Unmanned helicopter

A technology of unmanned helicopters and racks, which is applied in the field of drones and can solve problems such as inconvenient maintenance

Active Publication Date: 2021-06-04
ZHUHAI ZIYAN UAV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to overcome the above-mentioned deficiencies in the prior art, the present invention provides an unmanned helicop

Method used

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Embodiment Construction

[0047] see figure 1 and figure 2 , the present invention discloses an unmanned helicopter, including a frame 8 and a battery assembly 5, a power assembly 4, an avionics assembly 3, an empennage assembly 2 and a tripod assembly 1 arranged on the frame 8, and the battery assembly 5 includes a A battery box 50 detachably installed on the frame 8 and a battery located inside the battery box 50, the power assembly 4 includes a fixed frame 40 detachably mounted on the frame 8, a main shaft 41 mounted on the fixed frame 40, a motor 42 and a plurality of steering gears 43, the upper end of the main shaft 41 is provided with a rotor assembly 44, the output end of the steering gear 43 is connected to the rotor assembly 44, the output end of the motor 42 is connected to the main shaft 41, and the avionics The assembly 3 includes a bilge plate 30 detachably installed on the frame 8 and a mounting frame 31 arranged on the upper end of the bilge plate 30, the mounting frame 31 and the bil...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, and discloses an unmanned helicopter which comprises a rack and a battery assembly, a power assembly, an avionics assembly, an empennage assembly and a foot stool assembly which are arranged on the rack, and the battery assembly comprises a battery box detachably installed on the rack and a battery arranged in the battery box; the power assembly comprises a fixing frame detachably installed on the rack, a main shaft, a motor and a plurality of steering engines, the main shaft, the motor and the steering engines are installed on the fixing frame, the avionics assembly comprises a cabin bottom plate detachably installed on the rack and an installation frame arranged at the upper end of the cabin bottom plate, and a first circuit board and a second circuit board are installed on the installation frame and the cabin bottom plate respectively. The empennage assembly comprises a tail pipe detachably installed on the rack and a tail rotor wing arranged at the tail of the tail pipe, and the foot stool assembly comprises a foot stool body detachably installed at the lower end of the rack. The whole large system of the unmanned helicopter is divided into functional units which can be separated from one another, and each functional unit is high in integration level and convenient to design, assemble, maintain, transport and the like.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned helicopter. Background technique [0002] An unmanned helicopter generally includes a main fuselage, an empennage, and a tripod. Most of the existing unmanned helicopters adopt the design method of taking the whole machine as a whole. There are also some unmanned helicopters that design and assemble the main fuselage as a whole. The main fuselage includes a frame as the backbone, and various components used to complete the flight function are scattered on the frame. . Therefore, when the existing unmanned helicopters are assembled, debugged, maintained and transported, all need to be carried out for the whole machine. It is not easy to ensure the accuracy during assembly; during maintenance, it is often necessary to overhaul the whole machine due to the failure of individual components, which brings great difficulties to fault diagnosis, and it will...

Claims

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Application Information

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IPC IPC(8): B64C27/06B64C1/06B64D27/24B64C5/02B64C25/32
CPCB64C27/06B64C1/068B64D27/24B64C5/02B64C25/32B64C2025/325B64U30/20B64U50/19B64U10/10
Inventor 李钊刘一唐知杨王江平梅粲文
Owner ZHUHAI ZIYAN UAV CO LTD
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