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Modular airplane model provided with capacitor power supply

An aircraft model and capacitor technology, which is applied in the field of mold aircraft, can solve the problems of reduced anti-vibration capability, poor neutral point characteristics, large size of induction equipment, etc., and achieves the effect of improving seismic performance and small size

Inactive Publication Date: 2018-07-10
许美兰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The operator of the toy aircraft cannot set various parameters for controlling the flight of the toy aircraft on the azimuth indicator of the toy aircraft without an operation panel
In addition, the volume of all the induction devices of the modular aircraft model with capacitor power supply is also relatively large, which leads to the reduction of the vibration isolation ability of the modular aircraft model with capacitor power supply, and also makes the neutral point characteristics worse

Method used

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  • Modular airplane model provided with capacitor power supply

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Embodiment Construction

[0011] Embodiments of the present invention will now be described in conjunction with the accompanying drawings.

[0012] see figure 1 , the present invention has a modular aircraft model with a capacitor power supply, which is used for a toy aircraft, and is connected with the receiving device and the tail rudder servo on the toy aircraft, including a remote control device 22 and an induction device 33 connected with the remote control device 22, on the remote control device 22 An operation panel 23 is provided, and a liquid crystal display 231 is arranged on the operation panel 23 , and a plurality of buttons 232 and 233 are arranged below the liquid crystal display 231 on the operation panel 23 . In combination with the plurality of buttons 232 and 233 and the LCD display 231, the operator of the toy aircraft can precisely set the parameters required to control the flight of the toy aircraft.

[0013] The sensing device 33 has a maximum diameter of not more than 30 mm and ...

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Abstract

The invention discloses a modular airplane model provided with a capacitor power supply. The modular airplane model comprises a remote control device and induction equipment which is connected to theremote control device, wherein an operating panel is arranged on the remote control device; a liquid crystal display screen is arranged on the operating panel; and a plurality of buttons are additionally arranged at the lower side of the liquid crystal display screen on the operating panel. According to the modular airplane model provided with the capacitor power supply provided by the invention,various parameters required by the toy aircraft (the airplane model) can be set and changed at any time via the plurality of buttons, and changes of the set parameters can be displayed in real time via the liquid crystal display screen, so that required parameters can be precisely set by an operator. In addition, the adopted induction equipment is small in volume; therefore, the anti-seismic property of the anti-seismic property is enhanced.

Description

technical field [0001] The invention relates to a mold aircraft, in particular to a positioning control system installed on the toy aircraft. Background technique [0002] When the toy aircraft is in a hovering state in the air, sometimes it is hit by a crosswind, and at this time, the tail rudder of the toy aircraft will deviate in the horizontal direction. In order to correct this offset phenomenon, a modular airplane model with a capacitor power supply capable of adjusting direction is usually installed on the tail rudder of the toy aircraft. When the tail rudder of the toy aircraft deviates, the modular aircraft model with capacitor power supply will send a corresponding control signal to the tail rudder servo on the toy aircraft, and the tail rudder will make the tail rudder move in the opposite direction to the offset direction through the tail rudder servo. action, thereby resisting the deflection of the tail rudder. [0003] In the prior art, the azimuth indicator ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): A63H27/18A63H30/02
CPCA63H27/02A63H30/02
Inventor 许美兰
Owner 许美兰