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Gear Geometry and Applied Theory Episode 2 Part 6 ppsx
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P1: GDZ/SPH P2: GDZ
CB672-15 CB672/Litvin CB672/Litvin-v2.cls February 27, 2004 0:44
15.8 Undercutting and Pointing 433
The derivation of line L is based on the following considerations:
(i) Equation (15.8.1) yields
∂rc
∂uc
duc
dt +
∂rc
∂θc
dθc
dt = −v(cσ) c . (15.8.3)
Here, ∂rc/∂uc , ∂rc/∂θc , and v
(cσ) c are three-dimensional vectors represented in system Sc of the pinion rack-cutter.
(ii) Equation (15.8.2) yields
∂ f
∂uc
duc
dt +
∂ f
∂θc
dθc
dt = − ∂ f
∂ψσ
dψσ
dt . (15.8.4)
(iii) Equations (15.8.3) and (15.8.4) represent a system of four linear equations in two
unknowns: duc/dt and dθc/dt. This system has a certain solution for the unknowns
if matrix
A =
∂rc
∂uc
∂rc
∂θc
−v
(cσ) c
∂ f
∂uc
∂ f
∂θc
− ∂ f
∂ψσ
dψσ
dt
(15.8.5)
has the rank r = 2. This yields
1 =
∂xc
∂uc
∂xc
∂θc
−v(cσ) xc
∂yc
∂uc
∂yc
∂θc
−v(cσ)
yc
∂ f
∂uc
∂ f
∂θc
− ∂ f
∂ψσ
dψσ
dt
= 0 (15.8.6)
2 =
∂xc
∂uc
∂xc
∂θc
−v(cσ) xc
∂zc
∂uc
∂zc
∂θc
−v(cσ) zc
∂ f
∂uc
∂ f
∂θc
− ∂ f
∂ψσ
dψσ
dt
= 0 (15.8.7)
3 =
∂yc
∂uc
∂yc
∂θc
−v(cσ)
yc
∂zc
∂uc
∂zc
∂θc
−v(cσ) zc
∂ f
∂uc
∂ f
∂θc
− ∂ f
∂ψσ
dψσ
dt
= 0 (15.8.8)
P1: GDZ/SPH P2: GDZ
CB672-15 CB672/Litvin CB672/Litvin-v2.cls February 27, 2004 0:44
434 Modified Involute Gears
4 =
∂xc
∂uc
∂xc
∂θc
−v(cσ) xc
∂yc
∂uc
∂yc
∂θc
−v(cσ)
yc
∂zc
∂uc
∂zc
∂θc
−v(cσ) zc
= 0. (15.8.9)
Equation (15.8.9) yields the equation of meshing f (uc , θc , ψσ ) = 0 and is not applied for investigation of singularities. The requirement that determinants 1, 2,
and 3 must be equal to zero simultaneously may be represented as
2
1 + 2
2 + 2
3 = 0. (15.8.10)
Equation (15.8.10) enables us to obtain for determination of singularities the following function:
F (uc , θc , ψσ ) = 0 (15.8.11)
NOTE. In most cases, it is sufficient for derivation of function F = 0 to use instead
of (15.8.10) only one of the three following equations:
1 = 0, 2 = 0, 3 = 0. (15.8.12)
An exceptional case, when application of (15.8.10) is required, is discussed in
Section 6.3.
Singularities of the pinion may be avoided by limitation by line L of the rack-cutter
surface c that generates the pinion. The determination of L [Fig. 15.8.1(a)] is based
on the following procedure:
(1) Using equation of meshing f (uc , θc , ψσ ) = 0, we may obtain in the plane of parameters (uc , θc ) the family of contact lines of the rack-cutter and the pinion. Each
contact line is determined for a fixed parameter of motion ψσ .
(2) The sought-for limiting line L is determined in the space of parameters (uc , θc ) by
simultaneous consideration of equations f = 0 and F = 0 [Fig. 15.8.1(a)]. Then,
we can obtain the limiting line L on the surface of the rack-cutter [Fig. 15.8.1(b)].
The limiting line L on the rack-cutter surface is formed by regular points of the rackcutter, but these points will generate singular points on the pinion tooth surface.
Limitations of the rack-cutter surface by L enable us to avoid singular points on the
pinion tooth surface. Singular points on the pinion tooth surface can be obtained by
coordinate transformation of line L on rack-cutter surface c to surface σ .
Pointing
Pointing of the pinion means that the width of the topland becomes equal to zero.
Figure 15.8.2(a) shows the cross sections of the pinion and the pinion rack-cutter. Point
Ac of the rack-cutter generates the limiting point Aσ of the pinion when singularity of
the pinion is still avoided. Point Bc of the rack-cutter generates point Bσ of the pinion
profile. Parameter sa indicates the chosen width of the pinion topland. Parameter αt
indicates the pressure angle at point Q. Parameters h1 and h2 indicate the limitation of
P1: GDZ/SPH P2: GDZ
CB672-15 CB672/Litvin CB672/Litvin-v2.cls February 27, 2004 0:44
15.9 Stress Analysis 435
(mm)
(mm)
Figure 15.8.1: Contact lines Lcσ and limiting line L: (a) in plane (uc , θc ); (b) on surface c .
location of limiting points Ac and Bc of the rack-cutter profiles. Figure 15.8.2(b) shows
functions h1(N1) and h2(N1) (N1 is the pinion tooth number) obtained for the following
data: αd = 25◦, β = 30◦, parabola coefficient of pinion rack-cutter ac = 0.002 mm−1,
sa = 0.3 m, parameter s12 = 1.0 [see Eq. (15.2.3)], and module m = 1 mm.
15.9 STRESS ANALYSIS
This section covers stress analysis and investigation of formation of bearing contact
of contacting surfaces. The performed stress analysis is based on the finite element
method [Zienkiewicz & Taylor, 2000] and application of a general computer program
[Hibbit, Karlsson & Sirensen, Inc., 1998]. An enhanced approach for application of
finite element analysis is presented in Section 9.5.