Anmechanical arm vertical folding structure of a rotor unmanned aerial vehicle

An unmanned, vertical folding technology for rotors, applied in the direction of air flow, fuselage, and aircraft parts that affect the surface of the aircraft, can solve problems such as affecting the overall aesthetics, complex structure, exposed structural parts, etc., and achieve fast and efficient folding. , to avoid left and right swing, to ensure the effect of stability

Inactive Publication Date: 2018-12-18
CHANGXING HAIPU MACHINERY TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to address the deficiencies of the prior art, by setting the engaging parts to cooperate with the adjusting parts, so that when in use, the mounting seat of the machine arm is connected with the mounting seat of the fuselage, so that the connection is firm and the structural parts are not tight. Leakage; when disassembled, the clamping part and the adjusting part are disengaged, and the adjusting part can be manually pressed, and the limit part can be moved synchronously to limit the fuselage components, thus solving the problem of complex structure and exposed structural parts, which affect the overall appearance sexual technical issues

Method used

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  • Anmechanical arm vertical folding structure of a rotor unmanned aerial vehicle
  • Anmechanical arm vertical folding structure of a rotor unmanned aerial vehicle
  • Anmechanical arm vertical folding structure of a rotor unmanned aerial vehicle

Examples

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Embodiment 1

[0051] Such as figure 1 Shown, the vertical folding structure of the machine arm of a kind of rotor UAV is characterized in that, comprises:

[0052] Arm mount 1;

[0053] The storage assembly 2 is located at the front end of the arm mounting base 1, and it includes a built-in part 21, an adjustment part 22 that is slidably arranged in the built-in part 21 and slides up and down along the vertical direction, and the The regulating part 22 is hingedly connected to the limiting part 24 and the turning part 23 arranged at the lower end of the built-in part 21; and

[0054] Fuselage component 3, the fuselage component 3 includes a fuselage mounting seat 31, a snap-fitting member 32 arranged on the upper end of the fuselage mounting seat 31 and overlapped with the adjusting member 22, and an engaging member 32 arranged on the fuselage The mounting piece 33 at the lower end of the mounting base 31 .

[0055] In this embodiment, by setting the engaging part 32 to engage with the a...

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PUM

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Abstract

The invention relates to a mechanical arm vertical folding structure of a rotor unmanned aerial vehicle. The structure comprises a mechanical arm mounting seat, a storage assembly, a fuselage assembly, a clamping assembly and a mounting member. AThe storage assembly is located at the front end of the arm mounting base, comprising a built-in member, an adjusting member slidably arranged in the built-in member and sliding up and down in the vertical direction, and a flip member arranged at a lower end portion of the built-in member; n the fuselage assembly comprises a fuselage mounting seat, aclamping member arranged at the upper end of the fuselage mounting seat and overlapped with the adjusting member, and a mounting member is arranged at the lower end of the fuselage mounting seat; Theinvention solves the technical problems that the structure is complex, the structural parts are exposed, and the overall aesthetics is affected.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a vertical folding structure of a rotor unmanned aerial vehicle. Background technique [0002] Today, with the rapid development of drones, the application fields of unmanned aerial vehicles are constantly expanding. Both industrial drones and consumer drones have made great progress, especially small and micro drones represented by multi-rotor unmanned aerial vehicles. For human aircraft, the mainstream arms of UAVs currently use integrated arms, which are not easy to store, bulky, and increase transportation costs. Therefore, some UAVs have adopted folding devices, but the connection is not firm and easy to loosen. Hidden danger. [0003] The patent document with the patent number CN2014207507421 discloses the disassembly of the joint sleeve assembly of the arm of the multi-rotor UAV, which includes a joint pipe clamp seat, a joint pipe clamp sleeve and a wren...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C1/30
CPCB64C1/069B64C1/30
Inventor 倪瑞华
Owner CHANGXING HAIPU MACHINERY TECH CO LTD
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