Annex – 2014 Guidelines on the Method of
Calculation of the Attained Energy Efficiency Design Index (EEDI) for New Ships, as
Amended
CONTENTS
1 Definitions
2 Energy Efficiency Design Index (EEDI), including equation
-
2.1 CF ; Conversion factor between fuel consumption and
CO2 emission
-
2.2 Vref ; Ship speed
-
2.3 Capacity
-
2.3.1 Bulk carriers, tankers, gas carriers, LNG carriers, ro-ro cargo ships
(vehicle carriers), ro-ro cargo ships, ro-ro passenger ships, general cargo
ships, refrigerated cargo carrier and combination carriers
-
2.3.2 Passenger ships and cruise passenger ships
-
2.3.3 Containerships
-
2.4 Deadweight
-
2.5 P ; Power of main and auxiliary engines
-
2.5.1 PME ; Power of main engines
-
2.5.2 PPTO ; Shaft generator
-
2.5.3 PPTI ; Shaft motor
-
2.5.4 Peff ; Output of innovative mechanical energy
efficient technology
-
2.5.5 PAEeff ; Auxiliary power reduction
-
2.5.6 PAE ; Power of auxiliary engines
-
2.6 Vref, Capacity and P
-
2.7 SFC ; Specific fuel consumption
-
2.8 fj ; Correction factor for ship specific design
elements
-
2.8.1 fj ; Ice-class ships
-
2.8.2 fj ; Shuttle tankers
-
2.8.3 fjroro ; Ro-ro cargo and ro-ro passenger
ships
-
2.8.4 fj ; General cargo ships
-
2.8.5 fj ; Other ship types
-
2.9 fw ; Weather factor
-
2.10 feff ; Availability factor of innovative energy
efficiency technology
-
2.11 fi ; Capacity factor
-
2.11.1 fi ; Ice-class ships
-
2.11.2 fi ; Ship specific voluntary structural
enhancement
-
2.11.3 fi ; Bulk carriers and oil tankers under
Common Structural Rules (CSR)
-
2.11.4 fi ; Other ship types
-
2.12 fc ; Cubic capacity correction factor
-
2.12.1 fc ; Chemical tankers
-
2.12.2 fc ; Gas carriers
-
2.12.3 fcRoPax; Ro-ro passenger ships
-
2.12.4 fc bulk carriers designed to carry light
cargoes; Wood chip carriers
-
2.13 Lpp ; Length between perpendiculars
-
2.14 fl ; Factor for general cargo ships equipped
with cranes and other cargo-related gear
-
2.15 ds ; Summer load line draught
-
2.16 Bs ; Breadth
-
2.17 ▽ ; Volumetric displacement
-
2.18 g ; Gravitational acceleration
-
APPENDIX 1 A generic and simplified power plant
-
APPENDIX 2 Guidelines for the development of electric power tables for EEDI
(EPT-EEDI)
-
APPENDIX 3 A generic and simplified marine power plant for a cruise passenger ship
having non-conventional propulsion
-
APPENDIX 4 EEDI calculation examples for use of dual fuel engines
1 Definitions
1.1 MARPOL means the International Convention for the Prevention of Pollution
from Ships, 1973, as modified by the Protocols of 1978 and 1997relating thereto, as
amended.
1.2 For the purpose of these Guidelines, the definitions in chapter 4 of MARPOL Annex
VI, as amended, apply.
2 Energy Efficiency Design Index (EEDI)
The attained new ship Energy Efficiency Design Index (EEDI) is a measure of ships'
energy efficiency (g/t · nm) and calculated by the following formula:
* If part of the Normal Maximum Sea Load is provided by shaft generators,
SFCME and CFME may – for that part of the
power – be used instead of SFCAE and CFAE
** In case of PPTI(i) > 0, the average weighted value of
(SFCME · CFME) and (SFCAE ·
CFAE) to be used for calculation of Peff
Where:
| Type of fuel
|
Reference
|
Lower calorific value
(kJ/kg)
|
Carbon content
|
CF
(t-CO2/t-Fuel)
|
| 1 Diesel/Gas Oil
|
ISO 8217 Grades DMX through DMB
|
42,700
|
0.8744
|
3.206
|
| 2 Light Fuel Oil (LFO)
|
ISO 8217 Grades RMA through RMD
|
41,200
|
0.8594
|
3.151
|
| 3 Heavy Fuel Oil (HFO)
|
ISO 8217 Grades RME through RMK
|
40,200
|
0.8493
|
3.114
|
| 4 Liquefied Petroleum Gas
(LPG)
|
Propane
|
46,300
|
0.8182
|
3.000
|
| Butane
|
45,700
|
0.8264
|
3.030
|
| 5 Liquefied Natural Gas (LNG)
|
|
48,000
|
0.7500
|
2.750
|
| 6 Methanol
|
|
19,900
|
0.3750
|
1.375
|
| 7 Ethanol
|
|
26,800
|
0.5217
|
1.913
|
-
-
In case of a ship equipped with a dual-fuel main or auxiliary engine, the
CF-factor for gas fuel and the
CF-factor for fuel oil should apply and be
multiplied with the specific fuel oil consumption of each fuel at the
relevant EEDI load point. Meanwhile, gas fuel should be identified whether
it is regarded as the "primary fuel" in accordance with the formula
below:
-
-
fDFliquid = 1 - fDFgas
-
where,
-
fDFgas is the fuel availability ratio of gas fuel corrected for
the power ratio of gas engines to total engines, fDFgas should
not be greater than 1;
-
Vgas is the total net gas fuel capacity on board in
m3. If other arrangements, like exchangeable (specialized) LNG
tank-containers and/or arrangements allowing frequent gas refuelling are
used, the capacity of the whole LNG fuelling system should be used for
Vgas . The boil-off rate (BOR) of gas cargo
tanks can be calculated and included to Vgas if it
is connected to the fuel gas supply system (FGSS);
-
Vliquid is the total net liquid fuel capacity on
board in m3 of liquid fuel tanks permanently connected to the
ship's fuel system. If one fuel tank is disconnected by permanent sealing
valves, Vliquid of the fuel tank can be ignored;
-
ρgas is the density of gas fuel in
kg/m3;
-
ρliquid is the density of each liquid fuel in
kg/m3;
-
LCVgas is the low calorific value of
gas fuel in kJ/kg;
-
LCVliquid is the low calorific value
of liquid fuel in kJ/kg;
-
K gas is the filling rate for gas fuel
tanks;
-
Kliquid is the filling rate for liquid fuel tanks;
-
Ptotal
is the total installed engine power, PME
and PAE in kW;
-
Pgasfuel
is the dual fuel engine installed power, PME
and PAE in kW;
-
.1 If the total gas fuel capacity is at least 50% of the fuel capacity
dedicated to the dual fuel engines , namely fDFgas ≥ 0.5, then
gas fuel is regarded as the "Primary fuel," and fDFgas = 1 and
fDFliquid = 0 for each dual fuel engine.
-
.2 If fDFgas < 0.5, gas fuel is not regarded as the "primary
fuel." The CF and SFC in the EEDI
calculation for each dual fuel engine (both main and auxiliary engines)
should be calculated as the weighted average of CF
and SFC for liquid and gas mode, according to
fDFgas and fDFliquid, such as the original item of
PME(i)· CFME(i)
· SFCME(i) in the EEDI calculation is to be
replaced by the formula below.
-
PME(i) · (fDFgas(i)·(CFME
pilot fuel(i) · SFCME pilot fuel(i) + CFME
gas(i) · SFCME gas(i)) + fDFliquid(i) ·
CFME liquid(i) · SFCME liquid(i))
-
.2 Vref is the ship speed, measured in nautical miles per
hour (knot), on deep water in the condition corresponding to the capacity
as defined in paragraphs 2.3.1 and 2.3.3 (in case of passenger ships and
cruise passenger ships, this condition should be summer load draught as provided
in paragraph 2.4) at the shaft power of the engine(s) as defined in paragraph 2.5
and assuming the weather is calm with no wind and no waves.
-
.3 Capacity is defined as follows:
-
.1 For bulk carriers, tankers, gas carriers, LNG carriers, ro-ro cargo ships
(vehicle carriers), ro-ro cargo ships, ro-ro passenger ships, general cargo
ships, refrigerated cargo carrier and combination carriers, deadweight
should be used as capacity.
-
.2 For passenger ships and cruise passenger ships, gross tonnage in
accordance with the International Convention of Tonnage Measurement of Ships
1969, annex I, regulation 3, should be used as capacity.
-
.3 For containerships, 70% of the deadweight (DWT) should be used as
capacity. EEDI values for containerships are calculated as
follows:
-
.1 attained EEDI is calculated in accordance with the
EEDI formula using 70% deadweight for capacity.
-
.2 estimated index value in the Guidelines for
calculation of the reference line is calculated using 70% deadweight
as:
-
-
.3 parameters a and c for containerships in table 2 of
regulation 21 of MARPOL Annex VI are determined by plotting
the estimated index value against 100% deadweight i.e. a = 174.22 and
c=0.201 were determined.
-
.4 required EEDI for a new containership is calculated
using 100% deadweight as:
Required EEDI = (1-X/100) · a · 100% deadweight –c
Where X is the reduction factor (in percentage) in
accordance with table 1 in regulation 21 of MARPOL Annex VI relating to the applicable
phase and size of new containership.
-
.4 Deadweight means the difference in tonnes between the displacement of a
ship in water of relative density of 1,025 kg/m3 at the summer load
draught and the lightweight of the ship. The summer load draught should be taken
as the maximum summer draught as certified in the stability booklet approved by
the Administration or an organization recognized by it.
-
.5 P is the power of the main and auxiliary engines, measured in kW. The
subscripts ME(i) and AE(i) refer to the main
and auxiliary engine(s), respectively. The summation on i is for all
engines with the number of engines (nME) (see diagram in
appendix 1).
-
.1 PME(i) is 75% of the rated installed power
(MCRfootnote) for each main engine (i).
For LNG carriers having diesel electric propulsion system,
PME(i) should be calculated by the following
formula:

Where:
MPPMotor(i) is the rated output of motor specified
in the certified document.
η(i) is to be taken as the product of electrical
efficiency of generator, transformer, converter, and motor, taking into
consideration the weighted average as necessary.
The electrical efficiency, η(i) , should be taken
as 91.3% for the purpose of calculating attained EEDI. Alternatively, if the
value more than 91.3% is to be applied, the η(i)
should be obtained by measurement and verified by method approved by the
verifier.
For LNG carriers having steam turbine propulsion systems,
PME(i) is 83% of the rated installed power
(MCRSteamTurbine) for each steam
turbine(i).
The influence of additional shaft power take off or shaft power take in is
defined in the following paragraphs.
-
.2 Shaft generator
In case where shaft generator(s) are installed, PPTO(i)
is 75% of the rated electrical output power of each shaft
generator. In case that shaft generator(s) are installed to steam turbine,
PPTO(i) is 83% of the rated electrical output
power and the factor of 0.75 should be replaced to 0.83.
For calculation of the effect of shaft generators two options are
available:
Option 1:
.1 The maximum allowable deduction for the calculation of Σ
PME(i) is to be no more than
PAE as defined in paragraph 2.5.6. For this
case, Σ PME(i) is calculated as:

Option 2:
.2 Where an engine is installed with a higher rated power output than that
which the propulsion system is limited to by verified technical means, then
the value of Σ PME(i) is 75% of that limited power
for determining the reference speed, Vref and for
EEDI calculation. The following figure gives guidance for determination of Σ
PME(i):

-
.3 Shaft motor
In case where shaft motor(s) are installed, PPTI(i)
is 75% of the rated power consumption of each shaft motor
divided by the weighted average efficiency of the generator(s), as
follows:

Where:
PSM,max(i) is the rated power consumption of
each shaft motor
is the weighted average efficiency of the
generator(s)
In case that shaft motor(s) are installed to steam turbine,
PPTI(i) is 83% of the rated power consumption and the
factor of 0.75 should be replaced to 0.83.
The propulsion power at which Vref is measured, is:
Σ PME(i) + Σ PPTI(i), Shaft
Where:
Σ PPTI(i), Shaft = Σ (0.75
·PSM,max(i) ·
ηPTI(i))
ηPTI(i) is the efficiency of each shaft motor
installed
Where the total propulsion power as defined above is higher than 75% of the
power the propulsion system is limited to by verified technical means, then
75% of the limited power is to be used as the total propulsion power for
determining the reference speed, Vref and for EEDI
calculation.
In case of combined PTI/PTO, the normal operational mode at sea will
determine which of these to be used in the calculation.
-
.4 Peff(i) is the output of the innovative
mechanical energy efficient technology for propulsion at 75% main engine
power.
Mechanical recovered waste energy directly coupled to shafts need not be
measured, since the effect of the technology is directly reflected in the
Vref.
In case of a ship equipped with a number of engines, the CF
and SFC should be the power weighted average of all the
main engines.
In case of a ship equipped with dual-fuel engine(s), the CF
and SFC should be calculated in accordance with
paragraphs 2.1 and 2.7.
-
.5 PAEeff (i) is the auxiliary power reduction due
to innovative electrical energy efficient technology measured at
PME(i).
-
.6 PAE is the required auxiliary engine power to
supply normal maximum sea load including necessary power for propulsion
machinery/systems and accommodation, e.g. main engine pumps, navigational
systems and equipment and living on board, but excluding the power not for
propulsion machinery/systems, e.g. thrusters, cargo pumps, cargo gear,
ballast pumps, maintaining cargo, e.g. reefers and cargo hold fans, in the
condition where the ship engaged in voyage at the speed
(Vref) under the condition as mentioned in
paragraph 2.2.
-
.1 For ships with a total propulsion power
of 10,000 kW or above,
PAE is defined as:

-
.2 For ships with a total propulsion power below 10,000 kW, PAE
is defined as:

-
.3 For LNG carriers with a reliquiefaction system or compressor(s),
designed to be used in normal operation and essential to maintain the
LNG cargo tank pressure below the maximum allowable relief valve
setting of a cargo tank in normal operation, the following terms
should be added to above PAE formula in
accordance with 1, 2 or 3 as below:
-
.1 For ships having re-liquefaction system:
+ CargoTankCapacityLNG
✕ BOR ✕ COPreliquefy ✕
Rreliquefy
Where:
CargoTankCapacityLNG is the LNG Cargo Tank
Capacity in m3.
BOR is the design rate of boil-off gas of entire ship per
day, which is specified in the specification of the building
contract.
COPreliquefy is the coefficient of
design power performance for reliquefying boil-off gas per unit
volume, as follows:

COPcooling is the coefficient of design
performance of reliquefaction and 0.166 should be used. Another
value calculated by the manufacturer and verified by the
Administration or an organization recognized by the
Administration may be used.
Rreliquefy is the ratio of boil-off gas
(BOG) to be re-liquefied to entire BOG, calculated as
follows.

-
.2 For LNG carriers with direct diesel driven propulsion system
or diesel electric propulsion system, having compressor(s) which
are used for supplying high-pressured gas derived from boil-off
gas to the installed engines (typically intended for 2-stroke
dual fuel engines):

Where:
COPcomp is the design power performance
of compressor and 0.33 (kWh/kg) should be used. Another value
calculated by the manufacturer and verified by the
Administration or an organization recognized by the
Administration may be used.
-
.3 For LNG carriers with direct diesel driven propulsion system
or diesel electric propulsion system, having compressor(s) which
are used for supplying low-pressured gas derived from boil-off
gas to the installed engines (typically intended for 4-stroke
dual fuel engines):
footnote
For LNG carriers having diesel electric propulsion system,
MPPMotor(i) should be used instead
MCRME(i) for PAE
calculation.
For LNG carriers having steam turbine propulsion
system and of which electric power is primarily supplied by
turbine generator closely integrated into the steam and feed
water systems, PAE may be treated as
0(zero) instead of taking into account electric load in
calculating SFCSteamTurbine.
-
.4 For ship where the PAE value
calculated by paragraphs 2.5.6.1 to 2.5.6.3 is significantly
different from the total power used at normal seagoing, e.g. in
cases of passenger ships (see NOTE under the formula of EEDI),
the PAE value should be estimated by
the consumed electric power (excluding propulsion) in conditions
when the ship is engaged in a voyage at reference speed
(Vref) as given in the electric
power tablefootnote, divided by the average efficiency
of the generator(s) weighted by power (see appendix 2).
-
.6 Vref, Capacity and P should be
consistent with each other. As for LNG carries having diesel electric or steam
turbine propulsion systems, Vref is the relevant speed
at 83% of MPPMotor or MCRSteamTubine
respectively.
-
.7 SFC is the certified specific fuel consumption, measured in g/kWh, of
the engines or steam turbines.
-
.1 The subscripts ME(i) and AE(i)
refer to the main and auxiliary engine(s), respectively. For engines
certified to the E2 or E3 test cycles of the NOX Technical Code 2008, the engine
Specific Fuel Consumption (SFCME(i)) is that
recorded in the test report included in a NOX technical file for
the engine(s) at 75% of MCR power of its torque rating. For engines
certified to the D2 or C1 test cycles of the NOX Technical Code 2008, the engine
Specific Fuel Consumption (SFCAE(i)) is that recorded on the
test report included in a NOX technical file at the engine(s) 50%
of MCR power or torque rating. If gas fuel is used as primary fuel in
accordance with paragraph 4.2.3 of the Guidelines on survey and
certification of the energy efficiency design index (EEDI), SFC
in gas mode should be used. In case that installed engine(s) have no
approved NOX Technical File tested in gas mode, the SFC of
gas mode should be submitted by the manufacturer and confirmed by the
verifier.
The SFC should be corrected to the value corresponding to the ISO
standard reference conditions using the standard lower calorific value of
the fuel oil (42,700kJ/kg), referring to ISO 15550:2002 and ISO 3046-1:2002.
For ships where the PAE value calculated by
paragraphs 2.5.6.1 to 2.5.6.3 is significantly different from the total
power used at normal seagoing, e.g. conventional passenger ships, the
Specific Fuel Consumption (SFCAE) of the auxiliary
generators is that recorded in the test report included in a NOX
technical file for the engine(s) at 75% of MCR power of its torque
rating.
SFCAE is the power-weighted average among
SFCAE(i) of the respective engines i.
For those engines which do not have a test report included in a
NOX technical file because its power is below 130 kW, the
SFC specified by the manufacturer and endorsed by a competent
authority should be used.
At the design stage, in case of unavailability of test report in the
NOX file, the SFC specified by the manufacturer and
endorsed by a competent authority should be used.
For LNG driven engines of which SFC is measured in kJ/kWh should be
corrected to the SFC value of g/kWh using the standard lower
calorific value of the LNG (48,000 kJ/kg), referring to the 2006 IPCC
Guidelines.
Reference lower calorific values of additional fuels are given in the table
in paragraph 2.1 of these Guidelines. The reference lower calorific value
corresponding to the conversion factor of the respective fuel should be used
for calculation.
.2 The SFCSteamTurbine should be calculated by
manufacturer and verified by the Administration or an organization
recognized by the Administration as follows:
-

Where:
.1 Fuel consumption is fuel consumption of boiler per hour
(g/h). For ships of which electric power is primarily supplied by
Turbine Generator closely integrated into the steam and feed water
systems, not only PME but also electric
loads corresponding to paragraph 2.5.6 should be taken into
account.
-
.2 The SFC should be corrected to the value of LNG using the
standard lower calorific value of the LNG (48,000 kJ/kg) at SNAME
Condition (condition standard; air temperature 24°C , inlet
temperature of fan 38°C, sea water temperature 24°C).
-
.3 In this correction, the difference of the boiler efficiency based
on lower calorific value between test fuel and LNG should be taken
into account.
- .8 fj is a correction factor to account for ship specific design
elements:
-
.1 The power correction factor, fj, for ice-classed
ships should be taken as the greater value of fj0
and fj,min as tabulated in table 1 but not greater
than fj,max = 1.0.
For further information on approximate correspondence between ice classes,
see HELCOM Recommendation 25/7footnote.
Table 1: Correction factor for power fj for
ice-classed ships
| Ship type
|
fj0
|
fj,min depending on the ice class
|
| IA Super
|
IA
|
IB
|
IC
|
| Tanker
|
|
0.15Lpp0.30
|
0.27Lpp0.21
|
0.45Lpp0.13
|
0.70Lpp0.06
|
| Bulk
carrier
|
|
0.47Lpp0.09
|
0.58Lpp0.07
|
0.73Lpp0.04
|
0.87Lpp0.02
|
| General cargo ship
|
|
0.31Lpp0.16
|
0.43Lpp0.12
|
0.56Lpp0.09
|
0.67Lpp0.07
|
| Refrigerated cargo ships
|
|
0.47Lpp0.09
|
0.58Lpp0.07
|
0.73Lpp0.04
|
0.87Lpp0.02
|
-
-
.2 The factor fj, for shuttle tankers with
propulsion redundancy should be fj = 0.77. This
correction factors applies to shuttle tankers with propulsion redundancy
between 80,000 and 160,000 dwt. Shuttle tankers with propulsion redundancy
are tankers used for loading of crude oil from offshore installations
equipped with dual-engine and twin-propellers need to meet the requirements
for dynamic positioning and redundancy propulsion class notation.
-
.3 For ro-ro cargo and ro-ro passenger ships fjRoRo
is calculated as follows:
; If fjRoRo > 1 then
fj = 1
where the Froude number, FnL , is
defined as:

and the exponents ɑ, β ,ɣ and δ are defined as follows:
| Ship
type
|
Exponent:
|
| ɑ
|
β
|
ɣ
|
δ
|
| Ro-ro cargo ship
|
2.00
|
0.50
|
0.75
|
1.00
|
| Ro-ro passenger ship
|
2.50
|
0.75
|
0.75
|
1.00
|
-
.4 The factor fj for general cargo ships is calculated as
follows:
; If fj > 1 then
fj = 1
Where
; If Fn▽ > 0.6 then
Fn▽ = 0.6
and

-
.5 For other ship types, fj should be taken as 1.0.
-
.9 fw is a non-dimensional coefficient indicating the decrease
of speed in representative sea conditions of wave height, wave frequency and wind
speed (e.g. Beaufort Scale 6), and is determined as follows:
-
.1 for the attained EEDI calculated under regulations 20 and 21 of MARPOL
Annex VI, fw is 1.00;
.2 when fw is calculated according to the subparagraph
.2.1 or .2.2 below, the value for attained EEDI calculated by the formula in
paragraph 2 using the obtained fw should be referred to as
"attained EEDIweather";
-
.1 fw can be determined by conducting
the ship specific simulation on its performance at representative sea
conditions. The simulation methodology should be based on the
Guidelines developed by the Organizationfootnote and the method and outcome for an
individual ship should be verified by the Administration or an
organization recognized by the Administration; and
-
.2 in cases where a simulation is not conducted, fw
should be taken from the "Standard fw " table/curve.
A "Standard fw " table/curve is provided in the
Guidelinesfootnote for each ship type defined in regulation 2 of MARPOL Annex VI, and expressed as a
function of capacity (e.g. deadweight). The "Standard
fw " table/curve is based on data of actual speed
reduction of as many existing ships as possible under the
representative sea condition.
fw and attained EEDIweather, if calculated, with the
representative sea conditions under which those values are determined,
should be indicated in the EEDI Technical File to distinguish it from
the attained EEDI calculated under
regulations 20 and 21 of MARPOL Annex VI.
-
.10 feff(i) is the availability factor of each innovative energy
efficiency technology. feff(i) for waste energy recovery system
should be one (1.0)footnote.
-
.11 fi is the capacity factor for any technical/regulatory
limitation on capacity, and should be assumed to be one (1.0) if no necessity of
the factor is granted.
- .1 The capacity correction factor, fi, for ice-classed ships
should be taken as the lesser value of fi0 and fi,
max as tabulated in Table 2, but not less than fi,
min = 1.0. For further information on approximate
correspondence between ice classes, see HELCOM Recommendation 25/7footnote.
Table 2: Capacity correction factor fi for ice-classed
ships
| Ship
type
|
fi0
|
fi,max depending on the ice class
|
| IA Super
|
IA
|
IB
|
IC
|
| Tanker
|
|
2.10Lpp-0.11
|
1.71Lpp-0.08
|
1.47Lpp-0.06
|
1.27Lpp-0.04
|
| Bulk
carrier
|
|
2.10Lpp-0.11
|
1.80Lpp-0.09
|
1.54Lpp-0.07
|
1.31Lpp-0.05
|
| General cargo
ship
|
|
2.18Lpp-0.11
|
1.77Lpp-0.08
|
1.51Lpp-0.06
|
1.28Lpp-0.04
|
| Containership
|
|
2.10Lpp-0.11
|
1.71Lpp-0.08
|
1.47Lpp-0.06
|
1.27Lpp-0.04
|
| Gas carrier
|
|
1.25
|
2.10Lpp-0.12
|
1.60Lpp-0.08
|
1.25Lpp-0.04
|
- Note: Containership capacity is defined as 70% of the DWT.
-
.2 fi VSEfootnote for ship specific voluntary structural
enhancement is expressed by the following formula:

where:
DWTreferencedesign = Δship -
lightweightreferenceddesign
DWTemhanceddesign = Δship -
lightweightemhanceddesign
For this calculation the same displacement (Δ) for reference and enhanced
design should be taken.
DWT before enhancements (DWTreference design) is the
deadweight prior to application of the structural enhancements. DWT after
enhancements (DWTenhanced design) is the deadweight
following the application of voluntary structural enhancement. A change of
material (e.g. from aluminum alloy to steel) between reference design and
enhanced design should not be allowed for the fi VSE
calculation. A change in grade of the same material (e.g. in steel type,
grades, properties and condition) should also not be allowed.
In each case, two sets of structural plans of the ship should be submitted
to the verifier for assessment. One set for the ship without voluntary
structural enhancement; the other set for the same ship with voluntary
structural enhancement (alternatively, one set of structural plans of the
reference design with annotations of voluntary structural enhancement should
also be acceptable). Both sets of structural plans should comply with the
applicable regulations for the ship type and intended trade.
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.3 for bulk carriers and oil tankers, built in accordance with the Common
Structural Rules (CSR) of the classification societies and assigned the
class notation CSR, the following capacity correction factor
fiCSR should apply:
fiCSR = 1 + (0.08 · LWTCSR /
DWTCSR)
Where DWTCSR is the deadweight determined by paragraph 2.4
and LWTCSR is the light weight of the ship.
.4 for other ship types, fi should be taken as one (1.0).
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.12 fc is the cubic capacity correction factor and should be
assumed to be one (1.0) if no necessity of the factor is granted.
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.1 for chemical tankers, as defined in regulation
1.16.1 of MARPOL Annex II, the following cubic capacity correction
factor fc should apply:
fc = R
-0.7 ─ 0.014, where R is less than 0.98
or
fc = 1.000, where R is 0.98 and above;
where: R is the capacity ratio of the deadweight of the ship (tonnes)
as determined by paragraph 2.4 divided by the total cubic capacity of the
cargo tanks of the ship (m3).
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.2 for gas carriers having direct diesel driven propulsion system
constructed or adapted and used for the carriage in bulk of liquefied
natural gas, the following cubic capacity correction factor
fcLNG should apply:
fcLNG = R -0.56
where: R is the capacity ratio of the deadweight of the ship (tonnes)
as determined by paragraph 2.4 divided by the total cubic capacity of the
cargo tanks of the ship (m3).
Note: This factor is applicable to LNG carriers defined as gas
carriers in regulation 2.26 of MARPOL Annex VI and should not be
applied to LNG carriers defined in regulation
2.38 of MARPOL Annex VI.
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.3 For ro-ro passenger ships having a DWT/GT-ratio of less than 0.25, the
following cubic capacity correction factor, fcRoPax,
should apply:

Where DWT is the Capacity and GT is the gross tonnage in accordance with the
International Convention of Tonnage Measurement of Ships 1969, annex I,
regulation 3.
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.4 For bulk carriers having R of less than 0.55 (e.g. wood chip
carriers), the following cubic capacity correction factor, fc
bulk carriers designed to carry light cargoes, should apply:
fc bulk carriers designed to carry light cargoes =
R -0.15
where: R is the capacity ratio of the deadweight of the ship (tonnes)
as determined by paragraph 2.4 divided by the total cubic capacity of the
cargo holds of the ship (m3).
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.13 Length between perpendiculars, Lpp,
means 96% of the total length on a waterline at 85% of the least moulded depth
measured from the top of the keel, or the length from the foreside of the stem to
the axis of the rudder stock on that waterline, if that were greater. In ships
designed with a rake of keel the waterline on which this length is measured should
be parallel to the designed waterline. Lpp should be
measured in metres.
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.14 fl is the factor for general cargo ships equipped
with cranes and other cargo-related gear to compensate in a loss of deadweight of
the ship.
fl = fcranes .
fsideloader .
froro
fcranes = 1 If no cranes are present.
fsideloader = 1 If no side loaders are present.
froro = 1 If no ro-ro ramp is present.
Definition of fcranes :

where
SWL = Safe Working Load, as specified by crane manufacturer in metric tonnes
Reach = Reach at which the Safe Working Load can be applied in metres
N = Number of cranes
For other cargo gear such as side loaders and ro-ro ramps, the factor should be
defined as follows:


The weight of the side loaders and ro-ro ramps should be based on a direct
calculation, in analogy to the calculations as made for factor
fivse.
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.15 Summer load line draught, ds, is the vertical
distance, in metres, from the moulded baseline at mid-length to the waterline
corresponding to the summer freeboard draught to be assigned to the ship.
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.16 Breadth, Bs, is the greatest moulded breadth of the
ship, in metres, at or below the load line draught, ds.
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.17 Volumetric displacement, ∇, in cubic metres (m3), is the volume of
the moulded displacement of the ship, excluding appendages, in a ship with a metal
shell, and is the volume of displacement to the outer surface of the hull in a
ship with a shell of any other material, both taken at the summer load line
draught, ds, as stated in the approved stability
booklet/loading manual.
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.18 g is the gravitational acceleration, 9.81m/s2.
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