Section 2 Stability
Clasification Society 2024 - Version 9.40
Clasifications Register Guidance Information - Guidance Note for the Classification, Safe Design, Construction and Operation of Tugs, August 2018 - Chapter 3 Statutory - Section 2 Stability

Section 2 Stability

2.1 Scope of application

In general, tugs having a Load Line length LLL equal to or greater than 24 m may be assigned class only after it has been demonstrated that their intact stability is adequate. Adequate intact stability means compliance with standards laid down by the relevant Administration.

The content of this Section may also be applied to tugs with a Load Line length LLL of less than 24 m in length as desired.

2.2 Openings

2.2.1 General

Openings in the hull, superstructures or deckhouses which cannot be closed weathertight should be considered as unprotected openings and, consequently, as down-flooding points for the purpose of stability calculations (the lower edge of such openings should to be taken into account).

2.2.2 Ventilation openings of machinery space and emergency generator room

It is recognised that for tugs, due to their size and arrangement, compliance with the requirements of ICLL Reg. 17(3) for ventilators necessary to continuously supply the machinery space and the emergency generator room may not be practicable. Lesser heights of the coamings of these particular openings may be accepted by the administration if the openings:
  • are positioned as close to the centreline and as high above the deck as practicable in order to maximise the downflooding angle and to minimise exposure to green water;
  • are provided with weathertight closing appliances in combination with suitable arrangements, such as separators fitted with drains;
  • are equipped with efficient protective louvers and mist eliminators;
  • have a coaming height of not less than 900 mm above the deck;
  • are considered as unprotected openings and, consequently, as down-flooding points for the purpose of stability calculations.

2.3 Intact stability

2.3.1 Loading conditions

The following standard loading conditions should be included in the stability booklet:
  • lightship condition;
  • tug in lightest anticipated loading condition, with full stores and fuel;
  • same condition as above, but with 10 per cent stores, provisions and consumables;
  • tug in the departure condition at the waterline corresponding to the maximum draught, with full stores, provisions and consumables;
  • same condition as above, but with 10 per cent stores, provisions and consumables.

For the lightship condition, not being an operational loading condition, the administration may accept that part of the mentioned criteria is not fulfilled.

In case a tug is fitted with water ballast tanks the lightest anticipated loading condition may be a ballast condition (in particular for larger tugs).

When a tropical freeboard is to be assigned to the tug, the corresponding loading conditions should also be included.

For the loading condition corresponding to the maximum draught, when necessary, deck cargo may be applied to arrive at the required draught. Attention should be paid to the associated wind profile for verification of the severe wind and rolling criterion, refer to part A, 2.3 of the International Code on Intact Stability, 2008.

Additional loading conditions that should be included in the stability booklet:
  • tug in the worst anticipated operating conditions for towing, covering the relevant range of draughts, for type notation tug;
  • tug in the worst anticipated operating conditions for escorting, covering the relevant range of draughts, for type notation escort tug.

Further loading conditions may be included when deemed necessary or useful by the administration.

2.3.2 Stability criteria

The intact stability of tugs should comply with the provisions given in part A, 2.2 and 2.3 of the International Code on Intact Stability, 2008, except that the alternative criteria given in part B, 2.4.5, which apply to offshore supply vessels, may be used for tugs of similar design and characteristics.

With reference to Part B, 5.1.4 of the International Code on Intact Stability, 2008, tugs should possess an adequate reserve of stability to withstand the anticipated heeling moment arising from the towline. It is considered that this requirement is complied with in case a tug meets the additional stability criteria as specified in Ch 3, 2.3 Intact stability 2.3.3 and/or Ch 3, 2.3 Intact stability 2.3.4, as applicable.

2.3.3 Additional stability criteria for type notation tug

All the loading conditions reported in the trim and stability booklet which are intended for towing operations should also be checked in order to investigate the tug’s capability to withstand the effect of the transverse heeling moment induced by the combined action of the towline force and the thrust vector (self-tripping), and induced by the hydrodynamic resistance of the hull (tow-tripping).

The stability calculations should to be performed on the basis of the design bollard pull, as defined in Ch 1, 1.3 Definitions 1.3.1.

For tugs capable of towing over the stern as well as over the bow, this check should be performed for both towing situations, duly taking into account the location of the associated towing points. If different values of the ahead and astern design bollard pull are available, it may be acceptable to consider the ahead bollard pull for towing over the stern and the astern bollard pull for towing over the bow.

The values of the ahead and astern design bollard pull, as applicable, should be specified by the designer in the stability booklet. In addition, an arrangement drawing with the location of the towing point(s) and propulsion unit(s) should be included in the stability booklet. In this drawing the longitudinal and vertical distance, in m, from each of the towing points to the relevant centrelines of the propulsion unit(s) and the baseline, respectively, should be clearly specified.

Preliminary stability calculations on the basis of estimated bollard pull values may be submitted for (preliminary) examination. If after completion of the bollard pull test the measured bollard pull values exceed the estimated values, the stability calculations should be updated for the measured bollard pull values. It is recommended to include a reasonable margin in the estimated values (on the basis of design experience).

A tug may be considered as having sufficient stability to withstand the self-tripping heeling moment if the following condition is satisfied with (see Figure 3.2.1 Heeling and righting arm curves):
  • AB
where
A = Area, in m rad, contained between the righting arm and the heeling arm curves, measured from the heeling angle θC to the heeling angle θD;
B = Area, in m rad, contained between the heeling arm and the righting arm curves, measured from zero heel (θ = 0) to the heeling angle θC;
θC = Heeling angle of equilibrium, corresponding to the first intersection between heeling and righting arm curves;
θD = Heeling angle, to be taken as the lesser of:
  • heeling angle corresponding to the second intersection between heeling and righting arms heeling and righting arm curves;
  • angle of down-flooding.

Figure 3.2.1 Heeling and righting arm curves

The self-tripping heeling arm curve should be calculated as follows:
where
bHi = Heeling arm induced by one thruster or group of thrusters i, in m, calculated as follows:
TBPi = Amount of thrust, in kN, generated by one thruster or group of thrusters i. The sum of all the individual thrusts is to be equal to the design bollard pull, as defined in Ch 1, 1.3 Definitions 1.3.1;
where
hi = Vertical distance, in m, between the towing point (fairlead, staple, towing hook or equivalent fitting) and the horizontal centreline of the propulsion unit or group of units i, as relevant for the considered towing situation;
r = Transverse distance, in m, between the centreline and the towing point (fairlead, staple, towing hook or equivalent fitting), to be taken equal to zero when the towing point is fixed at the vessel’s centreline;
ci = Coefficient to be taken equal to:

ci = 0,50 for tugs with non-azimuth propulsion unit or group of units (conventional tug, see Ch 1, 2.2 Typical tug arrangements 2.2.2);

ci = 1/(1 + d i/LLL) for a single azimuthing thruster

ci = 0,90/(1 + d i/LLL) for tugs with a group of two azimuthing thrusters (tractor tug and ASD tug, see Ch 1, 2.2 Typical tug arrangements 2.2.3 and Ch 1, 2.2 Typical tug arrangements 2.2.4, respectively, as well as similar tug designs), as relevant for the considered towing situation, but is in no case to be taken as less than:
  • 0,70 for ASD tugs towing over the stern and tractor tugs towing over the bow
  • 0,50 for ASD tugs towing over the bow and tractor tugs towing over the stern, respectively;
Δ = Loading condition displacement, in t;
ϴ = Angle of heel, in deg;
di = Longitudinal distance, in m, between the towing point (fairlead, staple, towing hook or equivalent fitting) and the vertical centreline of the propulsion unit or group of units i, as relevant for the considered towing situation;
LLL = Load Line length, in m.

A tug may be considered as having sufficient stability to withstand the tow-tripping heeling moment if the first intersection between the righting arm curve and the tow-tripping heeling arm curve occurs at an angle of heel less than the angle of down-flooding.

The tow-tripping heeling arm curve is to be calculated as follows:
where
Ci = Lateral traction coefficient, taken equal to:

without being taken lower than 0,1 and greater than 1;

Ls = Longitudinal distance, in m, from the aft perpendicular to the towing point;
Lpp = Length between perpendiculars, in m;
C2 = Angle of heel correction for C1, taken equal to:

without being taken lower than 1;

ϴd = Angle to deck edge, in deg, taken equal to:
f = Freeboard amidships, in m;
γ = Specific water density, in t/m3, to be taken equal to 1,025;
V = Lateral velocity, in m/s, to be taken equal to 2,57 (5 kn);
Ap = Lateral projected area, in m2, of the underwater hull;
C3 = Distance from the centre of Ap to the waterline as a fraction of the draught related to the heeling angle, taken equal to:

without being taken lower than 0,5 and greater than 0,83;

T = Loading condition draught, in m.

2.3.4 Additional stability criteria for type notation escort tug

All the loading conditions reported in the trim and stability booklet which are intended for escorting operations should also be checked in order to investigate the tug’s capability to withstand the effect of the transverse heeling moment induced by the combined action of the following forces:
  • hydrodynamic forces acting on the hull and appendices;
  • thrust forces;
  • steady towline force.

The stability calculations should to be performed on the basis of the highest anticipated heeling moment for the considered loading condition, which should to be obtained from the results of full scale tests, model tests, or, alternatively; the results of an accepted computer simulation program (refer to Ch 3, 2.3 Intact stability 2.3.5).

For each relevant loading condition the evaluation of the highest anticipated heeling moment should be performed for the applicable range of speeds and towline angles, as defined in the escort towing arrangement plan (see Ch 2, 2.3 Towing arrangements for Escort Tugs 2.3.4). As a minimum, the conditions corresponding to the design maximum steering force Fs,MAX, and design maximum braking force Fb,MAX, as defined in Ch 1, 1.3 Definitions 1.3.2, should be included in the evaluation.

The highest anticipated heeling moment should be assumed constant for the purpose of the stability calculations.

The value of the highest anticipated heeling moment should be specified by the designer in the stability calculations. In addition, an arrangement drawing with the location of the towing points and propulsion units should be included in the stability booklet. In this drawing the longitudinal and vertical distance, in m, from the towing point to the relevant centrelines of the propulsion units and the baseline, respectively, should be clearly specified.

Preliminary stability calculations on the basis of estimated highest heeling moment and associated heeling arm values may be submitted for (preliminary) examination. If after verification of the heeling arm values on the basis of the results of escort performance trials, model tests or an accepted computer simulation program (refer to Ch 3, 2.3 Intact stability 2.3.5) the final values exceed the estimated values, the stability calculations should be updated for the final heeling moment and heeling arm values. It is recommended to include a reasonable margin in the estimated values (on the basis of design experience).

An escort tug may be considered as having sufficient stability to withstand the heeling moment arising from the towline, if the three following conditions are satisfied with:
where
A = Righting arm curve area, in m rad, measured from the heeling angle θC to a heeling angle of 20 deg (see Figure 3.2.2 Definition of areas A and B);
B = Heeling arm curve area, in m rad, measured from the heeling angle θC to a heeling angle 20 deg (see Figure 3.2.2 Definition of areas A and B);
C = Righting arm curve area, in m rad, measured from the zero heel (θ = 0) to the heeling angle θD (see Figure 3.2.3 Definition of areas C and D);
D = Heeling arm curve area, in m rad, measured from zero heel (θ = 0) to the heeling angle θD (see Figure 3.2.3 Definition of areas C and D);
θC = Heeling angle of equilibrium corresponding to the first intersection between heeling arm and righting arm curve, to be obtained when the highest anticipated heeling moment resulting from the steady towline force Ft as defined in Ch 1, 1.3 Definitions 1.3.2, is applied to the escort tug;
θD = Heeling angle, to be taken as the lesser of:
  • the angle of down-flooding;
  • 40 deg;
  • the heeling angle corresponding to the second intersection between heeling and righting arms heeling and righting arm curves.

Figure 3.2.2 Definition of areas A and B



Figure 3.2.3 Definition of areas C and D

2.3.5 Escort performance simulations

Where the highest anticipated heeling moment is obtained from the results of a computer simulation program, the basic assumptions and theoretical models underlying the software should be presented in detail to Lloyd’s Register. Items to be detailed include:
  • hydrodynamic lift and drag computation (hull and appendices);
  • modelling of thrust forces;
  • interaction effects between hull, skeg and (steerable) propulsion units;
  • flow separation effects;
  • water pile-up effects;
  • effects of waves and/or swell;
  • dynamic effects before a steady state is reached (e.g. during initiation and turning manoeuvres) and scaling effects (if any).
  • Meshing details
  • Model assumptions and relevant limitations

A validation report, containing comparisons between simulation results and full scale and/or model test results, should also be presented.

A clear description of the input and output data should be provided, along with explanations on how the output data are obtained/calculated by the software.

As a minimum, for each relevant loading condition (see Ch 3, 2.3 Intact stability 2.3.1) the following set of results should be provided in tabular form as function of the escort speed for the rated values of the steering force Fs,R and the braking force Fb,R:
  • Rated steering force Fs,R or steering force Fs corresponding to rated braking force Fb,R, as applicable;
  • Rated braking force Fb,R or braking force Fb corresponding to rated steering force Fs,R, as applicable;
  • Corresponding towline force Ft;
  • All corresponding forces acting in transverse direction (hydrodynamic, thrust and towline);
  • Corresponding heeling angle;
  • Corresponding heeling moment;
  • Corresponding towline angle relative to the escorted ship (see α in Figure 1.1.1 Typical escort configuration);
  • Corresponding drift angle of the escort tug (see β in Figure 1.1.1 Typical escort configuration).

Note that the highest anticipated values of the steering force, braking force, towline force and heeling moment do not normally all occur in the same condition (defined by the position of escort tug relative to the escorted ship and the drift angle), although more than one parameter may have its highest value in a particular condition. Hence it is suggested to consider at least two conditions: one for the highest anticipated steering force and one for the highest anticipated braking force. In case the highest anticipated heeling moment and/or towline force do not occur in either one of these two conditions, the relevant conditions should be added.

It is recommended that the results of the escort performance simulations are presented in the form of diagrams showing the envelope of the (steady state) combinations of steering and braking forces obtained from the simulations. Such diagrams should cover the applicable escort speed range, with a recommended step of 2 knots.

2.3.6 Escort performance trials

Escort performance trials at full scale or model scale may be carried out in order to obtain the characteristics of escort tugs.

The trials should cover the applicable range of loading conditions and escort speeds.

The following documents should be submitted for information prior to testing:
  • Relevant loading conditions, defined by draught (or displacement) and trim, for which the tug is designed to perform escort services;
  • Applicable range of test speeds of the escorted ship: the speed is defined as the relative speed with respect to the sea, taking into account current effects;
  • Main propulsion characteristics, in particular power and maximum orientation angle of the rudder(s) (propellers);
  • Preliminary calculation of the rated steering force Fs,R, rated braking force Fb,R and rated steady towline force Ft,R as defined in Ch 1, 1.3 Definitions 1.3.2, as well as the corresponding heeling moments and heeling angles, for the range of test speeds;
  • Calculation of the route deviation of the escorted ship (for testing purposes the escorted ship is to be selected so that the route deviation induced by the tug is kept reasonably small;
  • Preliminary stability calculations for the above-mentioned conditions;
  • Escort towing arrangement plan, including the load cell and specification of the components;
  • Documentation relevant to the Bollard Pull test, see Ch 1, 1.3 Definitions 1.3.1.
Prior to commencing the escort performance trials the following data should be recorded:
  • Wind speed and direction;
  • Sea state, including significant wave height and peak period;
  • Current speed and direction;
  • Water depth;
  • Loading condition of the escort tug: draught (or displacement) and trim;
  • Loading condition of the escorted ship.

Testing should be performed over the applicable range of towline angles as defined in the escort towing arrangement plan. The length of the towline and the angle of the towline with the horizontal plane should represent a typical operating condition.

As a minimum, the following data should be collected during testing for post-processing and analysis:
It is also recommended to that the following data is measured:
  • Power setting and orientation angle of rudder(s) (propellers) of the escort tug;
  • Time needed to swing the tug from the equilibrium position to its mirror position.
For each combination of loading condition and test speed:
  • The rated steering force Fs,R and rated braking force Fb,R should be calculated on the basis of the corresponding measured steady towline force Ft and the associated measured towline angle, drift angle and the angle between the towline and the horizontal plane;
  • The maximum heeling arm should be calculated on the basis of the corresponding measured steady towline force Ft, as defined in Ch 1, 1.3 Definitions 1.3.2, the associated measured heeling angle and the GZ curve applicable to the loading condition considered (The GZ curve should be based on the escort tug in upright position before commencing the escort operation).
As a minimum, for each tested loading condition the following set of results should be provided in tabular form as a function of the escort speed for the rated values of the steering force Fs,R and the braking force Fb,R:
  • Rated steering force Fs,R or steering force Fs corresponding to rated braking force Fb,R, as applicable;
  • Rated braking force Fb,R or braking force Fb corresponding to rated steering force Fs,R, as applicable;
  • Corresponding towline force Ft,R;
  • Corresponding heeling angle;
  • Corresponding heeling moment;
  • Corresponding towline angle relative to the escorted ship (see α in Figure 1.1.1 Typical escort configuration);
  • Corresponding drift angle of the escort tug (see β in Figure 1.1.1 Typical escort configuration).

The highest anticipated values of the steering force, braking force, towline force and heeling moment do not normally all occur in the same condition (defined by the position of escort tug relative to the escorted ship and the drift angle), although more than one parameter may have its highest value in a particular condition. Hence it is suggested to consider at least two conditions: one for the highest anticipated steering force and one for the highest anticipated braking force. In case the highest anticipated heeling moment and/or towline force do not occur in either one of these two conditions, the relevant conditions should be added.

For model testing, due consideration should be given to scale effects for establishing the escort tug characteristics at full scale from the model test results.

2.3.7 Operating information for type notation escort tug

Additional operating information should be provided in the stability booklet in relation to the design limitations related to the assignment of the type notation escort tug, in line with Pt B, Ch 3.8 of the International Code on Intact Stability, 2008.

As a minimum, the following information should be included:
  • Design service restriction notation and environmental conditions for performing escort operations;
  • The maximum escort speed VMAX (see Ch 1, 1.3 Definitions 1.3.2);
  • A table with permissible values of heeling angle and steady towline force as function of loading condition and escort speed (based on the rated steering and braking forces as obtained from Ch 3, 2.3 Intact stability 2.3.5 orCh 3, 2.3 Intact stability 2.3.6, as applicable);
  • Instructions to the master regarding the handling of the escort tug and the associated towing equipment, demonstrating the implementation of effective means to limiting the steady towline force and heeling angle within the permissible limits and the use of the emergency quick-release device. In this context “Effective means” might include, but is not limited to, adjustable audible or visible alarms, providing a warning to the master when the heeling angle and/or steady towline force exceeds the permissible value(s) applicable to the relevant loading condition and escort speed.

The table with permissible values of heeling angle and steady towline force as function of loading condition and escort speed should be displayed in the wheelhouse next to the control desk or another appropriate location.

2.3.8 Icing considerations

For tugs operating in areas where ice accretion is expected due consideration should be given to the stability affecting effect of added weight due to ice accretion.

To this end, relevant loading conditions, including ice accretion should be included in the stability booklet, together with detailed calculations of the expected ice accretion a required by Pt B, Ch 6 of the International Code on Intact Stability, 2008.

2.3.9 Elements reducing stability

Provisions should be made for a safe margin of stability at all stages of the voyage, due regard being given to additions of weight, such as those due to absorption of water and icing and to losses of weight such as those due to consumption of fuel and stores.

2.3.10 Alterations

Where any alterations are made to a tug or its towing equipment so as to materially affect the stability information supplied to the master, amended stability information should be provided.

During the lifetime of the vessel, it is recommended that periodical lightweight surveys are undertaken to verify any changes in lightship displacement and longitudinal centre of gravity. In the case that case significant deviations are found in comparison with the approved stability information, it may be necessary to (re-)incline the tug and/ or reassess the strength and stability of the vessel.


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