发明名称 INVERTED AIRCRAFT ENGINE CONFIGURATION - RADIATOR LOCATION
摘要 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).
申请公布号 WO0063541(A1) 申请公布日期 2000.10.26
申请号 WO2000GB01531 申请日期 2000.04.19
申请人 SENECA TECHNOLOGY LIMITED;WILKSCH, MARK, CONRAD 发明人 WILKSCH, MARK, CONRAD
分类号 F01M1/12;F01M11/06;F01P3/18;F02B3/06;F02B39/14;F02B67/10;F02B75/02;(IPC1-7):F01P3/18 主分类号 F01M1/12
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