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Novel light and flexible high-altitude flight device

A flying device and lightweight technology, applied in the field of model aircraft, can solve the problems of increasing the weight of the whole aircraft, the overall complex and bloated helicopter, and the overall structure of the fuselage, etc., and achieve the effects of light weight, simple structure and reasonable placement.

Inactive Publication Date: 2019-02-26
许美兰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Generally, model airplanes have many components, the overall structure of the fuselage is complicated, and the placement of each component is unreasonable and stable.
Fixing the battery requires adding some additional fixtures, making the helicopter complex and bloated as a whole, increasing the weight of the whole machine

Method used

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  • Novel light and flexible high-altitude flight device
  • Novel light and flexible high-altitude flight device
  • Novel light and flexible high-altitude flight device

Examples

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Embodiment Construction

[0012] The present invention will be further described below in conjunction with the accompanying drawings.

[0013] The main body frame 140 is a supporting mechanism for the main body of the fuselage, which can maintain the stability of spare parts during the flight of the fuselage. The main shaft 6 and the main frame form the supporting mechanism of the main body of the fuselage. The main body frame is erected above the tripod and connected with the tail body for supporting several control components on the main body of the fuselage.

[0014] The present invention mainly consists of: horizontal frame 1, left vertical frame 2, right vertical frame 3, upper main shaft fixing frame 4, lower main shaft fixing frame 5, single steering gear fixing plate (not shown), double steering gear fixing plate 7, gyroscope Instrument fixed plate 8, tailpipe fixed frame 9 and motor fixed frame 10 are formed.

[0015] The specific connection method: the left vertical framework 2 and the righ...

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PUM

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Abstract

The invention provides a novel light and flexible high-altitude flight device. The flight device comprises a horizontal frame, a vertical frame, an upper main shaft fixing rack, a lower main shaft fixing rack and a dual-steering gear fixing rack, the vertical frame is fixed to the horizontal frame, the vertical frame is composed of a left vertical frame and a right vertical frame, the upper and lower main shaft fixing frames are fixed between the left and right vertical frames, and the dual steering gear fixing frame is fixed at the rear portions of the left and right vertical frames. The flight device has the advantages that the main body structure is simple, perfect, reasonable and applicable, and the flight device can effectively fix components installed on a model aircraft.

Description

technical field [0001] The invention relates to the field of model airplanes, in particular to a novel lightweight and flexible high-altitude flying device. Background technique [0002] Generally, model airplanes have many components, the overall structure of the fuselage is complicated, and the placement of each component is unreasonable and stable. Fixing the battery needs to add some additional fixtures, which makes the helicopter complex and bloated as a whole, and increases the weight of the whole machine. Contents of the invention [0003] Based on the deficiencies of the prior art, the main purpose of the present invention is to provide an applicable aircraft model main frame assembly with a simple appearance and a reasonable structure. [0004] In order to achieve the above object, the present invention provides a novel lightweight and flexible high-altitude flying device, comprising a horizontal frame, a vertical frame, an upper main shaft fixing frame, a lower ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18
CPCA63H27/02
Inventor 许美兰
Owner 许美兰
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