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Man-electric hybrid double-layer rotorcraft

A gyrocopter and electric hybrid technology, applied in the field of aircraft, can solve the problems of limited application scope and the need for taxiing distance on the take-off runway.

Inactive Publication Date: 2021-02-05
GUANGDONG GUOSHIJIAN TECH DEV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its advantage is that it has lower requirements on the take-off runway but still needs to glide distance, and it cannot hover in the air. The application range is limited

Method used

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  • Man-electric hybrid double-layer rotorcraft
  • Man-electric hybrid double-layer rotorcraft
  • Man-electric hybrid double-layer rotorcraft

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Embodiment Construction

[0022] The technical solutions of the present invention will be described below in conjunction with the accompanying drawings and embodiments.

[0023] Such as Figure 1 to Figure 5 As shown, a human-electric hybrid double-deck rotorcraft of the present invention includes a cabin 1, and a human-electric hybrid device is provided in the cabin 1, and the human-electric hybrid device includes a human drive unit 12, an electric drive unit 13, a crank wheel 18 and the connecting rod 25, the connecting rod 25 is fixed on the crank wheel 18, the human drive unit 12 and the electric drive unit 13 are respectively connected to the crank wheel 18 through the transmission structure, the top of the cabin 1 is provided with a flying device, and the flying device includes the first flying unit With the second flight unit, the first flight unit includes a sleeve 11, a two-rotation bearing 10 and lower rotors 7 symmetrically fixed on both sides of the two-rotation bearing 10, the second rotat...

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PUM

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Abstract

The invention relates to the technical field of aircrafts, in particular to a man-electric hybrid double-layer rotorcraft. The rotorcraft comprises a cabin, and a man-electric hybrid power device is arranged in the cabin; the man-electric hybrid power device comprises a man-powered driving unit, an electric driving unit, a crank wheel and a connecting rod, wherein the connecting rod is fixed to the crank wheel; the manpower driving unit and the electric driving unit are connected to the crank wheel through transmission structures, a flying device is arranged at the top of the cabin and comprises a first flying unit and a second flying unit, and the first flying unit comprises a sleeve, a second rotating bearing and lower-layer rotors symmetrically fixed to the two sides of the second rotating bearing; the second rotating bearing is fixed on the sleeve, and the sleeve is fixed in the cabin; the second flight unit comprises a transmission rod, a first rotating bearing and upper-layer rotor wings symmetrically fixed to the two sides of the first rotating bearing, the first rotating bearing is fixed to one end of the transmission rod, and the other end of the transmission rod penetrates through the sleeve and is hinged to a connecting rod of the man-electric hybrid power device; and the transmission rod is connected with the sleeve through a linear bearing.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a human-electric hybrid double-deck rotorcraft. Background technique [0002] The lift device of an aircraft is a device based on aerodynamics. According to the structure, it can be divided into fixed wings and rotors. Fixed wing aircraft generally have a fuselage and symmetrically arranged fixed wings, which are powered by propellers to obtain greater flight speeds. and mobility. The principle of flight is that there is a relative speed between the fixed wing and the air, and the air interacts with the sides of the fixed wing to generate lift so that the aircraft obtains flight capability. The disadvantage of fixed-wing aircraft is that it cannot hover in the air, and needs to taxi on the runway to take off or land and support the construction of airport facilities. A rotorcraft such as a helicopter is characterized in that it does not need a runway when it takes off and can ...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/12B64C27/32B64C27/10B64C31/04B64D27/02
CPCB64C27/08B64C27/12B64C27/32B64C27/10B64C31/04B64D27/02B64D27/026
Inventor 王志成
Owner GUANGDONG GUOSHIJIAN TECH DEV CO LTD
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