CN110449849A - Waveform turbine (gear) processing method - Google Patents
Waveform turbine (gear) processing method Download PDFInfo
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- CN110449849A CN110449849A CN201910808724.1A CN201910808724A CN110449849A CN 110449849 A CN110449849 A CN 110449849A CN 201910808724 A CN201910808724 A CN 201910808724A CN 110449849 A CN110449849 A CN 110449849A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/14—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass gear parts, e.g. gear wheels
Abstract
The invention discloses a kind of waveform turbine (gear) processing methods, include the following steps: (1), prepare round bar pin type tooling: round bar pin type tooling includes the oval body of rod (101), step inner hole is equipped in the described oval body of rod (101) one end, the oval body of rod (101) one end side is provided with dowel hole (102);(2), it blanking and is heat-treated;(3), part mid-module, numerical control turning machine model: XKC-30F vehicle: are processed by part process schematic diagram.The method of the present invention design rationally, successfully processes waveform turbine parts peculiar using XKC-S16B lathe and special tooling, has captured processing problem, broken external monopolization, reduced the purchasing price of parts peculiar, produced good economic benefit.
Description
Technical field
The present invention relates to machine tooling field, specially a kind of parts peculiar waveform turbine (gear) processing method.
Background technique
Waveform turbine (as shown in Figure 5) is the key part of lubricating oil pump in certain vehicle, is all for many years to rely on import,
The manufacturing process country is not yet broken through, and existing processing method needs dedicated copying lathe (not can guarantee the notch and end face wave at step
Shape has relative positional relationship) or five kinematic axis machining center.Existing turbine (gear) processing technology, to the step of end face and
Taper WEDM is relatively easy to, and the wave mode end face main critical technological point of part is that its part end face is three-dimensional waveform curvature portion
Processing technology, the present invention can be not only made to meet the emphasis technique that the production domesticization of key components and parts needs and carries out and break through
China gets rid of the technology dependence to developed country, and to domestic equipment manufacturing technical level is promoted, to turning-milling complex processing
Center has certain facilitation using horizontal raising.
For at present, when being normally applied complex milling machine tool based on milling radial shape, when milling axial shape
Seldom.Processing difficulties have been captured under the continuous tackling key problem of technical staff, using turning-milling complex processing, have passed through test of many times, success
The part (waveform turbine) for the imported product that is enough to match in excellence or beauty is processed.
Summary of the invention
It is an object of the present invention to provide a kind of processing methods for being directed to parts peculiar waveform turbine (gear), are processed by this
Technique (model XKC-S16B) can realize the processing of end face waveform three-dimensional structure on CNC sliding headstock auto-lathe, while can control it
Angle position of the remaining processing department split-phase for waveform.
The present invention is achieved by the following technical scheme:
A kind of waveform turbine (gear) processing method, includes the following steps:
(1), round bar pin type tooling is prepared
Round bar pin type tooling includes the oval body of rod, and step inner hole, the oval body of rod one are equipped in described oval body of rod one end
End side surface is provided with dowel hole.
(2), it blanking and is heat-treated.
(3), part mid-module, numerical control turning machine model: XKC-30F vehicle: are processed by part process schematic diagram;
The part mid-module completed the process includes turbine body, and the turbine body side is integrally extended with technique collet round bar, institute
Stating technique collet round bar end face has the step matched with the step inner hole in oval body of rod one end convex, and the turbine body is another
One side is reserved with the boss for machine-shaping part side step, and part axial hole is machined at the boss.
(4) it beats location hole: opening up dowel hole on the technique collet round bar of part mid-module.
(5) turnning and milling is compound: numerical control lathe, lathe model: XKC-S16B complex milling machine tool, processes end face waveform;
According to the shape of forming part, middle part is hole axle, then front end face is specially that 8 type faces are distributed with centered on hole axle,
Respectively type face 1, type face 2, type face 3, type face 4, type face 5, type face 6, type face 7, type face 8, medium-sized face 2 and type face 6 are symmetrical simultaneously
As concave plane, type face 4 and type face 8 are symmetrically and as convex flat face, inclined-plane of the type face 1 as connecting-type face 2 and type face 8, type face 3
As the inclined-plane in connecting-type face 2 and type face 4, inclined-plane of the type face 5 as connecting-type face 4 and type face 6, type face 7 is used as connecting-type face 6
With the inclined-plane in type face 8, hole axle has part side step between type face 1 and type face 3.Similarly, part rear end face is specially
8 type faces, respectively type face 9, type face 10, type face 11, type face 12, type face 13, type face 14, type face are distributed with centered on hole axle
15, type face 16, medium-sized face 9 is corresponding with type face 7, and type face 10 is corresponding with type face 8, and type face 11 is corresponding with type face 1, type face 12 and type
Face 2 is corresponding, and type face 13 is corresponding with type face 3, and type face 14 is corresponding with type face 4, and type face 15 is corresponding with type face 5, and type face 16 and type face 6 are right
It answers.
Process is as follows:
Firstly, part mid-module to be inserted into the step inner hole of round bar pin type tooling one end by its technique collet round bar, so
Afterwards by pin shaft insertion process collet round bar and the corresponding dowel hole of the oval body of rod, part mid-module and round bar pin type are completed
The assembly of tooling;Round bar pin type tooling is finally installed on machine tool chief axis;
Start lathe, milling cutter is made to start to rotate into milling preparation state;At this point, milling cutter is located at part front end face;Use lathe
X, Z, C three-shaft linkage functional localization milling cutter to type face 8 and 1 transition arc of type face starting point;With the function of Z, C two-axle interlocking
According to the requirement of part front shape, point-by-point fitting processes the transition arc between type face 8 and type face 1, then finishing type face 1
Processing;Type face 1 is after processing is completed with the transition arc between point-by-point fit approach processing type face 1 and type face 2;Transition arc processing
After the completion, forming surface 2 is processed with C s function;Be fitted point by point with Z, C two-axle interlocking function again process type face 2 and type face 3 it
Between transition arc, the then processing in finishing type face 3;After the completion of type face 3, processed between type face 3 and type face 4 with point-by-point fitting
Transition arc;Forming surface 4 is processed with C s function again;To first circulation that end face waveform is completed herein;With such
It pushes away, completes the processing of the part front totally 2 waveform cycles;
The rear end face that milling cutter is moved to part, using X, Z, C three-shaft linkage functional localization milling cutter of lathe to type face 16 and type face 9
Between transition arc starting point;Point-by-point fitting is required to process according to part front shape with the function of Z, C two-axle interlocking
Transition arc between type face 16 and type face 9, the then processing in finishing type face 9;Then with point-by-point fit approach processing type face 9 with
Transition arc between type face 10;Transition arc after processing is completed, with C s function processing type face 10;Again with Z, C two-axle interlocking function
It can be fitted the transition arc processed between type face 10 and type face 11, and then the processing in finishing type face 11 point by point;It is then point-by-point quasi-
Close the transition arc processed between type face 11 and type face 12;Forming surface 12 is processed with C s function again;To end is completed herein
First waveform cycle of surface wave shape reverse side;And so on, complete the processing of the reverse side of the part totally 2 waveform cycles;
The front and back waveform of part adjusts milling cutter to angle corresponding with type face 1 after processing is completed, with C, X two-axle interlocking function
Degree, the mobile control end face step of Z axis to corresponding depth, Y-axis movement process end face step one side;Then with the rotation of C axis
To milling cutter angle corresponding with type face 3, Y-axis is mobile to process end face step another side, completes the side of part front end face
Step processing.
(6), tooth processed: using gear-hobbing machine in turbine body edge tooth.
(7), it removes technique remainder: according to part requirements, removing technique collet round bar.
(8), pincers worker deburring: removal teeth portion burr, polishing section.
(9), it is surface-treated: whole nitridation.
The method of the present invention has a characteristic that
1, the manufacturing process of end face waveform portion
The processing of the part portion waveform (curved surface) is X, Z, C three-shaft linkage function by XKC-S16B lathe, passes through numerical control
Macro programming, control lathe require to process waveform (curved surface) according to part shape.
Solving by the three-shaft linkage of numerically-controlled machine tool needs five axis equipment to process the shape being just able to achieve, and reduces use and sets
It is standby that grade has saved fund;So that the shape of three-dimension curved surface is controlled by nc program, the numerous of manufacture pattern is eliminated
A trivial and secondary pattern can only manufacture a kind of limitation of part, so that process more has controllability.
2, the waveform requirements of end face part have relative positional relationship with the notch at step
The position control of the part is by designed, designed " round bar pin type " connecting tooling, with the split ring pin connection part
Technique clamping part, to guarantee that the part is synchronous with lathe C shaft angle degree, numerical control program control lathe complete waveform (curved surface),
And guarantee the part waveform and other end step at notch relative positional relationship.
Each end face waveform of the part can be arbitrarily controlled by the connection XKC-S16B machine tool of the tooling and step lacks
Angle position at mouthful, can control effectively to it, precision can reach 0.1 °.
The method of the present invention design rationally, successfully processes waveform turbine dedicated zero using XKC-S16B lathe and special tooling
Part has captured processing problem, has broken external monopolization, reduces the purchasing price of parts peculiar, produces economic effect well
Benefit.
Detailed description of the invention
Fig. 1 shows the assembled front views of part after processing is completed and round bar pin type tooling.
Fig. 1 a indicates the assembly overall diagram of part and round bar pin type tooling after processing is completed.
Fig. 2 indicates the assembly process figure of part and round bar pin type tooling after processing is completed.
Fig. 2 a indicates the assembling process overall diagram of part and round bar pin type tooling after processing is completed.
Fig. 3 indicates part (non-cutting technique collet round bar) schematic diagram after processing is completed.
Fig. 3 a indicates part mid-module schematic diagram.
Fig. 4 a indicates part front end face (front) schematic diagram, and front has part step.
Fig. 4 b indicates part rear end face (back side) schematic diagram.
Fig. 5 indicates to carry out three-dimensional modeling schematic diagram to processing part with Soldiworks software according to X-Y scheme.
Fig. 6 indicates part mid-module pictorial diagram.
Fig. 7 indicates XKC-S16B machine tool motion axial coordinate schematic diagram, in figure: face lathe, C axis as machine tool chief axis, into
Side-to-side movement is carried out as Z axis while row rotary motion;X-axis moves forward and backward;Y-axis moves up and down.
In figure: 100- part (waveform turbine), the oval body of rod of 101-, 102- dowel hole, 103- pin shaft, 201- turbine
Body, 202- technique collet round bar, 203- step is convex, 204- boss, 205- part axial hole.
Specific embodiment
Specific embodiments of the present invention are described in detail with reference to the accompanying drawing.
A kind of waveform turbine (gear) processing method, includes the following steps:
(1), round bar pin type tooling is prepared
As shown in Fig. 2,2a, round bar pin type tooling includes the oval body of rod 101, and step inner hole is equipped in oval 101 one end of the body of rod,
Oval 101 one end side of the body of rod is provided with dowel hole 102.
(2), blanking, material 42CrMo, size 25 × 55mm of φ, and be heat-treated: quenched 24-33HRC.
(3), part mid-module, surface roughness 3.2, using numerical control vehicle device vehicle: are processed by part process schematic diagram
Bed-type number: XKC-30F.
As shown in Figure 3a, the part mid-module completed the process includes turbine body 201, and 201 side of turbine body integrally extends
There is technique collet round bar 202,202 end face of technique collet round bar has to match with the step inner hole in oval 101 one end of the body of rod
The step of conjunction convex 203,201 another side of turbine body are reserved with the boss 204 for machine-shaping part side step, boss
Part axial hole 205 is machined at 204.
(4) it beats location hole: opening up dowel hole 102 on the technique collet round bar 202 of part mid-module.
(5) turnning and milling is compound: numerical control lathe, lathe model: XKC-S16B complex milling machine tool, processes end face waveform.
According to the shape of forming part, middle part is hole axle, then part front end face (front) is specially centered on hole axle
8 type faces are distributed with, as shown in fig. 4 a, respectively type face 1, type face 2, type face 3, type face 4, type face 5, type face 6, type face 7, type face
8, medium-sized face 2 and type face 6 are symmetrically and as concave plane, and type face 4 and type face 8 are symmetrically and as convex flat face, and type face 1 is as connection
The inclined-plane in type face 2 and type face 8, inclined-plane of the type face 3 as connecting-type face 2 and type face 4, type face 5 are used as connecting-type face 4 and type face 6
Inclined-plane, inclined-plane of the type face 7 as connecting-type face 6 and type face 8, hole axle between type face 1 and type face 3 have part side platform
Rank.Similarly, part rear end face (back side) is specially that 8 type faces are distributed with centered on hole axle, as shown in Figure 4 b, respectively type face
9, type face 10, type face 11, type face 12, type face 13, type face 14, type face 15, type face 16, then as the two sides of a waveform (front
And the back side), medium-sized face 9 is corresponding with type face 7, and type face 10 is corresponding with type face 8, and type face 11 is corresponding with type face 1, type face 12 and type face
2 is corresponding, and type face 13 is corresponding with type face 3, and type face 14 is corresponding with type face 4, and type face 15 is corresponding with type face 5, and type face 16 and type face 6 are right
It answers;That is: type face 12 and type face 16 are symmetrical and as convex flat face, and symmetrically and as concave plane, type face 11 is made for type face 14 and type face 10
For the inclined-plane in connecting-type face 10 and type face 12, inclined-plane of the type face 13 as connecting-type face 12 and type face 14, type face 15 is as connection
The inclined-plane in type face 14 and type face 16, inclined-plane of the type face 9 as connecting-type face 16 and type face 10.
XKC-S16B uses main shaft internal hidden type structure, and revolving speed is high, noise is small, wide adaptability;It is various accurate small parts
Ideal equipment, the batch Continuous maching especially suitable for thin and long shafts complex parts.Specific process is as follows:
Firstly, part mid-module is inserted into the step inner hole of round bar pin type tooling one end by its technique collet round bar 202,
The step of 202 end face of technique collet round bar convex 203 realizes radial positioning, then by pin shaft 103(split ring pin) insertion process
In collet round bar 202 and the corresponding dowel hole 102 of the oval body of rod 101, part mid-module and round bar pin type tooling are completed
Assembly, as shown in Fig. 1,1a;Round bar pin type tooling is finally mounted as a whole on machine tool chief axis.
Start power unit of machine tool, milling cutter is made to start to rotate into milling preparation state;At this point, milling cutter is located at part front end
Face;Using lathe X, Z, C three-shaft linkage functional localization milling cutter to type face 8 and 1 transition arc of type face starting point;With Z, C two
The function of axis linkage processes the transition arc between type face 8 and type face 1, connects according to the requirement of part front shape, point-by-point fitting
The processing in finishing type face 1;Type face 1 is after processing is completed with the transition circle between point-by-point fit approach processing type face 1 and type face 2
Arc;Transition arc processes forming surface 2 after processing is completed, with C s function;Processing is fitted point by point with Z, C two-axle interlocking function again
Transition arc between type face 2 and type face 3 out, the then processing in finishing type face 3;After the completion of type face 3, processed with point-by-point fitting
Transition arc between type face 3 and type face 4;Forming surface 4 is processed with C s function again;To the of end face waveform is completed herein
One circulation;And so on, complete the processing of the part front totally 2 waveform cycles;As shown in fig. 4 a.
The rear end face that milling cutter is moved to part, using lathe X, Z, C three-shaft linkage functional localization milling cutter to type face 16 with
The starting point of transition arc between type face 9;Point-by-point fitting is required to add according to part front shape with the function of Z, C two-axle interlocking
Work goes out the transition arc between type face 16 and type face 9, then the processing in finishing type face 9;Then with point-by-point fit approach processing type
Transition arc between face 9 and type face 10;Transition arc after processing is completed, with C s function processing type face 10;Again with two axis of Z, C
Linkage function is fitted the transition arc processed between type face 10 and type face 11, and then the processing in finishing type face 11 point by point;Then
Point-by-point fitting processes the transition arc between type face 11 and type face 12;Forming surface 12 is processed with C s function again;To herein
Complete first waveform cycle of end face waveform reverse side;And so on, complete the reverse side of the part totally 2 waveform cycles plus
Work;As shown in Figure 4 b.
Note: X-axis linkage is not needed when processing waveform type face, but needs mobile X-axis when cutter movement and positioning.
The front and back waveform of part is after processing is completed, extremely corresponding with type face 1 with C, X two-axle interlocking function adjustment milling cutter
Angle, the mobile control end face step of Z axis to corresponding depth, Y-axis movement processes end face step one side;Then with C axis
Rotation to milling cutter angle corresponding with type face 3, Y-axis movement processes end face step another side;As shown in Fig. 3 and Fig. 4 a,
Complete the side step processing of part front end face.
For the size for controlling effective teeth portion, added using the waveform that same branch cutter completes tow sides in clamped one time
Work.Guarantee the consistent of tow sides deformation, guarantees the positional relationship of step and waveform.As shown in fig. 6, in part mid-module
Turbine body on process waved surface and side step.
(6), tooth processed: using gear-hobbing machine in turbine body edge tooth;Gear-hobbing machine lathe model: MIKRON 102-05.Gear hobbing
It is to process gear by generating principle, is processed with hobboing cutter and helical teeth and cylindrical gear pair tooth are equivalent to wheel.This be it is a kind of very
Mature Gear Processing mode, the mode of gear hobbing process the part work gear part, and design parameter see the table below.Reference diameter
Guarantee concentricity, accuracy class: 7-7-7tGB/T10089-1998 with hole.Shaft end is lengthened by clamping, the small shaft end of centering is come
Guarantee concentricity.
(7), it removes technique remainder: according to part requirements, removing technique collet round bar 202;Wire cutting machine tool model: DK7740 is protected
Demonstrate,prove overall length and size.
(8), pincers worker deburring: removal teeth portion burr, polishing section.
(9), be surface-treated: whole nitridation nitrogenizes depth >=0.3, and surface hardness is greater than 600HV.Increase the wear-resisting of part
Property, surface hardness, fatigue limit and resistance to corrosion, improve the service life of part.
It is verified through production, this technique is suitble to produce in enormous quantities, full by testing and being mounted on the experiment that carries out an acceptance inspection on certain vehicle
Sufficient requirement, product stability match in excellence or beauty import lubricating oil pump, reduce production cost.
It should be noted last that the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, although ginseng
It is described in detail according to the embodiment of the present invention, those skilled in the art should understand that, to technical solution of the present invention
It is modified or replaced equivalently, without departure from the spirit and scope of technical solution of the present invention, the present invention should all be covered by
In the protection scope of claims.
Claims (1)
1. a kind of waveform turbine (gear) processing method, characterized by the following steps:
(1), round bar pin type tooling is prepared
Round bar pin type tooling includes the oval body of rod (101), and step inner hole is equipped in the described oval body of rod (101) one end, described
The oval body of rod (101) one end side is provided with dowel hole (102);
(2), it blanking and is heat-treated;
(3), part mid-module, numerical control turning machine model: XKC-30F vehicle: are processed by part process schematic diagram;
The part mid-module completed the process includes turbine body (201), and turbine body (201) side is integrally extended with technical clamp
Head round bar (202), the technique collet round bar (202) end face have and the step inner hole phase in the oval body of rod (101) one end
The step of cooperation is convex (203), and turbine body (201) another side is reserved with the boss for machine-shaping part side step
(204), part axial hole (205) are machined at the boss (204);
(4) it beats location hole: opening up dowel hole (102) on the technique collet round bar (202) of part mid-module;
(5) turnning and milling is compound: numerical control lathe, lathe model: XKC-S16B complex milling machine tool, processes end face waveform;
According to the shape of forming part, middle part is hole axle, then front end face is specially that 8 type faces are distributed with centered on hole axle,
Respectively type face 1, type face 2, type face 3, type face 4, type face 5, type face 6, type face 7, type face 8, medium-sized face 2 and type face 6 are symmetrical simultaneously
As concave plane, type face 4 and type face 8 are symmetrically and as convex flat face, inclined-plane of the type face 1 as connecting-type face 2 and type face 8, type face 3
As the inclined-plane in connecting-type face 2 and type face 4, inclined-plane of the type face 5 as connecting-type face 4 and type face 6, type face 7 is used as connecting-type face 6
With the inclined-plane in type face 8, hole axle has part side step between type face 1 and type face 3;Similarly, rear end face is specially with hole
Be distributed with 8 type faces centered on axis, respectively type face 9, type face 10, type face 11, type face 12, type face 13, type face 14, type face 15,
Type face 16, medium-sized face 9 is corresponding with type face 7, and type face 10 is corresponding with type face 8, and type face 11 is corresponding with type face 1, type face 12 and type face 2
Corresponding, type face 13 is corresponding with type face 3, and type face 14 is corresponding with type face 4, and type face 15 is corresponding with type face 5, and type face 16 is corresponding with type face 6;
Process is as follows:
Firstly, part mid-module is inserted into the step of round bar pin type tooling one end by its technique collet round bar (202)
Hole, it is then that pin shaft (103) insertion process collet round bar (202) and the corresponding dowel hole (102) of the oval body of rod (101) is interior,
Complete the assembly of part mid-module and round bar pin type tooling;Round bar pin type tooling is finally installed on machine tool chief axis;
Start lathe, milling cutter is made to start to rotate into milling preparation state;At this point, milling cutter is located at part front end face;Use lathe
X, Z, C three-shaft linkage functional localization milling cutter to type face 8 and 1 transition arc of type face starting point;With the function of Z, C two-axle interlocking
According to the requirement of part front shape, point-by-point fitting processes the transition arc between type face 8 and type face 1, then finishing type face 1
Processing;Type face 1 is after processing is completed with the transition arc between point-by-point fit approach processing type face 1 and type face 2;Transition arc processing
After the completion, forming surface 2 is processed with C s function;Be fitted point by point with Z, C two-axle interlocking function again process type face 2 and type face 3 it
Between transition arc, the then processing in finishing type face 3;After the completion of type face 3, processed between type face 3 and type face 4 with point-by-point fitting
Transition arc;Forming surface 4 is processed with C s function again;To first circulation that end face waveform is completed herein;With such
It pushes away, completes the processing of the part front totally 2 waveform cycles;
The rear end face that milling cutter is moved to part, using X, Z, C three-shaft linkage functional localization milling cutter of lathe to type face 16 and type face 9
Between transition arc starting point;Point-by-point fitting is required to process according to part front shape with the function of Z, C two-axle interlocking
Transition arc between type face 16 and type face 9, the then processing in finishing type face 9;Then with point-by-point fit approach processing type face 9 with
Transition arc between type face 10;Transition arc after processing is completed, with C s function processing type face 10;Again with Z, C two-axle interlocking function
It can be fitted the transition arc processed between type face 10 and type face 11, and then the processing in finishing type face 11 point by point;It is then point-by-point quasi-
Close the transition arc processed between type face 11 and type face 12;Forming surface 12 is processed with C s function again;To end is completed herein
First waveform cycle of surface wave shape reverse side;And so on, complete the processing of the reverse side of the part totally 2 waveform cycles;
The front and back waveform of part adjusts milling cutter to angle corresponding with type face 1 after processing is completed, with C, X two-axle interlocking function
Degree, the mobile control end face step of Z axis to corresponding depth, Y-axis movement process end face step one side;Then with the rotation of C axis
To milling cutter angle corresponding with type face 3, Y-axis movement processes end face step another side;
(6), tooth processed: using gear-hobbing machine in turbine body edge tooth;
(7), it removes technique remainder: according to part requirements, removing technique collet round bar (202);
(8), pincers worker deburring: removal teeth portion burr, polishing section;
(9), it is surface-treated: whole nitridation.
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001035854A1 (en) * | 1999-11-17 | 2001-05-25 | 3M Innovative Properties Company | Mill blank for dental prosthesis |
US8864438B1 (en) * | 2013-12-05 | 2014-10-21 | Siemens Energy, Inc. | Flow control insert in cooling passage for turbine vane |
CN104139303A (en) * | 2013-05-07 | 2014-11-12 | 金宏昌机械有限公司 | Turn-milling combined machining device and machining method thereof |
CN208147066U (en) * | 2018-04-09 | 2018-11-27 | 珠海市电气控制设备有限公司 | A kind of precision harmonic gear processes complete tooling and gear numerical control process equipment |
CN109332819A (en) * | 2018-11-15 | 2019-02-15 | 冯丹纯 | Spherical involute tooth form spiral bevel gear gear-shaping method and its cutting cutter and lathe |
-
2019
- 2019-08-29 CN CN201910808724.1A patent/CN110449849B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001035854A1 (en) * | 1999-11-17 | 2001-05-25 | 3M Innovative Properties Company | Mill blank for dental prosthesis |
CN104139303A (en) * | 2013-05-07 | 2014-11-12 | 金宏昌机械有限公司 | Turn-milling combined machining device and machining method thereof |
US8864438B1 (en) * | 2013-12-05 | 2014-10-21 | Siemens Energy, Inc. | Flow control insert in cooling passage for turbine vane |
CN208147066U (en) * | 2018-04-09 | 2018-11-27 | 珠海市电气控制设备有限公司 | A kind of precision harmonic gear processes complete tooling and gear numerical control process equipment |
CN109332819A (en) * | 2018-11-15 | 2019-02-15 | 冯丹纯 | Spherical involute tooth form spiral bevel gear gear-shaping method and its cutting cutter and lathe |
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