Unmanned quadcopter has electric motors with propellers that are placed are made with inclination relative to central portion of frame that is installed on top of flat central portion of frame and is completely located no higher than level of upper edges of propellers
2024-12-27
专利权人NIKITIN P V (NIKI-Individual)
申请日期2024-12-27
专利号RU232704-U1
成果简介NOVELTY - The unmanned quadcopter has a frame (6) that contains four supporting beam supports (3) attached to the central portion of the frame equipped with platforms on their outer ends on which electric motors (5) with propellers are placed. A housing in which a flight controller, a video camera and an on-board power source are installed. The central portion of the frame is made flat located below the platforms on which the electric motors with propellers are placed, and is connected with a bend to these platforms by units of beam support made with an upward slope relative to the central portion of the frame at an angle of 160-170° . The electric motors with propellers are placed are made with an inclination relative to the central portion of the frame in the direction of the quadcopter flight at an angle of 15-30° , and the frame is installed on top of the flat central portion of the frame and is completely located no higher than the level of the upper edges of the propellers. USE - Unmanned quadcopter. ADVANTAGE - The aerodynamic performance of quadcopter is improved by reducing the aerodynamic drag of the quadcopter when it is flown around by an air stream is achieved by the fact that in an unmanned quadcopter. DESCRIPTION OF DRAWING(S) - The drawing shows a schematic diagram of the unmanned quadcopter. 3Inclined beam support 5Electric motor 6Frame
IPC 分类号B64U-010/14
国家俄罗斯
专业领域信息技术
语种英语
成果类型专利
文献类型科技成果
条目标识符http://119.78.100.226:8889/handle/3KE4DYBR/13759
专题中国科学院新疆生态与地理研究所
作者单位
NIKITIN P V (NIKI-Individual)
推荐引用方式
GB/T 7714
NIKITIN P V. Unmanned quadcopter has electric motors with propellers that are placed are made with inclination relative to central portion of frame that is installed on top of flat central portion of frame and is completely located no higher than level of upper edges of propellers. RU232704-U1[P]. 2024.
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