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CPP propeller - Towards high performance pitch control - Wärtsilä

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WÄRTSILÄ TECHNICAL JOURNAL 01.2008<br />

<strong>Towards</strong> <strong>high</strong> <strong>performance</strong> <strong>pitch</strong> <strong>control</strong><br />

AUTHOR: Milinko Godjevac, Research Engineer, Wärtsilä in the Netherlands<br />

This article discusses a novel <strong>control</strong> strategy for a <strong>control</strong>lable <strong>pitch</strong> <strong>propeller</strong> (<strong>CPP</strong>) driven by a diesel engine.<br />

This new <strong>control</strong> strategy should contribute to more effective use of the complete power train.<br />

Fig. 1 – Dredger and its <strong>control</strong> system.<br />

Load<br />

<strong>control</strong><br />

Setpoint<br />

load<br />

prop. shaft torque<br />

Pitch<br />

<strong>control</strong><br />

Setpoint<br />

<strong>pitch</strong><br />

Mechanical load<br />

Setpoint<br />

speed<br />

Electrical load<br />

Electronical load sharing<br />

communication when<br />

running parallel<br />

Pitch<br />

feedback<br />

hydraulics<br />

Speed<br />

governor<br />

VIKING 25<br />

Propulsion gearbox<br />

OD<br />

box<br />

6.6 kV<br />

10MW<br />

Propulsion<br />

clutch<br />

Flywheel<br />

Wärtsilä<br />

12V46<br />

Main<br />

generator<br />

Fuel preservation is important for the future of mankind.<br />

Any increase in efficiency offers not only fuel savings,<br />

but also reduced engine emissions and more ecological<br />

solutions. For this reason, <strong>control</strong> strategies for developing<br />

<strong>high</strong>ly efficient propulsive thrust to a ship are important.<br />

The traditional ship with a <strong>CPP</strong>, driven by a diesel<br />

engine, is <strong>control</strong>led via the “combinator”, which sets<br />

the optimum combination of <strong>pitch</strong> and shaft rotational<br />

speed for stationary ship conditions at no waves and other<br />

added ship resistance conditions (“ideal” condition). The<br />

combinator consists of running up/down and look-up<br />

tables for the (pre-set) optimal <strong>pitch</strong> and rotational speed<br />

combination. The “optimum” is not only influenced<br />

by fuel consumption considerations, but also by the<br />

<strong>propeller</strong> noise and cavitation issues. In contrast to ideal<br />

conditions, at sea or maneuvering conditions necessitate<br />

the adjustment of shaft speed and/or <strong>pitch</strong>. In references<br />

[1] and [2] it was also shown that engine speed<br />

disturbances, caused by the seaway, could be suppressed<br />

better by <strong>pitch</strong> <strong>control</strong> than by <strong>control</strong>ling the fuel rack.<br />

The time needed to get the rotational shafting (diesel<br />

engine, gearbox and <strong>propeller</strong>) from one shaft-speed level<br />

to another is measured in the magnitude of a few seconds.<br />

For ships with large power take-offs using generators, the<br />

<strong>CPP</strong> <strong>pitch</strong> is used to compensate for fast and <strong>high</strong> frequent<br />

load changes of the generator, as well as for the seaway. For<br />

dredgers (see Figure 1), the generator is used to drive the<br />

dredge pump, which can jump in load from minimum to<br />

maximum and vice versa, rather quickly. The diesel engine<br />

load is kept constant by continuous and fast <strong>pitch</strong> changes.<br />

The existing situation<br />

Figure 2 shows the simplified <strong>CPP</strong> actuating system and<br />

<strong>pitch</strong> <strong>control</strong>. The oil volumes in the <strong>pitch</strong> actuating<br />

cylinder and the oil pipelines are <strong>control</strong>led by counter<br />

balancing valves. When no pressure exists at the ahead<br />

and astern ports of the oil-distribution box, these counter<br />

balancing valves (CBV) are closing. When these are closed,<br />

the <strong>propeller</strong> <strong>pitch</strong> stays as it is. These counter balance<br />

valves, together with the proportional valves with load<br />

sensing, make the task of the <strong>pitch</strong> <strong>control</strong>ler rather easy.<br />

But the cost is a rather slow actuating <strong>pitch</strong>, which can<br />

have different dead times from one <strong>pitch</strong> change to another.<br />

This has to be overcome in order to have fast and accurate<br />

<strong>pitch</strong> <strong>control</strong>.<br />

p<br />

in detail 49


[ MARINE / IN DETAIL ]<br />

[ MARINE / IN DETAIL ]<br />

Fig. 2 – Simplified <strong>CPP</strong> <strong>control</strong> system.<br />

p S<br />

, p C1<br />

, p C2<br />

(bar)<br />

Fig. 4 – Block diagram of the new pressure <strong>control</strong>ler.<br />

50 in detail<br />

feedback sensor<br />

header tank<br />

or pump<br />

xy<br />

U pv<br />

Valve<br />

drive<br />

Pitch<br />

Controller<br />

0 set<br />

Pitch setpoint<br />

OD-box<br />

Q C1<br />

, p C1<br />

p S<br />

, Q S<br />

CBV<br />

Q C2<br />

, p C2<br />

i 1<br />

i 2<br />

proportional<br />

valve<br />

p S<br />

, p C1<br />

, p C2<br />

, p H1<br />

(bar)<br />

p R<br />

, Q R<br />

<strong>pitch</strong> ahead<br />

p H<br />

hub<br />

load<br />

sensing<br />

setp.<br />

valve<br />

<strong>pitch</strong><br />

Fig. 3 – Modeled and measured results of <strong>CPP</strong> actuating model and <strong>pitch</strong> <strong>control</strong>.<br />

load-sensing <strong>control</strong><br />

pressure <strong>control</strong><br />

<strong>pitch</strong> position <strong>control</strong><br />

P v,max<br />

S<br />

(C|D)&E<br />

α act<br />

+<br />

C+<br />

S 2<br />

–<br />

S 1<br />

+<br />

–(C|D)<br />

N<br />

A|C<br />

4 + –<br />

u<br />

B|D S 5<br />

P ahead<br />

P astern<br />

ΔP is<br />

α ref<br />

C<br />

+<br />

–<br />

C ΔP_yoke<br />

C <strong>pitch</strong><br />

D C+δ D+δ<br />

C load sensing<br />

i prv<br />

p S<br />

p C1<br />

p C2<br />

p H1<br />

E<br />

(C|D)&E<br />

S 6<br />

+<br />

C main valve<br />

X m, ref –<br />

i valve<br />

–(C+δ/D+δ)<br />

X m, act<br />

main spool<br />

position <strong>control</strong><br />

The current situation for in-stationary<br />

maneuvering conditions and for increased<br />

vessel resistance in seaway, calls for a “load<br />

<strong>control</strong>” to be used. The traditional load<br />

<strong>control</strong> performs rather coarsely and is not<br />

able to precisely <strong>control</strong> the diesel engine<br />

load as a function of the actual shaft speed.<br />

This load <strong>control</strong> overrides the <strong>pitch</strong> set by<br />

the combinator, and reduces it in order to<br />

keep the diesel engine within its operating<br />

envelope. To avoid unnecessary <strong>pitch</strong><br />

changes in adverse weather, the passive<br />

load <strong>control</strong> is provided with an automatic<br />

adjusting dead zone. When <strong>pitch</strong><br />

fluctuations, caused by the passive load<br />

<strong>control</strong> action, are sensed and when these<br />

are periodic, the dead zone will be<br />

increased step by step until the periodic<br />

fluctuations have been removed. In heavy<br />

seaway, this results in an increased service<br />

margin and reduced average diesel engine<br />

loads of up to 60 or 70% of the CSR point.<br />

This passive load <strong>control</strong> automatically<br />

takes care of “good seamanship” needs,<br />

but it results in a lack of usage of the<br />

propulsion plant.<br />

As opposed to passive load <strong>control</strong>,<br />

active load <strong>control</strong> implies an active <strong>pitch</strong><br />

change in order to keep the load on the<br />

engine under <strong>control</strong>. This was investigated<br />

in [3] where the measurements were<br />

carried out on board a 9000 cargo tonner.<br />

These measurements indicate active load<br />

<strong>control</strong> as being ineffective and causing<br />

additional wear to the <strong>pitch</strong> adjusting<br />

system. However, looking at the spectrum<br />

analysis presented in the report [3], it can<br />

be clearly seen that the <strong>pitch</strong> adjusting<br />

system was three to four times slower<br />

than necessary to suppress torque<br />

oscillations. Thus these measurements and<br />

conclusions needed further investigation.<br />

In order to investigate if the load<br />

<strong>control</strong> could be used in the seaway, the<br />

<strong>CPP</strong> actuation and <strong>control</strong> system has<br />

been mathematically modelled [4].<br />

The model contains the following main<br />

elements:<br />

Pitch actuating mechanism.<br />

External <strong>pitch</strong> actuating force model<br />

(hydro-dynamic forces and moments).<br />

Hub mounted <strong>pitch</strong>-actuating cylinder.<br />

Oil supply lines and <strong>pitch</strong><br />

feedback pipes.<br />

Counter balance valve.<br />

Oil-distribution box.<br />

Hydraulic proportional valves,<br />

load sensing and pumps.<br />

Feedback sensors and <strong>pitch</strong><br />

closed loop <strong>control</strong>ler.


WÄRTSILÄ TECHNICAL JOURNAL 01.2008<br />

The study indicated that the response<br />

of the <strong>CPP</strong> system is slow, mainly because<br />

of the fact that oil has to be compressed<br />

prior to each <strong>pitch</strong> change. The oil must<br />

be compressed to the point that the hub<br />

pressure reaches the threshold level of the<br />

Coulomb friction. The dead time before<br />

<strong>pitch</strong> change can easily vary from 0.5<br />

seconds to 3.0 seconds. Figure 3<br />

shows modeled and measured results<br />

for the <strong>pitch</strong> change. The results show<br />

good correlation between the model<br />

and the actual response as measured.<br />

brake cylinder<br />

frame<br />

brake<br />

leakage valve<br />

mass actuator<br />

Schematical drawing of the test bench.<br />

load<br />

Pressure <strong>control</strong><br />

In the <strong>control</strong>lable <strong>pitch</strong> <strong>propeller</strong>, a<br />

counter balance valve is installed in the<br />

shaft line in order to maintain the <strong>pitch</strong><br />

should the hydraulics fail. In the new<br />

<strong>control</strong>ler, the counter balance valve is<br />

kept open whilst there is no change in<br />

<strong>pitch</strong>. This required the <strong>control</strong> strategy to<br />

be changed. Whilst there was no change<br />

in <strong>pitch</strong> position, the hydraulic pressure<br />

had to ensure that the <strong>pitch</strong> could not<br />

change, but as soon as a change of <strong>pitch</strong><br />

becomes necessary, the position <strong>control</strong><br />

actuates the yoke so that the desired <strong>pitch</strong><br />

is achieved. Then it is switched back to<br />

differential pressure <strong>control</strong> to maintain<br />

the <strong>pitch</strong>. Figure 4 shows the new <strong>control</strong><br />

strategy [5], which will be described below.<br />

When the <strong>pitch</strong> setpoint α ref<br />

changes,<br />

the <strong>pitch</strong> error increases so that condition<br />

C or D becomes true as soon as the <strong>pitch</strong><br />

error exceeds a certain value. Condition C<br />

indicates that the <strong>pitch</strong> error is negative,<br />

meaning that the <strong>pitch</strong> α act<br />

has to be<br />

decreased, while condition D indicates<br />

the opposite. Assuming that the <strong>pitch</strong><br />

has to be increased (condition D is true),<br />

the pressure <strong>control</strong>ler will increase the<br />

differential pressure in the hub-cylinder to<br />

the upper limit of the friction band. This<br />

is ensured by condition D switching S4 to<br />

set the upper part of the curve. In this way,<br />

the Coulomb friction band in the system is<br />

quickly crossed as pressure buildup is more<br />

efficient when carried out by a pressure<br />

<strong>control</strong>ler than by a position <strong>control</strong>ler.<br />

When the required differential pressure<br />

is set by the pressure <strong>control</strong>ler CΔ P_yoke<br />

with certain accuracy, condition E<br />

becomes true, so that S6 switches from<br />

pressure <strong>control</strong> to <strong>pitch</strong> position <strong>control</strong>.<br />

At the same time, S2 activates the<br />

electronic load-sensing to ensure a loadindependent<br />

yoke speed when the <strong>pitch</strong><br />

is changed, which is done by the <strong>pitch</strong><br />

Fig. 5 – Test bench set-up.<br />

position <strong>control</strong>ler C <strong>pitch</strong><br />

. The reference<br />

<strong>pitch</strong> is set δ more accurately than an<br />

error in the <strong>pitch</strong> is detected to prevent<br />

chattering and unwanted switching<br />

between the pressure and position <strong>control</strong>.<br />

When the required <strong>pitch</strong> is achieved,<br />

S6 switches back to pressure <strong>control</strong> and<br />

load sensing is turned off by S2. Now the<br />

pressure <strong>control</strong>ler sets the differential<br />

pressure needed to hold the <strong>pitch</strong>, given by<br />

the mean between the upper and the lower<br />

part of the exemplified curve of Figure 2.<br />

When the <strong>pitch</strong> set point changes, or<br />

when the pressure difference set to hold<br />

the <strong>pitch</strong> is not adequate due to changes in<br />

the seaway or weather leading to a change<br />

in <strong>pitch</strong>, the same procedure starts again to<br />

match the actual <strong>pitch</strong> with its set point.<br />

Note that the validity of Figure 2 can<br />

be extended by taking shaft speed N and<br />

ship speed through water u into account,<br />

as <strong>pitch</strong>, shaft speed, and ship speed<br />

define the thrust and the hydrodynamic<br />

forces acting on the blades, thus the <strong>pitch</strong><br />

actuating force. This extension would<br />

make the pressure <strong>control</strong>ler more reliable.<br />

In house tests<br />

In order to verify the model shown in<br />

Figure 4, a special test set-up has been<br />

constructed in Wärtsilä in the Netherlands.<br />

Figure 5 shows the test bench set-up.<br />

Results obtained from the workshop test<br />

bench indicate a better <strong>performance</strong> with<br />

the new <strong>control</strong> strategy and a reduction in<br />

dead time, Figure 6 shows the results from<br />

the new and old <strong>control</strong>lers. With the<br />

new <strong>control</strong>ler, it appears to be possible to<br />

follow seaway, because a sine as a <strong>pitch</strong> set<br />

point having a frequency of 0.1 Hz (wave<br />

encounter frequency) and an amplitude<br />

of 10% of the stroke, can be tracked.<br />

During the test bench measurements,<br />

it became clear that the non-linear<br />

differential pressure <strong>control</strong>ler is<br />

substantially faster than a linear differential<br />

pressure <strong>control</strong>ler. Furthermore, with<br />

the new <strong>control</strong> strategy switching<br />

between pressure and position <strong>control</strong>,<br />

the <strong>pitch</strong> can be set in a system with<br />

<strong>high</strong> Coulomb friction and a load<br />

force while no instability occurs. p<br />

in detail 51


[ MARINE / IN DETAIL ]<br />

[ MARINE / IN DETAIL ]<br />

position [%]<br />

position [%]<br />

Fig. 6 – Seaway simulation for a pressure (up) and position (bottom) <strong>control</strong>ler.<br />

power (%)<br />

10<br />

0<br />

–10<br />

10<br />

0<br />

–10<br />

5 10 15 20 25 30 35 40<br />

5 10 15 20 25 30 35 40<br />

100<br />

80<br />

60<br />

40<br />

20<br />

load limit<br />

load <strong>control</strong> curve<br />

f 1<br />

f 4<br />

f 5<br />

f 2<br />

f 3<br />

0 20 40 60 80 100<br />

rpm (%)<br />

a1<br />

a2<br />

a3<br />

a4<br />

a5<br />

old<br />

new<br />

V<br />

0.93V<br />

0.86V<br />

0.71V<br />

lines of specific<br />

fuel consumption<br />

(kg kW 1 h –1 )<br />

respect to the reliability of the mechanical<br />

system. The dynamics of the oil pipes<br />

and the response of the hydraulic system<br />

are shifting towards a resonant frequency.<br />

Friction in the system introduces<br />

non-linear effects and makes tuning of<br />

the <strong>control</strong>ler very difficult. Last but not<br />

least, tribology and reliability aspects<br />

of the bearings have to be considered.<br />

More active <strong>pitch</strong> <strong>control</strong> means more<br />

movement and would therefore result<br />

in <strong>high</strong>er wear. In [6] the big amplitude<br />

sliding has been reported as not being a<br />

problem for conventional use of a <strong>CPP</strong><br />

under designed conditions. However,<br />

this <strong>high</strong> <strong>control</strong> means more small<br />

amplitude and (relatively) <strong>high</strong> frequency<br />

sliding, which should be done in such<br />

a manner that fretting will not occur.<br />

On the other hand, the operation of<br />

a <strong>CPP</strong> in seaways is easily carried out<br />

in an improper manner causing <strong>control</strong><br />

movement due to a mismatch between<br />

the seaway and the actuator. From several<br />

references (vessels which are currently<br />

in operation) where a more active <strong>pitch</strong><br />

<strong>control</strong> has been used, the indication is<br />

that this has never led to increased wear<br />

problems. Also, the misuse of the <strong>CPP</strong> will<br />

lead to increased dynamic loads. Without<br />

improvements to the hydraulic system,<br />

the use of the <strong>CPP</strong> in seaways would be<br />

too slow to follow the wave and would<br />

lead to increased dynamic loads. For new<br />

ship systems where such a solution needs<br />

consideration, the consequence of the<br />

increased use should be studied as well.<br />

When done properly, it is expected that the<br />

new solution will contribute to fuel savings<br />

by a factor of several percentage points.<br />

Fig. 7 – Operating envelope of a propulsion plant.<br />

CONCLUSION<br />

There are two main applications that can<br />

benefit from the present work, but both<br />

have the same starting point. The work<br />

presented above is an attempt to make the<br />

<strong>pitch</strong> <strong>control</strong> faster and more dynamic,<br />

thereby giving a reduced service margin.<br />

The first application is for dredgers, where<br />

the reduced service margin results in<br />

more power for the dredging equipment,<br />

and quicker suppression of disturbances.<br />

The second application is for cargo ships<br />

52 in detail<br />

sailing in rough seas. Figure 7 shows the<br />

operating envelope of a propulsion plant,<br />

with the old <strong>control</strong> system propulsion<br />

plant operating in the red point. With the<br />

new <strong>control</strong> system, the service margin<br />

would be smaller and the operating point<br />

will go up. These effects result in <strong>high</strong>er<br />

speed and lower fuel consumption, a<br />

rough estimate of which is between 2 and<br />

5% of the specific fuel consumption.<br />

However, besides the benefits, there<br />

are several issues to be considered with<br />

REFERENCES:<br />

1. H T Grimmelius, D Stapersma, ‘Control<br />

optimisation and load prediction for<br />

marine diesel engines using a mean<br />

value simulation model’, ENSUS 2000,<br />

Newcastle-upon-Tyne (September 2000).<br />

2. H T Grimmelius, D Stapersma, ‘The impact<br />

of propulsion plant <strong>control</strong> on diesel engine<br />

thermal loading’, CIMAC Conference,<br />

Hamburg (May 2001).<br />

3. S. van der Steenhoven, ‘Monitoring 9000<br />

tonner’, Wärtsilä internal report,<br />

(September 2003).<br />

4. J. Bakker, A. Wesselink, ‘The use of nonlinear<br />

models in the analysis of <strong>CPP</strong><br />

actuator behavior’, WMTC Conference,<br />

London (March 2006).<br />

5. J.H.H. Huijbers, ‘Non-linear <strong>propeller</strong><br />

<strong>pitch</strong> <strong>control</strong>’, MSc thesis, TU Eindhoven,<br />

(December 2007).<br />

6. M. Godjevac, T. van Beek, H. Grimmelius,<br />

D. Stapersma, ‘Wear mechanism of a <strong>CPP</strong>’,<br />

WMTC Conference, London (March 2006).

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