
110 5 Crankcase and cylinder liners
rial pairing selected for the two components. In order to reduce wear, the running surface
should be smooth and the lubrication between the sliding partners must be ensured. The
type and quality of the running surface effects oil consumption as well as the wear of the
two components.
5.4.2 Cylinder surfaces in aluminum crankcases
The monolithic aluminum crankcase is based on a hypereutectic AlSi alloy (such as AlSi17),
whereas the cylinder surfaces are produced by chemical etching or mechanical exposure
(special honing) of the primary silicon crystals. The disintegration rate of the silicon crystals
must not exceed an upper limit for both processes.
For quasi-monolithic crankcases, the bores are coated, for example, with a galvanic MAHLE
NIKASIL
®
layer (Figure 5.27) or plasma thermal spraying. Alternatively, cylinder surfaces can
be produced with local material engineering, by laser alloying (e.g., with silicon) or by using
Al matrix composite materials (preforms) with subsequent finishing.
The dominant design, however, is the heterogeneous crankcase, in which cast-in or inserted
cylinder liners made of GJL form the cylinder surfaces.
In addition to the general requirements for cylinder surfaces, additional conditions must be
met when using cylinder liners. The wall thickness and material strength must be sufficient,
so that the cylinder liners do not crack. The finite element analysis allows the design and
material selection to be adapted to the loads due to assembly, temperature, peak cylinder
pressure, and piston side forces. Stresses originating from assembly are essentially deter-
mined by the number, tightening torque, and arrangement of cylinder head bolts as well as
the selected cylinder head gasket. Figure 5.13 shows a typical gas pressure and side force
curve as a function of the crank angle. The maximum side force occurs after the maximum
gas pressure, while the side force acts transverse to the pin axis only in the piston contact
area.
Based on temperature distribution, side forces and bolt arrangement, the loads on the
liners, as well as stresses and deformations vary around the circumference. In Figure 5.14,
using the example of the bottom side of the flange of a cylinder liner, the resultant stresses
for the load case of assembly and temperature and the superposition of all load cases at
maximum side force are depicted. The maximum stress occurs in the area of the radius of
the liner flange, which is in contact with the crankcase. Using fatigue strength charts, the
effects of changes in design and material on the local safety factor are evaluated.