Maag, Tooth F Lank Modifications
Maag, Tooth F Lank Modifications
Maag, Tooth F Lank Modifications
For Leaders
Introduction
The gear teeth in gear-driven produc- In a torque-transmitting gear, the along the path of contact and an even
tion plants and marine main propulsion toothed parts of the rotors are sub- load distribution along the face width
units occupy very little space. However, ject to elastic deflections due to the are achieved at a certain load – usually
this very specific space, along with many tooth load. nominal load – and oil temperature in
other factors, is essential for successful spite of the all load and temperature
plant operation. Optimum, highly re- The teeth bend, the pinion and wheel influences. Moreover the teeth should
liable torque transmission between the bodies twist, bend and expand under move into and out of mesh with as little
two gear rotors by the tooth flanks is the effect of the centrifugal force. The impact as possible so as to minimize
also crucial. churning and frictional losses in the gear noise.
teeth and the frictional losses in the
Maximum-precision grinding of pure bearings heat up the gear drive com- The necessary magnitudes (degrees) of
involute tooth flanks as shown in ponents, causing additional thermal modification are relatively small. They
Figure 1 is not in itself sufficient to distortions. The mean temperature of normally amount to a few thousandths
achieve such high reliability. A contact the pinion usually settles at a higher or hundredths of a millimetre. But even
check of the mating tooth flanks on a level than that of the wheel. The tem- these small modifications substantially
contact checking stand using Prussian perature varies across the face width. improve the tooth load bearing pattern
blue would show contact over the full The temperature distribution is also in- and the safety of power transmission.
tooth height and over 100% of the fluenced by the type of tooth lubrica- The inevitable conclusion to be drawn
face width – geometrically ideal, but tion (cooling). For this reason, the the- from this is that high precision is es-
potentially disastrous in nominal opera- oretical tooth form must be modified sential in the manufacturing of tooth-
ting conditions. such that a «trapezoidal» load variation modified gears. If the tooth deviations
are roughly of the same dimensional
order as the degree of modification,
modification loses its sense.
Base cylinder helix Involute helicoid
To reap the full benefits of flank modi-
fications it is very important to accu-
rately measure the finished machined
Straight line generator gears. This involves not only measuring
pitch (single and cumulative pitch devi-
ations), but also profile and helix con-
tours.
Figure 1: Involute helicoid tooth flank surface with helix angle (bb) and base lead angle (cb)
Tooth load distribution along the path of contact
in the transverse section, profile modification
Figure 2: Deformation and meshing interference in loaded, pure involute spur gears
Figure 2 shows the interference at the
first point of contact (point A) of a pure
involute tooth form without profile
modifications. This interference is due (Root) (Tip)
to the bending deflections of teeth 1
and 2, which are in contact with each
other at point D. The resulting shock
100% Load
generates noise and may diminish the
strength of the gear teeth in all their Load
aspects, including the oil film on the
tooth flanks with the risk of scuffing at
0% Load
the tips and roots of the mating gear
teeth.
Gear driven
Figure 3 shows the profile modification
(profile diagram) of the pinion and the
«trapezoidal» tooth load distribution
obtained along the path of contact
without engagement shock by ap-
plying tip and root relief to the pinion
(A, H, I, E).
Path of contact
Tip relief
Root relief
Pinion driving
Fig. 3: Load variation & profile diagram for involute spur gears with tip & root relief
Even tooth load distribution along
the face width, lead modification
In order to obtain an even tooth load side (leading end of face width) to the The mean temperature of the pinion is
distribution along the face width (face warmer exit side (trailing end of face higher than the mean temperature of
load factor KHß, KFß close to unity) a lead width). The side faces of the rotors, the mating gear-wheel. This tempera-
modification is always applied to the especially the larger side face of the ture difference causes a pitch difference
pinion to compensate for the bending gear-wheel, have a cooling effect. between between the pinion and gear-
and torsional deflections and thermal wheel which should be compensated
distortions of the gear mesh. Careful Figure 4a shows typical measurements in the transverse section by the profile
consideration of thermal distortions is with thermocouples of the bulk tem- modification and in the axial direction
essential for gears with pitch line velo- peratures of a high speed pinion. The by the lead modification. A simple rule
cities above approximately 80 m/s. resulting thermal tooth flank distor- exists for the axial pitch difference.
tions of the pinion and wheel have an
Those distortions originate from heat asymmetric barrel shape (figure 4b). If the pinion is driving (reduction gear)
arising from the power loss in the heavy tooth contact occurs at the trail-
meshing zone caused by the displace- ing end of the face width; if the pinion
ment of the air / oil mixture out of the is driven (increasing gear) heavy tooth
tooth spaces. In a helical gear this dis- contact occurs on the leading end of
placement moves along the face width the face width.
(screw pump effect) from the cooler
Gear-wheel Gear-wheel
Figure 4b: Gear contact at nominal speed with / without lead modification
Pinion, face width in mm
100 100
Torque [%] 50
0 Torque [%]
0
even tooth load Pinion driving
distribution
even tooth load even tooth load
distribution distribution
Bending deflection
Torsional deflection
Torsional deflection
Figure 5: Single helical gear – deflection, thermal distortion and lead modification Figure 6: Double helical gear – deflection, thermal distortion and lead modification
Marine gears with special low noise re- Figure 9 shows the actual deflections
quirements operate mainly under part- and thermal distortions of a MAAG high-
load conditions. speed turbo gear with a pitch line velo-
city of approximately 170 m/s. At this
Figures 7 and 8 show the lead modifi- high speed the thermal distortions exert
cation of a single helical and a double a major influence in absolute terms.
helical marine gear. The advantage of
the single helical gear, which stems Figure 9 also shows the resulting lead
from the extremely long tooth contact modification and the tooth bearing pat-
over the net face width – even at no terns of the working and non-working
load – is clearly visible. flanks as obtained during contact check-
ing with Prussian blue and used to align
the gear, as well as the full-load, full-
speed bearing pattern checked with
Dykem Red.
1410
ø 637.03
ø 560
55 55 55 55
0.031
Figure 7: Lead modification of a single helical marine gear Figure 8: Lead modification of a double helical marine gear
Concluding statement
Representatives worldwide
MAAG Gear AG
Sulzer-Allee 46
P.O.Box 65
CH-8404 Winterthur
Switzerland
Tel. +41 (0) 52 26 28 888
Fax +41 (0) 52 26 28 707
maag-gear@maag-gear.ch
www.maag-gear.com
Printed in Switzerland.