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Flapping wing mechanism with controllable pitch angle of left and right wings and manual flapping wing machine

A technology of flapping wing and pitch angle, which is applied in the field of aviation aircraft and aircraft mechanism, can solve the problems of ignoring mechanical analysis, etc., and achieve the effect of convenient operation, simple setting and lightening of leg load

Inactive Publication Date: 2019-04-19
成东明
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The superficial understanding refers to people’s understanding of the wings and body of birds, a pair of interdependent contradictory subjects such as lift and load, which superficially explains the basic movements of flapping wings. There are many ideas, but most of them ignore it. The most basic scientific method of mechanical analysis

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  • Flapping wing mechanism with controllable pitch angle of left and right wings and manual flapping wing machine
  • Flapping wing mechanism with controllable pitch angle of left and right wings and manual flapping wing machine

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Embodiment Construction

[0036] The present invention will be described in detail below in conjunction with the accompanying drawings and specific examples, so that those skilled in the art can understand the present invention. Before the description, it should be noted that the orientation or positional relationship of the "center", "upper", "lower", "left", "right", "horizontal" in the terminology is only based on the orientation of the orthopter itself in the figure and positional relationship; in addition, the terms "installation", "connection", "fixed connection", etc. should be understood in a broad sense, which can be fixed connection, detachable connection, or integrated connection; As far as people are concerned, as long as various changes are within the spirit and scope of the present invention defined and determined by the appended claims, these changes are obvious, and all inventions and creations using the concept of the present invention are included in the protection list.

[0037] A fl...

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Abstract

The invention relates to a flapping wing mechanism with controllable pitch angle of left and right wings and a manual flapping wing machine. The flapping wing machine comprises a left wing, a right wing, wing shaft assembly pipes, an upper cross beam of a machine frame, a bottom rod of the machine frame, left and right side rods of the machine frame, a manual pulling handle, a pitch angle handwheel, a pedal rod, a left wheel, a right wheel, a left suspension cable main cable, a right suspension cable main cable, a left suspension cable, a right suspension cable and other related settings. Theflapping wing mechanism further comprehensively applies the flapping wing pitch self-adjustment, machine body roll-over and machine body pitch control system. When a human body lifts and crouches, hands and feet exert force together, so that the wings automatically generate periodic motions of downward flapping at a depression angle and upward sliding at an elevation angle, and at the same time, complex motions of rolling, climbing and subduction can be superimposed, and thus completely controllable flight of the human flapping wing machine is realized. Compared with the prior art, the flapping wing mechanism has comprehensive application, has the characteristics of optimized structure, light weight, flexible operation and convenient take-off and landing, is suitable for outdoor competitive activities and the like, and has a certain development prospect.

Description

technical field [0001] The invention belongs to the field of aviation vehicles and aircraft mechanisms, and in particular relates to a flapping mechanism with controllable pitch and pitch angles of left and right wings and a human-powered flapping airplane. Background technique [0002] On the flapping wing aircraft, there are many successful reports and patents all over the world. But in the aspect of manpower flapping wing aircraft research, there is no relatively successful report at present. [0003] In terms of fixed-wing human-powered flight, according to Science Network (kexue.com), the world record for long-distance flight of a human-powered aircraft is 115.11 kilometers created by the Massachusetts Institute of Technology in 1988. The net weight of the world-record "Daedalus" 70 pounds (about 31 kilograms), the whole journey took 3 hours and 54 minutes, and the speed was 29.5 kilometers per hour. At present, this record has not been broken. [0004] According to n...

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 成东明
Owner 成东明
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