| 摘要 |
An inverted aircraft i.c. piston engine (10), such as a two-stroke, compression-ignition (diesel), incorporates: a wet sump lubrication system, with a combined under-slung camshaft or valve gear cover and sump housing (30); a turbo-charger (24), located above the wet sump operational oil level (33) and lubricated from the wet sump system, with gravity return to the sump.
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