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Aircraft model with auxiliary leveling blade control system

A control system and auxiliary balance technology, which is applied in the field of model aircraft with auxiliary balance blade control system, can solve problems such as difficulties, operator and airframe safety threats, and achieve the effect of ensuring safe use and smooth flight movement.

Inactive Publication Date: 2019-03-15
马铿杰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Generally, the balance of model aircraft is controlled by manual power, so there are high requirements for operation. For beginners, it is very difficult to go from unfamiliar to proficient.
At the same time, model airplanes use the high-speed rotation of the propellers to bring lift. This strong centrifugal force poses a severe test to the steering action of model airplanes. Model airplanes may also lose their balance due to strong centrifugal force when turning. fall out, endangering the safety of its operator and the body itself

Method used

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  • Aircraft model with auxiliary leveling blade control system
  • Aircraft model with auxiliary leveling blade control system
  • Aircraft model with auxiliary leveling blade control system

Examples

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Embodiment Construction

[0019] refer to figure 1 , which illustrates the disassembly of an embodiment of the present invention; refer to figure 2 , illustrating a schematic assembly of an embodiment; refer to image 3 , illustrates a bottom view of the blade fixing device of an embodiment; in this embodiment, the self-balancing headstock device includes an aircraft drive shaft 1, a rotating block 11, a rotating block bearing 111, a rotating block strip groove 112, a cylinder Pin 113, fixed through hole 114, rotating device 2, a pair of main blades 20, main blade bolts 201, main blade nuts 202, a pair of balance blades 21, balance blade bolts 211, balance blade nuts 212, balance rods 22, balance rods Bearing 221, blade fixing device 23, blade fixing device slot 231, vertical through hole 232, horizontal through hole 233, counterweight sleeve 24, hexagon socket bolt 241, "ten" shaped frame 25 that forms an acute angle with the horizontal plane, balance baseball shape Overcoat 26, spherical overcoat ...

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Abstract

The invention discloses an aircraft model with an auxiliary leveling blade control system, which comprises an aircraft driving shaft and a rotating device fixedly connected with the driving shaft, wherein the rotating device comprises an auxiliary main blade and an auxiliary leveling blade which are connected through a blade fixing device. According to the aircraft model with auxiliary leveling blade control system, the whole fuselage can be automatically leveled in the steering process, so that the flying motion of the aviation aircraft can be more stable and smooth, and the model airplane cannot be disintegrated due to the out-of-control of centrifugal force.

Description

technical field [0001] Aircraft model with sub-balance blade control system. Background technique [0002] Generally, the balance of model aircraft is controlled by manual power, so there are high requirements for operation. For beginners, it is very difficult to go from unfamiliar to proficient. At the same time, model airplanes use the high-speed rotation of the propellers to bring lift. This strong centrifugal force poses a severe test to the steering action of model airplanes. Model airplanes may also lose their balance due to strong centrifugal force when turning. If it falls out, the safety of its operator and the body itself is threatened. Therefore, automatic balance has become the endless pursuit of various aircraft model manufacturers and aircraft model enthusiasts. [0003] Therefore, need to invent a kind of model aircraft that can automatically balance in motion to solve the above problems. Contents of the invention [0004] The present invention aims at th...

Claims

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Application Information

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