107350531B (en) | A kind of step cutter | |
CN206263329U (en) | A kind of multiple-cutting-edge postwave blade milling cutter | |
CN113894341A (en) | Ceramic milling cutter suitable for rough machining | |
CN105642985A (en) | High-speed milling cutter for wall plates of storage boxes | |
Wang et al. | Effects of geometric structure of twist drill bits and cutting condition on tool life in drilling 42CrMo ultrahigh-strength steel | |
CN205888261U (en) | Long dark step reamer for spot facing work | |
CN112428025A (en) | Method for constructing two-dimensional wear graph of cutter to optimize safe cutting area | |
CN207086999U (en) | Process aluminium alloy Integral alloy high-speed milling cutter | |
CN101745680B (en) | Cemented carbide profile milling cutter with large helix angle | |
Luo et al. | On the machinability and surface finish of superalloy GH909 under dry cutting conditions | |
CN201609780U (en) | Active type chip breaking drill bit | |
CN206382607U (en) | A kind of diamond screw-on cutter | |
CN201030447Y (en) | Highly effective auger-drill head | |
CN107952969A (en) | A kind of hard alloy valve base lathe tool and its application | |
CN107552816A (en) | High temperature alloy finishes efficient chip breaking rhombus turning insert | |
CN206536059U (en) | The special interior close tooth milling cutter of cooling of back of the body arc surface in one kind finishing turbine blade |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170620 Termination date: 20191201 |