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Simulation running debugging device for steering engine of model airplane

A technology for simulating operation and steering gear, which is applied in the field of model aircraft, which can solve the problems of safety threats and difficulties of the operator and the airframe, and achieve the effect of smooth and smooth flight movement and ensure the safety of use.

Inactive Publication Date: 2018-05-25
马铿钧
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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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  • Simulation running debugging device for steering engine of model airplane
  • Simulation running debugging device for steering engine of model airplane
  • Simulation running debugging device for steering engine of model airplane

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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 a simulation running debugging device for a steering engine of a model airplane. The device comprises an aviation aircraft drive shaft and a rotation device which is fixedly connected with the drive shaft, the rotation device comprises a pair of main blades and a pair of balance blades, and the main blades are connected with the balance blades through a blade fixing device.According to the simulation running debugging device for the steering engine of the model airplane, a whole aircraft body can be automatically balanced in the steering process, the flying motion of an aviation aircraft can be more stable and smooth accordingly, and the situation can be avoided that the aviation aircraft is broken up due to out-of-control centrifugal force.

Description

technical field [0001] The invention relates to a model airplane, in particular to a model airplane capable of self-balancing in motion. 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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18A63H27/133
CPCA63H27/02A63H27/12
Inventor 马铿钧
Owner 马铿钧
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