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Unmanned plane

A technology of unmanned aerial vehicles and fuselage, which is applied in the field of unmanned aerial vehicles, which can solve the problems of unstable installation of power arm, inconvenient installation of rotor, poor rigidity of fuselage, etc., and achieve compact structure, reduced model size, and improved stability Effect

Pending Publication Date: 2017-12-05
天津市宏宇天翔科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, most multi-rotor UAVs have poor rigidity and stability of the fuselage, unstable installation of the power arm, and inconvenient installation of the rotor. Therefore, it is necessary to provide a UAV that is easy to assemble, stable in connection, and strong in rigidity.

Method used

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Embodiment Construction

[0019] Below, the substantive features and advantages of the present invention will be further described in conjunction with examples, and the present invention includes but is not limited to the listed embodiments.

[0020] see Figure 1-7 As shown, an unmanned aerial vehicle includes multiple groups of rotors 40, a fuselage 10 made of metal and a triangular truss type power arm 20 made of metal, and the triangular truss type power arm is connected to the rotor power system 30 through a limit mounting plate 80 (see Figure 6 As shown), the installation positions of the adjacent two groups of rotors are arranged one above and one below relative to the fuselage.

[0021] see figure 2 As shown, the fuselage includes an outer shell 12 and an openable upper cover 11 , a metal support frame 13 and a plurality of battery boxes 50 made of metal are arranged inside the outer shell, and a landing gear 60 is connected to the lower part of the fuselage.

[0022] Wherein, the battery ...

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Abstract

The invention relates to an unmanned plane, which comprises multiple rotors, a metal fuselage and triangular truss-type power arms. The triangular truss-type power arm is connected to a rotor power system through a limit mounting plate. Adjacent two rotors are arranged up and down relative to the fuselage. The fuselage comprises a shell and an upper cover which can be opened. The bottom of the fuselage is connected to an undercarriage. The unmanned plane of the present invention has excellent rigidness, good stability and high flight efficiency.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a novel unmanned aerial vehicle. Background technique [0002] UAVs are widely used in military and civilian fields. At present, most multi-rotor UAVs have poor rigidity and stability of the fuselage, unstable installation of the power arm, and inconvenient installation of the rotor. Therefore, it is necessary to provide a UAV that is easy to assemble, stable in connection, and strong in rigidity. Contents of the invention [0003] The purpose of the present invention is to solve the above-mentioned technical problems, and to provide an unmanned aerial vehicle with an all-metal structure. [0004] To achieve the above object, the present invention adopts the following technical solutions: [0005] An unmanned aerial vehicle, comprising multiple sets of rotors, a fuselage made of metal, and a triangular truss-type power arm, the triangular truss-ty...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C1/06B64C27/08B64C25/04
CPCB64C1/06B64C25/04B64C27/08B64C39/02B64U50/19B64U10/10
Inventor 苗海王滨
Owner 天津市宏宇天翔科技有限公司