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    • 5. 发明公开
    • MULTI-SHAFT POWER SOURCE UNMANNED FLIGHT EQUIPMENT
    • 多轴电源无人飞行设备
    • EP3279087A1
    • 2018-02-07
    • EP17182959.1
    • 2017-07-25
    • Ewatt Technology Co., Ltd.
    • ZHAO, GuochengLUO, WeiQI, Pengcheng
    • B64C27/08B64C27/12B64C27/59B64D35/04
    • F02B61/04B64C27/08B64C27/12B64C27/14B64C27/59B64C39/024B64C2201/027B64C2201/044B64C2201/108B64D35/04F02B67/06F02B73/00F02B75/16F16H1/222F16H7/02F16H37/065
    • The present invention discloses a multi-shaft power source unmanned flight equipment, and belongs to the technical field of unmanned aerial vehicles. The multi-shaft power source unmanned flight equipment comprises a frame (1), a plurality of rotor sets (2) and a power device (3). The plurality of rotor sets (2) are rotatably fixed on the frame (1), and the power device (3) is correspondingly movably connected with each rotor set (2) respectively. Power is provided for flight of the unmanned flight equipment by the power device (3) with oil drive characteristics, mechanical kinetic energy is generated by burning a combustion material pre-injected in the power device (3), and rotors (21) in each rotor set (2) correspondingly connected with the power device are driven to rotate, thereby replacing the traditional electric multi-rotor unmanned aerial vehicle structure adopting electric modes such as batteries, electronic speed controllers and the like to supply power and provide power for the rotation of the rotors (21); and the unmanned flight equipment has the characteristics of long duration and strong loading capacity.
    • 本发明公开了一种多轴动力源无人飞行器,属于无人机技术领域。 该多轴动力源无人飞行器包括机架(1),多个转子组(2)和动力装置(3)。 多个转子组(2)可转动地固定在机架(1)上,动力装置(3)分别与每个转子组(2)对应活动连接。 动力装置(3)为具有油驱特性的无人飞行装备提供动力,通过燃烧预先注入动力装置(3)中的燃烧材料产生机械动能,并且每个转子(21)中的转子 驱动与动力装置对应连接的转子组(2)旋转,从而代替采用电池,电子调速器等电动模式的传统电动多旋翼无人机结构为旋转动力提供动力并提供动力 的转子(21); 无人飞行器具有持续时间长,载重能力强的特点。
    • 7. 发明授权
    • AIR LEADING-TYPE STRATIFIED SCAVENGING TWO-STROKE INTERNAL-COMBUSTION ENGINE
    • 空气引导式分层清除双行程内燃机
    • EP3006693B1
    • 2017-09-20
    • EP15188711.4
    • 2015-10-07
    • Yamabiko Corporation
    • YAMAZAKI, TakahiroTSUNODA, HidekazuOSAWA, Hisato
    • F02B25/14F02F3/24
    • F02F3/24F02B25/02F02B25/14F02B75/02F02B75/16F02B2075/025F02F1/22F02F7/0004
    • The efficiency of charging air to a scavenging channel is enhanced by generating a gas flow in a piston groove simultaneously with the piston groove coming into communication with an air port. A piston groove 8 formed in a peripheral surface of a piston includes a pressure transmission through hole 10, and the pressure transmission through hole 10 consistently communicates with a crankcase. In the course of the piston moving up, upon a pressure in the crankcase becoming negative, the negative pressure in the crankcase affects the piston groove 8 through the pressure transmission through hole 10. Consequently, a pressure in the piston groove 8 is released to the crankcase through the pressure transmission through hole 10. Upon the piston moving up and the piston groove 8 being thereby brought into communication with the air port 4a, air enters the piston groove 8 through the air port 4a ((III) of FIG. 1).
    • 通过在活塞槽与空气端口连通的同时在活塞槽中产生气流,增强了向扫气通道充入空气的效率。 在活塞的外周面上形成的活塞槽8包括压力传递通孔10,并且压力传递通孔10始终与曲轴箱连通。 在活塞的过程中向上移动,当在曲轴箱中的压力成为负,在曲轴箱中的负压通过通孔10因此压力传递会影响活塞槽8,在活塞槽8的压力被释放到 曲轴箱穿过孔10中的压力传输在活塞向上移动并且活塞槽8从而被带入与所述空气口4a连通,空气通过空气口4a进入活塞凹槽8(图的(III)。1) 。
    • 8. 发明授权
    • Engine
    • 发动机
    • EP2860381B1
    • 2017-05-31
    • EP13190931.9
    • 2013-10-30
    • Yamaha Hatsudoki Kabushiki Kaisha
    • Iida, Kaichi
    • F02F7/00
    • F01L13/0036F01L1/267F01L2001/0535F02B75/16F02F7/006F02F2007/0063
    • A first head section is arranged between a first cylinder side wall and a second head section in the axial direction of a cam shaft. The second head section is arranged between a second cylinder side wall and the first head section in the axial direction of the cam shaft. The distance between the first cylinder side wall and the first head section in the axial direction of the cam shaft is shorter than the distance between the second cylinder side wall and the second head section in the axial direction of the cam shaft. The distance to the first head section in a cylinder axial direction from a third virtual plane, which includes the axis of a crank shaft and is perpendicular to a cylinder axis, is shorter than the distance to the second head section in the cylinder axial direction from the third virtual plane.
    • 第一头部沿凸轮轴的轴向设置在第一缸侧壁和第二头部之间。 第二头部在凸轮轴的轴向上布置在第二缸侧壁和第一头部之间。 第一缸侧壁与第一头部在凸轮轴的轴向上的距离比第二缸侧壁与第二头部在凸轮轴的轴向上的距离短。 从包括曲轴的轴线且与气缸轴线垂直的第三假想平面到气缸轴线方向上的第一头部部分的距离短于第二头部部分在气缸轴线方向上的距离, 第三个虚拟平面。