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T.
W88102 - KIVI-NVTS PREDICTION OF SEAKEEPING' CHARACTERI STICS AND
WORKABILITY OF
OFFSHORE SUPPORT VESSELS
By: R.P. Dallinga and A.B. Aalbers
Septenther 1986.
PREDICTION OF SEAKEEPING CHARACTERISTICS AND WORKABILITY
OF OFFSHORE SUPPORT VESSELS
Ir.. R.P. Dailinga and Drs. A.B.. Aalbers
MARIN, Ocean Engineering Division Wageningen, The Netherlands
effect of environmental factors like the frequency, and persistence of adverse weather conditions, and the. effect of operational
1. INTRODUCTION
1.1. General
The growing number of offshore constructions such as pipe lines, fixed platforms, under water manifolds etc. leads to an increasing demand for diving Operations for carrying out inspection and
main-tenance. These operations usually take place frotn a tobile basis: a
diving support vessel designed to stay on station by means of dy namic positioning. Such a ship is provided with one or more moon-pools and with cranes for handling diving bells and other equip-.
ment.
In the design phase of a diving support vessel it is useful to have a realistic insight in the motion behaviour, the station-keepi-ng capability and the acceleration levels on board of the ship. With respect to the diving operations it is alsO necessary to have early information on the behaviour of the moonpool. If for a certain area of operation the long term Sea cOnditions are known this informa-tion may be used to obtain a workability predicinforma-tion. This iS an
important factor ixi the economic evaluation of the project..
Computer calculation methods are available to make Such workability predictions fOr a. specific ôase as well as to investigate e.ffects
of changes in criteria, environmental conditions and ship
behav-iour.
In the present paper a set of criteria will be assumed valid for a hypothetical diving support vessel, calculation methods for mo-tions, acceleramo-tions, drift forces, wind and current forces, moon-pool relative motions and dynamic positiOning simulation are pro-posed. Thereupon a workability predictbn is made for a realistic
1.. Ship particulars
The. sections of a diving support vessel are showr in Figure 1. This
shape is used for the calculations and workability prediction. The main particulars of two alternative vessel sizes are shown in Table
1. An anti-roll tank is present in the smallest, vessel.
The moonpool is circular in shape and smooth walled. A thruster arrangement with two tunnel thrusters at the bow and two aimuthing
thrusters at the. stern was adopted.
l.3o Environment.
The NOrth Sea is chosen as the operational area for the diving sup-port vessel design. Environmental conditions of this area are
available in the form of wave scatter diagrams, water depth data, current data and information concerning the duration. of the sea conditions. In Figure 2 a typical wave scatter diagram is shown. Figure 3 shows a representative distribution of the length of good weather periods, Figure 4 indicates the average duration of these calm weather periods, and he average nuber of these periods per
year.
TheSe descriptions of the environmental conditions were compiled
2. WORKABILITY CRITERIA
2.l Ship motions and accelerations.
Lin4tations exist for the operation of equipment arid, cranes which can be expressed in ters of maximuth allowable accelerations and
ship mOtions (i.e. heave,, pitch and roll). For instance, a ditiamic
analysis of crane operations taking into accOunt shoOk loads and dynamic load amplification in the hoist wire and ax,rn.im allowable
side loads due to swing.
will lead
to criteria in terms of angular motionS and accelerationsat
the crane location. [5].'Pubiishe4 of f shore experience of diving companies helps to select criteria, for ship motions [6 and 7].
'For the present paper the following Set of hip motion and acceler-. ation criteria was adopted:
Surge Sway Yaw
I
Heave. 3.0 rn Pitch 4.0 deg. Roll. . 6.0 deg..Vert.
acc. St. 1 2.5 rn/s2 (stern crane)Vert. acc.. St. 8 1.8 rn/s2 (mOOnpool)
Transv. acc. St. 8 1.5 rn/s2 (moonpool tane) (1Q m above keel)
See dynamic positioning (Section 2.3)
The above limit values are the most probable single amplitude
2.2. Moonpool relative motion
The moonpool is used to lower equipment or diving bells to large depth. The relative water fnotions inside the moonpool may hamper diving bell passage [8 and 9]. Although application of aeration. will reduce the risk of slamming loads to a diving bell, a work-ability limit may still apply. For this study the criterion was set
at 2.5 in maximum single amplitude for 1000 oscillations.
2.3. Positioning accuracy
Irrespective of the accuracy of the dynanUc positioning reference system, the low frequency variations of the ship's position have to
be within certain limits. For diving operatiofis an overall accuracy of 2.5% of the water depth was assumed to be required. Furthermore,
it was assumed that the accuracy of the reference system iight lead to a pOsition deviation of 1% of the water depth, which has to be subtracted from the maximum allowable excursion. For constant wind and current, the maximum pOsition variatiOns in X and Y direction due to low frequency wave drift forces should be 1.5 in for 100 in water depth.
!4:. Oper tions scenario
For a workability assessment the operations scenario plays an im-portant role. The criteria given above may for instance be exceeded
somewhat before work. is actually stopped while the criteria must be
satisfied before work is resumed. Also, it is possible to have con-siderable inefficiency occurring after a bad weather period in
six coupled diffeential equations. In the present approach the. following linear equations Qf motion are solved in the frequency
domain: 6
z
j=1
(Mkj 1- ak.) cos(wt + c.) - w bk sin(wt + c.) +
= + 4)7()}
-6
iw E
j=l
j
ajA. description of the numerical solution of the potential problem is given by Van Oortmerssen [10].
cos(wt +
J aj Fak cos(wt (1)
The hydrodynamic (motion-induced) reaction forces and the (wave-induced) excitation forces are calculated by means of
a
cOmputerprogram based on three-dimensional linear potential theory, In this theory the. fluid is assumed to be ideal apd irrotationál.
t js assumed that in case of zero speed the flow .ield around the moving body in waves can be described by a velocity potential:
X(Lt) =
4(y)
exp(-iwt) ... (2)
This function is regarded as the linear sum of independent contri-butions due to diffraction from all modes of motion, the incident
3.2. Non-linear roll damping atid the anti-roll tank
F roll, the potential daping is very small so additional damping mechanisms have great influence on the motion response at reso-nance. These mechanisms comprise linear as well as noti-linear con-tributions. For the present calculations the following roll damping
contributions were considered:
=BF
+ BE Bw + BBKbeing respectively the frictional, eddy, wave (potential) and bilge keel damping coefficients obtained after applying equivalent un-.
earization of the non-linear components. Since the calculations are
carried out for zero speed the contribution of the lift effects in the damping
is not
taken into accOunt. The damping contributionsare
determined by means of empirical relations depending on theshape of the vessel as proposed by Ikeda et al. [ii].
For the 80 in long ship a U-type anti-roll tank was designed,
applying the theory given by Stigter [12]. Its dimensions are chosen such that the tank natural oscillation period is somewhat shorter than the natural roll period of the Ship, resulting in an
optimized roll reduction according to the findings of Van der aunt
[13].
The roil counteracting moment generated by the U-tank may be
ex-preSsed as an added inertia, a damping and a restoring coefficient
adaptation in the equation of motion of roll:
(M44 + a44 +
La44 )4
+(B44 + b44)4
+. (c44 + Ac44 )4
= Fa4
cos(t +
o4)
(5)The damping coefficient of the U-tank for the 80 m vessel is added to the effect of the additional dtnping mechanisms given in
equa-tion (4).
3.3. Moonpool relative rñotions
A mathematical model is used [14] taking into account. the coupling of the fnoonpool relative motions with the local ship vertical
mo-tion. The relative motion is found by solving:
{pA'('r + h) + %}h +bi + b2i i + pgAh +
+ + pA(T + h) + ah}z + (ehZ + bh)z + pgAz = Fwh . . . (6)
Non-linear terms are. present in this equation of motion so that it
is solved in the time domain using regular waves of a defined
am-plitude as input..
-From diffraction theory calculations with a separate facet repre-sentation [15] for the mbonpooi keel opening it is possible to de-termine the wave forge acting on the water in the moonpool and the interaction coefficients between local heave and relative motions. In this approach a. frictionless, weightless and volueless piston is thought to lay flush with the ship keel in the moonpool, sepa-rating the moonpool cOntents from the outside.
The quadratic damping coefficient is estimated using model test results and literature [8, 14, 16, 17 and 18]. The quadratic damping depends on the internal configuration of the moonpool as
well as on the inflow and outflow energy losses. For this work the interior of the moonpool was chosen smooth walled so that the
3.4. Dynamic. positioning
For the low frequency motions the three equations of motion (surge,
sway and yaw) are being solved in the time domain. These equations include cOnstant added mass and damping terms (neglecting frequency
dependence)1 environmental forces (wind, waves and current) and
thruster forces. The Sway and yaw equations are coupled whereas the surge equation is coupled to the previous two mOdes by thruster
forces only.
The environmental forces are separated in wave, wind and current forces assuming there is no interaction between them. (Note that
experience with model test results shows that, fOr instance,
cur-rent can have a significant influence on wave drift forces).
The current forces are calculated using an empiricaL database of
model test data.
Wind forces are determined by dividing the structure above the waterline into geometric components. For the part of the hull below the upper cOntinuous deck wind resistance coefficients have been derived from [l9 arid 20]. Wind forces on the remainder of the supetStructure are added to the above values. These are found by adding the contributions of all superStrudture components taking
shadowing. effects, solidity effects and three-dimensional effects into account. This is done as set out in [21]. A realistic wind profile is assumed and the instantaneous wind direction with
re-spect to the ship's slow yaw drift motions is considered. The
effects of dynamic wind load variations are neglected.
The wave drift forces are calculated frOm quadratic drift force transfer functions obtained with the help of the diffractiOn theory computer program (see Section 3.1) applying the direct integration
functions are incorporated in the simulation program and the aver-age drift forces are computed by:
(2)
= 2f S(w) [F. (w a.)j (7)
0
For the dynamic behaviour the drift force spectral density func-tions are approximated f rpm the following relationShip [23, 24 an 25]:
(2)
8
f
S(w) S(w + ii) [F' W±1i)]2 dw0
ç
in which (similar to the Newman approach):
w+u)
!(2)(W
+, w+.)
I S I . (9)
Using the averages and the spectral densities of the low frequency
excitation a force record can. be generated. The procedure was- out-lined by Nierihuis [26]. The excitation forces in each time step are
calculated for the actual heading with respect to the waves.
The thruster forces present in the equations of motions are calcu-lated taking thruster/thruSter interactions into account [25]. Also
thrust degradation effects are considered1 due to:.
thruster-hull interaction (for bow thrusters, stern thruster as
well as if present - main propellers);
iifluence of cUrretit (using open-water diagrams fo main propel-lers and azimuthing thrusters) and.;
interaction between main propellers and stern thrusters - if
ap-plicable.
For this purpose use is made of theoretical calculations for
thruster-thruster interaction and model test data for the. other phenomena.
The control algorithm of. the D.P. simulation program is a schematic
representation of a real contrOl system. For every time step the total required restoring forces (longitudinal and transverse forces and the yaw moment) are determined using a PID controller. The coefficients of Proportional and derivative terms of the controller
are estimated using optirtum control theory [25].
The resulting required forces are divided over all available prO-pulsors using an optimizing allocation routine. This routine
mm-imises the consumed power while satisfying all three force con-straints (if within the limits of the propulsion system) and the constraints imposed by maximum and minimum thrust for each
propel-ler.
The minimization process is based on the method of Davidon,
Fletcher and Powell; it includeS a penalty function approach tO ac-cOunt for the constraints.
Finally it may be noted that the D.P. simulation program accounts for time delays caused by e.g. filtering and thruster hardware as would be found on the prototype. In practice with a low-pass filter it is neOessary to filter the position measurements, eliminating
wave frequency contributions to avoid wave frequent thruster modulation.
3.5. Short-term statistics
For a
floating vessel in waves the frequencies of wave-inducedmotions and loads are reasonably narrow-banded. In that case the significant crest-to-trough value of the stochastically varying
motion or load signal may be defined as:
al/3 '"uO - - .-,
'w,'w, - - (10)
g(v)
{F(VN)}N_l
.f(v)
in which the spectral density function
of the signal u is
ob-tained by spectral techniques from the response functions.
Generally,
the. stochastical signal u
is stationary and shows a
GauSsian distribution of the ensemble of Samples taken at constant
time intervals. The crest-to-trough values follow the Rayleigh
dis-tribution function and -the probability of exceedance Of one
indi-vidual amplitude Üa is given by:
u
-2
F()
F(ua>
= 1
-
f
f(ua)dua = exp(-
2m0
(11)
In a record of N amplitudes ÜaI the maximum value is defined as the
largest value in the ensemble
(u1....
UN). Each element jn the
ensemble has a probability density f(u). When ordering the ensemble
as to the magnitude of the elements, the probability density
func-tions of the k-th element Vk is given by Ochi and Bolton, ref.
[27]:
g(v)
= f(vk)
.(){F(vk)}k{1
- F(Vk)
. .(12)
in which
(1) is the probability that the element
is present in
the ensemble,
and
(2)
is the binomial distribution giving the probability
that the. value of
Vis indeed the k-th element in the
ordered ensentble.
The distribution of the maximum value of the ensemble (v1
is given by:
. . . .
(13)
According to Longuet-Higgins
tlie
most probable maximum value is
given by the value of vN for which
g(v) attains its peak value,
After some simplifications this requirethent leads to the familiar expression for the most probable maximum in an ensemble Of N
val-ues:
Ua max. m.pr. U1!3 v'½ in N (14)
This expression is used to relate the criteria given in Section 2.1
to limit, values of the significant motions in a sea State.
Knowing the distribution function g(v) it is possible to indicate
the confidence margins of a Rayleigh distribution. For a
stochasti-cally varying signal with N oscillations the distribution of the crest-to-trough values may be determined by statistical analysis
arid be plotted on Rayleigh distribution paper. At various
probabil-N-k+1
-ity levels (= ) the function g(v) can be evaluated and -for
instance 10%- confidence limits be indicated.
In the next section this analysis will be applied to the roll
re-.ponse of sothe tested vessels in order to discuss the validity of a Rayleigh distribution of these non-'lihear signals.
3.6. Wave. climate
Wave climate' information is Often available in terms of a so-called
scatter. diagram which relates combinations of significant wave. 'height and average wave period to the elativè frequency of occur-rence. If the operations with the vessel do not show "memory"
ef-fects
(if
e. the work can be stopped and resumed at any time withoutloss of efficiency) a Scatter diagram provides a means of calculat-ing' the average downtime due to weather. If, however, the occur-rence of downtime gives rise to inefficiencies (for instance, due to .the fact that part of the work has to be repeated or because extra work is generated) also the number of downtime periods
con-stituting the total downtime becomes an important factor in the aSsessment of the workability of the vessel.
In the present Study the prediction Of the downtime is based on a
time domain realization of sea "states" (defined arbitrarily), each defined by a (fixed) relation between wind speed, wave height and
average wave period The realizations, a "long-term" sequence of
"short-term" Sea states of constant, duration were generated
accord-ing to a method proposed by Rothkopf { 28]. At' the end Of each time step (say 2 hours) the sea state for the next time step s
gener-ated.. The probability of going from one particular sea "State'1' to any other sea "state" is given by a so-called, transition matrix; a tn-diagonal matrix, allowing only steps to adjacent sea "States", was uSed. Rothkopf shows that the transition probabilities can be derived simply from the average frequency of occurrence of each of the sea states, the average persistence of good (or bad) weather and the duration of the individual time steps. The method is
out-lined in Appendix I.
In recent years the application of this quantitative, method in the management of offshore operations has received considérablS atten-tion. One may refer to work by Shell'[2.9], 'Hoffman [3o 31], chen
[32,33], Hutchisori [34]., MacCallum [35'], Sánchez-Arcjila [36] and Kupras [37].
4. RESULTS
4.1. Ship motions
The heave and pitch motions may be determined from response func-tions applying spectral analysis techniques. For non-linear roll this technique is not, readily applicable. However, after applying equivalent linearization on the expressions for the roll damping as given by Ikeda. et al. [ii], it is possible to present the roll behaviour by carrying out speotral calculations for a ranqe of roll response functions each valid for a certain sinificant roil angle.
For the 80 m diving support vessel in beam seas the result of such an approach is shown in Figure 6. It may be concluded that non-linearity leads to relatively smaller ratios between roIl angle and wave height for increasing wave height at wave periods close to
roll resonance.
The effect of the U-type anti-roll tank is indicated in Figure 5. Due to the increase in damping the resonance peak in the roll
response. is practically diminished arid as a consequence the non-linearity in the curves is smaller. The magnitude of the roll motions of the Stabilized vessel i.s considerably less than for the unstabilized vessel. See Fiure 6. It was considered necessary to investigate whether the roll motions of this type of ship follows a
Rayleigh distribution, in order to be able to use Longuet-Higgins' expression for the most probable maximum, equation (14).
In Figure 7 is shown that the measured roIl, crest-to-trough
dis-tribution for two of the three investigate.d vessels lies, within the
10% confidence margins of the theoretical Rayleigh distribution, while the third measured distribution is somewhat at the low side. This lead to the conclusion that by applying equation (14) to re-late the most probable maximum criterion value to a significant roll limit is not unjustified but may lead to somewhat conservative
results. On the other hand it is made quite clear that the actual
maximum value encountered in an arbitrary ensemble may differ con
.siderably frOm the most probable.
In Figure 8 a comparison has been made of the pitch motiOns of, the
80 in vessel and the 110 in vessel in bow quarterin seas. The effect
of increasing the size of the ship is most prohounced in the lower
sea states with short period waves.
4.2. Moonpool relative motions
For head sea cOnditions the moonpool response function was
calcu-lated for two wave amplitudes: 1.0 m and 3.0 in. The results are
shown in Figure 9 for the 80 m vesse1 Since the relative motion is
governed by a combination of wave force, interaction effects and non-linear reaction forces, the wave height effect in the behaviour is different at different frequencies because the phase differences between the contributions vary with frequency.
Due to the reasonable symmetry of the ship with respect to the nioonpool location, the moonpool response is assumed identical for head-on and stern-on waves as well as for bow- quartering and stern
quartering waves.
It is clearly shown that the -highest relative motions may be
expected in beam sea conditions.
For the 110 in vessel the same conclusions are valid although the reduced heave motions in the shorter wave period range will
-4.2. Climate characteristics
Characteristic parameters in the present simulation procedure are the average duration of good (or bad) weather periods, their fre-quency of occurrence and the frefre-quency of occurrence of the indi-vidual sea states. Figure 10 shows the relation between the wave height and the above parameters. They were derived from the data in Figures 3 and 4 and data.presented by Vik et al. [4] and Mo ét al.
[2]. The data agree very well as far as the. number of severe storms is concerned.
Figure 11 shows the distributiOn of the duration of good weather periods as derived frOm the simulations. The results indicate a considerable spreading in the duration of good weather periods.
This tendency is reflected iti all results of the present
investiga-tion. This is also illustrated in Figure 12, in which a typical example of a climate realization is shown. The transition matrix on which the simulations ae based is shown in Table 2.
Figure 11 also Slows that if for a certain job interruption.s have very serious consequences and should be avoided, a very high aver-age operability is required.. For instance, limiting the average number of interruptions to one per thonth requires 98% average operability.
The spreading inthe results indicates that a largeaniount of reli-able data is required for a validation of the above method (or simi1ar simulation procedures). Figure 13 shows a comparison of the cumulative distributions derived from field data and simulations.
The results show considerable discrepancies, especially at the longer durations.
Wave hindcast data published by Bales [3.8] can be used to check one
of the baSic assumptions underlying the, simulation procedure. In this procedure the probability P(iI1) to remain in a particular sea
state is independent of the history of the process. The probability of exceeding a. duration of N* steps in this particular sea state
becOmes:
P(N > N* = epNmn(uI
i))
yielding an exponential distribution for P(N > N*).
In Figures 14 and 15 hindcast data for the North Sea are shown. Especially the lOwer sea states show distributions of duration which correspond very well with the above distributions. The tran-sition probabilities P(ili) derived from these data agree very well with thOse derived from the data in Figure 4 as far as the lower
5. WORKABILITY PREDICTION
As outlined in the foregoing, a workability prediction is based on a large number of data and assumptions. The input information
con-sists of:.
Ship data:
- dynamic positioning characteristics;
- frequency response functions for all required quantities;
- wave climate informatiOn in terms of the frequency of occurrence of sea .tate and the frequency or average duration of workable
sea states.
Operational data:
a set of criteria for operable weather conditions;. - a stt.ategy for the operation.
One of the basic assumptions in the wo;kability prediction method is the applicability of the Rayleigh distribution for the predic-tion of extreme values. This assumppredic-tion was discussed in Secpredic-tion 4
and in ref. [39 and 4.0].
It is essential to realize that the output information (the down-time, job duration, etc.) must be regarded as a stochastic vari-able. If the operational scenario is very complex and the simula-tion time is restricted statistical tests may be required. to judge
the significance of the results [41].
5..l.Workability in beam seas
A rough indication of the downtime in beam seas can be obtained by disregarding the effects of the operations scenario, See Figure 16. It shows that the roll response limits operations over nearly the entire wave period range prevailing in the scatter diagram. In
short period waves the relative wave elevation in the moonpool iS a limIting factor. The acceleration limitS are not indjcated in Fig-ure 16 because these appear not to be a determining factor in the workability prediction. The average workability and the effect of
the anti-roll tank is indicated below:
80 m diving support vessel average workability in beam seas
Stabilized 47%
Unstabilized 33%
Consideing the operational limitS impoed by the relative wave elevation in the present moonpool design, it must be concluded that it is no use to further decrease the roll response -if
possible-for it will not yield a larger operability.
In Figure 16 also the limiting sea states for dynamic positioning are indicated. Two values of the available thruster power are
i-n-vestigated and the results.
5.2. Workability in bow quartering waves
Figure 17 indicates that the roll motions in bow quartering seas are, like it was in beam seas, a major factor limiting the opera-tions of a diving support vessel. In short period waves the pitch response becomes a limiting factor. As in the beam seas case the accelerations are not a determining factor for the workability. Disregarding the operations scenario the workability becomes as
Average workability
in bow quartering waves
Vessel 80 m 80 m
110 m
Anti-roll tank no yes no
Criteria: roll only
pitch only heave only
roll, pitch and heave
The dynamic positioning simulations
for bow quartering waves reveal
that the reduction in thruster power from (0.8 0.8 MW) fore and
(1.5 + 1.5 MW) aft to (0.4 + 0.4 MW) fore and (1.0 +
1.0 MW) aft is
hardly affecting the workability of the 80 m vessel since the roll
and pitch requirements prevail (see Figure 18).
The limit sea State for the lowest thruster power configuration in
the. long wave period range is about 4 m significant
wave height,
mainly due to the associated wind speed. In the Short wave period range the wave drift forces are dominant and the limiting
condi-tions become lower with decreasing wave period
Weather simulations for workability in bow quartering waves
Assuming a job which requires 240 hours to complete in ideal
weath-er conditions, simulations were made to predict the
characteristics
Of the actual job durations in the North Sea wave climate.
The re-sult
are ifidicated in Table 3 and Figures 19 and 20. The limit sea
state serving as start and stop criterion was derived
from the
limiting Sea states in Figure 17. It was assumed that work could be
stopped without loss of efficiency and could be resumed without delay as the starting/stopping criterion was met.
45% 71% 97%
66% 66% 78%
93% 93% 96%
The spreading in the düratiôn of the workable periods is reflected in the duration of the jobs. Operating at a w average workability
drastically increases the spreading of, the. job durations leading to. occurrence of excessive job durations.
5.4. Scenario.
A penalty on the interruptior of a job is an example of a. sitnpie
operational. scenario. The simulation for the stabilized 80 m vessel in bow quartering Seas. was repeated with a. penalty of 24 hours on
every interruption due to adverse weather. In Figure 21 arid Table 3
the cumulative, distributions of the job durations are compared. It is shown that te average job duration. increases by some 60% be-cause the good weather periods of short duration give no progress in. the work. Also the spreading is wider, i.ea 10% of the jobs 'wOuld last lOnger than 1070 hours, whereas the simulations without penalty indicate a job duration of only 5 hours at this 10% ex
6. CONCLUSIONS
Regarding the results of the preSent investigation the following
conclusiOns seem justified:
The roll respOnse of diving support Vessels.is a major factor in limiting diving operations. Installation of an anti-roll tank
may be very useful in reducing the downtime.
The duration of workable periods of time Shows a very large spreading1 which. is reflected in all results. This phenomenon may lead to large differences in job completion time between
otherwisS similar veSsels on similar jobs.
Although simulation procedures based on the tn-diagonal transi-tion matrices are widely used, the basic assumptransi-tions uhderiing the procedure have not been validated thotoughly. In this re-spect the neglection of physical wave growth and decay processes
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"Kryloff-Bogoliubo.ff's solution to decaying oscillations. in. marine systems". ISP, Vol. 27, No. 313, 1980.
G!F. KnOtt and J.0. Flower:
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"Prediction of wind and current loads on VLCC's". Oil
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"Rules for the construction and classification of mobile off-shore units", Det Norske Veritas, 1975 (reprint 1980) and 1983..
J.A. Pinkster:
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J.A. Pinkster:
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vesSels moored at
sea". Paper SPE 4837, EUropa Spring Meeting
of SPE-AIME, Amsterdam, 1974..
J.A. Pinkster:
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Department of Experimental Methods in Mechanics, Udine,
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APPENDIX I
Definitions and notations in the climate description
Each climate record is regarded as a sequence of
short-term sea "states" in which the environmental conditions
are assumed to be stationary. Each "state" can represent an arbitrary
combination of
wind speed and direction, current speed and direction,
wave height
and, period, spectral shape and direction. rn the
present method,
sea states are defined following the Beaufort scale and assuming so-linear wind and waves.
Workable or "good" weather of class i is defined as a period of time in which the waves are lower than those in class i (those of
class 1 to i-i). The trafisitjon from one individual
sea -state i to
the sea state in the next time step is given by
a tn-diagonal transition matrix, which allows the continuation of
sea state i, increasing the sea state to state 1+1 or decreasing
the sea state to i-i. The related probabilities are. denoted
as
P(iIi),
P(i+lJi)and P(i-lJi).
The average duration of a period of workable weather
equals the total amount of time spent in workable sea states
divided by the number of workable periods. If the frequency of occurrence of each
sea state is given by f(i,) it is given by:
i-i Z f(j) = j=1
-GWP''
-NGWP (i) with:NGWP = average nurtber of workable periods per unit of time
= average duration of workable periods
GWP
i-i
E f(i) = fraction of time spent in workable
sea states. i=l
The probability of starting or ending a period of workable weather
at an arbitrary time step equals the ratio of the average number Of
workable periods per unit of time and the number of
simulation steps per unit of time:
(i)
PGW(1)
=l/t
t 1 . . . .1-2
It. equals the probability of entering a workable period, down from
sea state i to i-i Or -leaving a workable period from sea State i-i up o Sea state i:
GWP = f(i)
P(i-lIi)
=f(i-l)P(iI
The average duration Of a period of downtime (time steps with sea
states i, i+1, ..., n) follows froth the total amount of time spent in non-workable, periods and the average number of non-workable
periods: -i-i f(j) 1 - E. f(j) Ci) ,-BWP -
-BWPNw
with representing the average numTber of non-workable periods
per unit of time; which 'of, course equals the average number of
wOrkable periods NGWP!
Based on information on the average number of workable weather win dows or their duration the transition probabilities follow from:
p(i-iJ
i) (t-3) 1 E f(j) =-1 PGWP(1+l)t
,(i+l) P(i+lIi) - ,-, GW f(j)fU)
Gwp(i+l) f(i) tNGwP(1) :f(i) f(i) DGWP(1) f(i)
-(I-5a)
P(.iJi)
1 - P(i+lJi)P(i-j.Ij)
Keeping in mind tha Ue average nUmber of
workable periods equals the average number of downtime periods the above can also be ex
pressed in terms. of the average length of the downtie
periods: P(i+1
Ii)
P(i-iJi) = PBwp(+1)BwP'
f(i) f(i) DBWP PBWP(1)Lt.wp(i)
f(i) f(i) BWPor:.
P(i-lIj)
=P(i!j-l) . . . . . . . (I-Sc) and.: n E f(j) j=t±1 f(i) n Z f(j) f(U
(1-6)
(I-7a) (r-.7b)P(iji) = 1 -
P(i+lIi)
-
P(i-lji)1+1 Sea i
state
i-i
Time
Figure I-A - Climate S ulation procedures
Downtime Downtime
Sea state at t+t bra *
Figure I-B - Transition matrix
1 2 3 i-I i i+1 n-i n
1 2 3 i-i i i+1 ñ-1 -n
(I)
P(112) P(2i) P(212) P(2J3) P(32) P(313) P(4f P(i-21i-1) P(i-lk-1) P(i-1i)-pciliii
P(ili) P(ili+i) P(i+lIi) P(I+iJi+1) P(i+21j+i) P(n-21n-1) P(n-1n-1) P(n-lIn) P(nln-1) P(n!n) + Sea State at t braPP power anti-roll tank in 0 110 B m 16.2 22.3 P. rn, 4.4 6.0 - 0f7 0.7 v 3992 10303 in 1.5 1.5 9.6 13.1 in water - 0.36 0.36 -- 0.25 0.25 Iloonpool; diameter in 6.0 6.0 locatiOn - St. 8, St. 8,
centre -line centre .1-me
Thrusters: Bow tunnel;
locations - St 18 5 and 19 St 18 5 and 19
diameter rn 2.0 2.0
power - MW 0..8 0.4
Stern thruster:
locations - St 1, 4 0 rn St 1, 4 0 in
from centre line from centre line
diameter in 2.2 2.2 power MW 1.5 - 1.0 Bilge keels: length in 0.35 L 0.35 height in 0 45 0 45 Ahti-roll tmk: type -. U-tank length 'in 8.0 duct height m 0.8
wing tank width in 2 5
volume . rn3
-Table 2 - Transition matrix 1 0.944 0.056 0.000 0.000 0.000 0.000 0.000 p.000 2 0.031 0.919 0.050 O.000 0.000 0.000 0.000 0.000 3 0.00O 0.085 0.849 0.066 0.000 0.000 0.000 0.000 4 0.000 0.000 0.134 0.786 0.080 0.000 0.000 0.000 0.000 0.000 0.000 0.177 0.739 0.084 0.000 0.000 0.000 0.000 0.000 0.000 0.228 0.664 0.108 0.000 000O 0,:000 0.:000 0.000 0.000 0.323 0.524 0.152 8 0.000 0.000 0.000 0.000 0,000 0.000 0.913 0.087
Sea Séã state T+2 (hours)
state T
TabIe 3 - Effect of roll stabilization aid ship size onworkability
Scenario: job duration calm water : 240 hours
Criteria for Stopping/resuming operations: 2+1,3 = 6 deg. Heading : bow quartering seas
Desôription Unit 80 m vessel
unstabilized 80 m vessel stabilized 110 m vessel unstabilized Climate characteristics:
I4miting wave height m 1.6 2.2 2.2 2.8
Average duration wokable periods hrs 49.3 71.1 71.1 103.8 Standard deviation düràtion
workable periods hrs 33.1 63.8- 63.8 94.5
Nuiner of workable periods per year - 80.3 92.0 92.0 66.0
Job óharacteristics:
Penalty on interrupting operations hrs 0 0 24 0
Average duration hrs 529.2 356.5 569.3 30.7
Standard deviation duration hrs 285.4 188.1 325.7 157.7
Duration with 10% exceedance hrs 805.0 512.0 1070.0 410.0
12 0 0 0 0 11 94 17
/
8 .73 011/
K1
0 0 0>7
0 8 12Mean Zero-UpCrosSing period T2 (s)
Figure 2 Wave climate scatter diagram
11(
49 58 61 12 23 11 4 25 6 2 20100 50 c3 !11 <1:rn: <4 m <5 rn <. rn <7 rn 10 20 50 Duration (hours) 100 200 500 1000
Figure 3 - Cumulative distribution Of good weather periods during
10000 5000 1000 DGWP 500, (hours) 10 0 Number of periods Duration GWP 2 £ Mo et al. [2]
Viketal. (4]
* In house dataFigure 4 - Number of good weather periods per hour and average
duration as a function of wave height (North Sea)
10 3 5 6 8 9 10 ç113 (m) 500 50 GWP (1/hour) S 100 50
-15 for a1/3 = 10 deg.
I
/
/
/
/
,
6 al/3 10 deg. = 15 deg. 0.5 1.0 1.. 5 w (rad/s)Fiure 5 - Roll response fr 80 i diving uppor-t vessel in regular
beam waves
10
E
-w
C) 30 20 10 0 Stabilized ----Unstabilized 10.2-11..1 / / / / / /
1/
/
/
/
i' .6 5.6 6.5/7//,
i1i '/7/.
0 5 10 15 ZW1I3 (m)102 99 90 70 50 C) 14 U S 30 U C) S (0 C, .0, C, C) '4-4 0 >1 -4 .0 I0 .0 0 14 1 0.1. 0 V S.
'
Research vesselDiving support vessel
IPilot vessel
-'
/
igure 7 - Distribution of measured crest-to-trough values for roll
in .i.rregular beam seas (resonance conditions)
10
5
Bow quartering seas - JONSWAP
80 spectra - in vessel 110 in vessel 5.6-6.5
6.5-7.5/
8.4 10.3/
10.3/
.1Ii ;',1"
/
-Il/ri t
I,,,, /
1/1/
,T2=4.6s
0 5 10 15 w1/3 (rn)in in 2. 0 4th 0 in L 4.) 0 .0 0. 0 3. 0
Ca1cuation for 1 tn wave amp1itue
Cculai for 3mwaveàmplitude
Beam waves 6'
1g,7j...
it.-\
\
\
..
/
\
'-
.!___-...'
.--'
ii
. Head waves - / ¼.' .%\
\
0 05 1.0 1.5Wave frequency (rad/s)
Fiure 9
MOorpoo]. response functions for 80 tin diving support
2 5 5.0 7.5 w1/3 max. (in)
14 a) 100 0.1 -
---1-H
F---2.8 2. 2 1 .6 -Lih-i ting wak7e height (m) 10 100 1000 10000 Duration (hours)6 2 0-0
'u
a
ma
a
a,
--
---
---U
LA
uauaasaumaaaaaaaaaai
amaaaaaaaaaaaaaaaau
uaaaaaaaaaauaaaaaaaa
ammamamanaimammamu
10 10 20 20 30 30 40 40 0 10 20 30 40 Time (days)Figure 12 - Sample climate. rea1.zations
8
6
4
2
1000
-
aon
--Field data
10 - 100 1000 10000
Duration (hours)
Figure 13 Cumulative distribution, of duration of good weather periods
1.0
05
0 2 a) c01
a) 0.05 x a). 141 0 0.02 a) 0.01 0.005 0.002 0.001 0 w1'3 = 2-3 in o'
1-2xn A Duration (hours)Figure 14. - Cumulative distribution f duration, of individual sea
states .
1.0 0.5
02
0.i
a, 0.005 0.0020.00i
8-9 in ' o 6-7xn a =5-6ni-A 4-5m b 3-4m -I' 0.05 l.i 0 0.02 -a, 0.01-0 12 24 - 36 48 60 72 84 Dutation (hours)Figure 15 - Cumulative distribution of duration Of individual sea
12
0
Beam seas - V5 = 0 kn. - JONSWAP spectra
High power thrusters 0 0
1
0: Low power thrusters 4 Transverse::::ti01.1
0 -i-Heave Roll: stabilized Lunstabjljzed&I
.. . '4I 20 4 5 55 58 49 23 1 4(
it
o'
8 12 16Mean zero-uperossing period T2 (s)
12
Bow quartering seas - 0 kn. JONSWAP spectra
80 vessel vessel
---110
in ino'
oo4jo
(stabilized) i \ 0 1 0 4 i o (unstabilized)I
\\ \
o1
Pitch 0 i7 'S256
1\
11 12 61 94\__._;__'
82 31 29 03O
Heave 5 5 0 0 16 120 141 732o-4-2---crt
Roll (unstabilized) 55558492311
4 2 1 0 0 4 8 12 16Mean zero-uperossing period Cs)
Figure 17 -. Workability of 80 m and 110 n diving support vessel in bOw quartering seas
:..
.wA10
3.5
1 O
S
11 4 2 1
Low power thrusters
Pitch 80 m vessel 110 m vessel High power thrusters Roll: stab iii zéd uristabilized 12 4
Bow quartering seas - V = 0 kn. JONSWAP spectra
Mean zero-uperossing period
2
Figure 18 Workability of 80 m diving support vessel in bow
quartering seas
0.4 0.3 0.2 110 in vessel. unstabilized 0.1 >1 C) C) 0 I, -C) 0.2 80 rn vessel 0.1 stahi lizéd 0.2 80 in vessel 0.1 unstàbilized 200 400 600 800 1000 1200 1400
Job duration (hours)
1.0 0.00.1 80 in vessel stabi 1 izéd 110 In vessel unstabilized 8.0 th vessel uristabilized
Excess duration (hours)
Figure 20 Cumulative distribution of job duration
(exöess o 240 hburs daith water duration)
1.0 w C) C 0.1 C) a, U.' 0 >1 C) C a, 0.01 a, 0.001 24 hOur penalty on interruption of operations 0 penalty 80 in vessel stabilized 0 250 500 - 750 000
Excess dürat-jon (hours)
Figure 21 - Cumulative, distribution of job duration (excess of 240 hours cairn water duration)