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Helicopter based on gyroscope principle

A technology for helicopters and gyroscopes, applied in the field of helicopters, can solve the problems of driver and passenger helicopter property safety safety hazards, driver's line of sight and driving attitude skew, driving safety increase, etc., to achieve good safety performance, stable center of gravity, and avoid dizziness. Effect

Active Publication Date: 2017-06-09
武汉八维时空信息技术股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, in traditional helicopters, when turning or encountering external environmental influences, the helicopter will produce certain fluctuations, which will cause the driver's sight and driving posture to be skewed, which will increase the risk of driving safety, and will be harmful to the driver, passengers and helicopter. Own property security poses certain security risks

Method used

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  • Helicopter based on gyroscope principle
  • Helicopter based on gyroscope principle
  • Helicopter based on gyroscope principle

Examples

Experimental program
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Effect test

Embodiment 1

[0047] Such as figure 1 , 2 , shown in 3, a kind of helicopter based on gyroscope principle, helicopter comprises: cockpit 1, energy device 2, first adjustment frame 3, second adjustment frame 4, support 5 and a plurality of power devices 6; On the top of the energy device 2; the inner wall of the first adjustment frame 3 is slidingly connected with the outer wall of the power device 2 through a pair of symmetrically arranged adjustment pulleys 301; The outer wall of an adjustment frame 3 is rotatably connected; the bracket 5 is arranged on the bottom of the energy device 2; a plurality of power devices 6 are evenly arranged on the outer wall of the second adjustment frame 4; the control system inside the cockpit 1 controls a pair of adjustment pulleys 301 rotates so that the cockpit of the cockpit 1 remains in front of the moving direction; the control system controls a pair of adjustment rotating shafts 401 to rotate so that the cockpit 1 remains horizontal;

[0048]The co...

Embodiment 2

[0061] Such as Figure 4 As shown, the present embodiment provides a helicopter based on the gyroscope principle. The difference from Embodiment 1 is that the interior of the energy device 2 is composed of a plurality of energy cells 201; the plurality of energy cells 201 are slidingly arranged inside the energy device 2; The system controls the movement of multiple energy batteries 201 so that the center of gravity of the combination of the cockpit 1 and the energy device 2 is stable;

[0062] Since the interior of the cockpit 1 can be set with an appropriate number of seats and some necessary items according to the needs, when the passengers enter the interior of the cockpit 1, the center of gravity of the cockpit 1 will change, and at this time, the energy battery 201 of the control system is used to move , so that the center of gravity of the combination of the cockpit 1 and the energy device 2 is stable, which can ensure the smooth flight of the present invention.

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Abstract

The invention creatively discloses a helicopter based on a gyroscope principle. The helicopter comprises a cockpit, an energy device, a first adjusting frame, a second adjusting frame, a support frame, and a plurality of power devices; the cockpit is arranged at the top of the energy device; the inner wall of the first adjusting frame is in sliding connection with the outer walls of the power devices through a pair of symmetrically-arranged adjustable pulleys; the inner wall of the second adjusting frame is in rotational connection with the outer wall of the first adjusting frame through a pair of symmetrically-arranged adjustable rotating shafts; the support frame is arranged at the bottom of the energy device; the plurality of power devices are uniformly arranged on the outer wall of the second adjusting frame. The helicopter creatively disclosed by the invention has the benefits that the structure is novel; with the help of the pair of adjustable pulleys and the pair of adjustable rotating shafts, the cockpit is kept horizontal, and a cab of the cockpit is over against the moving direction of the helicopter creatively disclosed by the invention; the safety performance is good, the driving of a driver is facilitated, and the dizziness of the driver and passengers is avoided.

Description

technical field [0001] The invention relates to the technical field of helicopters, in particular to a helicopter based on the gyroscope principle. Background technique [0002] A traditional helicopter includes a cockpit, a propeller, and a bracket installed at the bottom of the cockpit. The propeller is used to provide lift for the movement of the helicopter, thereby completing the flight work of the helicopter. [0003] However, in traditional helicopters, when turning or encountering external environmental influences, the helicopter will produce certain fluctuations, which will cause the driver's sight and driving posture to be skewed, which will increase the risk of driving safety, and will be harmful to the driver, passengers and helicopter. Own property safety causes certain potential safety hazard. Contents of the invention [0004] The purpose of the present invention is to provide a helicopter based on the gyroscope principle, which has a novel structure, and wi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C17/06B64C27/08B64C27/20B64D25/00
CPCB64C17/06B64C27/08B64C27/20B64D25/00
Inventor 罗德纯黄哲捷宋晓强罗德龙
Owner 武汉八维时空信息技术股份有限公司
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