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Aircraft with support frame structure

An aircraft and support frame technology, applied in the field of aircraft with a support frame structure, can solve problems such as damage to unmanned aircraft, and achieve the effects of avoiding influence, strong controllability, and enhancing operation effects

Pending Publication Date: 2018-07-10
科力沃(深圳)科技技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When shooting or other operations, the fixed support frame brings a lot of inconvenience to the operation
And if the support frame is removed, when the aircraft lands, the fuselage will directly touch the ground, which will cause damage to the unmanned aircraft.

Method used

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  • Aircraft with support frame structure
  • Aircraft with support frame structure
  • Aircraft with support frame structure

Examples

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Embodiment Construction

[0029] In order to fully understand the technical content of the present invention, the technical solutions of the present invention will be further introduced and illustrated below in conjunction with specific examples, but not limited thereto.

[0030] Such as Figure 1 to Figure 10 It is a drawing of an embodiment of the present invention.

[0031] An aircraft with a supporting frame structure, such as Figure 1 to Figure 2 As shown, it includes an aircraft body 10 and a support frame structure 20 located at the lower end of the aircraft body 10 . The support frame structure 20 includes a retractable power part 21 , a transmission assembly 22 arranged at the power output end of the retractable power part 21 , and a support rod set 23 arranged at the power output end of the transmission assembly 22 . After the aircraft body 10 takes off, the support rod group 23 moves under the action of the retractable power part 21, and rises to both sides of the aircraft body 10, so as ...

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PUM

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Abstract

The invention relates to an aircraft with a support frame structure. The aircraft comprises an aircraft body and a support frame structure disposed at the lower end of the aircraft body; and the support frame structure comprises a retracting and releasing power component, a transmission assembly disposed at the power output end of the retracting and releasing power component, and a set of supportrods disposed at the power output end of the transmission assembly. The influence of the support frame structure on the operation of the aircraft body is avoided by arranging the support frame structure which can be automatically retracted and released on the aircraft body. The aircraft with the support frame structure is simple in structure and high in maneuverability, and the working effect of the aircraft body is enhanced.

Description

technical field [0001] The invention relates to flying equipment, more specifically to an aircraft with a support frame structure. Background technique [0002] Due to its powerful functions, unmanned aerial vehicles are increasingly favored by all walks of life. The support frame of many unmanned aircrafts on the market is fixed. When shooting or other operations, the fixed support frame brings a lot of inconvenience to the operation. And if the support frame is removed, when the aircraft lands, the fuselage will directly touch the ground, which will cause damage to the unmanned aircraft. [0003] Therefore, a suitable support frame must be considered to adapt the drone to work and land. Contents of the invention [0004] The object of the present invention is to overcome the defects of the prior art and provide an aircraft with a support frame structure. [0005] To achieve the above object, the present invention adopts the following technical solutions: [0006] An...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/10B64C1/06B64C1/30B64D47/08
CPCB64C1/063B64C1/30B64C25/10B64D47/08B64U10/10B64U2101/30
Inventor 王轶
Owner 科力沃(深圳)科技技术有限公司