358 MAN B&W Low-Speed Engines
Most of the design concepts of the large bore Mark 9 engines are shared
by the ME-B series, including a piston with high topland, PC ring, twin stay
bolts, thin shell bearings, low friction guide shoes and thrust cams. The struc-
tural parts of the S35/40ME-B engines were designed to secure the rigid-
ity and strength required for the higher output. The bedplate is of welded
design, but the normal cast part for the main bearing girders is made from
rolled steel plates. The aim was to achieve homogeneity of the material used
for that bearing area with no risk of casting imperfections arising during final
machining.
A new main bearing concept was under development at the launch of the
engines to decrease the production cost of the bedplate. In the new design,
the bedplate and bearing caps are finish machined as separate parts, with the
caps positioned by means of the bearing shell and kept in position with the
force from hydraulically tightened studs and high-friction coated shims placed
between bearing cap and bedplate. The proven main bearing design used on all
MAN B&W small bore engine designs, however, was to be retained until the
new development was completed.
A framebox of the proven triangular guide plane design with twin stay-
bolts—now standard on all updated MAN B&W engine types—was specified
to provide excellent support for the guide shoe forces.
Two possibilities are available for the cylinder frame—nodular cast iron
(KF) or a welded design with integrated scavenge air receiver—but it was
decided to use the cast solution because of the material’s high strength and
high E-modulus in countering the high ignition force. Furthermore, compared
with C3Cu material, the weight of a six-cylinder S35ME-B cylinder frame can
be reduced by 3 tonnes, corresponding to a 12 per cent cost reduction for the
frame.
A semi-built crankshaft, in one piece, is made of S34CrNi or S42Cr1 mate-
rial. Even though the stroke–bore ratio was raised for the new engines, the
cylinder distance is only slightly increased. Comprehensive FEM calculations
were performed to ensure that the geometry (including the journal diameters)
of the shaft was optimized for maintaining the rigidity, shrink-fit and stresses at
the same level as for the MC-C engines.
Based on the design introduced for the MC-C engine, the thrust bearing
is very compact. Addressing the increased propeller thrust resulting from the
higher engine power, a flexible thrust cam secures a more even force distribu-
tion on the pads. The overall dimension of the parts can thus be smaller than
that with the old design.
A connecting rod design based on that applied throughout the small bore
engine programme (initially introduced for the L35MC model) is used. To
reduce the production cost and oscillating forces, however, the new design is a
combination of those used in the MC-C and 35MC engines. The crosshead pin
design is taken from the S50MC-C engine, with the bearing dimensions based
on long experience with the S35MC engine (exploiting a hardened running sur-
face for the pin). The guide shoe is of the new low friction design.