Digital true tooth surface modelling method of spiral bevel gear.
Shuai, Mo ; Yidu, Zhang
1. Introduction
Spiral bevel gear have been found widely used in helicopter, truck
transmissions and reducers for transformation of rotation and torque
between intersected axes. Design of spiral bevel gear has been a topic
of research by many scholars both in home and abroad. Obscure
mathematical theory of spatial mesh of spiral bevel gear, complex
machining method, and numerous parameters involved in machining
processing, make it difficult to establish the precisely digital true
tooth surface. So many papers only discussed standard spherical involute
tooth surface. In order to study the CAM technology and CAE technology
for stress analysis of spiral bevel gear, obtain the digital true tooth
surface are much needed.
Many scholars all over the world have studied spiral bevel gear
technology [1-14]. Their research methods for spiral bevel gear modeling
can be concluded as the followed. Establish the equation of spherical
involute based on geometric parameters of spiral bevel gear via
mathematical methods, get the spherical involute curve via inputting
equation into a CAD software or programming, and then scan or loft for
the tooth surface [1-3]. Take advantage of ready-made commercial
software, like the plug-in of UG to build spiral bevel gear, to
automatically get the three-dimensional model by inputting basic
parameters [4]. Obtain discrete point coordinates of tooth surface from
Gleason Summary of Machine Settings, and then import them into a CAD
software [5]. Calculate a set of coordinates of discrete points of the
standard tooth surface through programming numerical values, and import
those points into a CAD software for the tooth surface. These research
results are of great significance under the given research phase.
In order to accurately grasp the effects of machining adjustment
parameters on tooth surface error, tooth contact, and transmission
error, it is an unavoidable task to seek a new method to model the true
tooth surface. Modeling tooth surface with spherical involute, obviously
treats the tooth surface as a standard involute tooth surface, taking
for granted that all tooth surfaces are the same in view of the basic
geometric parameters. As a matter of fact, the tooth surface of spiral
bevel gears finally processed in practical industry, is anything but the
absolutely standard spherical involute; and the tooth surface is only
partial conjugate surface instead of absolutely conjugate surface. Tooth
surfaces even with the same basic gear parameters can be different,
since various factors contribute to their precise shapes. Contact area,
transmission error and other design requirement will change tooth
surfaces by adjusting machine adjustment parameters. Meanwhile,
different designers will make various microscopic tooth surfaces, with
different machine adjustment parameters, tooth contact forces, stress
distributions and service lifespan. The former three methods failed to
take machining adjustment parameters' effects on the microscopic
tooth surface into consideration. Modeling through extracting discrete
point coordinates of tooth surface from Gleason Summary of Machine
Settings for a true tooth surface is indeed a big step forward, but it
still could not get rid of the constraints of Gleason software, Gleason
underlying algorithms and machine.
So the technology of true tooth surface precise modeling based on
machining adjustment parameters becomes a pressing need. To study the
effects of various machining adjustment parameters on tooth surface
error and property of spiral bevel gear, precise tooth surfaces based on
the given machining adjustment parameters are needed. The prerequisite
to the contrastive study of theoretic tooth surface and error surface
also lies in a precise and reliable tooth surface 3D model. Then, the
machining adjustment parameters can be changed to gain the corresponding
digitized true tooth surface, which can lay a solid basis for the
subsequent finite element analysis of gear contact and transmission
error analysis. Only in this way, are the conclusions from studies of
instructive importance and reference value to practical production. Once
the tooth surface model is not precise, all subsequent conclusions will
become unhelpful and useless.
2. Mathematical model of gear tooth surface
2.1. Machine coordinate system of gear
The gear calculated in this paper is left hand (LH), and the cutter
is mounted on the lower right of cradle during processing, so the cutter
coordinate system is set in the lower right of cradle coordinate system
as shown in Fig. 1. Subscript 2 in the coordinate system represents
Gear, and Subscript 1 represents Pinion. Coordinate systems [S.sub.m],
[S.sub.a], and [S.sub.b] are fixed coordinate systems, rigidly connected
to the machine. Coordinate systems [S.sub.2] and [S.sub.c] are movable
coordinate systems, rigidly connected to Gear and cradle. [S.sub.g] is
the cutter coordinate system of Gear, rigidly connected to [S.sub.c],
the cradle coordinate system. As shown in Fig. 2, [[PSI].sub.c] and
[[PSI].sub.2] are the current angles of rotation of cradle and gear
respectively. [DELTA][E.sub.m] stands for blank offset, [DELTA][E.sub.B]
for sliding base, [DELTA][X.sub.D] for machine center to back, [S.sub.r]
for radial setting, q for basic cradle angle, and [y.sub.m] for machine
root angle.
[FIGURE 1 OMITTED]
[FIGURE 2 OMITTED]
2.2. Equation of head-cutter surfaces
Gear is processed by generation method, using alternate blade
cutter to simultaneously produce the convex side and concave side. When
establishing the mathematical model of cutter, head-cutter is divided
into two segments a and b as shown in Fig. 3. Segment a is the straight
line part, while segment b is the fillet part. In the equations, the
superscript of matrix in equation indicates the corresponding specific
segment, and the subscript means the corresponding reference coordinate
system. For example, Eq. (1) [r.sub.g] is the vector function for cutter
surfaces of segment a; Eq. (2) [n.sub.g] is the normal vector for cutter
surfaces of segment a; Eq. (3) [r.sub.g] is the vector function for
cutter surfaces of segment b; and Eq. (6) [n.sub.g] is the normal vector
for cutter surfaces of segment b. The meanings of scalar symbols
[X.sub.[omega]], [R.sub.g], [P.sub.[omega]], [[alpha].sub.g], [R.sub.g],
[R.sub.[mu]], [P.sub.[omega]2] and [[lambda].sub.[omega]] are explained
in the corresponding figures and tables. Fig. 4 shows the generating
tool cones for the concave side and convex side.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (1)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (2)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (3)
[X.sub.[omega]] = [R.sub.g] [- or +] [[rho].sub.[omega]] (1 -sin
[[alpha].sub.g])/cos [[alpha].sub.g], (4)
[R.sub.g] = [R.sub.u] + [[P.sub.[omega]2]/2], (5)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (6)
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
The generating surfaces for the gear parabolicprofile head-cutter
are formed by rotation of the blade about [z.sub.g] of the head-cutter,
[[theta].sub.g] is the rotation angle. The apex of the parabola is
located at point M determined by parameter [S.sub.g0], called the
parabola vertex location parameter, [[alpha].sub.g] is the blade angle
at point M, [a.sub.c] is the parabola coefficient, [[rho].sub.w] is the
radius of circular arc profile of the fillet. In the case of grinding,
the profiles shown in Fig. 5 represent the axial profiles of the
grinder. Fig. 6 shows the generating surfaces of the parabolic-profile
head-cutter.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (8)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (9)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (10)
[FIGURE 5 OMITTED]
[FIGURE 6 OMITTED]
Eq. (7) [r.sub.g] is the vector function for parabolic-profile
cutter surfaces of segment a; Eq. (8) [n.sub.g] is the normal vector for
parabolic-profile cutter surfaces of segment a; Eq. (9) [r.sub.g] is the
vector function for parabolic-profile cutter surfaces of segment b; and
Eq. (10) [n.sub.g] is the normal vector for parabolic-profile cutter
surfaces of segment b. The geometrical significance of same scalar
symbols in matrix can be found in Fig. 3 to Fig. 6.
2.3. Equation of gear tooth surface
Superscript of matrix in equation indicates the corresponding
specific segment; subscript indicates the corresponding reference
coordinate system; and the symbol in the bracket indicates the variable.
For instance, [M.sub.2g] matrix represents the coordinates transferring
from [S.sub.g] to [S.sub.2]. Other transformational matrix share the
similar meaning. Eqs. (11) and (20) are the vector function transferring
from cutter coordinate system to gear coordinate system for segment a
and b. Eqs. (18) and (21) refer to the mesh conditions for Gear tooth
surface of segment a and b. Eqs. (19) and (22) mean the vector equation
for gear tooth surface of segment a and b:
[r.sup.(a).sub.2](0) ([s.sub.g], [[theta].sub.g], [[psi].sub.2]) =
[M.sub.2g] ([[psi].sub.2]) [r.sup.(a).sub.g] ([s.sub.g],
[[theta].sub.g]), (11)
[M.sub.2g] ([[psi].sub.2]) =
[M.sub.2b2][M.sub.b2a2][M.sub.a2m2][M.sub.m2c2][M.sub.c2g], (12)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (13)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (14)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (15)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (16)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (17)
([partial derivative][r.sup.(a).sub.2]/[partial
derivative][s.sub.g] [partial derivative][r.sup.(a).sub.2]/[partial
derivative][[theta].sub.g]) [partial
derivative][r.sup.(a).sub.2]/[partial derivative][[psi].sub.2] =
[f.sup.(a).sub.2g] ([s.sub.g], [[theta].sub.g], [[psi].sub.2]) = 0, (18)
[R.sup.(a).sub.2] ([[theta].sub.g], [[psi].sub.2]) =
[r.sup.(a).sub.2] ([s.sub.g]([[theta].sub.g], [[psi].sub.2]),
[[theta].sub.g], [[psi].sub.2]), (19)
[r.sup.(b).sub.2] ([[lambda].sub.[omega]], [[theta].sub.g],
[[psi].sub.2]) = [M.sub.2g] ([[psi].sub.2]) [r.sup.(b).sub.g]
([[lambda].sub.[omega]], [[theta].sub.g]), (20)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (21)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (22)
3. Mathematical model of pinion tooth surface
3.1. Machine coordinate system of pinion
Pinion is processed by the method of modified roll, using the
inside and outside blade cutters to process the concave and convex sides
of tooth surface. Pinion is RH, and the cutter is mounted on the upper
right of cradle, so the cutter coordinate system is set in the upper
right of cradle coordinate system as shown in Figs. 7 and 8. Subscript 1
in coordinate system represents pinion. Subscript p represents cutter
for pinion. Other symbols share the similar definitions with those of
gear.
[FIGURE 7 OMITTED]
[FIGURE 8 OMITTED]
3.2. Equation of head-cutter surfaces
Both the inside and outside cutters are used in the processing of
pinion, and the mathematical model for cutter is established as shown in
Figs. 9 and 10.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (23)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (24)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (25)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (26)
[FIGURE 9 OMITTED]
[FIGURE 10 OMITTED]
3.3. Equation of pinion tooth surface
Eqs. (27) and (28) are the vector function transferring from cutter
coordinate system to pinion coordinate system for segment a and b. Eqs.
(42) and (43) are the meshing equations of pinion for segment a and b,
[v.sub.m1] is the relative velocity between workpiece (pinion) and
cutter at coordinate system [S.sub.m1].
[r.sup.(a).sub.1] ([s.sub.p], [[theta].sub.p], [[psi].sub.1]) =
[M.sub.1p] ([[psi].sub.c1]) [r.sup.(a).sub.p] ([s.sub.p],
[[theta].sub.p]), (27)
[r.sup.(b).sub.1] ([s.sub.f], [[theta].sub.p], [[psi].sub.c1]) =
[M.sub.1p] ([[psi].sub.c1]) [r.sup.(b).sub.p] ([s.sub.f],
[[theta].sub.p]), 28)
[M.sub.1p] ([[psi].sub.c1]) =
[M.sub.1b1][M.sub.b1a1][M.sub.a1m1][M.sub.m1c1][M.sub.c1p], (29)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (30)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (31)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (32)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (33)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII], (34)
[[psi].sub.1] = [m.sub.1c] ([[psi].sub.1c] - C[[psi].sup.2.sub.cl]
- D[[psi].sup.3.sub.cl]), (35)
[v.sup.(a).sub.m1] = [([[omega].sup.(p).sub.m1] -
[[omega].sup.(1).sub..sub.m1]) x [r.sub.m1]] -
([bar.[o.sub.m1][o.sub.a1]] x [[omega].sup.(1).sub.m1]), (36)
[r.sub.m1] = [M.sub.m1c1][M.sub.c1p] [r.sup.(a).sub.p] ([s.sub.p],
[[theta].sub.p]), (37)
[bar.[o.sub.m1][o.sub.a1]] = [[0 -[DELTA][E.sub.m1]
[DELTA][X.sub.B1]].sup.T], (38)
[[omega].sup.(1).sub.m1] = [[cos [[gamma].sub.m1] 0
sin[[gamma].sub.m1]].sup.T], (39)
[[omega].sup.(p).sub.m1] = [[0 0 [m.sub.1c]
([[psi].sub.cl])].sup.T] , (40)
[m.sub.1c]([[psi].sub.cl]) = 1 /
[m.sub.1c](1-2C[[psi].sub.cl]-3D[[psi].sup.2.sub.cl]), (41)
[n.sup.(a).sub.ml] [v.sup.(a).sub.ml] =
[f.sup.(a).sub.1p]([s.sub.p], [[theta].sub.p], [[psi].sub.c1]) = 0, (42)
[n.sup.(b).sub.ml] [v.sup.(b).sub.m1] = [f.sup.(b).sub.1p]
([[lambda].sub.f], [[theta].sub.p], [[psi].sub.cl]) = 0. (43)
4. Machining adjustment parameters calculation
Gear is processed by generation method with alternate blade cutter,
while pinion is processed with two cutters, each processing one side of
the tooth. According to spatial mesh theory, program the mathematical
principle of the construction of the tooth surface of the above gear and
pinion, and solve the nonlinear equations. Make use of Matlab to program
and calculate the machining adjustment parameters of gear and pinion,
then put in the above parameters to get their tooth surface discrete
point clouds. Fig. 11 is the technology roadmap of tooth surface
modeling, Table 1 is design parameters of gear set; Tables 2 and 3 are
the calculated adjusting parameters for gear and pinion respectively.
[FIGURE 11 OMITTED]
5. Digital true tooth surface modeling
Fig. 12 to Fig. 15 are the process of point cloud data input to
software, Figs. 16 and 17 are the process of tooth surface modeling. The
curved surface reconstructed in the 3D software via leading point cloud
documents by means of reverse engineering, is not smooth but stitched by
many small curved surfaces, as shown in Figs. 18 and 19. A crack seems
to be in the middle of the curved surface, which not only influences the
visual effects, but also prevents contact analysis and solution in FEA,
and even contact setting. Therefore, it's necessary to adopt other
methods or approaches to deal with the reconstruction. The digitized and
high-precision true tooth surfaces under the study of this paper are
shown in Figs. 20 and 21.
[FIGURE 12 OMITTED]
[FIGURE 13 OMITTED]
[FIGURE 14 OMITTED]
[FIGURE 15 OMITTED]
[FIGURE 16 OMITTED]
[FIGURE 17 OMITTED]
[FIGURE 18 OMITTED]
[FIGURE 19 OMITTED]
[FIGURE 20 OMITTED]
[FIGURE 21 OMITTED]
6. Gear cutting experiment
To verify the technical advancement and practicability in
engineering digitized true tooth surface of spiral bevel gear based on
machining adjustment parameters, this study, gets the NC codes via NC
process simulation software from 3D model with machining adjustment
parameters and then inputs the codes to five-axis NC machine tools to
conduct gear cutting experiments. Gear cutting experiment is made in
YH606 CNC Curved Tooth Bevel Gear Generator made in China. The gear and
pinion after processing are as shown in Fig. 22.
[FIGURE 22 OMITTED]
7. Conclusion
According to the spatial meshing theory, both the machining
adjustment parameters of gear and pinion, and the discrete point clouds
of tooth surface based on machining adjustment parameters have been
calculated through programming. By establishing digitized and
high-precision true tooth surface of spiral bevel gear, and conducting
the gear cutting processing experiments on the five-axis NC machine
tools, the advancement and practicability of spiral bevel gear true
tooth surface precise modeling based on machining adjustment parameters
have been verified, which lays a solid foundation for tooth loading
contact analysis of the digitized true tooth surface and design of
non-standard spiral bevel gear in the future.
http://dx.doi.Org/10.5755/j01.mech.21.2.8397
Acknowledgment
This thesis is supported by Aeronautical Science Foundation of
China (Grant No. 20130451010), National Science, Technology Major
Project(Grant No. 2013ZX040 01061), National Key Technology Support
Program(Grant No. 2014BAF08B01), Beijing Engineering Technological
Research Center of High-efficient & Green CNC Machining Process and
Equipment funded programs (Grant No.Z141104004414067), and the
Innovation Foundation of BUAA for PhD Graduates. Thanks also go to Dr.
Wang Peng for his constant assistance in the course of the research.
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Mo Shuai *, Zhang Yidu **
* State Key Laboratory of Virtual Reality Technology and Systems,
School of Mechanical Engineering & Automation, Beihang University,
Beijing Engineering Technological Research Center of High-efficient
& Green CNC Machining Process and Equipment, Beijing 100191, China,
E-mail: moshuai2010@163.com
** State Key Laboratory of Virtual Reality Technology and Systems,
School of Mechanical Engineering & Automation, Beihang University,
Beijing Engineering Technological Research Center of High-efficient
& Green CNC Machining Process and Equipment, Beijing 100191, China,
E-mail: ydzhang@buaa.edu.cn
Received October 15, 2014
Accepted March 12, 2015
Table 1
Design parameters of gear set
Parameters Pinion Gear
Number of teeth 9 33
Module, mm 4.838 4.838
Shaft angle, [omicron] 90.0 90.0
Pressure angle, [omicron] 22.0 22.0
Hand of spiral RH LH
Mean spiral angle, [omicron] 32.0 32.0
Face width, mm 27.5 27.5
Pitch angles,[omicron] 15.2551 74.7449
Root angles,[omicron] 13.8833 69.5833
Face angles, [omicron] 20.4167 76.1167
Addendum, mm 6.64 1.76
Dedendum, mm 2.79 7.67
Clearance, mm 1.03 1.03
Table 2
Machining adjustment parameters of gear
Parameters Convex Concave
Cutter radius [R.sub.[mu]], mm 63.5 63.5
Blade angle [[alpha].sub.g], [omicron] -22.0 -22.0
Point width [P.sub.[omega]2], mm 2.54 2.54
Root filler radius [[rho].sub.[omega]], mm 1.524 1.524
Radial distance [S.sub.r2], mm 64.3718 64.37 18
Cradle angle [q.sub.2] ([omicron]) -56.78 -56.78
Blank offset [DELTA][E.sub.m2] (mm) 0 0
Sliding base [DELTA][X.sub.B2] (mm) -0.2071 -0.2071
Machine center to back [DELTA][X.sub.D2] 0 0
Machine root angle [[gamma].sub.m2], [omicron] 69.5833 69.5833
Velocity ratio [m.sub.2c2] 1.032331 1.032331
Table 3
Machining adjustment parameters of pinion
Parameters Convex Concave
Cutter radius [R.sub.p], mm 69.7529 59.9195
Blade angle [[alpha].sub.p], [omicron] -22.0 22.0
Root filler radius [[rho].sub.f], mm 0.635 0.635
Radial distance [S.sub.r1], mm 66.0406 62.7677
Cradle angle [q.sub.1], [omicron] 52.8382 59.4386
Blank offset [DELTA][E.sub.m1], mm -3.4163 4.4841
Sliding base [DELTA][X.sub.B1], mm -1.0519 -0.2013
Machine center to back [DELTA][X.sub.D1] 1.0079 -2.5371
Machine root angle [[gamma].sub.m1], [omicron] 13.8833 13.8833
Velocity ratio [m.sub.1c] 3.8726 3.6963
Modified roll coefficient C 0.00175 -0.002
Modified roll coefficient D -0.01 -0.007