5.1 General
5.1.1
The design fatigue life is divided into a number of time periods due to
different loading conditions and due to limitation of the corrosion protection. It is
assumed that the corrosion protection (i.e. coating system) is only effective for a
limited number of years during which the structural details are protected, i.e. in-air
environment. During the remaining part of the design life as specified in Table 5, the
structural details are unprotected i.e. exposed to corrosive environment.
5.1.2
The elementary fatigue damage, given in [5.2], is the damage accumulated during a
specific loading condition (j) associated with a specific environmental condition
either protected condition, i.e. in-air environment, or unprotected condition, i.e.
corrosive environment.
The combined fatigue damage, given in [5.3], is the combination of damage
accumulated for a specific loading condition (j) for the in-air and corrosive
environment time.
Total fatigue damage, given in [5.4], is the sum of the combined fatigue damages obtained
for all loading conditions.
5.2 Elementary fatigue damage
5.2.1
The elementary fatigue damage for each fatigue loading condition (j) is to be
calculated independently for both protected in-air environment and unprotected corrosive
environment, based on the fatigue stress range obtained for the predominant load case as
follows:

where:
ND : Total number of wave cycles experienced by ship during the design
fatigue life, taken as:
ND = 31.557×106 (f0TD) / (4 log
L)
f0 : Factor taking into account time in seagoing operations excluding
time in loading and unloading, repairs, etc.
α(j) : Fraction of time in each loading condition given in Ch 9, Sec 1, Table
1 for oil tanker and in Ch 9, Sec 1, Table 3 for bulk carrier.
ΔσFS, (j) : Fatigue stress range at the reference probability level of
exceedance of 10-2, in N/mm2.
NR : Number of cycles corresponding to the reference probability of
exceedance of 10
-2.
ξ : Weibull shape parameter,
Γ(x) : Complete Gamma function.
K2 : Constant of the design S-N curve, as given in Table 2 for in-air
environment and in Table 3 for corrosive environment.
μ
(j) : Coefficient taking into account the change of
inverse slope of the S-N curve,
m,
- For in-air environment:


- For corrosive environment:
μ(j) =
1.0
γ (a,x) : Incomplete Gamma function.
Δσq : Stress range, in N/mm2, corresponding to the
intersection of the two segments of design S-N curve at N = 107 cycles, as
given in Table 2.
Δ
m : Change in inverse slope of S-N curve at N=10
7 cycles.
5.3 Combined fatigue damage
5.3.1
The combined fatigue damage in protected in-air environment and unprotected corrosive
environment for each loading condition (j) is to be calculated as follows:

where:
DE,air(j) : The elementary fatigue damage for in-air
environment for loading condition (j) given in [5.2.1].
DE,corr(j) : The elementary fatigue damage for corrosive
environment for loading condition (j) as calculated in [5.2.1].
Table 5 : Time in corrosive
environment, TC
Location of weld joint or structural detail
|
Time in corrosive environment TC,in
years
|
Water ballast tank
|
10
|
Oil cargo tank
|
Lower part (1) of bulk cargo hold and water ballast
cargo hold
|
Bulk cargo hold and water ballast cargo hold except lower part
(1)
|
5
|
Void space
Other areas
|
(1) Lower part means
cargo hold part below a horizontal level located at a distance of 300 mm
below the frame end bracket for holds of single side skin construction
or 300 mm below the hopper tank upper end for holds of double side skin
construction (see Pt 2, Ch 1, Sec 2, Figure 1).
|
5.4 Total fatigue damage
5.4.1
The total fatigue damage for all applicable loading conditions is calculated as
follows:

where:
D(j) : Combined fatigue damage for each applicable loading condition,
as given in [5.3].
5.5 Fatigue life calculation
5.5.1 The fatigue life, TF, is taken as:

otherwise.
where:
Dair : Total fatigue damage for all loading conditions in-air
environment taken as:

Dcorr : Total fatigue damage for all loading conditions in corrosive
environment taken as:
