KISSsoft Release 03/2015 G
For Everyone Who Want to Make a Better World
File
Name
:
Unnamed
Changed by:
Maruti
on: 31.05.2016
at: 23:20:12
Important hint: At least one warning has occurred during the calculation:
1-> Calculation of scuffing:
The entered gear pair data is outside the boundary of the calculation method!
The application of ISO/TR 13989-2 has following limitations:
1.0 m/s <= v(=0.4 m/s) <= 50.0 m/s
CALCULATION OF A HELICAL GEAR PAIR
Drawing or article number:
Gear 1:
0.000.0
Gear 2:
0.000.0
Calculation method
ISO 6336:2006 Method B
------- GEAR 1 -------- GEAR 2 --
Power (kW)
Speed (1/min)
Torque (Nm)
Application factor
Required service life (h)
Gear driving (+) / driven (-)
Working flank gear 1: Right flank
[P]
[n]
[T]
[KA]
[H]
5.000
100.0
477.5
66.7
716.2
1.25
+
20000.00
-
1. TOOTH GEOMETRY AND MATERIAL
(geometry calculation according to
DIN 3960:1987)
------- GEAR 1 -------- GEAR 2 -Center distance (mm)
[a]
91.500
Centre distance tolerance
ISO 286:2010 Measure js7
Normal module (mm)
[mn]
3.5000
Pressure angle at normal section (°)
[alfn]
20.0000
Helix angle at reference circle (°)
[beta]
15.0000
Number of teeth
[z]
20
30
Facewidth (mm)
[b]
23.00
23.00
Hand of gear
right
left
Accuracy grade
[Q-ISO 1328:1995]
6
6
Inner diameter (mm)
[di]
0.00
0.00
Inner diameter of gear rim (mm)
[dbi]
0.00
0.00
Material
Gear 1:
Gear 2:
Type of profile modification:
none (only running-in)
Tip relief (µm)
[Ca]
2.0
2.0
Lubrication type
Type of oil
Lubricant base
Kinem. viscosity
2/10
oil bath lubrication
Oil: ISO-VG 220
Mineral-oil base
oil at
40 °C (mm²/s)
[nu40]
220.00
Kinem. viscosity
oil at 100 °C (mm²/s)
FZG test A/8.3/90 (
ISO 14635-1:2006)
Specific density at 15 °C (kg/dm³)
Oil temperature (°C)
[nu100]
[FZGtestA]
[roOil]
[TS]
17.50
12
0.895
70.000
Working pressure angle at normal section (°)
Helix angle at operating pitch circle (°)
Base helix angle (°)
Reference centre distance (mm)
Sum of profile shift coefficients
Profile shift coefficient
Tooth thickness (Arc) (module) (module)
Tip alteration (mm)
Reference diameter (mm)
Base diameter (mm)
Tip diameter (mm)
(mm)
Tip diameter allowances (mm)
Tip form diameter (mm)
(mm)
Active tip diameter (mm)
Active tip diameter (mm)
Operating pitch diameter (mm)
(mm)
Root diameter (mm)
Generating Profile shift coefficient
Manufactured root diameter with xE (mm)
Theoretical tip clearance (mm)
Effective tip clearance (mm)
Active root diameter (mm)
(mm)
Root form diameter (mm)
(mm)
Reserve (dNf-dFf)/2 (mm)
Addendum (mm)
(mm)
Dedendum (mm)
(mm)
Roll angle at dFa (°)
Roll angle to dNa (°)
Roll angle to dNf (°)
Roll angle at dFf (°)
Tooth height (mm)
Virtual gear
no. of teeth
Normal-tooth thickness at tip circle (mm)
(mm)
Normal-tooth thickness on tip form circle (mm)
(mm)
Normal space width at root circle (mm)
(mm)
Max. sliding velocity at tip (m/s)
Specific sliding at the tip
Specific sliding at the root
Mean specific sliding
Sliding factor on tip
Sliding factor on root
Pitch on reference circle (mm)
Base pitch (mm)
Transverse pitch on contact-path (mm)
Lead height (mm)
Axial pitch (mm)
Length of path of contact (mm)
Length T1-A, T2-A (mm)
Length T1-B (mm)
Length T1-C (mm)
Length T1-D (mm)
Length T1-E (mm)
Length T1-T2 (mm)
Diameter of single contact point B (mm)
Diameter of single contact point D (mm)
Addendum contact ratio
Minimal length of contact line (mm)
Nominal circum. force at pitch circle (N)
Axial force (N)
Radial force (N)
Normal force (N)
Nominal circumferential force per mm (N/mm)
Only as information: Forces at operating pitch circle:
Nominal circumferential force (N)
Axial force (N)
Radial force (N)
Circumferential speed reference circle (m/s)
Circumferential speed operating pitch circle (m/s)
Resonance speed (min-1)
[nE1]
Resonance ratio (-)
[N]
Subcritical range
Running-in value (µm)
[ya]
Bearing distance l of pinion shaft (mm)
[l]
Distance s
of pinion shaft (mm)
[s]
Outside diameter of pinion shaft (mm)
[dsh]
Load in accordance with Figure 13, ISO 6336-1:2006
[-]
0:a), 1:b), 2:c), 3:d), 4:e)
Coefficient K' according to Figure 13, ISO 6336-1:2006
[K']
Without support effect
Tooth trace deviation (active) (µm)
[Fby]
from deformation of shaft (µm)
[fsh*B1]
(fsh (µm) = 5.94, B1= 1.00, fHb5 (µm) = 6.00)
Tooth without tooth trace modification
Position of Contact pattern: favorable
from production tolerances (µm)
[fma*B2]
(B2=
1.00)
Tooth trace deviation, theoretical (µm)
[Fbx]
Running-in value (µm)
[yb]
Dynamic factor
Integral temperature-criteria
Lubricant factor
Tooth mass temperature (°C)
theM-C = theoil + XS*0.70*theflaint
Integral scuffing temperature (°C)
Flash factor (°K*N^-.75*s^.5*m^-.5*mm)
Running-in factor (well run in)
Contact ratio factor
Dynamic viscosity (mPa*s)
Mean coefficient of friction
Geometry factor
Meshing factor
Tip relief factor
Integral tooth flank temperature (°C)
Required safety
Safety factor for scuffing (intg.-temp.)
Safety referring to transferred torque
DIN 3967 cd25 DIN 3967 cd25
[As.e/i]
-0.070 / -0.110
Number of teeth spanned
Base tangent length (no backlash) (mm)
Actual base tangent length ('span') (mm)
(mm)
Diameter of contact point (mm)
[k]
[Wk]
[Wk.e/i]
[ΔWk.e/i]
[dMWk.m]
Theoretical diameter of ball/pin (mm)
[DM]
Eff. Diameter of ball/pin (mm)
[DMeff]
Theor. dim. centre to ball (mm)
[MrK]
Actual dimension centre to ball (mm)
[MrK.e/i]
Diameter of contact point (mm)
[dMMr.m]
Diametral measurement over two balls without clearance (mm)
[MdK]
Actual dimension over balls (mm)
[MdK.e/i]
Diametral measurement over rolls without clearance (mm)
[MdR]
Actual dimension over rolls (mm)
[MdR.e/i]
Chordal tooth thickness (no backlash) (mm)
Actual chordal tooth thickness (mm)
Reference chordal height from da.m (mm)
Tooth thickness (Arc) (mm)
(mm)
['sn]
['sn.e/i]
[ha]
[sn]
[sn.e/i]
Backlash free center distance (mm)
Backlash free center distance, allowances (mm)
dNf.i with aControl (mm)
Reserve (dNf0.i-dFf.e)/2 (mm)
Tip clearance
Centre distance allowances (mm)
Runout (µm)
Single flank composite, total (µm)
Single flank composite, tooth-to-tooth
Radial composite, total (µm)
Radial composite, tooth-to-tooth (µm)
[FrT]
[FisT]
[fisT]
[FidT]
[fidT]
(µm)
21.00
42.00
15.00
36.00
14.00
Axis alignment tolerances (recommendation acc. ISO TR 10064:1992, Quality
Maximum value for deviation error of axis (µm)
[fSigbet]
Maximum value for inclination error of axes (µm)
[fSigdel]
21.00
42.00
15.00
36.00
14.00
6)
12.00 (Fb= 12.00)
24.00
8. ADDITIONAL DATA
Weight - calculated with da (kg)
[Mass]
Total weight (kg)
[Mass]
Moment of inertia (System referenced to wheel 1):
calculation without consideration of the exact tooth shape
single gears
((da+df)/2...di) (kg*m²)
[TraeghMom]
System
((da+df)/2...di) (kg*m²)
[TraeghMom]
Torsional stiffness (MNm/rad)
[cr]
Mean coeff. of friction (acc. Niemann)
[mum]
Wear sliding coef. by Niemann
[zetw]
Gear power loss (kW)
[PVZ]
(Meshing efficiency (%)
[etaz]
0.931
1.898
2.828
0.0005059
0.002393
0.001569
0.5
1.0
0.111
0.923
0.092
98.159)
9. DETERMINATION OF TOOTH FORM
Data for the tooth form calculation :
Data not available.
10. SERVICE LIFE, DAMAGE
Required safety for tooth root
Required safety for tooth flank
[SFmin]
[SHmin]
1.40
1.00
Service life (calculated with required safeties):
System service life (h)
[Hatt]
Tooth root service life (h)
Tooth flank service life (h)
1123
[HFatt]
[HHatt]
1.168e+004
1123
Damage calculated on basis of required service life
[H] ( 20000.0 h)
F1%
F2%
H1%
H2%
171.26
569.70
1781.14
983.07
Damage calculated on basis of system service life
[Hatt] ( 1122.9 h)
F1%
9.62
REMARKS:
9/10
F2%
31.99
H1%
100.00
H2%
55.19
3511
2034
-
Specifications with
[.e/i] imply: Maximum [e] and Minimal value [i] with
consideration of all tolerances
Specifications with
[.m] imply: Mean value within tolerance
- For the backlash tolerance, the center distance tolerances and the tooth thickness
deviation are taken into account. Shown is the maximal and the minimal backlash corresponding
the largest resp. the smallest allowances
The calculation is done for the Operating pitch circle..
- Calculation of Zbet according Corrigendum 1 ISO 6336-2:2008 with Zbet = 1/(COS(beta)^0.5)
- Details of calculation method:
cg according to method B
KV according to method B
KHb, KFb according method C
fma following equation (64), fsh following (57/58), Fbx following (52/53/57)
KHa, KFa according to method B
- For the coefficients ZL, ZV, ZR, ZW, ZX, YdrelT, YRrelT and YX, the logarithmically interpolated value taken from the values for the
fatigue strength and
the static strength based on the number of load cycles is used..
End of Report