Unmanned plane take-off and landing rack and unmanned plane

A technology for landing gear and drones, applied in the field of drones, can solve problems such as docking instability and drone docking instability

Active Publication Date: 2018-05-11
BYD CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] An object of the present disclosure is to provide a landing gear for unmanned aerial vehicles to solve the problem of unsteady docking of unmanned aerial vehicles when landing
[0004] Another object of the present disclosure is to provide an unmanned aerial vehicle to solve the problem of unstable docking when landing

Method used

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  • Unmanned plane take-off and landing rack and unmanned plane
  • Unmanned plane take-off and landing rack and unmanned plane
  • Unmanned plane take-off and landing rack and unmanned plane

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Embodiment Construction

[0054] Specific embodiments of the present disclosure will be described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the present disclosure, and are not intended to limit the present disclosure.

[0055] In this disclosure, unless stated to the contrary, the used orientation words such as "up and down" usually refer to the up and down of the UAV in a stable flight state and when it lands, and "inside and outside" are for In terms of the contour of the corresponding component itself.

[0056] The present disclosure provides an unmanned aerial vehicle landing gear, a landing platform and a landing device matched with the landing gear. Such as figure 1 and figure 2 As shown, the UAV landing gear 2000 provided by the present disclosure includes a landing gear body 2100 arranged at the bottom of the UAV 1000 and a locking mechanism 2200 accommodated in ...

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Abstract

The present disclosure relates to an unmanned plane take-off and landing rack and an unmanned plane, wherein the unmanned plane take-off and landing rack includes a take-off and landing rack body (2100) disposed at the bottom of the unmanned plane (1000) and a locking mechanism (2200) accommodated in the take-off and landing rack body (2100). The side wall of the take-off and landing rack body (2100) is provided with a guide hole (2110), and the outer wall of the take-off and landing rack body (2100) is protruded to form stoppers (2130). The stoppers are spaced above the guide hole, and the locking mechanism includes a locking block (2210) and a drive mechanism for driving the locking block to extend out and retract from the guide hole. When the unmanned plane lands on a take-off and landing platform, the upper part of the unmanned plane is positioned by the stoppers on the outer wall of the take-off and landing rack body, the lower part of the unmanned plane is positioned by the locking block, the stability of the unmanned plane is improved when the unmanned plane is docked. The locking block can be extended out and retracted from the take-off and landing rack body, and the locking and unlocking of the unmanned plane can be realized separately.

Description

technical field [0001] The present disclosure relates to the technical field of unmanned aerial vehicles, and in particular, relates to an unmanned aerial vehicle landing gear and an unmanned aerial vehicle. Background technique [0002] At present, many drones are equipped with landing gear for adaptive landing on the landing platform. In related technologies, the drone is not stable enough to land on the landing platform stably. In addition, due to the When the UAV lands, the positioning accuracy is required to be high, and it needs to land with zero deviation, so the operation is more complicated. And because it is often necessary to add an intelligent control system, the cost is relatively high. In addition, the current UAV take-off and landing platform can only adapt to a single type of UAV, but cannot adapt to multiple types of UAVs, and cannot dock multiple UAVs at the same time. Contents of the invention [0003] An object of the present disclosure is to provide ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/04B64F1/00B60P3/11
CPCB60P3/11B64C25/04B64F1/007B64C25/00B64F1/00
Inventor 杜淼森赵自强王悦赵炳根
Owner BYD CO LTD
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