Answer EKG Question 10
Q10.
A. Explain Creep; Brenelling; Fretting; Fretting corrosion; State, with
reasons, where these may occur in ship propulsion System.
Answer: A. Explain Creep; Brinelling; Fretting; Fretting corrosion
1. Creep:-
Creep
may be defined as the slow plastic deformation of a material under a
constant stress. A material may fail under creep conditions at a much
lower stress and elongation than would be ascertained in a straight
tensile test. Hence tests have to be conducted to determine a limiting
creep stress with small creep rate.
Creep test:-
The
creep test consists of applying a fixed load to a test piece which is
maintained at a uniform temperature. The test is a long term one and a
number of specimens of the same material are subjected to this test
simultaneously, all at different stresses but at the same temperature.
In this way the creep rate and limiting stress can be determined, these
values depend upon how the material is going to be employed.
$\displaystyle \mathrm{e=e_o+Vt}$ ,
Fine
grained materials creep more readily than coarse grained because of
their greater amorphous metal content, i.e. the structure-less metal
between the grains.
2. Brinelling:-
Brinelling is the permanent indentation of a hard surface. It is named after the Brinell scale of hardness.
Brinell
Test: This test consists of indenting the surface of a metal by means
of a 10 mm diameter hardened steel ball under load.
The Brinell number is a function of the load applied and the area of indentation, thus:
Brinell number =Load in Newtons /Area of indentation in mm-sq.
Only the diameter of the indentation is required and this is determined by a low powered microscope with a sliding scale.
Tables
have been compiled to avoid unnecessary calculations in ascertaining
the hardness numeral. Loads normally employed are 30,000 N for steels,
10,000 N for copper and brasses and 5,000 N for aluminum.
Duration
of application of the load is usually 15 seconds. (Industry is still
using the old system of calculating Brinell numbers, i.e. load in
kilograms/area of indentation in mm2. Hence, their Brinell numbers will
be less by a factor of 10.)
3. Fretting:-
Fretting
can combine many of the wear processes described earlier. The
oscillatory motion causes fatigue wear, which can be enhanced by
adhesion. The wear can also be combined with corrosion – principally
oxidation – and the corrosion products can be abrasive. The fact that no
macroscopic sliding takes place often means that wear debris cannot
escape, but is trapped between the surfaces.
4. Fretting corrosion
Fretting
is a phenomenon of wear which occurs between two mating surfaces
subjected to cyclic relative motion of extremely small amplitude of
vibrations. Fretting appears as pits or grooves surrounded by corrosion
products. The deterioration of material by the conjoint action of
fretting and corrosion is called 'Fretting Corrosion.' Fretting is
usually accompanied by corrosion in a corrosive environment. It occurs
in bolted parts, engine components and other machineries.
Factors affecting fretting
1
Contact load: - Wear is a linear function of load and fretting would,
therefore, increase with increased load as long as the amplitude is not
reduced.
2
Amplitude: - No measurable threshold amplitude exists below which
fretting does not occur. An upper threshold limit, however, exists above
which a rapid increase in the rate of wear exists. Amplitude
oscillations as low as 3 or 4 nm are sufficient.
3
Number of cycles: - The degree of fretting increases with the number of
cycles. The appearance of surface changes with the number of cycles. An
incubation period is reported to exist during which the damage is
negligible. This period is accompanied by a steady-state period, during
which the fretting rate is generally constant. In the final stage, the
rate of fretting wear is increased.
4
Temperature:- The effect of temperature depends on the type of oxide
that is produced. If a protective, adherent, compact oxide is formed
which prevents the metal-to-metal contact, fretting wear is decreased.
For example, a thick layer of oxide is formed at 650° C on titanium
surface. The damage by fretting is, therefore, reduced at this
temperature. The crucial factor is not the temperature by itself, but
the effect of temperature on the formation of oxide on a metal surface.
The nature and type of the oxide is the deciding factor.
5
Relative humidity:- The effect of humidity on fretting is opposite to
the effect of general corrosion where an increase in humidity causes an
increase in the rate of corrosion, and an increase in dryness causes a
decrease in corrosion. Fretting corrosion is increased in dry air rather
than decreased for metals which form rust in air. In case of fretting,
in dry air, the debris which is formed as a consequence of wear on the
metal surface is not removed from the surface and, therefore, prevents
direct contact between two metallic surfaces. If the air is humid,
debris becomes more mobile and it may escape from the metal surface,
providing sites for metal-to-metal contact.
Fretting proceeds in three stages:
(a)
The first stage is the metallic contact between two surfaces. The
surfaces must be in close contact with each other. The contact occurs at
few sites, called asperities (surface protrusions). Fretting can be
produced by very small movements, as little as 10–8 cm.
(b)
The second stage is oxidation and debris generation. There is a
considerable disagreement between the workers on whether the metal is
oxidized prior to its removal or after its removal. It is possible that
both processes may occur, each process being controlled by conditions
which lead to fretting. In either case, the debris is produced as a
result of oxidation.
(c) Initiation of cracks at low stresses below the fatigue limit.
B. State, with reasons, where these may occur in ship propulsion System.
1.Common
example of creep failure is the cracking of the expansion bellows after
a long period of operation of the main engine. The failure occurs
because of the alternate conditions of working state and idle state.
During working condition the bellow is at about 3500 C and in idle state it is at about 350 C . This situation leads to creep failure.
2. Brinelling in the propulsion systems is the damage to the fuel pump, exhaust valve rollers and cam profiles.
3.
fretting and fretting corrosion can be seen in the deformation or
reduction in the shank diameter of the bottom end bolts of medium speed
auxiliary engines. The wear in the shank diameter is caused by fretting
action due to the variation in the stresses the bolt is subjected to and
this wear is called fretting wear. Similarly the coupling bolts of the
propeller shafting is subjected to fretting caused by the variation in
transmission of torque due to heavy seas during bad weather.
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