Charpy Impact Test Report
Table of Contents
Statement of Intent…………………………………………………………………………………..3
Background……………………………………………………………………………………………….3
Equipment…………………………………………………………………………………………………5
Procedure………………………………………………………………………………………………….6
Data and Analysis………………………………………………………………………………………7
Conclusions……………………………………………………………………………………………….11
Works Cited………………………………………………………………………………………………12
Statement of Intent The purpose of the experiment was to run a Charpy Impact Test and compare the energy absorbed between 4130 steel and A36 hot rolled steel and find the ductile to brittle transition for each.
Background
The Charpy test works by suspending a notched specimen at both ends and then breaking the specimen by
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The DTBT starts to occur at -12°F and it ends at around 200°F with it tapering off after that. The graph of the data is Figure 3. As shown, this graph does not look like a typical DTBT graph. There are outliers at points 4, 5, 7, 10, 15, 19, and 20. With the data collected, the transition temperature starts at -12°F with 69.5ft-lb of energy absorbed, but the standard is different. The standard transition temperature is -100°F with 15ft-lb of energy absorbed.(Brockenbrough 1.20-1.21) As shown in Figure 4, these are the samples lined up from coldest to warmest. You can see the DTBT. It starts at sample 5 and ends at sample 9.
Figure 3
Figure 4
B. 4130 Steel
Temp
Energy Absorbed
Temp
Energy Absorbed
°F
ft - lb
°F
ft - lb
-330
6
76
25.5
-266
3.5
115.9
27
-262
9
130
26
-197
11
164.6
37
-136
15
180
47
-127.8
12.5
200
41
-90
18
202.6
42
-70
21
225
46
-50
6
253.2
27
26
26
274
51
69.5
27.5
293.8
59
The material was very brittle at extremely low temperature, but the energy absorbed was higher than the A36 steel. The DTBT starts to occur at -90°F and it ends at around 200°F with it
Thermo-mechanically affected zone (TMAZ): In this region, the material has been plastically deformed by the friction stir welding tool, and the heat from the process will also have exerted some influence on the material. In the case of aluminium, it is possible to get significant plastic strain without recrystallization in this region, and there is generally a distinct boundary between the recrystallized zone and the deformed zones of the TMAZ. In the earlier classification, these two sub-zones were treated as distinct microstructural regions. However, subsequent work on other materials has shown that aluminium behaves in a different manner to most other materials, in that it can be extensively deformed at high temperature without recrystallization. In other materials, the distinct recrystallized region (the nugget) is absent, and the whole of the TMAZ appears to be recrystallized. This is certainly true of materials which have no thermally induced phase transformation which will in itself induce recrystallization without strain, for example pure titanium, b titanium alloys, austenitic stainless steels and copper. In materials such as ferritic steels and a-b titanium alloys (e.g.Ti-6Al-4V), understanding the microstructure is made more difficult by the thermally induced phase transformation, and this can also make the HAZ/TMAZ boundary difficult to identify
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at each temperature was calculated resulting in negative values, signifying the reaction was spontaneous. As temperature increased thevalues got less negative. The values ranged from -579 kJ to -510 kJ. The smallestvalue was -579 kJ at 6.0 oC (279 K) and the largest was -75.3 at 55.0 oC (328 K). The only value that did not agree with the other numbers was thevalue at 55.0 oC (328 K) having the largest value of -75.3 (kJ), which resulted in some discrepancies in the graph and a really poor best fit line when observing the graph ofverses temperature for the Al/Mg cell in figure 1 making it difficult to observe any trends. The positivevalue for the graph indicates an endothermic reaction, therefore the surroundings loses heat and its entropy decreases as can be observed by the -value for the slope of the graph.
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