Annex – 2014 Guidelines on the Method of Calculation of the Attained Energy Efficiency Design Index (EEDI) for New Ships
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Statutory Documents - IMO Publications and Documents - Resolutions - Marine Environment Protection Committee - Resolution MEPC.245(66) – 2014 Guidelines on the Method of Calculation of the Attained Energy Efficiency Design Index (EEDI) for New Ships – (Adopted on 4 April 2014) - Annex – 2014 Guidelines on the Method of Calculation of the Attained Energy Efficiency Design Index (EEDI) for New Ships

Annex – 2014 Guidelines on the Method of Calculation of the Attained Energy Efficiency Design Index (EEDI) for New Ships

  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 1997 relating 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)

 

* 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
  Note: This formula may not be applicable to a ship having diesel-electric propulsion, turbine propulsion or hybrid propulsion system, except for cruise passenger ships and LNG carriers.

 Where:

  • .1 CF is a non-dimensional conversion factor between fuel consumption measured in g and CO2 emission also measured in g based on carbon content. The subscripts ME(i) and AE(i) refer to the main and auxiliary engine(s) respectively. CF corresponds to the fuel used when determining SFC listed in the applicable test report included in a Technical File as defined in paragraph 1.3.15 of NOX Technical Code ("test report included in a NOX technical file" hereafter). The value of CF is as follows:


    Type of fuel Reference Carbon content CF (t-CO2/t-Fuel)
    1 Diesel/Gas Oil ISO 8217 Grades DMX through DMB 0.8744 3.206
    2 Light Fuel Oil (LFO) ISO 8217 Grades RMA through RMD 0.8594 3.151
    3 Heavy Fuel Oil (HFO) ISO 8217 Grades RME through RMK 0.8493 3.114
    4 Liquefied Petroleum Gas (LPG) Propane 0.8182 3.000
      Butane 0.8264 3.030
    5 Liquefied Natural Gas (LNG)   0.7500 2.750
    6 Methanol   0.3750 1.375
    7 Ethanol   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.

  • Example:


    CF,Gas = 2.750
    CF-Pilotfuel = 3.114
    SFCME Pilotfuel = 6 g/kWh
    SFCME Gas = 160 g/kWh
     
    EEDI = (PME x (CF Pilotfuel x SFCME Pilotfuel + CF Gas x SFCME Gas )) + …
    EEDI = (PME x (3.114 x 6 + 2.750 x 160)) + …

    Calculation examples are set out in appendix 4.

  • .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:

        or

      • 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:

      • P SM ,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:

        Where:

        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.

      • Note: The shaft motor's chain efficiency may be taken into consideration to account for the energy losses in the equipment from the switchboard to the shaft motor, if the chain efficiency of the shaft motor is given in a verified document.

    • .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 x BOR x COPreliquefy x 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 ships 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.

    • .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 f j for ice-classed ships

          fj,min depending on the ice class
      Ship type fj0 IA Super IA IB IC
      Tanker 0.15Lpp 0.30 0.27Lpp 0.21 0.45Lpp 0.13 0.70Lpp 0.06
      Bulk carrier 0.47Lpp 0.09 0.58Lpp 0.07 0.73Lpp 0.04 0.87Lpp 0.02
      General cargo ship 0.31Lpp 0.16 0.43Lpp 0.12 0.56Lpp 0.09 0.67Lpp 0.07
      Refrigerated cargo ships 0.47Lpp 0.09 0.58Lpp 0.07 0.73Lpp 0.04 0.87Lpp 0.02
    • .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:

      where the Froude number, FnL , is defined as:

      and the exponents α, β,γ and δ are defined as follows:


        Exponent:
      Ship type α β γ 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:

      Where

      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.


        fi,max depending on the ice class
    Ship type fi0 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 VSE footnote for ship specific voluntary structural enhancement is expressed by the following formula:

      where:

      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.

    • .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:

      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).

  • .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.

    • .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 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)

    • .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:

      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.

    • .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.

  • .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.

  • .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 meters


    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 .

  • .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.

  • .16 Breadth, Bs , is the greatest moulded breadth of the ship, in metres, at or below the load line draught, ds .

  • .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.

  • .18 g is the gravitational acceleration, 9.81m/s2.


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