发明名称 INVERTED AIRCRAFT ENGINE CONFIGURATION - RADIATOR LOCATION
摘要 <p>An inverted aricraft i.c. piston engine (10), such as a two-stroke, compression-ignition (diesel), incorporates a lubricant (oil) and/or coolant heat exchanger (20), mounted upon the engine, below an exposed crankshaft (13), and/or enclosed crankshaft housing (12), adjacent a propeller mounting location (17).</p>
申请公布号 WO2000063541(A1) 申请公布日期 2000.10.26
申请号 GB2000001531 申请日期 2000.04.19
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