Section 3 Design
Clasification Society 2024 - Version 9.40
Clasifications Register Rules and Regulations - Rules and Regulations for the Classification of Ships, July 2022 - Part 5 Main and Auxiliary Machinery - Chapter 5 Gearing - Section 3 Design

Section 3 Design

3.1 Symbols

3.1.1 For the purposes of this Chapter the following symbols apply:

a = centre distance, in mm
b = face width, in mm
d = reference diameter, in mm
da = tip diameter, in mm
dan = virtual tip diameter, in mm
db = base diameter, in mm
dbn = virtual base diameter, in mm
den = virtual diameter to the highest point of single tooth pair contact, in mm
df = root diameter, in mm
dfn = virtual root diameter, in mm
dn = virtual reference diameter, in mm
ds = shrink diameter, in mm
dw = pitch circle diameter, in mm
fma = tooth flank misalignment due to manufacturing errors, in μm
fpb = maximum base pitch deviation of wheel, in μm
fSh = tooth flank misalignment due to wheel and pinion deflections, in μm
fSho = intermediary factor for the determination of f Sh
gα = length of line of action for external gears, in mm:
= 0,5 + 0,5 - a sinαtw

for internal gears:

= 0,5 - 0,5 + a sinαtw
h = total depth of tooth, in mm
hao = basic rack addendum of tool, in mm
hF = bending moment arm for root stress, in mm
hW = sum of actual tooth addenda of pinion and wheel, in mm
mn = normal module, in mm
n = rev/min of pinion
q = machining allowances, in mm
qs = notch parameter
q' = intermediary factor for the determination of
u = gear ratio = ≥ 1
v = linear speed at pitch circle, in m/s
x = addendum modification coefficient
yα = running in allowance, in μm
yβ = running in allowance, in μm
z = number of teeth
zn = virtual number of teeth
=
Cγ = tooth mesh stiffness (mean total mesh stiffness per unit face width), in N/mm μm
Ft = nominal tangential tooth load, in N
= 19,098 x 106
Fβ = total tooth alignment deviation (maximum value specified), in μm
Fβx = actual longitudinal tooth flank deviation before running in, in μm
Fβy = actual longitudinal tooth flank deviation after running in, in μm
HV = Vickers hardness number
KA = application factor
K = transverse load distribution factor
K = longitudinal load distribution factor
K = transverse load distribution factor
K = longitudinal load distribution factor
Kv = dynamic factor
K = dynamic factor for spur gears
K = dynamic factor for helical gears
Kγ = load sharing factor
P = transmitted power, in kW
Pr = radial pressure at shrinkage surface, in N/mm2
Pro = protuberance of tool, in mm
Ra = surface roughness − arithmetical mean deviation (C.L.A.) as determined by an instrument having a minimum wavelength cut-off of 0,8 mm and for a sampling length of 2,5 mm, in μm
Spr = residual undercut left by protuberance in mm
SF min = minimum factor of safety for bending stress
SFn = tooth root chord in the critical section, in mm
SH min = minimum factor of safety for Hertzian contact stress
SR = rim thickness of gears, in mm
YB = rim thickness factor
YD = design factor
YDT = deep tooth factor
YF = tooth form factor
YR rel T = relative surface finish factor
YS = stress correction factor
YST = stress correction factor (relevant to the dimensions of the standard reference test gears)
Yx = size factor
Yβ = helix angle factor
Yδ rel T = relative notch sensitivity factor
ZE = material elasticity factor
ZH = zone factor
ZR = surface finish factor
ZV = velocity factor
ZX = size factor
Zβ = helix angle factor
= contact ratio factor
αen = pressure angle at the highest point of single tooth contact, in degrees
αn = normal pressure angle at reference diameter, in degrees
αt = transverse pressure angle at reference diameter, in degrees
αtw = transverse pressure angle at pitch circle diameter, in degrees
αF en = angle for application of load at the highest point of single tooth contact, in degrees
β = helix angle at reference diameter, in degrees
βb = helix angle at base diameter, in degrees
γ = intermediary factor for the determination of f Sh
α = transverse contact ratio
=
αn = virtual transverse contact ratio
β = overlap ratio
= total contact ratio
ρao = tip radius of tool, in mm
ρc = relative radius of curvature at pitch point, in mm
ρF = tooth root fillet radius at the contact of the 30° tangent, in mm
σy = yield or 0,2 per cent proof stress, in N/mm2
σB = ultimate tensile strength, in N/mm2
σF = bending stress at tooth root, in N/mm2
σF lim = endurance limit for bending stress in N/mm2
σFP = allowable bending stress at the tooth root, in N/mm2
σH = Hertzian contact stress at the pitch circle, in N/mm2
σH lim = endurance limit for Hertzian contact stress, in N/mm2
σHP = allowable Hertzian contact stress, in N/mm2

Subscript:

1 = pinion
2 = wheel
0 = tool.

3.2 Tooth form

3.2.1 The tooth profile in the transverse section is to be of involute shape, and the roots of the teeth are to be formed with smooth fillets of radii not less than 0,25m n.

3.2.2 All sharp edges left on the tips and ends of pinion and wheel teeth after hobbing and finishing are to be removed.

3.3 Tooth loading factors

3.3.1 For values of application factor, K A see Table 5.3.1 Values of K A .

Table 5.3.1 Values of K A

Main and auxiliary gears K A
Main propulsion engine reduction gears:  
  Hydraulic coupling or equivalent on input 1,10
  High elastic coupling on input 1,30
  Other coupling 1,50
Auxiliary gears:  
  Electric and engine drives with hydraulic
coupling or equivalent on input
1,00
  Engine drives with high elastic coupling
on input
1,20
  Engine drives with other couplings 1,40

3.3.2 Load sharing factor, Kγ. When a gear drives two or more mating gears where the total transmitted load is not evenly distributed between the individual meshes, a factor, K γ, is to be applied. K γ is defined as the ratio between the maximum load through an actual path and the evenly shared load. This is to be determined by measurements. Where a value cannot be determined in such a way, the values in Table 5.3.2 Values of K y may be considered:

Table 5.3.2 Values of K y

  K y
Spur Gear 1,0
Epicyclic Gears  
  • Up to 3 planetary gears
1,0
  • 4 planetary gears
1,2
  • 5 planetary gears
1,3
  • 6 planetary gears and over
1,4

3.3.3 Dynamic factor, K v, is to be calculated as follows when all the following conditions are satisfied:

  • spur gears (β = 0°) and helical gears with β ≤ 30°
  • pinion with relatively low number of teeth, z1 < 50
  • solid disc wheels or heavy steel gear rim

Or this method may also be applied to all types of gears if:

And to helical gears where β > 30°

  1. For spur gears and for helical gears with ∊β ≥ 1:

    Where K A F t/b is less than 100 N/mm, the value 100 N/mm is to be used.

    Numerical values for the factor K 1 are to be as specified in the Table 5.3.3 Values of K 1 .

    Table 5.3.3 Values of K 1

      K 1
    ISO accuracy Grade
      3 4 5 6 7 8
    Spur Gears 2,1 3,9 7,5 14,9 26,8 39,1
    Helical Gears 1,9 3,5 6,7 13,3 23,9 34,8

    For all accuracy grades the factor K2 is to be in accordance with the following:

    • for spur gears K2 = 0,0193
    • for helical gears K2 = 0,0087

    Factor K 3 is to be in accordance with the following:

  2. For helical gears with overlap ratio ∊β < 1, the value Kv is to be determined by linear interpolation between values determined for spur gears (K) and helical gears (K) in accordance with:

    K v = K – ∊ β (KK )

    K is the Kv value for spur gears, in accordance with (a)

    K is the Kv value for helical gears, in accordance with (b)

3.3.4 Longitudinal load distribution factors, K and K:

Calculated values of K > 2 are to be reduced by improved accuracy and helix correction as necessary:

where
F βy = Fβxyβ and
Fβx = 1,33 fSh + fma
f ma = 2/3 Fβ at the design stage, or
f ma = 1/3 Fβ where helix correction has been applied
fSh = where
fSho = 23γ10−3 μm mm/N for gears without helix correction and without end relief, or
= 16γ10−3 μm mm/N for gears without helix correction but with end relief, where
γ = for single helical and spur gears
= for double helical gears

The following minimum values are applicable, these also being the values where helix correction has been applied:

fSho = 10 x 10−3 μm mm/N for helical gears, or
= 5 x 10−3 μm mm/N for spur gears

For through-hardened steels and surface hardened steels running on through-hardened steels:

For surface hardened steels, when

yβ = 0,15Fβx
  • yβ ≤ 6 μm
K Fβ = KHβn
where
n =

Note 1. is to be taken as the smaller of

Note 2. For double helical gears is to be substituted for b in the equation for n.

3.3.5 Transverse load distribution factors, KHα and KFα

  1. Values K and K for gears with total contact ratio ∊γ ≤ 2

  2. Values K and K for gears with total contact ratio ∊γ > 2

    Limiting conditions for K

    If K > when calculated in accordance with (a) or (b), then K =

    If K< 1 when calculated in accordance with (a) or (b), then K= 1

    Limiting conditions for K:

    If K > when calculated in accordance with (a) or (b), then K

    If K < 1 when calculated in accordance with (a) or (b), then K = 1

where

When tip relief is applied fpb is to be half of the maximum specified value:

yα = for through-hardened steels, when
  • yα μm and
yα = 0,075 fpb for surface hardened steels, when
  • yα ≤ 3 μm

When pinion and wheel are manufactured from different materials:

yα =

3.3.6 Tooth mesh stiffness, C γ:

Cγ =
where
q' =

For internal gears z n2 = ∞

Other calculations methods for C γ will be specially considered.

3.4 Tooth loading for surface stress

3.4.1 The Hertzian contact stress, σH, at the pitch circle is not to exceed the allowable Hertzian contact stress, σHP.

where
ZH =
ZE = 189,8 for steel

Z, contact ratio factor is to be calculated as follows:

for helical gears:

Z = for < 1 and
Z = for ≥ 1

for spur gears:

Zβ =
ZR =

where

The peak-to-valley roughness determined for the pinion Rz1 and for the wheel R z2 are mean values for the peak-to-valley roughness Rz measured on several tooth flanks.

relative radius of curvature:

where:

For internal gears, db has a negative sign.

If Ra, the surface roughness of the tooth flanks is given then the following approximation may be applied:

CZR is to be taken from Table 5.3.4 Values of CZR .

For values of Zx, see Table 5.3.5 Values of Zx

σH lim, see Table 5.3.6 Values of endurance limit for Hertzian contact stress, σH lim

S H min, see Table 5.3.7 Factors of safety.

Table 5.3.4 Values of CZR

σH lim C ZR
σHlim < 850 N/mm2 0,1500
850 N/mm2 ≤ σH lim ≤ 1200 N/mm2 = 0,32-0,0002 σHlim
σHlim>1200 N/mm2 0,080

Table 5.3.5 Values of Zx

Pinion heat treatment Zx
Carburised andinduction-hardened
  • mn≤ 10
  • 10 < mn < 30
  • 30 ≤ m n
  • 1,00
  • 1,05 - 0,005mn
  • 0,9
Nitrided
  • m n < 7,5
  • 7,5 < mn < 30
  • 30 ≤ mn
  • 1,00
  • 1,08 - 0,011mn
  • 0,75
Through- hardened All modules 1,00

Table 5.3.6 Values of endurance limit for Hertzian contact stress, σH lim

Heat treatment σH lim N/mm2
Pinion Wheel
Through-hardened Through-hardened 0,46σB2 + 255
Surface-hardened Through-hardened 0,42σB2 + 415
Carburised, nitrided orinduction-hardened Soft bath nitrided(Tufftrided) 1000
Carburised, nitrided orinduction-hardened Induction-hardened 0,88 HV2 + 675
Carburised ornitrided Nitrided 1300
Carburised Carburised 1500

Table 5.3.7 Factors of safety

  SH min SF min
Main propulsion gears 1,4 1,8
Auxiliary gears 1,15 1,40

3.5 Tooth loading for bending stress

3.5.1 The bending stress at the tooth root, σF is not to exceed the allowable tooth root bending stress σFP

For values of SF min, see Table 5.3.7 Factors of safety

σF lim, see Table 5.3.8 Values of endurance limit for bending stress, σF lim

Stress correction factor Y ST = 2.

3.5.2 Tooth form factor, Y F:

where h F, αF en and SFn are shown in Figure 5.3.1 Normal tooth section.

where
v = tan v –H
G = + x
H =
E = mn - hao tan αn + - (1 - sinαn)

E, hao, αn, Spr and ρao are shown in Figure 5.3.2 External tooth forms

where
dan = d n + d a - d
dn =
dbn = dn cos αn
εan =
γe = + inv. αn - inv. αen
where
αen = arc cos
=
where
αF en = αen − γe.

Table 5.3.8 Values of endurance limit for bending stress, σF lim

Heat treatment σF lim N/mm2
Through-hardened carbon steel 0,09σB + 150
Through-hardened alloy steel 0,1σB + 185
Soft bath nitrided (Tufftrided) 330
Induction hardened 0,35 HV + 125
Gas nitrided 390
Carburised A 450
Carburised B 410

Note 1. A is applicable for Cr Ni Mo carburising steels.

Note 2. B is applicable for other carburising steels.

3.5.3 For internal tooth forms the form factor is calculated, as an approximation, for a substitute gear rack with the form of the basic rack in the normal section, but having the same tooth depth as the internal gear:

where αF en is taken as being equal to αn

d en2 is calculated as d en for external gears, and

d fn = d − d fd n.

Figure 5.3.1 Normal tooth section

3.5.4 Stress concentration factor, Ys

where
L =
qs =

when qs< 1 the value of Ys is to be specially considered.

The formula for Ys is applicable to external gears with αn = 20° but may be used as an approximation for other pressure angles and internal gears.

3.5.5 Helix angle factor Yβ

but Y b ≥ 1 − 0,25 εb ≥ 0,75.

Figure 5.3.2 External tooth forms

3.5.6 Rim thickness factor, YB

Factor YB is to be determined as follows:

  1. For external gears

    If SR/h ≥ 1,2 then YB = 1

    If 0,5 < SR/h <1,2 then YB = 1,6∙ln

    Where

    SR = rim thickness of external gears, mm

    The case SR/h ≤ 0,5 is to be avoided.

  2. For internal gears

    If SR/m n ≥ 3,5 then YB = 1

    If 1,75 < SR/mn <3,5 then YB = 1,15∙ln

    where

    SR = rim thickness of internal gears, mm

    The case SR /mn ≤ 1,75 is to be avoided.

3.5.7 Deep tooth factor YDT

The deep tooth factor, YDT, adjusts the root stress to take into account high precision gears and contact ratios within the range of virtual contact ratio 2,05 ≤ ∊αn ≤ 2,05 where:

Factor YDT is to be determined from Table 5.3.9 Values of deep tooth factor, Y DT :

Table 5.3.9 Values of deep tooth factor, Y DT

  Y DT
ISO Accuracy Grade ≤ 4 and ∊αn > 2,5 0,7
ISO Accuracy Grade ≤ 4 and 2,05< ∊αn ≤ 2,5 2,366– 0,666⋅∊αn
In all other cases 1,0

3.5.8 Relative notch sensitivity factor, Yδ rel T

ρ’ = slip-layer thickness is to be taken from Table 5.3.10 Slip-layer thickness, ρ’

Table 5.3.10 Slip-layer thickness, ρ’

Material ρ’, (mm)
Case-hardened steels, flame or induction-hardened steels 0,0030
  500 N/mm2 0,0281
Through-hardened steels, yield point R e = 600 N/mm2 0,0194
  800 N/mm2 0,0064
  1000 N/mm2 0,0014
Nitrided steels 0,1005
Note: The given values of ρ’ can be interpolated for values of R e not stated above

3.5.9 Relative surface finish factor, YR rel T

YR rel T = 1,674 − 0,529 (6Ra + 1)0,1for through-hardened, carburised and induction hardened steels, and
YR rel T = 4,299 − 3,259 (6R a + 1)0,005for nitrided steels.

3.5.10 Size factor, Y x

Yx = 1,00, when m n ≤ 5
Yx = 1,03 − 0,006m n for through hardened steels
Yx = 0,85, when m n ≥ 30
Yx = 1,05 − 0,01m n for surface-hardened steels
Yx = 0,80, when m n ≥ 25.

3.5.11 Design factor, YD

YD = 0,83 for gears treated with a controlled shot peening process
YD = 1,5 for idler gears
YD = 1,25 for shrunk on gears, or
YD = 1 + , otherwise
YD = 1,00.

3.6 Factors of safety

3.6.1 Factors of safety are shown in Table 5.3.7 Factors of safety.

3.7 Design of enclosed gear shafting

3.7.1 This sub-Section is applicable to solid shafting enclosed within the gearcase of single input/single output gearing. Alternative configurations and hollow shaft designs, final gear wheel shafts and thrust shafts are to be in accordance with Pt 5, Ch 6, 3.3 Final gear wheel shafts and Pt 5, Ch 6, 3.4 Thrust shafts respectively.

3.7.2 The diameter of the enclosed gear shafting adjacent to the pinion or wheel is to be not less than the greater of db or dt, where:

= where
S b = 45 + 0,24 (σu – 400) and
S s = 42 + 0,09 (σu – 400)
L = span between shaft bearing centres, in mm
α n = normal pressure angle at the gear reference diameter, in degrees
β = helix angle at the gear reference diameter, in degrees
d w = pitch circle diameter of the gear teeth, in mm
σ u = specified minimum tensile strength of the shaft material, in N/mm2.

Note P in kW and R in rpm are as defined in Pt 5, Ch 1, 3.3 Power ratings.
Numerical value used for σu is not to exceed 800 N/mm2 for gear and thrust shafts.

3.7.3 For the purposes of the above it is assumed that the pinion or wheel is mounted symmetrically spaced between bearings.

3.7.4 Outside a length equal to the required diameter at the pinion or wheel, the diameter may be reduced, if applicable, to that required for dt.

3.7.5 For bevel gear shafts, where a bearing is located adjacent to the gear section, the diameter of the shaft is be not less than dt. Where a bearing is not located adjacent to the gear the diameter of the shaft will be specially considered.


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