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Multi-rotor aircraft system of helicopter

A multi-rotor aircraft and aircraft technology, applied in the field of flight, can solve the problems of inflexibility, discount of rescue effect, inaccessibility, etc., and achieve the effect of wide application

Inactive Publication Date: 2017-09-29
镇江市丹徒区硕源材料科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the helicopter is relatively large and not flexible enough to approach and stop at the target location very closely, which greatly reduces the rescue effect

Method used

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  • Multi-rotor aircraft system of helicopter

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0026] The following describes the helicopter-aircraft system of the present invention in detail by combining embodiments.

[0027] First, manufacture the aircraft frame, install the motors on the frame (generally more than 3 motors), and install the blades on the motors. Then install the high barometer, GPS module, gyroscope, accelerometer sensor and various control circuits, remote control system, wire control system, etc.

[0028] Then install people / load components, such as platforms, cabins, etc., on the lower part of the aircraft. And install the control system of the aircraft on the manned or loaded parts to facilitate the personnel to control the aircraft.

[0029] Install rescue channels, camera / monitoring systems, manipulators, etc.

[0030] Install a buffer system at the bottom of the aircraft.

[0031] Install an elastic safety rope on the aircraft and fix it to the helicopter.

[0032] Fix the generator on the helicopter, and connect the power supply line of the motor on t...

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PUM

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Abstract

The invention discloses a multi-rotor aircraft system of a helicopter. The system comprises the helicopter and a multi-rotor aircraft, wherein the multi-rotor aircraft may be manned. The system provided by the invention has the characteristic that the system overcomes the problem of non-flexibility of the helicopter.

Description

Technical field [0001] The invention belongs to the field of flight, in particular to a helicopter multi-rotor aircraft system. Background technique [0002] At present, natural disasters such as earthquakes, floods, and mudslides, as well as emergencies such as falling into the water, being trapped in the mountains due to disasters, leakage of chemical dangerous goods, and fires in high-rise buildings, etc., make people and property in danger from time to time, making fire and rescue work very difficult. important. [0003] Currently, helicopters are mainly used for rescue. However, the helicopter is relatively large and not flexible enough to approach and stop at the target location very close, which greatly reduces the rescue effect. Summary of the invention [0004] Purpose of the invention: In order to make full use of the maneuverability of helicopters and the advantages of multi-rotor aircraft, such as flexibility, small size and hovering capability, the present invention p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D5/00
CPCB64C39/02B64C39/024B64D5/00
Inventor 王淑妍杨卫国孙文畅
Owner 镇江市丹徒区硕源材料科技有限公司
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