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| EFFECT OF ALTITUDE AND TEMPERATURE |
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Altitude and temperature have a direct effect on the molecular structure of air. An adjustment in CFM (l/sec) must be made to accommodate such changes and to provide for efficient drilling. At high altitudes there are less molecules in a given volume of air than at lower altitudes. Therefore, when the compressor displaces a given volume at a higher altitude, the air will be less dense. When less dense air is supplied to a down hole hammer a lower operating pressure will result.
High ambient temperature has much the same effect on air. At high ambient temperatures the air becomes less dense and at low ambient temperatures the air becomes more dense. These changes also require an adjustment to the air supply.
The following table may be used as a reference to calculate the air volumes necessary to maintain a given operating pressure at different altitudes and at different ambient temperatures. |
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CFM CORRECTION FACTORS FOR AMBIENT TEMPERATURE AND ALTITUDE [You may have to scroll right on your browser to view the entire chart] |
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| ALTITUDE | |||||||||||||||||
| Feet | 0 | 1,000 | 2,000 | 3,000 | 4,000 | 5,000 | 6,000 | 7,000 | 8,000 | 9,000 | 10,000 | 11,000 | 12,000 | 13,000 | 14,000 | 15,000 | |
| Metres | 0 | 305 | 610 | 914 | 1,219 | 1,524 | 1,829 | 2,134 | 2,438 | 2,743 | 3,048 | 3,353 | 3,658 | 3,962 | 4,267 | 4,572 | |
| Temperature | |||||||||||||||||
| °F | °C | ||||||||||||||||
| -40 | -40 | 0.805 | 0.835 | 0.866 | 0.898 | 0.932 | 0.968 | 1.004 | 1.043 | 1.084 | 1.127 | 1.170 | 1.217 | 1.266 | 1.317 | 1.371 | 1.426 |
| -30 | -34 | 0.824 | 0.855 | 0.886 | 0.920 | 0.954 | 0.991 | 1.028 | 1.068 | 1.110 | 1.154 | 1.198 | 1.246 | 1.297 | 1.349 | 1.403 | 1.460 |
| -20 | -29 | 0.844 | 0.875 | 0.907 | 0.941 | 0.976 | 1.014 | 1.052 | 1.092 | 1.136 | 1.180 | 1.226 | 1.275 | 1.327 | 1.380 | 1.436 | 1.494 |
| -10 | -23 | 0.863 | 0.895 | 0.928 | 0.962 | 0.999 | 1.037 | 1.076 | 1.117 | 1.161 | 1.207 | 1.254 | 1.304 | 1.357 | 1.411 | 1.469 | 1.528 |
| 0 | -18 | 0.882 | 0.915 | 0.948 | 0.984 | 1.021 | 1.060 | 1.100 | 1.142 | 1.187 | 1.234 | 1.282 | 1.333 | 1.387 | 1.443 | 1.501 | 1.562 |
| 10 | -12 | 0.901 | 0.935 | 0.969 | 1.005 | 1.043 | 1.083 | 1.123 | 1.167 | 1.213 | 1.261 | 1.310 | 1.362 | 1.417 | 1.474 | 1.534 | 1.596 |
| 20 | -7 | 0.920 | 0.954 | 0.990 | 1.026 | 1.065 | 1.106 | 1.147 | 1.192 | 1.239 | 1.288 | 1.338 | 1.391 | 1.447 | 1.506 | 1.566 | 1.630 |
| 30 | -1 | 0.939 | 0.974 | 1.010 | 1.048 | 1.087 | 1.129 | 1.171 | 1.217 | 1.265 | 1.315 | 1.365 | 1.420 | 1.478 | 1.537 | 1.599 | 1.664 |
| 40 | 4 | 0.959 | 0.994 | 1.031 | 1.069 | 1.110 | 1.152 | 1.195 | 1.241 | 1.290 | 1.341 | 1.393 | 1.449 | 1.508 | 1.568 | 1.632 | 1.698 |
| 50 | 10 | 0.978 | 1.014 | 1.051 | 1.091 | 1.132 | 1.175 | 1.219 | 1.299 | 1.316 | 1.368 | 1.421 | 1.478 | 1.538 | 1.600 | 1.664 | 1.732 |
| 60 | 16 | 0.997 | 1.034 | 1.072 | 1.112 | 1.154 | 1.198 | 1.243 | 1.291 | 1.342 | 1.395 | 1.449 | 1.507 | 1.568 | 1.631 | 1.697 | 1.766 |
| 70 | 21 | 1.016 | 1.054 | 1.093 | 1.133 | 1.176 | 1.221 | 1.267 | 1.316 | 1.368 | 1.422 | 1.477 | 1.536 | 1.598 | 1.662 | 1.730 | 1.800 |
| 80 | 27 | 1.035 | 1.074 | 1.113 | 1.155 | 1.198 | 1.244 | 1.291 | 1.341 | 1.394 | 1.449 | 1.505 | 1.565 | 1.628 | 1.694 | 1.762 | 1.834 |
| 90 | 32 | 1.055 | 1.094 | 1.134 | 1.176 | 1.221 | 1.267 | 1.315 | 1.365 | 1.419 | 1.475 | 1.533 | 1.594 | 1.658 | 1.725 | 1.795 | 1.868 |
| 100 | 38 | 1.074 | 1.114 | 1.154 | 1.198 | 1.243 | 1.290 | 1.339 | 1.390 | 1.445 | 1.502 | 1.560 | 1.623 | 1.689 | 1.756 | 1.828 | 1.902 |
| 110 | 43 | 1.093 | 1.133 | 1.175 | 1.219 | 1.265 | 1.313 | 1.363 | 1.415 | 1.471 | 1.529 | 1.588 | 1.652 | 1.719 | 1.783 | 1.860 | 1.936 |
| 120 | 49 | 1.112 | 1.153 | 1.196 | 1.240 | 1.287 | 1.336 | 1.386 | 1.440 | 1.497 | 1.556 | 1.616 | 1.681 | 1.749 | 1.819 | 1.893 | 1.970 |
| Instructions: | 1. Determine ambient conditions of air temperature (°F or °C) and altitude. (Feet or Metres) | ||||||||||||||||
| 2. Find corrections factor from this table. | |||||||||||||||||
| 3. Multiply the correction factor by the SCFM needed to obtain ACFM under conditions given. | |||||||||||||||||