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    • 1. 发明申请
    • Multi-Cylinder Two-Stroke Radial Engine
    • 多气缸双冲程径向发动机
    • US20080283002A1
    • 2008-11-20
    • US11658554
    • 2006-04-04
    • Ioannis MantheakisAntonios Voulgarelis
    • Ioannis MantheakisAntonios Voulgarelis
    • F02B75/22
    • F02B75/222F02B75/32F02B2075/025
    • Multi-cylinder two-stroke radial engine, specially intended for use in models with a cubature in the order of 0.30-1.20 in3 and particularly for model aircraft applications. It comprises (FIG. 1) a cylindrical body (1) on the perimeter of which there are radially positioned cylinders (2) inside which travel pistons (2a) connected by means of connecting rods (6) to a configuration of an equal number of crankshafts (8a) that pass through the cylindrical body (1) and their gear wheels (8b) engage with a gear wheel (3a) of the central axis (3) in the interior of the body (1), which comprises the crankcase of the engine and is structured in such a way that the desired compression is achieved. A feature of the invention is the even distribution and simultaneous ignition of the combustible mixture in all cylinders by means of an even distribution arrangement, which according to one application of the invention, comprises a reed valve (40) which reciprocates for the two strokes of operation between the fuel intake channel 13a on the backplate of the engine and the reed retainer (41) that fits to the latter
    • 多缸二冲程径向发动机,特别用于在<3> <3>中具有0.30-1.20级的立方体的模型中,特别适用于模型飞机应用。 它包括(图1)周边的圆柱体(1),其上有径向定位的气缸(2),其内部通过连杆(6)将活塞(2a)连接到相等数量的构型 通过圆柱体(1)和它们的齿轮(8b)的曲轴(8a)与主体(1)内部的中心轴线(3)的齿轮(3a)接合, 包括发动机的曲轴箱,并且以这样一种方式被构造成实现了所需的压缩。 本发明的一个特征是通过均匀分配装置在所有气缸中均匀分布和同时点燃可燃混合物,根据本发明的一个应用,其包括一个簧片阀(40) 在发动机的背板上的燃料进入通道13a和与其配合的筘座(41)之间的操作