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Engine power, %R1<br />

100<br />

R1<br />

R1+<br />

Engine power, %R1<br />

100<br />

R1<br />

90<br />

R3<br />

90<br />

80<br />

R3<br />

Rx1<br />

Rx2<br />

Rating line<br />

slope = α<br />

80<br />

R4<br />

R2<br />

R2+<br />

70<br />

R4<br />

R2<br />

80<br />

90<br />

100<br />

Engine speed, %R1<br />

60<br />

70<br />

80<br />

90<br />

100<br />

Engine speed, %R1<br />

Fig. 2: For the RT-flex82C, RTA82C, RT-flex82T and<br />

RTA82T engines the layout fields are exten<strong>de</strong>d to the ratings<br />

R1+ and R2+ at the same powers as R1 and R2 respectively<br />

but with increased shaft speed.<br />

[08#049]<br />

that the lower CMCR speeds allow flexibility in<br />

selection of the optimum propeller with consequent<br />

benefits in propulsion efficiency and thus lower fuel<br />

consumption in terms of tonnes per day.<br />

One feature to be borne in mind when selecting<br />

the rating point for the <strong>de</strong>rated engine is the rating<br />

Fig. 4: Since the 1980s engine ratings have been selected over<br />

a steadily smaller area of the layout field.<br />

[08#051]<br />

Engine power, %R1<br />

100<br />

90<br />

80<br />

70<br />

60<br />

70<br />

R3<br />

R4<br />

Area of recent<br />

CMCR selection<br />

80<br />

Area of CMCR<br />

selection in<br />

the 1980s<br />

90<br />

R1<br />

100<br />

R2<br />

Engine speed, %R1<br />

Fig. 3: For a given ship, a rating line (slope α) can be applied<br />

to the layout field so that all rating points on that line would<br />

give the same ship speed with a suitably optimized propeller.<br />

Rating points at lower speeds on the rating line require<br />

a larger propeller diameter and give a greater propulsive<br />

efficiency.<br />

line (Fig. 3). This is the line through a CMCR rating<br />

point such that any point on the line represents<br />

a new power/speed combination that will give<br />

the same ship speed in knots. The points on the<br />

rating line all require the same propeller type but<br />

with different adaptations to suit the power/speed<br />

combination. In general, lower speeds of rotation<br />

require larger propeller diameters and thereby<br />

increase the total propulsive efficiency. Usually the<br />

selected propeller speed <strong>de</strong>pends on the maximum<br />

permissible propeller diameter. The maximum<br />

diameter is often <strong>de</strong>termined by operational<br />

requirements, such as <strong>de</strong>sign draught and ballast<br />

draught limitations, as well as class recommendations<br />

concerning propeller–hull clearance (pressure<br />

impulse induced by the propeller on the hull).<br />

The slope of the rating line (α) <strong>de</strong>pends broadly<br />

upon the ship type. It can range from 0.15 for<br />

tankers, bulk carriers and general cargo ships up to<br />

about 10,000 tdw to 0.22 for container ships larger<br />

than 3000 TEU and 0.25 for tankers and bulk<br />

carriers larger than 30,000 tdw.<br />

Changing engine selection strategies<br />

When the broad layout field was introduced in<br />

RTA engines in 1984 it was wi<strong>de</strong>ly welcomed by<br />

shipowners and shipbuil<strong>de</strong>rs. Afterwards RTA<br />

engines were frequently selected at ratings in the<br />

lower part of the layout field to gain the benefits of<br />

— 2 — © Wärtsilä Corporation, June 2008

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