首页> 外国专利> TWO-AXIAL PLATFORM FOR USE IN SMALL UNMANNED AIRCRAFT AND TRAXIAL PLATFORM FOR USE IN SMALL DIMENSIONAL UNMANNED AIRCRAFT

TWO-AXIAL PLATFORM FOR USE IN SMALL UNMANNED AIRCRAFT AND TRAXIAL PLATFORM FOR USE IN SMALL DIMENSIONAL UNMANNED AIRCRAFT

机译:用于小型无人驾驶飞机的两轴平台和用于小型无人驾驶飞机的两轴平台

摘要

1. A two-axis platform for use in a small unmanned aerial vehicle, comprising an assembled frame, a transmission unit and a shooting unit (1), characterized in that: the assembled frame contains a first bracket (2), a second bracket (4) and a third bracket ( 6), while the filming unit (1) is mounted on the first bracket (2), the first bracket (2) is rotary connected to the second bracket (4), the second bracket (4) is rotary connected to the third bracket (6); the transmission block contains the first an engine (3) and a second engine (5), wherein the first engine (3) directly drives pressing the first bracket (2) to rotate relative to the second bracket (4), and the second engine (5) directly drives the second bracket (4) to rotate relative to the third bracket (6) .2. The platform according to claim 1, characterized in that the X axis of rotation of the first bracket (2) is perpendicular to the Y axis of rotation of the second bracket (4). 3. The platform according to claim 1, characterized in that the stator of the first engine (3) is fixed to the first bracket (2), and the rotor of the first engine (3) is fixed to the second bracket (4); or the rotor of the first motor (3) is fixed to the first bracket (2), and the stator of the first motor (3) is fixed to the second bracket (4). 4. The platform according to claim 1, characterized in that the stator of the second engine (5) is fixed to the third bracket (6), and the rotor of the second engine (5) is fixed to the second bracket (4); or the rotor of the second motor (5) is fixed on the third bracket (6), and the stator of the second motor (5) is fixed on the second bracket (4) .5. The platform according to claim 1, characterized in that the center of gravity of the first bracket (2) and the film block (1) falls on the X axis of rotation of the first bracket (2) .6. The platform according to claim 1, characterized in that the center of gravity of the first bracket (2), the second bracket (4) and the film block
机译:1。一种用于小型无人机的双轴平台,包括组装的框架,传动单元和射击单元(1),其特征在于:组装的框架包括第一支架(2),第二支架。 (4)和第三支架(6),当将摄影单元(1)安装在第一支架(2)上时,第一支架(2)旋转连接到第二支架(4),第二支架(4) )旋转连接到第三支架(6);传动块包括第一发动机(3)和第二发动机(5),其中第一发动机(3)直接驱动压紧第一支架(2)相对于第二支架(4)旋转,第二发动机(5)直接驱动第二支架(4)相对于第三支架(6)旋转2。 2.根据权利要求1所述的平台,其特征在于,所述第一支架(2)的X旋转轴垂直于所述第二支架(4)的Y旋转轴。 3.根据权利要求1所述的平台,其特征在于,所述第一发动机(3)的定子固定至所述第一托架(2),并且所述第一发动机(3)的转子固定至所述第二托架(4)。 ;或者,第一电动机(3)的转子固定在第一支架(2)上,第一电动机(3)的定子固定在第二支架(4)上。 4.根据权利要求1所述的平台,其特征在于,所述第二发动机(5)的定子固定至所述第三托架(6),并且所述第二发动机(5)的转子固定至所述第二托架(4)。 ;或者,第二电动机(5)的转子固定在第三支架(6)上,第二电动机(5)的定子固定在第二支架(4)上.5。 2.根据权利要求1所述的平台,其特征在于,所述第一托架(2)和所述胶片块(1)的重心落在所述第一托架(2).6的X旋转轴上。 2.根据权利要求1所述的平台,其特征在于,所述第一托架(2),所述第二托架(4)和所述胶片块的重心

著录项

  • 公开/公告号RU2014113934A

    专利类型

  • 公开/公告日2015-10-20

    原文格式PDF

  • 申请/专利权人 ШЗ ДЦЗИ ТЕКНОЛОДЖИ КО. ЛТД;

    申请/专利号RU20140113934

  • 发明设计人 ВАН ТАО;

    申请日2011-09-15

  • 分类号B64D47/08;

  • 国家 RU

  • 入库时间 2022-08-21 14:56:49

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