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Wearable robot powering human flapping wing aircraft

A flapping aircraft and wearable technology, applied in the field of flapping aircraft

Pending Publication Date: 2018-11-27
CHINA UNIV OF GEOSCIENCES (WUHAN)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the series of problems existing in the development of the human flapping-wing aircraft, the present invention provides a wearable robot to assist the human flapping-wing aircraft, so as to optimize and improve various performance indicators of the manned flapping-wing aircraft

Method used

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  • Wearable robot powering human flapping wing aircraft
  • Wearable robot powering human flapping wing aircraft
  • Wearable robot powering human flapping wing aircraft

Examples

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Embodiment

[0036] The working principle block diagram (see figure 1 ), the structural representation of the human flapping-wing aircraft 35 assisted by the wearable robot (see figure 2 ).

[0037] Embodiment Wearable robot assists human flapping-wing aircraft 35, including: wearable assisting human flapping-wing flying robot 1, left wing 2, right wing 3, tail servo and transmission mechanism 4, power supply system, power-assisted take-off device 27; Assist human body flapping wing flying robot 1, including: wearer's helmet 5, wearer's joint angle sensor, main motor power-assisted wing beat mechanism 6 (see image 3 ), shape memory alloy wing pulse-assisted folding and deformation mechanism 7, wearer's flapping wing flying prone board 8, intelligent helmet controller, sensor series, global positioning system, brain wave instrument, wireless communication instrument, foldable telescopic vibration-absorbing caster 36 (See Figure 4 ), safety parachute device 9 (see figure 2 ); the wea...

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Abstract

The invention discloses a wearable robot powdering human flapping wing aircraft which comprises a wearable powering human flapping wing flight robot, a left wing, a right wing, a tail steering gear and transmission mechanism, a power system and a powering take-off gear. The wearable powering human flapping wing flight robot comprises a wearer's helmet, a wearer's joint angle sensor, a main motor powering wing flap mechanism, a shape memory alloy wing vein powering folding deformation mechanism, a wearer's flapping wing flight prone plate, an intelligent helmet controller, sensor series, a global positioning system, an electroencephalography, a radio communicator, a foldable and expandable vibration foot wheel and a safety parachute device. Through combination of the main motor powering wing flap mechanism, the shape memory alloy wing vein powering folding deformation mechanism, the tail steering gear and transmission mechanism and the intelligent helmet controller, the fun of human powering adaptive flapping wing flight is achieved, and safety, comfort, lightness and convenience in flapping wing flight experienced by human body are achieved.

Description

technical field [0001] The invention belongs to the technical field of flapping-wing aircraft, relates to a human-body flapping-wing aircraft, and more particularly relates to a human-body flapping-wing aircraft assisted by a wearable robot. Background technique [0002] The flapping wing aircraft refers to an aircraft that imitates flying creatures in nature and generates lift and forward force through the active movement of the wings, also known as the flapping wing aircraft. Flapping-wing flight is a flight mode commonly used by flying creatures in nature. Compared with fixed-wing and rotary-wing flight modes, flapping-wing flight can generate lift and thrust at the same time only by flapping the wing surface. It has high flight efficiency and good maneuverability. Advantages of compact structure. The manned flapping-wing aircraft has always been the dream of human beings to experience the free flight of individuals in the air like birds, and it was once the focus of peo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C33/02
CPCB64C33/00B64C33/02
Inventor 袁曦明袁一楠
Owner CHINA UNIV OF GEOSCIENCES (WUHAN)
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