Single-person suspension flying pedal

A pedal and single-person technology, applied in the field of single-person suspension flight pedals, can solve the problems of casualties and achieve the effect of improving safety

Inactive Publication Date: 2018-11-23
杭州青杉奇勋科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the deficiencies of the prior art, the present invention provides a single-person suspension flight pedal, which solves the problem that the speed of the single-person suspension aircraft needs to be adjusted when the single-person suspension aircraft is in use, otherwise the sudden landing will inevitably cause casualties. , using the cooperation of the shoulder strap placer and the shoulder strap body, it achieves the fixation of the shoulders, which is equivalent to the effect of a seat belt, and greatly improves the safety of the aircraft

Method used

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Embodiment Construction

[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0024] Such as Figure 1-4 As shown, the present invention provides a technical solution: a single-person suspended flight pedal, including a suspended aircraft 1, the left and right sides of the front of the suspended aircraft 1 are fixedly connected with a shoulder belt placer 2, and the front of the shoulder belt placer 2 The upper part is fixedly connected with a shoulder belt body 12, the bottom of the shoulder belt placer 2 is fixedly connected with a fi...

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Abstract

The invention relates to the technical field of single-person suspension, and discloses a single-person suspension flying pedal, which comprises a suspension aircraft. The single-person suspension flying pedal solves the problem that when a single-person suspension aircraft is used, the speed of the single-person suspension aircraft needs to be regulated and controlled, for instance, when a testerfalls to the ground, only by controlling revolving speed, can the tester be guaranteed to fall to the ground stably, otherwise, casualties are inevitably caused if the tester falls to the ground suddenly. According to the technical scheme, a revolving speed adjustment panel is connected on the obverse side of a wind wheel revolving speed control panel, wherein the function of the revolving speedadjustment panel lies in controlling the magnitude of electric quantity, when the electric quantity is low, a revolving control motor is influenced by a motor, the revolving speed becomes low, otherwise, when the electric quantity is high, the revolving speed becomes high, wherein the revolving speed adjustment panel is divided into three gears, and a rotational stand column positioned and connected at the top of the revolving control motor rotates automatically to drive a propeller blade to rotate.

Description

technical field [0001] The invention relates to the technical field of single-person suspension, in particular to a single-person suspension flight pedal. Background technique [0002] With the invention and widespread use of the internal combustion engine, flight in the air has gradually become possible. In 1903, the Wright brothers of the United States took the lead in manufacturing an airplane capable of flying in the United States, and realized the dream of flying. Subsequently, aircraft and its related science and technology developed rapidly, but it was indeed a distant dream in China. With the development of the times, some people boldly proposed some methods and methods, but we have not seen any substantial progress. In 2011, Martin Corporation of the United States launched a high-profile single-person aerodynamic aircraft suitable for manning. [0003] When the single-person hovercraft is in use, it is necessary to control the speed of the single-person aircraft. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02
CPCB64C39/026
Inventor 王彬
Owner 杭州青杉奇勋科技有限公司
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