Man-machine integrated simulation sound-induction aircraft

Abstract

The invention discloses a man-machine integrated simulation sound-induction aircraft. The man-machine integrated simulation sound-induction aircraft comprises a power blade, wherein a power device is electrically connected to the power blade; a seat is connected to one side of the power device, and steering blades are electrically connected to the other side of the power device; pedal plates are connected to one side of the seat; an operating rod is connected to one sides of the pedal plates, and is electrically connected with a display screen; a windshield is connected to one side of the display screen, and is electrically connected with a speech receiver; the sound receiver is electrically connected with a helmet. According to the man-machine integrated simulation sound-induction aircraft disclosed by the invention, through the arrangement of the power blade and the steering blades, the takeoff and the transformation of the aircraft are realized; through the arrangement of the speech receiver and the helmet, the effective input of speech is realized, so that the aircraft is convenient to control; through the arrangement of the operating rod and the display screen, various control for the aircraft is realized; the man-machine integrated simulation sound-induction aircraft is simple in structure, small in size and low in cost, so that the development of the aircraft is facilitated, and the aircraft is convenient to use.

Description

technical field [0001] The invention belongs to the field of aircraft, and in particular relates to a man-machine integrated simulated acoustic aircraft. Background technique [0002] At present, with the development of science and technology, people yearn for flying, and great progress has been made in the research and development of aircraft. [0003] Existing manned aircraft are generally large in size and expensive, which more and more restricts the widespread operation of the aircraft. On the other hand, as the control of the existing aircraft is mostly controlled by the joystick or the operating platform, the operation process is prone to errors, and the operation reaction time is long, which seriously affects the safe operation of the aircraft. Contents of the invention [0004] The purpose of the present invention is to provide a man-machine integrated simulated acoustic aircraft to solve the problems raised in the above-mentioned background technology. [0005] ...

AI Technical Summary

Problems solved by technology

[0003] Existing manned aircraft are generally large in size and expensive, which increasingly restricts the widespread operation of aircraft

On the other hand, as the existing aircraft control mostly adopts the control mode of joystick or operating platform, the operation process is prone to errors, and the operation reaction time is long, which seriously affects the safe operation of the aircraft.

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