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Rotor wing type toy plane stable in landing

A toy aircraft and rotor-type technology, applied in the field of toy aircraft, can solve problems such as bouncing and breaking, and achieve the effect of increasing stability and solving reaction force.

Inactive Publication Date: 2019-02-22
杭州大晨显示技术有限公司
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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 provide a rotary-wing type toy aircraft with stable landing, which solves the problem mentioned in the background technology that when the existing rotary-wing aircraft lands, if the landing speed is too fast, it is easy to occur when the aircraft lands. Bounce or break

Method used

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  • Rotor wing type toy plane stable in landing
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  • Rotor wing type toy plane stable in landing

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Embodiment Construction

[0024] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0025] Such as Figure 1-3 As shown, the embodiment of the present invention provides a rotary-wing toy aircraft with stable landing, including an aircraft body 1 and an aircraft wing 2 arranged on the aircraft body 1, and a fixed block 3 is fixedly installed on the bottom of the aircraft body 1, so that The bottom of the fixed block 3 is provided with a buffer plate 27, the top of the buffer plate 27 is fixedly equipped with a load-bearing block 4, and the tw...

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Abstract

The invention provides a rotor wing type toy plane stable in landing and relates to the field of toy planes. The rotor wing type toy plane stable in landing comprises a plane body and plane wings disposed on the plane body, fixing blocks are fixedly mounted at the bottom of the plane body, a buffering plate is disposed below the fixing blocks, and a load bearing block is fixedly mounted on the topof the buffering plate; connecting blocks are fixedly mounted on both sides of the top of the load bearing block, the tops of the connecting blocks are welded to the bottoms of pressing rods, and thetops of the pressing rods penetrate through the fixing blocks and extend into inner cavities of the fixing blocks. The fixing blocks are arranged, and partition plates, first lifting plates, second lifting plates are arranged in the fixing blocks for cooperating with hydraulic oil, so that the pressure generated during landing of the plane is buffered through the cooperation among the hydraulic oil, the first lifting plates and the second lifting plates, the reaction force of the ground to the plane during landing of the plane is counteracted, correspondingly landing of the plane is more stable, and the plane is protected from damage during landing.

Description

technical field [0001] The invention relates to the technical field of toy airplanes, in particular to a rotor-type toy airplane with stable landing. Background technique [0002] The rotary wing toy plane is a helicopter that can be controlled from a distance. Now the most common model is the RC helicopter model. Remote control helicopters are divided into two types: electric and oil-powered. The biggest difference from real helicopters is that there is an extra aileron for better control of the direction of the rotor. [0003] The take-off, flight, landing and other actions of the remote control helicopter mainly rely on the rotors to complete. When the blades of the main rotor rotate, an upward airflow relative to the air is generated, which naturally forms a lift force. The rotation speed of the rotor and the angle of each blade are transformed to cause the aircraft to complete various flight actions such as take-off, elevation, and landing. The forward flight of the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/133
CPCA63H27/12
Inventor 郭经洲程一龙王晓哲李辉
Owner 杭州大晨显示技术有限公司
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