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ENGINES, RING PROCESS |
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TOM |
Bag |
Item |
Frame |
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AIR-cooled aviation motor, experimental results with ring process on, by K. Peter |
222 |
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3511-3518 |
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K. Peter |
248 |
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40 120-40 12* |
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FUEL injection without injection pump, reported by A. M. Madle |
227 |
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70 55-70 63 |
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INJECTION quantities, necessary and favorable, in ring process practice on Jumo cylinder 211A |
107 |
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29490-29504 |
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109 |
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8336-8351 |
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INTERNAL combustion engines (Ring Process), U.S. Navy technical report 147-45, prepared by R. J. Bonder |
209 |
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80485-80502 |
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OTTO-Diesel engine, by F. Penzig |
111 |
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11287-11321 |
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PRECOMBUSTION, use of, in ring process |
248 |
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20 115-20 120 |
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PRECOMPRESSION chamber, use of, with ring process |
109 |
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9024-9041 |
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PRESSURES, peak, in ring process |
109 |
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8577-8594 |
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248 |
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20 47-20 52 |
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PROBLEMS, some special, of ring process, by M. Beutele |
222 |
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3519-3521 |
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248 |
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40 126-40 130 |
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R-FUEL quantity, minimum and optimum, for ring process on Jumo cylinder 211A |
248 |
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40 126-40 130 |
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RING process, application to MBW, type 132 N cylinder |
109 |
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8500-8514 |
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248 |
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10 47-10 51 |
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process, by F. Penzig |
222 |
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3500-3510 |
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process method |
109 |
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8595-8633 |
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194 |
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30526-30536 |
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248 |
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20 31-20 46 |
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248 |
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40 105-40 119 |
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TEMPERATURE, influence of, when operating aero engines by ring process |
109 |
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8428-8449 |
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248 |
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10 61-10 66 |
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TESTS with ring process at different compression ratios |
107 |
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29505-29526 |
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109 |
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8672-8698 |
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248 |
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20 13-20 21 |