A vertical take-off and landing fixed-wing cargo drone

A vertical take-off and landing, fixed-wing technology, applied in the field of unmanned aerial vehicles, can solve the problems of short cruising range, low flying speed, high price, etc., to achieve the effect of increasing the lift area, easy pitching attitude, and increasing the cruising range

Active Publication Date: 2022-02-08
天津零一智能科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, traditional rotor-type UAVs generally have problems such as high price, low flight speed, and short cruising range, which greatly limit the scope of application of rotor-type UAVs in logistics and transportation systems.
Although traditional fixed-wing cargo drones have a very impressive load capacity and cruising range, fixed-wing cargo drones often need a very flat runway to roll to achieve takeoff and landing, which puts forward very high requirements for the environment. , which makes it inapplicable in many cases
At the same time, the current loading and unloading of drones relies on manual work. In some remote areas with inconvenient transportation or places that are not convenient for human access, normal loading and unloading cannot be achieved.

Method used

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  • A vertical take-off and landing fixed-wing cargo drone
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  • A vertical take-off and landing fixed-wing cargo drone

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Embodiment Construction

[0024] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0025] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and thus should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be understood ...

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Abstract

The invention provides a vertical take-off and landing fixed-wing cargo unmanned aerial vehicle, which includes a fuselage, a mechanical arm is mounted under the middle beam of the fuselage, a cargo warehouse is arranged above, and winglets and landing gear are symmetrically installed on both sides. The first landing gear is A-shaped, the braces of the two landing gears are fixed to the middle beam through connecting rods, the first power system parallel to the fuselage is fixedly connected to the middle beam through the first carbon rod, and the second power system perpendicular to the fuselage The system is fixedly connected to the upper beam of the fuselage through the second carbon rod. An equipment compartment is arranged above the upper beam. The flight control, receiver, GPS and battery are loaded in the equipment cabin. The flight control signal is connected to the receiver and GPS, and the battery Power the flight controller, receiver and GPS. The vertical take-off and landing fixed-wing cargo unmanned aerial vehicle described in the present invention combines the advantages of the rotary-wing unmanned aerial vehicle and the fixed-wing unmanned aerial vehicle. Greatly increased cruising range.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicles, in particular to a vertical take-off and landing fixed-wing cargo unmanned aerial vehicle. Background technique [0002] The use of drones to realize the transportation of goods has attracted more and more attention. The cargo drones currently on the market are mainly four-rotor and six-rotor, which are used for distribution services at the end of the logistics system. Some large fixed-wing UAVs have also appeared, which are used for transportation services at the branch level of the logistics system. However, traditional rotor UAVs generally have problems such as high price, low flight speed, and short cruising range, which greatly limit the scope of application of rotor UAVs in logistics and transportation systems. Although traditional fixed-wing cargo drones have a very impressive load capacity and cruising range, fixed-wing cargo drones often need a very flat runway to roll to take o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C29/00B64C39/02
CPCB64C29/0025B64C39/02B64U10/25B64U70/80B64U50/19B64U30/20B64U2101/60B64U50/13
Inventor 武耀罡马超魏新超黄亚东王帅琪张辉
Owner 天津零一智能科技有限责任公司
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