Unmanned aerial vehicle battery mounting structure and unmanned aerial vehicle
A technology for installation structure and machine battery, which is applied in the field of aviation aircraft, can solve the problems of low battery disassembly efficiency and inconvenient operation, and achieve the effect of inconvenient operation and improved disassembly efficiency
Pending Publication Date: 2019-09-06
SHENYANG WOOZOOM TECH CO LTD
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- Abstract
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- Claims
- Application Information
AI Technical Summary
Problems solved by technology
When the battery needs to be charged or replaced, the operator usually manually removes each battery from the mounting bracket, and then fixes each battery on the installation when the charging or replacement is completed, which is inconvenient to operate and the battery disassembly efficiency is relatively low Low
Method used
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[0047] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below with reference to the drawings in the preferred embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail b...
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The invention discloses an unmanned aerial vehicle battery mounting structure and an unmanned aerial vehicle, relates to the technical field of aviation aircrafts, and mainly aims to enable the battery dismounting operation of the unmanned aerial vehicle to be convenient so as to improve the dismounting efficiency of batteries. Through the main technical scheme, the unmanned aerial vehicle batterymounting structure comprises a mounting rack, a fixed body and a driving part, wherein the fixed body is slidably connected to the interior of the mounting rack, and the fixed body is internally provided with a plurality of accommodating cavities for accommodating a plurality of batteries, the contour shapes of the accommodating cavities are matched with those of the batteries; the output end ofthe driving part is detachably connected with the fixed body, the driving part is used for being electrically connected with a flight control system of the unmanned aerial vehicle, and the driving part can drive the fixed body to slide into or slide out of the mounting rack under the control of the flight control system. The unmanned aerial vehicle battery mounting structure is mainly used for improving the battery dismounting efficiency of the unmanned aerial vehicle.
Description
technical field [0001] The invention relates to the technical field of aviation aircraft, in particular, to a battery installation structure for an unmanned aerial vehicle and an unmanned aerial vehicle. Background technique [0002] The application and development of UAVs in various industries is becoming more and more extensive. At this stage, UAVs have been applied to aerial photography, agricultural and forestry plant protection, geological exploration, power inspection, oil and gas pipeline inspection, highway accident management, forest fire prevention inspection and environmental pollution. Surveying and other fields. [0003] Among them, the multi-rotor drone is a kind of unmanned aerial vehicle capable of vertical take-off and landing, and most of them are electric drones. At present, multi-rotor UAVs are usually powered by multiple batteries, and each battery is usually fixed on the mounting frame of the fuselage with a magic cable tie or a baffle. When the batte...
Claims
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Patent Timeline
Login to View More IPC IPC(8): H01M2/10H01M2/20B64D27/24B60L53/80
CPCB64D27/24B60L53/80H01M2220/20B60L2200/10H01M50/20H01M50/50B64U50/19Y02T50/60Y02T10/70Y02T10/7072Y02E60/10
Inventor 边文全周丽霞肖川
Owner SHENYANG WOOZOOM TECH CO LTD