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OCTOBER 19-20, 2012 - YMCA University of Science & Technology

OCTOBER 19-20, 2012 - YMCA University of Science & Technology

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Proceedings <strong>of</strong> the National Conference on<br />

Trends and Advances in Mechanical Engineering,<br />

<strong>YMCA</strong> <strong>University</strong> <strong>of</strong> <strong>Science</strong> & <strong>Technology</strong>, Faridabad, Haryana, Oct <strong>19</strong>-<strong>20</strong>, <strong>20</strong>12<br />

<strong>of</strong> surface finish is best when the spindle speed is running at its highest i.e.,2800 rpm, depth <strong>of</strong> cut was adjusted<br />

to its maximum value <strong>of</strong> 0.075 in with a low feed rate <strong>of</strong> 10 in/min provided the least roughness amongst all<br />

given samples. The tool size <strong>of</strong> 0.5 inches in diameter used for this experiment did not show much variability in<br />

the surface roughness when compared to the tool size <strong>of</strong> 0.25 inches dia. The 0.25 inch tool size did give the<br />

highest and the lowest surface roughness when in combination with the other three parameters [R. Noorani,<br />

<strong>20</strong>09].<br />

3. Experimental Procedure<br />

The compositions <strong>of</strong> different alloys and different modification treatment are given in the Table 1 and Table 2.<br />

Table 1: Compositions <strong>of</strong> the alloys prepared<br />

Alloy<br />

Chemical composition<br />

Designation<br />

(wt. %)<br />

Fe Si Al<br />

S1 1 1 Balance<br />

S2 2 1 Balance<br />

Table 2: Sample size <strong>of</strong> different material<br />

Sample<br />

Al<br />

Fe<br />

Si<br />

Alloy<br />

No.<br />

(kg)<br />

(gm)<br />

(gm)<br />

A 4.90 53.00 53.00 Al-1Fe-1Si<br />

B 4.85 105.00 53.00 Al-2Fe-1Si<br />

4. Preparation <strong>of</strong> alloy<br />

The experimental alloys were prepared in an electric heating furnace in a clay bonded graphite crucible under the<br />

cover <strong>of</strong> Na-free flux. For alloy preparation, Pure Al and Fe were used. At around 600 0 C, weighted quantity <strong>of</strong><br />

99.9% pure aluminium and 99.9% pure Silicon metallic was charged. Just after melting, the molten alloy was<br />

covered with a sodium free flux (2% <strong>of</strong> melt). After melting, sufficient time was given for complete<br />

homogenization <strong>of</strong> the melt. The melt was frequently agitated with a graphite rod for complete mixing. The melt<br />

was then degassed with hexachloroethane. Degasser was wrapped in aluminium foil and plunged into the melt.<br />

After degassing the melt was cast in different moulds. The object is to vary the cooling rates.<br />

5. Pouring <strong>of</strong> melt at different moulds<br />

After complete homogenization at desired temperature the melt was poured in different mould to prepare<br />

different samples. There were five samples prepared which were poured in (a) 12 mm diameter permanent<br />

mould, (b) 25 mm thickness permanent (steel) flat mould, (c) 75 mm diameter permanent mould.The pouring<br />

temperature was maintained approximately at 880 0 C. The fluidity <strong>of</strong> the melt at this temperature was sufficient<br />

for casting test pieces. In all the cases, the mould was preheated approximately up to 1500 0 C to drive <strong>of</strong>f the<br />

moisture.<br />

6. Machinability <strong>of</strong> aluminum alloys<br />

Different samples have been made for machinability test <strong>of</strong> the alloys. The samples were cut in eight pieces from<br />

the cast piece 170 X 75 X <strong>20</strong>mm. The dimension <strong>of</strong> the samples used for milling operation is 40 X 18 X 8mm.<br />

For milling operation 16mm diameter HSS tool were used. The samples were machined under different<br />

parameter <strong>of</strong> machining.<br />

7. Result analysis<br />

Mechanical properties <strong>of</strong> both samples <strong>of</strong> Al alloys are discussed in detail. The hardness <strong>of</strong> the samples that cast<br />

in permanent mould is given in the Table 3.<br />

568

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