CN1413790A - Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool - Google Patents
Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool Download PDFInfo
- Publication number
- CN1413790A CN1413790A CN02139582.9A CN02139582A CN1413790A CN 1413790 A CN1413790 A CN 1413790A CN 02139582 A CN02139582 A CN 02139582A CN 1413790 A CN1413790 A CN 1413790A
- Authority
- CN
- China
- Prior art keywords
- cutter
- vector
- tool
- cutting
- formula
- 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.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C3/00—Milling particular work; Special milling operations; Machines therefor
- B23C3/16—Working surfaces curved in two directions
- B23C3/18—Working surfaces curved in two directions for shaping screw-propellers, turbine blades, or impellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C5/00—Milling-cutters
- B23C5/02—Milling-cutters characterised by the shape of the cutter
- B23C5/10—Shank-type cutters, i.e. with an integral shaft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C2210/00—Details of milling cutters
- B23C2210/08—Side or top views of the cutting edge
- B23C2210/084—Curved cutting edges
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Numerical Control (AREA)
Abstract
A conic drum-shaped cutting tool and its feed pitch, feed step length and method for calculating the position of cutting tool are disclosed. Its cutting part is a rotary surface. Its generating line is an arc with radius R. Its advantages are high productivity, high rigidity and high rotation flexibility. A method for laternally milling a centrifugal blade wheel with complex curved surface with the said cutting tool is also disclosed, which features less number of tracings, short tracing and high productivity.
Description
One, affiliated technical field
The present invention relates to the complex-curved Computerized Numerical Control processing technology such as arbitrary surface impeller in machining and Computerized Numerical Control processing technology field, particularly a kind of drum-taper type cutter tool and utilize the complex-curved method of drum-taper type cutter tool side milling.
Two, background technology
At present, the cutter that adopts usually in centrifugal impeller fine finishining is spherical cutter, and the effective radius of clean-up of spherical cutter is little, and working (machining) efficiency is low.
C.Y.Wu. (Arbitrary surface flank milling of fan, compressor, andimpeller blades.Transactions of the ASME, Journal of Engineering forGas Turbines and Power, Vol.117,1995, p534~p539), proposed to utilize the method for tapered knife side milling arbitrary surface impeller blade, its cutting edge is a taper seat, referring to Fig. 1.He has broken through the processing arbitrary surface and must adopt spherical cutter or slotting cutter to carry out this mode of thinking of contact processing, and the processing mode of line contact efficiently is applied in the processing of arbitrary surface, and this method working (machining) efficiency is far longer than spherical cutter.
Find in the practice that adopt tapered knife processing arbitrary surface to have following defective: 1) this method requires relatively harshness to the direction of cutter in processing blade shape and the processing, and leaf curling can not be too big, otherwise can not find suitable cutter Working position.For given position on the processing curve, the feasible direction territory of cutter is very little, and rotation leeway is little; 2) if cutter and blade bump, because the feasible direction territory of cutter is little, the cutter slewing area is little, interferes cutter spacing to be difficult to revise.Therefore, mill in the system process in arbitrary surface ternary centrifugal impeller integral body, this method may be failed.
Liu Xiongwei, Zhang Dinghua etc. (" digital control processing theory and programming technique " Beijing: China Machine Press, 1994); Introduced the thinking of utilizing drum knife side milling curved surface, referring to Fig. 2, adopted this sharp method, the contact length of cutter and finished surface is bigger.Just utilize drum knife to introduce the basic principle of side milling in the document, do not relate to the calculating of drum knife curved sides milling cutter position.
Because impeller channel is a slype, adopt the drum type cutter, the ratio of rigidity of cutter is less, influences machining accuracy.
Three, summary of the invention
Defective or deficiency at above-mentioned prior art existence, an object of the present invention is to provide a kind of drum-taper type cutter tool, the characteristics of this drum-taper type cutter tool are, Tool in Cutting partly is the surface of revolution, bus is one section circular arc that radius is R, and the surface of revolution and handle of a knife are tangent, the no cutting edge in cutter bottom, principle not take place to be cut to curved surface in the value of R in this cutter, and promptly the radius of curvature of curved surface contact point should be greater than the R value; Drum-taper type cutter tool of the present invention is a kind of cutting tool efficiently, kept drum knife and tapered knife working (machining) efficiency with respect to spherical knife up, overcome the little weakness of drum knife rigidity simultaneously, than tapered knife greater flexibility is arranged again, can avoid easily cutting and colliding, be the whole process tool of a kind of desirable arbitrary surface 3 d impeller.
Another object of the present invention provides a kind of method of utilizing the complex-curved centrifugal impeller of drum-taper type cutter tool side milling, may further comprise the steps:
1) calculating of cutter path spacing and cutting step length
(1) calculating of cutter path spacing
Comprise that 1. curved surface is along the method transversal radius of curvature R of vector b
bCalculating; 2. the Tool in Cutting face is along effective radius of clean-up r of vector b
cCalculating.
(2) calculating of cutting step length
2) cutter spacing data computing
Comprise the calculating of the calculating of generating tool axis vector l and cutter computer center.
The present invention adopts drum-taper type cutter processing impeller, and under same processing conditions, cutter path length is short, and required process time is few, promptly adopts this cutter fine finishining arbitrary surface impeller, and working (machining) efficiency will be 3 times of conventional method.Simultaneously, it has greater flexibility than tapered knife, is easy to revise the interference of cutter and blade in the processing; And rigidity is higher than drum knife.
Four, description of drawings
Fig. 1 is conical knife structure figure;
Fig. 2 is the drum knife structure chart;
Fig. 3 is a drum-taper type cutter structure chart of the present invention;
Fig. 4 utilizes drum-taper type cutter side milling curved surface schematic diagram;
Fig. 5 is the calculating schematic diagram of search spacing d;
The schematic cross-section of Fig. 6 drum-taper type cutter cutting tip;
Fig. 7 is definite schematic diagram of cutter computer center;
Fig. 8 is the cutter path that adopts drum-taper type cutter to form;
Fig. 9 is the cutter path that adopts spherical cutter to form.
Five, the specific embodiment
The present invention is described in further detail below in conjunction with specific embodiment that accompanying drawing and inventor provide.5.1 the proposition of drum taper
The present invention proposes a kind of utilize the complex-curved centrifugal impeller of highly-efficient processing cutting tool, claim that this cutter is a drum-taper type cutter, referring to Fig. 3.Tool in Cutting partly is the surface of revolution, and bus is one section circular arc that radius is R, and the surface of revolution and handle of a knife are tangent, the no cutting edge in cutter bottom.Drum-taper type cutter has kept drum knife and the tapered knife working (machining) efficiency with respect to spherical knife up, overcome the little weakness of drum knife rigidity simultaneously, than tapered knife greater flexibility being arranged again, can avoid easily cutting and colliding, is the whole process tool of the centrifugal 3 d impeller of a kind of desirable arbitrary surface.The choosing with curved surface principle not to take place to be cut to of R in this cutter, promptly the radius of curvature of curved surface contact point should be greater than the R value.5.2 the calculating of cutter path spacing and cutting step length
The situation of utilizing drum-taper type cutter side milling curved surface as shown in Figure 4, r (u, w) expression curved surface, cutter contact point is some C, some O is the computer center of cutter, l is the cutter axis orientation vector, unit vector f is a cutting direction, and n is that the per unit system that C is ordered is vowed vector b=n * f, these three vectors have been formed a rectangular coordinate system, and initial point is at a C.In the processing of five coordinates, cutter also has two rotary freedoms.The inceptive direction of getting cutter shaft is consistent with vector b, and at first initial generating tool axis vector is rotated an angle [alpha] around vector f; Then, cutter rotates one angle-β around vector n again, and positive direction determines that with right-handed system this is because during Tool in Cutting, cutter shaft must be inclined to one side to cutting direction f, drags the cutter cutting with formation.As can be seen from Figure, cutter shaft when initial position, α=0, β=0.
In the Surface NC Machining, must calculate cutter path spacing and cutting step length.
(1) calculating of cutter path spacing
Vow that perpendicular to method f does a cross section at the C point, then vector b and CC ' must be in this planes, and as shown in Figure 5, the curved surface section line that obtains can be approx with one section arc representation, and radius is that the C point is designated as R along the method transversal radius of curvature of direction b on the curved surface
bEqually, the Tool in Cutting face is along the also available one section circular arc approximate representation of the section line of direction b, and its radius is designated as r for the method transversal radius of curvature of cutter C point along direction b
c
For given R
b, r
cAnd residual height h, cutter path spacing d can calculate with following formula
1) curved surface is along the method transversal radius of curvature R of vector b
bCalculating
According to Differential Geometry knowledge, the tangent line b that curved surface C is ordered can be expressed as
b=r
ud
u+r
wd
w
Wherein, d
u, d
wBe respectively vector b at tangent vector r
u, r
wOn component.
Then the method transversal radius of curvature along direction b is
Wherein, I is a first fundamental form of surface, and E, F, G are respectively the first kind fundamental quantity of curved surface, and II is a second fundamental form of a surface, and L, M, N are respectively the second class fundamental quantity of curved surface.
If d
w=0, then
If d
w≠ 0, then formula (2) is done a conversion, have
As shown in Figure 4
b·f=0
I.e. (r
uDu+r
wDw) f=0
Thus
Formula (4) substitution formula (3) can be obtained the radius of curvature R of Surface Method transversal
bValue.2) the Tool in Cutting face is along effective radius of clean-up r of vector b
cCalculating
The Tool in Cutting face is dissectd along the plane of crossing cutter shaft, shown partial cross section as Fig. 6, wherein heavy line is a cutting edge, and some O is the computer center of cutter, and some O ' is the center of cutter revolution bus, and R is the bus radius, and C is a cutter contact point.With an O is the origin of coordinates, cutter shaft to radially respectively as reference axis z and r.α is the angle of O ' C and r axle.From figure as can be known, have point of contact, promptly put C and be in the cutting tip that heavy line is represented among Fig. 6, the maximum deflection value α of angle [alpha] in order to make cutter and curved surface
MaxShould satisfy:
By the geometrical relationship shown in Fig. 6, can obtain the coordinate that C orders and be:
By Fig. 4 and Fig. 6, can get according to Euler's formula, behind cutter tilt angle alpha and the β, at Tool in Cutting face contact point place, along the normal curvature of vector b direction be
k
c=k
1cos
2β+k
2sin
2β
Wherein, k
1And k
2Be respectively the principal curvatures of this contact point, k
1=1/R, k
2=1/r=1/ (Rcos α-(R-d
c/ 2))
So effective radius of clean-up r of cutter
cFor
r
c=1/k
c (5)
With formula (5) and formula (3) substitution formula (1),, can try to achieve cutter path spacing d because h is given.(2) calculating of cutting step length
In the multi-coordinate digital control processing of curved surface, the linear interpolation mode is generally adopted in the motion of cutter, and establishing the straight line approximate error that exists between the movement locus of cutter reality and the theoretical CC track is δ, and then cutting step length AB can be calculated as follows:
Wherein, K
fCurvature for tool track contact point place.5.3 cutter spacing data computing
The cutter spacing data comprise the calculating central position O and cutter axis orientation (unit vector) l of cutter, and the calculating of cutter spacing is relevant with the geomery of cutter.For the drum-taper type cutter tool, cutter spacing is calculated as follows.
(1) calculating of generating tool axis vector l
As shown in Figure 4, the initial position of generating tool axis vector is a vector b, at this moment, and α=β=0.At first making cutter is the center with an O ', around vector f anglec of rotation α, referring to Fig. 6.Making cutter again is the center with a C, around the vector n anglec of rotation-β.If generating tool axis vector is from the vector l of inceptive direction b behind vector f anglec of rotation α
1, then
l
1=b·cosα+n·sinα
Generating tool axis vector l
1Around vector n rotation-β angle, can obtain the final direction vector l of cutter shaft, have
l=l
1·cosβ-n×l
1·sinβ+n·(l
1·n)·(1-cosβ) (6)
(2) calculating of cutter computer center
Fig. 7 has shown cutter before and after vector f anglec of rotation α, the change situation of computer center.Wherein, some O ' is the center of circle of Tool in Cutting surface of revolution bus, some O
1Be the computer center of cutter initial position, some O
2Computer center for cutter behind the anglec of rotation α.
If vector O ' O
1Behind vector f anglec of rotation α is O ' O
2, vector O ' O
2After vector n rotation-β angle for vector O ' O (not expressing among the figure), then pass through rotation transformation after, the final computer center's point O of cutter is
O=O '+O ' O (7) by Fig. 6 and Fig. 7 as can be known
O′=C+n·R,O
1=C+n·(d
c/2)
Then
O′O
1=n·(d
c/2-R) (8)
Vector O ' O
2O ' O is respectively with vector
O′O
2=O′O
1·cosα+f×O′O
1·sin (9)
O′O=O′O
2·cosβ-n×O′O
2·sin?ββ+n·(O′O
2·n)·(1-cosβ) (10)
With formula (8) substitution formula (9), formula (9) substitution formula (10) can be tried to achieve O ' O,, can try to achieve final computer center's point O of cutter again with formula (10) substitution formula (7).
Formula (6) and formula (7) have been determined the O of computer center of cutter axis orientation l and cutter respectively, and (O l) determines the cutter spacing data thus.
Adopt drum-taper type cutter processing blade of the present invention, the result shows, its cutter path number is far smaller than the track number when adopting spherical cutter, the ratio of the two is generally about 1: 3, under same processing conditions, cutter path length is short, and required process time is few, promptly adopt the smart arbitrary surface processing of this cutter impeller, working (machining) efficiency will be 3 times of conventional method.Simultaneously, it has greater flexibility than tapered knife, is easy to revise in the processing interference of cutter and blade; And rigidity is higher than drum knife.
Embodiment:
Utilize spherical cutter and drum-taper type cutter respectively, the cutter path in the processing of centrifugal impeller blade five coordinates is generated discuss.Blade is an arbitrary surface, represents with the cubic B batten.Used spherical cutter diameter is d
c=32mm, drum-taper type cutter knife bar diameter d
c=32mm, R=70mm, h=25mm is referring to Fig. 1.Allowing residual height is 0.1mm, respectively to the cutter path in above-mentioned two kinds of cutters calculating blade processing.
Result of calculation such as Fig. 8 and shown in Figure 9 adopt drum-taper type cutter, and the track number of processing this blade is 16, and the track total length is 6631mm; And adopt spherical cutter track number to reach 39 more than, and the track total length is 16453mm, the ratio of the two is 1: 2.5.Under same cutting speed, the working (machining) efficiency that adopts drum-taper type cutter is 2.5 times of spherical cutter.
Claims (3)
1. a drum-taper type cutter tool comprises handle of a knife and cutting tip, it is characterized in that, Tool in Cutting partly is the surface of revolution, and bus is one section circular arc that radius is R, and the surface of revolution and handle of a knife are tangent, the no cutting edge in cutter bottom.
2. drum-taper type cutter tool as claimed in claim 1 is characterized in that, the R span in the described cutter is that the radius of curvature of curved surface contact point should be greater than the R value.
3. a method of utilizing the complex-curved centrifugal impeller of drum-taper type cutter side milling is characterized in that, may further comprise the steps:
1) calculating of cutter path spacing and cutting step length
A. set up coordinate system
If curved surface be r (u, w), cutter and curved surface r (u, w) contact point for the some C, computer center's point of cutter is O, and the cutter axis orientation vector is l, and unit vector f is a cutting direction, and n is that the per unit system that C is ordered is vowed, vector b=n * f, these three vectors have been formed a rectangular coordinate system, and initial point is at a C; In the processing of five coordinates, cutter also has two rotary freedoms; The inceptive direction of getting cutter shaft is consistent with vector b, and at first initial generating tool axis vector is rotated an angle [alpha] around vector f; Then, cutter rotates one angle-β around vector n again, and positive direction determines that with right-handed system this is because during Tool in Cutting, cutter shaft must drag the cutter cutting with formation to cutting direction f skew; Cutter shaft when initial position, α=0, β=0;
B. the calculating of cutter path spacing
Vow that perpendicular to method f does a cross section at the C point, then vector b and CC ' must be in this planes, and the curved surface section line that obtains can be approx with one section arc representation, and radius is that the C point is designated as R along the method transversal radius of curvature of direction b on the curved surface
b, same, the Tool in Cutting face is along the also available one section circular arc approximate representation of the section line of direction b, and its radius is designated as r for the method transversal radius of curvature of cutter C point along direction b
c
For given R
b, r
cAnd residual height b, cutter path spacing d can calculate with following formula
1. curved surface is along the method transversal radius of curvature R of vector b
bCalculating
According to Differential Geometry knowledge, the tangent line b that curved surface C is ordered can be expressed as
b=r
ud
u+r
wd
w
Wherein, d
u, d
wBe respectively vector b at tangent vector r
u, r
wOn component.
Then the method transversal radius of curvature along direction b is
Wherein, I is a first fundamental form of surface, and E, F, G are respectively the first kind fundamental quantity of curved surface, and II is a second fundamental form of a surface, and L, M, N are respectively the second class fundamental quantity of curved surface.
If d
w=0, then
If d
w≠ 0, then formula (2) is done a conversion, have
Because bf=0
I.e. (r
wDu+r
wDw) f=0
Thus
Formula (4) substitution formula (3) can be obtained the radius of curvature R of Surface Method transversal
bValue;
2. the Tool in Cutting face is along effective radius of clean-up r of vector b
cCalculating
The Tool in Cutting face is dissectd along the plane of crossing cutter shaft, and some O is the computer center of cutter, and some O ' is the center of cutter revolution bus, and R is the bus radius, and C is a cutter contact point;
With an O is the origin of coordinates, cutter shaft to radially respectively as reference axis z and r; α is the angle of O ' C and r axle; For cutter and curved surface are had point of contact, promptly put C and be in cutting tip, the maximum deflection value α of angle [alpha]
MaxShould satisfy:
Can obtain the coordinate that C orders is:
Can get according to Euler's formula, behind cutter tilt angle alpha and the β,, be along the normal curvature of vector b direction at Tool in Cutting face contact point place
k
c=k
1cos
2β+k
2sin
2β
Wherein, k
1And k
2Be respectively the principal curvatures of this contact point, k
1=1/R, k
2=1/r=1/ (Rcos α-(R-d
c/ 2))
So effective radius of clean-up r of cutter
cFor
r
c=1/k
c (5)
With formula (5) and formula (3) substitution formula (1),, can try to achieve cutter path spacing d because h is given
C. the calculating of cutting step length
In the multi-coordinate digital control processing of curved surface, the linear interpolation mode is generally adopted in the motion of cutter, and establishing the straight line approximate error that exists between the movement locus of cutter reality and the theoretical CC track is δ, and then cutting step length AB can be calculated as follows:
Wherein, k
fCurvature for tool track contact point place;
2) cutter spacing data computing
The cutter spacing data comprise the calculating central position O and cutter axis orientation (unit vector) l of cutter, and the calculating of cutter spacing is relevant with the geomery of cutter, and for the drum-taper type cutter tool, cutter spacing is calculated as follows:
1. the calculating of generating tool axis vector l
The initial position of generating tool axis vector is a vector b, and at this moment, it is the center with an O ' that α=β=0 at first makes cutter, and around vector f anglec of rotation α, making cutter again is the center with a C, around the vector n anglec of rotation-β; If generating tool axis vector is from the vector l of inceptive direction b behind vector f anglec of rotation α
1Then
l
1=b·cosα+n·sinα
Generating tool axis vector l
1Around vector n rotation-β angle, can obtain the final direction vector l of cutter shaft, have
l=l
1·cosβ-n×l
1·sinβ+n·(l
1·n)·(1-cosβ) (6)
2. the calculating of cutter computer center
Cutter calculates the change situation of center cutter before and after vector f anglec of rotation α; Wherein, some O ' is the center of circle of Tool in Cutting surface of revolution bus, some O
1Be the computer center of cutter initial position, some O
2Computer center for cutter behind the anglec of rotation α;
If vector O ' O
1Behind vector f anglec of rotation α is O ' O
2, vector O ' O
2After vector n rotation-β angle is vector O ' O, then pass through rotation transformation after, the final computer center's point O of cutter is
O=O '+O ' O (7) is promptly:
O′=C+n·R,O
1=C+n·(d
c/2)
Then
O′O
1=n·(d
c/2-R) (8)
Vector O ' O
2O ' O is respectively with vector
O′O
2=O′O
1·cosα+f×O′O
1·sinα (9)
O′O=O′O
2·cosβ-n×O′O
2·sinβ+n·(O′O
2·n)·(1-cosβ) (10)
With formula (8) substitution formula (9), formula (9) substitution formula (10) can be tried to achieve O ' O,, can try to achieve final computer center's point O of cutter again with formula (10) substitution formula (7).
Formula (6) and formula (7) have been determined the O of computer center of cutter axis orientation l and cutter respectively, and (O l) determines the cutter spacing data thus.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB021395829A CN1186157C (en) | 2002-12-05 | 2002-12-05 | Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB021395829A CN1186157C (en) | 2002-12-05 | 2002-12-05 | Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1413790A true CN1413790A (en) | 2003-04-30 |
CN1186157C CN1186157C (en) | 2005-01-26 |
Family
ID=4750154
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB021395829A Expired - Fee Related CN1186157C (en) | 2002-12-05 | 2002-12-05 | Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1186157C (en) |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102591260A (en) * | 2012-02-15 | 2012-07-18 | 西北工业大学 | Method for judging transient contact region of cutter and workpiece in five-axis milling process |
CN102581360A (en) * | 2012-03-22 | 2012-07-18 | 沈阳飞机工业(集团)有限公司 | Method for processing complex curved surface by numerical control processing progressive interpolation |
CN102649178A (en) * | 2012-05-17 | 2012-08-29 | 西安交通大学 | Five-axis solid milling efficient rough machining method of free-form surface centrifugal compressor impeller |
CN103157842A (en) * | 2011-12-16 | 2013-06-19 | 贵州永红航空机械有限责任公司 | Five-shaft milling method for complex curved surface |
CN103302340A (en) * | 2012-03-16 | 2013-09-18 | 沈阳飞机工业(集团)有限公司 | Numerical control machining progressive interpolation method |
CN103760817A (en) * | 2014-01-20 | 2014-04-30 | 北京航空航天大学 | Method for designing shape and size of generatrix of drum cutter |
CN105252053A (en) * | 2015-11-16 | 2016-01-20 | 重庆胜利工业(集团)有限公司 | Automatic milling machine for machining quincuncial petals |
CN105358277A (en) * | 2013-05-09 | 2016-02-24 | 株式会社Ihi | Wing surface finishing method and wing component |
CN105397163A (en) * | 2015-11-01 | 2016-03-16 | 四川泛华航空仪表电器有限公司 | Method for numerical control machining of impeller by utilization of macroprogram |
CN104384586B (en) * | 2014-09-30 | 2016-08-24 | 四川泛华航空仪表电器有限公司 | The method of four-shaft numerically controlled milling machine tool processing integral wheel |
CN105965077A (en) * | 2016-06-29 | 2016-09-28 | 北京动力机械研究所 | Tangential conical drum milling cutter |
CN106334972A (en) * | 2016-09-18 | 2017-01-18 | 大连理工大学 | Method for judging cutting edge contact in ball-end mill plane machining |
CN106513804A (en) * | 2016-11-29 | 2017-03-22 | 沈阳黎明航空发动机(集团)有限责任公司 | Milling method of blade of high-temperature alloy whole blade ring |
CN106853598A (en) * | 2015-12-08 | 2017-06-16 | 华南理工大学 | A kind of cylinder emery wheel curve surface grinding method of virtual ball knife radius |
CN107272582A (en) * | 2017-06-26 | 2017-10-20 | 山东理工大学 | Five axle drum type knife radius compensation methods are post-processed based on BA types five-axle number control machine tool |
CN108176887A (en) * | 2018-01-12 | 2018-06-19 | 大连理工大学 | Drum tapered ball end milling cutter method for customizing |
CN109530768A (en) * | 2018-11-06 | 2019-03-29 | 中国航发贵州黎阳航空动力有限公司 | A kind of processing method of blade tip chamfered edge thinning area |
CN110125490A (en) * | 2019-05-17 | 2019-08-16 | 淮阴工学院 | A kind of algorithm of the full blade side edge finish-milling Niemann worm gear surface of flat taper milling cutter |
CN111771172A (en) * | 2018-02-28 | 2020-10-13 | 大金工业株式会社 | Method for manufacturing machined product, tool path calculation method, machined product, and impeller |
CN112099433A (en) * | 2020-09-17 | 2020-12-18 | 中国航空制造技术研究院 | Adjusting method for near-net-shape blade reconstructed profile tool path |
-
2002
- 2002-12-05 CN CNB021395829A patent/CN1186157C/en not_active Expired - Fee Related
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103157842A (en) * | 2011-12-16 | 2013-06-19 | 贵州永红航空机械有限责任公司 | Five-shaft milling method for complex curved surface |
CN103157842B (en) * | 2011-12-16 | 2016-05-11 | 贵州永红航空机械有限责任公司 | Complex-curved five axle milling methods |
CN102591260A (en) * | 2012-02-15 | 2012-07-18 | 西北工业大学 | Method for judging transient contact region of cutter and workpiece in five-axis milling process |
CN102591260B (en) * | 2012-02-15 | 2013-11-06 | 西北工业大学 | Method for judging transient contact region of cutter and workpiece in five-axis milling process |
CN103302340B (en) * | 2012-03-16 | 2016-04-27 | 沈阳飞机工业(集团)有限公司 | The progressive interpolation of a kind of digital control processing |
CN103302340A (en) * | 2012-03-16 | 2013-09-18 | 沈阳飞机工业(集团)有限公司 | Numerical control machining progressive interpolation method |
CN102581360A (en) * | 2012-03-22 | 2012-07-18 | 沈阳飞机工业(集团)有限公司 | Method for processing complex curved surface by numerical control processing progressive interpolation |
CN102649178B (en) * | 2012-05-17 | 2013-07-31 | 西安交通大学 | Five-axis solid milling efficient rough machining method of free-form surface centrifugal compressor impeller |
CN102649178A (en) * | 2012-05-17 | 2012-08-29 | 西安交通大学 | Five-axis solid milling efficient rough machining method of free-form surface centrifugal compressor impeller |
CN105358277A (en) * | 2013-05-09 | 2016-02-24 | 株式会社Ihi | Wing surface finishing method and wing component |
US9694430B2 (en) | 2013-05-09 | 2017-07-04 | Ihi Corporation | Wing surface finishing method and wing component |
CN103760817A (en) * | 2014-01-20 | 2014-04-30 | 北京航空航天大学 | Method for designing shape and size of generatrix of drum cutter |
CN104384586B (en) * | 2014-09-30 | 2016-08-24 | 四川泛华航空仪表电器有限公司 | The method of four-shaft numerically controlled milling machine tool processing integral wheel |
CN105397163A (en) * | 2015-11-01 | 2016-03-16 | 四川泛华航空仪表电器有限公司 | Method for numerical control machining of impeller by utilization of macroprogram |
CN105252053A (en) * | 2015-11-16 | 2016-01-20 | 重庆胜利工业(集团)有限公司 | Automatic milling machine for machining quincuncial petals |
CN106853598A (en) * | 2015-12-08 | 2017-06-16 | 华南理工大学 | A kind of cylinder emery wheel curve surface grinding method of virtual ball knife radius |
CN105965077A (en) * | 2016-06-29 | 2016-09-28 | 北京动力机械研究所 | Tangential conical drum milling cutter |
CN106334972A (en) * | 2016-09-18 | 2017-01-18 | 大连理工大学 | Method for judging cutting edge contact in ball-end mill plane machining |
CN106513804A (en) * | 2016-11-29 | 2017-03-22 | 沈阳黎明航空发动机(集团)有限责任公司 | Milling method of blade of high-temperature alloy whole blade ring |
CN106513804B (en) * | 2016-11-29 | 2019-07-05 | 中国航发沈阳黎明航空发动机有限责任公司 | A kind of high temperature alloy entirety leaf joint blade milling method |
CN107272582A (en) * | 2017-06-26 | 2017-10-20 | 山东理工大学 | Five axle drum type knife radius compensation methods are post-processed based on BA types five-axle number control machine tool |
CN108176887A (en) * | 2018-01-12 | 2018-06-19 | 大连理工大学 | Drum tapered ball end milling cutter method for customizing |
CN111771172A (en) * | 2018-02-28 | 2020-10-13 | 大金工业株式会社 | Method for manufacturing machined product, tool path calculation method, machined product, and impeller |
CN111771172B (en) * | 2018-02-28 | 2021-09-28 | 大金工业株式会社 | Method for manufacturing machined product, tool path calculation method, machined product, and impeller |
US11167360B2 (en) | 2018-02-28 | 2021-11-09 | Daikin Industries, Ltd. | Method for manufacturing processed article, tool path calculation method, processed article, and impeller |
CN109530768A (en) * | 2018-11-06 | 2019-03-29 | 中国航发贵州黎阳航空动力有限公司 | A kind of processing method of blade tip chamfered edge thinning area |
CN110125490A (en) * | 2019-05-17 | 2019-08-16 | 淮阴工学院 | A kind of algorithm of the full blade side edge finish-milling Niemann worm gear surface of flat taper milling cutter |
CN112099433A (en) * | 2020-09-17 | 2020-12-18 | 中国航空制造技术研究院 | Adjusting method for near-net-shape blade reconstructed profile tool path |
CN112099433B (en) * | 2020-09-17 | 2021-12-24 | 中国航空制造技术研究院 | Adjusting method for near-net-shape blade reconstructed profile tool path |
Also Published As
Publication number | Publication date |
---|---|
CN1186157C (en) | 2005-01-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1413790A (en) | Drum taper tool and method for side milling complex cambered centrifugal impeller using drum taper tool | |
CN1319692C (en) | Multiple-cutting-edge cutter-bit and multiple-cutting-edge cutter-bit type cutting tool | |
CN104924158B (en) | Segmented grinding method for large rotor of screw compressor | |
CN1747807A (en) | Rotatable cutting tool with cutting inserts for chip removing machining | |
CN1781635A (en) | Drill | |
CN107451382B (en) | Control method for surface appearance of high-speed cutting workpiece | |
CN111002112B (en) | Grinding track solving method for end tooth chip dividing groove of end mill | |
JP6240559B2 (en) | Drill and drill manufacturing method | |
CN110032140B (en) | Spherical cutter shaft vector planning method in five-axis machining | |
CN2801351Y (en) | Straight handle large screw angle milling cutter for christmas tree type leaf root | |
CN109597357B (en) | Numerical control programming method and device for blade rotary milling process | |
CN113204852B (en) | Method and system for predicting milling surface appearance of ball-end milling cutter | |
Chen et al. | A novel mathematical model for grinding ball-end milling cutter with equal rake and clearance angle | |
CN201558984U (en) | Helical end milling cutter with wave-shaped cutting face | |
CN103862346A (en) | Non-instantaneous-pole envelope grinding method of spiral curved surface of superfine milling cutter | |
CN1791485A (en) | Cutting tool having a wiper nose corner | |
CN106660143B (en) | The processing method of ditch portion | |
CN103543691B (en) | Be applicable to the rotating shaft method for optimizing position of free form surface high speed and high precision processing | |
CN116363312A (en) | Modeling method and system for morphology model of milling surface | |
CN114918494B (en) | Design method of instantaneous equivalent model for gear generating and grinding | |
CN1230772C (en) | Process for contour control mochining of metal blocks | |
JP3284865B2 (en) | Fillet surface forming method | |
CN112507523B (en) | Method and device for establishing twist drill model | |
CN107977502A (en) | A kind of cylindrical work screw processing section profile calculation method based on OpenGL | |
CN1147375C (en) | Radial and mixed-flow three-component blade wheel single-shaft feed milling process |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
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: 20050126 Termination date: 20100105 |