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Novel light-weight 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 machine, the overall complexity and bulkiness of the helicopter, and the overall structure of the fuselage, etc., and achieve the effect of light weight, reasonable placement and simple structure

Inactive Publication Date: 2016-07-20
许美兰
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  • Summary
  • Abstract
  • Description
  • Claims
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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-weight and flexible high-altitude flight device
  • Novel light-weight and flexible high-altitude flight device
  • Novel light-weight and flexible high-altitude flight device

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Experimental program
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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-weight and flexible high-altitude flight device, which comprises a horizontal framework, vertical frameworks, an upper main shaft fixing frame, a lower main shaft fixing frame and a double-steering-engine fixing frame, wherein the vertical frameworks are fixed on the horizontal framework; the vertical frameworks consist of a left vertical framework and a right vertical framework; the upper main shaft fixing frame and the lower main shaft fixing frame are fixed between the left and right vertical frameworks; and the double-steering-engine fixing frame is fixed on the back part of the left and right vertical frameworks. A model airplane has the advantages that the main body structure is simple, perfect, reasonable and applicable; and each component arranged on the model airplane can be effectively fixed.

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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IPC IPC(8): A63H27/133
Inventor 许美兰
Owner 许美兰
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