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Invention Publication
CN105593487A 内燃机的冷却 有权

内燃机的冷却
Abstract:
公开了一种用于螺旋桨驱动飞机的发动机组件(10)，所述组件包括发动机(11)、由发动机(11)驱动的驱动轴(13)、以及包括用于接收驱动轴(13)的孔(24)的散热器(20)，孔(24)被定位成使得所述散热器(20)大致沿周向围绕驱动轴(13)。孔(24)可以采取各种形式，诸如在散热器(20)内部的孔洞或形成在所述散热器(20)内的不贯通的狭缝。
Abstract(English):

An engine assembly (10) for a propeller-driven aircraft is disclosed. The assembly includes an engine (11), a drive shaft (13) driven by the engine (11), and a radiator (20) comprising an aperture (24) for receiving the drive shaft (13). The aperture (24) is located such that the radiator (20) substantially circumferentially surrounds the drive shaft (13). The aperture (24) may take various forms, such as a hole within the interior of the radiator (20) or a blind slit formed within the radiator (20).

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