| 摘要 |
The present invention relates to devices for adapting a motor vehicle engine to a light aeroplane. Devices characterised in that they consist of a propeller shaft 1 mounted on the crankshaft 2 and guided on the engine housing 3, and of a unit 4 for the mounting and driving of the ignition device fixed to one end of the camshaft 5, at the opposite end from the propeller shaft 1. <IMAGE>
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