| 摘要 |
In the case of a method for conversion of an aircraft spark-ignition engine for driving a propeller, comprising a crankcase, a crankshaft, at least one cylinder having a cylinder head, a connecting rod and a piston, at least the cylinder with the cylinder head, possibly in conjunction with the piston, are replaced by corresponding components of a diesel engine, while retaining the crankcase, the crankshaft and/or the connecting rod.
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