1 Minimum Power Assessment is based on the solution of a one degree-of-freedom
manoeuvring equation in longitudinal direction to demonstrate that the ship can move
with the speed of 2.0 knots through water in wind and wave directions from head to
30 degrees off-bow for a situation of weather vaning. The assessment consists of the
following steps:
-
.1 calculate the maximum total resistance in the longitudinal ship direction
over wind and wave directions from head to 30 degrees off-bow;
-
.2 calculate corresponding required brake power and rotation speed of the
installed engine, considering the resistance and propulsion characteristics
of the ship including appendages; and
-
.3 check whether the required brake power does not exceed the maximum
available brake power of the installed engine, defined according to the
engine manufacturer data at the actual rotation speed of the installed
engine.
2 The maximum total resistance is defined as sum of the resistance in calm-water at
the 2.0 knots forward speed U and the maximum added resistance in seaway
Xa over wind and wave directions from head to 30 degrees off-bow.
Requirement
3 To satisfy the requirements of Minimum Power Assessment, the required brake power in the adverse conditions at the forward speed 2.0
knots through water should not exceed the available brake power of the installed
engine in the same conditions:
≤
4 The required brake power is calculated as
-
-
where
-
nP (1/s)
|
is the propeller rotation rate in
the specified adverse conditions and the specified forward
speed;
|
Q (N⋅m)
|
is the corresponding propeller
torque;
|
ηs
|
is the mechanical transmission
efficiency of the propeller shaft, approved for the EEDI
verification;
|
ηg
|
is the gear efficiency, approved
for the EEDI verification; and
|
ηR
|
is the relative rotative
efficiency.
|
5 The available brake power in the adverse conditions at the forward speed is
defined as the maximum engine output at the actual rotation speed, taking into
account maximum torque limit, surge/air limit and all other relevant limits in
accordance with the engine manufacturer's data.
Definition of propulsion point
6 The propeller rotation rate nP and the corresponding
propeller advance ratio J in the adverse conditions at the forward speed are defined
from the propeller open-water characteristics by solving the following equation:
-
-
where
-
KT
|
is the thrust coefficient of the
propeller, defined from the propeller open-water
characteristics;
|
T (N)
|
is the required propeller
thrust;
|
ρ (kg/m3)
|
is the sea water density, ρ = 1025
kg/m3;
|
ua (m/s)
|
is the propeller advance speed;
and
|
DP (m)
|
is the propeller diameter.
|
7 The corresponding torque of the propeller is calculated as
-
-
where
-
KQ
|
is the torque coefficient of the
propeller, defined from the propeller open-water
characteristics.
|
8 The propeller advance speed ua is calculated as
-
ua = U(1 − w)
-
where
-
U (m/s)
|
is the forward speed 2.0 knots
through water; and
|
W
|
is the wake fraction.
|
Definition of required propeller thrust
9 The required propeller thrust T is defined from the equation
-
-
where
-
Xs (N)
|
is the resistance in calm-water at
the forward speed including resistance due to
appendages;
|
Xa (N)
|
is the maximum added resistance in
seaway Xa; and
|
t
|
is the thrust deduction factor
taking into account suction force on the ship hull due to
propeller thrust.
|
Definition of calm water characteristics
10 The calm-water characteristics used for the assessment, such as calm-water
resistance, self-propulsion factors and propeller open-water characteristics, are
defined by the methods approved for EEDI verification, including:
-
.1 the calm-water resistance Xs, defined from the
following equation:
Xs = (1 + k)CF1ρSU2
where k is the form factor, CF is the frictional resistance
coefficient, ρ is sea water density, ρ = 1025 kg/m3, S is the
wetted surface area of the hull and the appendages and U is the forward
speed;
.2 the thrust deduction factor t and wake fraction w at the forward speed and
relative rotative efficiency ηR. Default conservative estimate may also be
used for thrust deduction factor and wave fraction; t=0.1 and w=0.15
respectively; and
.3 the propeller open-water characteristics KT(J) and
KQ(J).
Definition of added resistance
11 The maximum added resistance in seaway Xa is defined as sum of maximum
added resistance due to wind Xw, maximum added resistance due to waves
Xd and maximum added rudder resistance due to manoeuvring in seaway
Xr over wind and wave directions from head to 30 degrees off-bow.
Definition of wind resistance
12 The maximum added resistance due to wind Xw is calculated as
-
-
where
-
|
is the non-dimensional aerodynamic
resistance coefficient;
|
ε (degree)
|
is the apparent wind angle;
|
ρa
(kg/m3)
|
is the air density,
ρa=1.2 kg/m3;
|
vwr (m/s)
|
is the relative wind speed,
vwr=U + vwcosμ;
|
vw (m/s)
|
is the absolute wind speed, defined
by the adverse conditions in paragraph 1 of these
guidelines; and
|
AF
(m2)
|
|
13 The maximum added resistance due to wind Xw is defined as maximum over
wind directions from head ε=0 to 30 degrees off-bow ε=30.
14 The non-dimensional aerodynamic resistance coefficient is defined from wind tunnel tests or equivalent
methods verified by the Administrations or the Recognized Organizations.
Alternatively, it can be assumed with = 1.1, as the maximum over wind directions from head
to 30 degrees off-bow. If deck cranes are installed in the ship and the lateral
projected area of the deck cranes is equal to or exceeds 10% of the total lateral
projected area above the waterline of the ship, =1.4 should be assumed instead of =1.1.
Definition of added resistance due to waves
15 The maximum added resistance due to waves Xd is defined in accordance with either
-
.1 expression
-
.2 or spectral method
16 The maximum added resistance due to waves Xd is defined as
maximum over wave directions from head μ=0 to 30 degrees off-bow μ=30. The range of
peak wave periods TP applied in the assessment is from 3.6
to the greater one of 5.0 or 12.0 seconds, with the step of peak wave period
not exceeding 0.5 seconds.
17 The added resistance in short-crested irregular head waves may be regarded as the
maximum added resistance over wave directions from head to 30 degrees off-bow,
because in short-crested waves, the maximum added resistance over wave directions
from head waves to 30 degrees off-bow occurs in head waves.
18 The spreading function D(μ−μ′) is defined as cos2-directional
spreading. Alternatively, long-crested seaway may be assumed with D(μ−μ′) = 1; in
this case, the maximum added resistance due to waves Xd can be determined
by multiplying the added resistance in long-crested irregular head waves by the
correction factor 1.3, to consider that maximum of the added resistance in
long-crested waves does not always correspond to head wave direction.
19 The quadratic transfer functions of added resistance in regular waves
are defined from seakeeping tests or equivalent
methods verified by the Administrations or the Recognized Organizations.
Alternatively, the semi-empirical method specified in appendix of this document can
be used.
Definition of added rudder resistance due to manoeuvring in seaway
20 The maximum additional rudder resistance due to manoeuvring in seaway
Xr may be calculated for practicality in a simplified way as
Xr=0.03 · Ter, where Ter is the propeller thrust
excluding Xr from T.
APPENDIX TO APPENDIX 2 - SEMI-EMPIRICAL METHOD FOR QUADRATIC TRANSFER FUNCTIONS
OF ADDED RESISTANCE IN REGULAR WAVES
The method for the calculation of the quadratic transfer functions of added
resistance give in this appendix can be applied to wave directions from head to
beam. Therefore, this method can be used for obtaining the added resistance in
short-crested irregular waves of the head mean wave direction.
The quadratic transfer functions of added resistance in regular head to beam waves
X′d=, N/m2, can be calculated as a sum
X′d = X′dM + X′dR
of X′dM, the component of added resistance due to motion (radiation)
effect, and X′dR, the component of added resistance due to reflection
(diffraction) effect in regular waves.
The expression of X′dM is given as follows:
where
The expression of X′dR is given as follows:
where
-
is the added resistance due to
reflection/diffraction effect of the Siwaterline segment,
as shown in Figure 1.
-
Figure 1: Sketch of the waterline profile of a ship and related
definitions
when E1≤ β ≤ π
-
-
when π-E1 ≤ β ≤ π
-
-
when 0 ≤ β ≤ π-E2
-
-
when 0 ≤ β ≤ E2
-
-
where
-
-
ω0
|
is the
frequency of the incident wave;
|
|
is the draft
coefficient, calculated as
|
-
where for S1 and S2 segments
and for S3 and S4 segments
f(β) =