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351 Cleveland Articles
Block Component Locations, Why CNC a Block?
Below are three tables from a NOS 351 Cleveland XE block. The first table contains data from digitizing the block cylinders on our CNC machine. This block has had no machining since it left the factory about 40 years ago. The first column shows the blueprint location or where the cylinders are supposed to be in the X andY planes. The X plane is length wise of the block parallel to the crank centerline. The Y plane is cross wise of the block or perpendicular to the crank centerline. Any locational difference in the Y plane will effect the rod/stoke ratio and how the piston transfers load thru the connecting rod to the crank. Piston dwell at TDC is greatly effected by the Y plane location, not so how much dwell but if the dwell is biased before or after TDC. Any difference in the X plane can cause the valve to be shrouded more or less by the bore.
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Bluprint Location |
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Probed Location |
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Difference in Location |
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Right Bank 1st Cylinder |
Right Bank 1st Cylinder |
Right Bank 1st Cylinder |
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| X |
2.19 |
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2.1798 |
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-0.0102 |
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| Y |
0 |
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-0.0058 |
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-0.0058 |
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| Bore |
4 |
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3.9934 |
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-0.0066 |
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Right Bank 2nd Cylinder |
Right Bank 2nd Cylinder |
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| X |
6.57 |
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6.5607 |
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-0.0093 |
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| Y |
0 |
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-0.0052 |
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-0.0052 |
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| Bore |
4 |
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3.9925 |
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-0.0075 |
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Right Bank 3rd Cylinder |
Right Bank 3rd Cylinder |
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| X |
10.95 |
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10.9417 |
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-0.0083 |
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| Y |
0 |
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-0.004 |
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-0.004 |
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| Bore |
4 |
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3.9932 |
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-0.0068 |
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Right Bank 4th Cylinder |
Right Bank 4th Cylinder |
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| X |
15.33 |
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15.3239 |
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-0.0061 |
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| Y |
0 |
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-0.0029 |
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-0.0029 |
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| Bore |
4 |
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3.9933 |
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-0.0067 |
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Left Bank 1st Cylinder |
Left Bank 1st Cylinder |
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| X |
3.03 |
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3.0249 |
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-0.0051 |
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| Y |
0 |
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-0.008 |
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-0.008 |
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| Bore |
4 |
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3.9931 |
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-0.0069 |
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Left Bank 2nd Cylinder |
Left Bank 2nd Cylinder |
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| X |
7.41 |
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7.4064 |
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-0.0036 |
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| Y |
0 |
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-0.0071 |
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-0.0071 |
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| Bore |
4 |
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3.993 |
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-0.007 |
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Left Bank 3rd Cylinder |
Left Bank 3rd Cylinder |
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| X |
11.79 |
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11.7868 |
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-0.0032 |
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| Y |
0 |
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-0.0062 |
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-0.0062 |
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| Bore |
4 |
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3.9936 |
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-0.0064 |
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Left Bank 4th Cylinder |
Left Bank 4th Cylinder |
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| X |
16.17 |
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16.1685 |
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-0.0015 |
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| Y |
0 |
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-0.0053 |
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-0.0053 |
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| Bore |
4 |
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3.9914 |
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-0.0086 |
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End Of Report |
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End Of Report |
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The second table contains data from digitizing the lifter bores from the same block. The X and Y planes have the same orientation to the crank centerline. differences in Y location greatly effect cam degree or valve timing and differences in X location cause the lifter to contact the cam in a different location than designed. This is especially critical in flat tappet engines as the tappet location is important on how the lifter spins in the lifter bore.
| Lifter Angle |
45 |
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| Cam Centerline |
5.0441 |
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Probed |
Probed |
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Difference |
Difference |
| Lifter |
X position |
Y position |
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X Position |
Yposition |
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X position |
Y position |
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| 1 intake |
1.37 |
-3.56671 |
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1.3795 |
-3.538 |
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-0.0095 |
-0.02871 |
| 1 exhaust |
3.1 |
-3.56671 |
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3.1057 |
-3.5381 |
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-0.0057 |
-0.02861 |
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| 2 intake |
5.75 |
-3.56671 |
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5.7572 |
-3.5326 |
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-0.0072 |
-0.03411 |
| 2 exhaust |
7.48 |
-3.56671 |
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7.4894 |
-3.5325 |
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-0.0094 |
-0.03421 |
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| 3 intake |
10.13 |
-3.56671 |
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10.1402 |
-3.5324 |
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-0.0102 |
-0.03431 |
| 3 exhaust |
11.86 |
-3.56671 |
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11.8676 |
-3.5339 |
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-0.0076 |
-0.03281 |
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| 4 intake |
14.51 |
-3.56671 |
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14.5193 |
-3.5325 |
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-0.0093 |
-0.03421 |
| 4 exhaust |
16.24 |
-3.56671 |
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16.2474 |
-3.532 |
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-0.0074 |
-0.03471 |
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| 5 intake |
2.12 |
3.566715 |
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2.1093 |
3.5488 |
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0.0107 |
0.017915 |
| 5 exhaust |
3.85 |
3.566715 |
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3.8413 |
3.5513 |
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0.0087 |
0.015415 |
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| 6 intake |
6.5 |
3.566715 |
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6.4949 |
3.5538 |
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0.0051 |
0.012915 |
| 6 exhaust |
8.23 |
3.566715 |
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8.2235 |
3.5561 |
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0.0065 |
0.010615 |
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| 7 intake |
10.88 |
3.566715 |
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10.8736 |
3.5578 |
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0.0064 |
0.008915 |
| 7 exhaust |
12.61 |
3.566715 |
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12.6024 |
3.5634 |
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0.0076 |
0.003315 |
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| 8 intake |
15.26 |
3.566715 |
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15.2553 |
3.561 |
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0.0047 |
0.005715 |
| 8 exhaust |
16.99 |
3.566715 |
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16.9822 |
3.562 |
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0.0078 |
0.004715 |
The third table contains the data from digitizing the blocks deck height. Differences in deck height cause differences in compression ratio and heads not sitting square on the block. Twist in the decks cause twists in the heads which cause valve seats to become distorted in roundness and being unconcentric to the valve stems. Differences in height also cause intakes to not seal correclty.
9.2060 = Deck Height
Right Bank
9.1994 -0.0066 = Front Inner
9.2009 -0.0051 = Front Outer
9.2037 -0.0023 = Rear Inner
9.2023 -0.0037 = Rear Outer
Left Bank
9.2057 -0.0003 = Front Inner
9.2035 -0.0025 = Front Outer
9.2068 0.0008 = Rear Inner
9.2054 -0.0006 = Rear Outer
It can be seen from the three tables that the blocks cylinders bores, lifters bores and deck surfaces are not machined perfectly from the factory. Since this was a special race block from the factory this block should have better machining than regular passenger car or production blocks. It can also bee seen that traditional automotive machining does not correct any of these difficiencies because traditional machining centers from the existing bores and levels from existing surfaces. CNC machining of the block is a way to find and correct the difficiencies of a block to turn it into a fully blueprinted block, capaable of making the power the rest of the components can deliver. It has been theorized that these misplaced components in blocks cause the differences in engine performance seen from supposed identical engines. The components may be the same but the differences in goemetry cause the power differences.
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