CN204937507U

CN204937507U - The flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula

Info

Publication number: CN204937507U
Application number: CN201520597800.6U
Authority: CN
Inventors: 吴锜; 吴开震; 吴若谷; 吴若鼎; 吴若尧
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-08-10
Filing date: 2015-08-10
Publication date: 2016-01-06
Anticipated expiration: 2025-08-10

Abstract

The utility model belongs to flapping-wing aircraft preparing technical field, be specifically related to the flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula, agent structure comprises left gear, left outside connecting rod, left engine, left wing, left inside connecting rod, main framing, plumage bar, accessory pinna, right gear, right outside connecting rod, support, right wing, right inside connecting rod, body, head, fuselage, tail, left pipe link and right pipe link, left outside connecting rod, left inside connecting rod, the main framing of left pipe link and left wing and right outside connecting rod, right inside connecting rod, the main framing of right pipe link and right wing is formed the two four-bar linkage structure of specular formula centered by the axis of body, power is swatted for left wing and right wing provide symmetrical, the resistance difference formed when swatting up and down based on birds wing is the principle providing raising force of flying, realize the fly mechanics of Bird Flight state, its structure is simple, scientific in principle, and cost of manufacture is low, and be easy to regulation and control, flight effect is good, has a extensive future.

Description

The flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula

Technical field:

The utility model belongs to flapping-wing aircraft preparing technical field, is specifically related to the flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula, utilizes the wing design of birds wing structure, realizes flight regulation and control effect.

Background technology:

For a long time, people dream of can as birds on high in circle in the air, a lot of people imitates the wing having made birds, attempts to fly up and, all do not have successfully, people are by having carried out long analytical investigation to the flight theory of birds, grasped the principle of some flights, find the appearance profile of birds wing, the upper surface of wing is arc, the air-flow flow through from above during flight is faster than the air-flow flow through from below, thus forms the power risen, for the principle of birds flapping flight, people find after having carried out long Exploration and Research that the appearance profile except wing provides except raising force in high-speed motion, the muscle of birds and this body structure of wing also very important to the Automatic adjusument of air-flow, accessory pinna on plumage is non-symmetrical relative to plumage bar, wing upper flutter with under flutter time, accessory pinna one one conjunction, make the wing of birds upper flutter with under flutter time, the resistance of air is different, air is just different to the antagonistic force of wing, the wing of birds is flutterred with under flutter time the resistance difference that formed be that birds can fly up and another major reason be elevated, this important idea has had not yet to see bibliographical information or application case.

According to physics knowledge, the formula of air resistance is: F=ASV ², A is effective resistance area, and S is a coefficient relevant with mobile shape, and V is kinematic velocity; On the wing of birds, plane is arc, lower plane is spill, when birds wing is flutterred, the little F of S is also little, under when flutterring the large F of S also large, when birds carry out swatting action, flutter under birds wing faster than on flutter, under flutter V and be greater than and flutter V, F when below flutterring is greater than F when flutterring, and the antagonistic force of air is also like this; In addition, the feather of birds wing is asymmetric relative to plumage bar, when making to flutter, feather can open, air can flow through between feather, and it is also little that the S of wing reduces F, under when flutterring feather close, air not by, it is also large that the S of wing increases F, and the antagonistic force of air is also large, thus provide the strength of rising for birds.

At present, be US7255305B2 according to U.S. Patent number, US7607610B1, US7215305B2, US6802473, US7600712, US4139171, US5899408, US7007889, US7963478, US6824094, be referred to respectively in the document of US7410121 and US7255305 plumage imparity and on flutter, under the folding of feather when flutterring, but all do not mention that this folding provides the concept of lift for birds, also the wing all not proposing birds in numerous documents and report is flutterred with under flutter the resistance difference of formation, the scheme not designing flapping-wing aircraft based on the concept of resistance difference is disclosed.Therefore, research and develop the flapping-wing aircraft device of the two four-bar linkage structure of a kind of specular formula, have very much science and using value, also there is good society and application prospect.

Summary of the invention:

The purpose of this utility model is the shortcoming overcoming prior art existence, seek the flapping-wing aircraft device designing the two four-bar linkage structure of a kind of specular formula, the resistance difference formed when swatting up and down by means of birds wing is the principle providing raising force of flying, and realizes the structure design that freely circles in the air of aircraft.

To achieve these goals, the agent structure of the flapping-wing aircraft device of the two four-bar linkage structure of the specular formula that relates to of the utility model comprises left gear, left outside connecting rod, left engine, left wing, left inside connecting rod, main framing, plumage bar, accessory pinna, right gear, right outside connecting rod, support, right wing, right inside connecting rod, body, head, fuselage, tail, left pipe link and right pipe link; The body of fish shape framed structure is made up of head, fuselage and tail integral type, head is pointed arcuate structure, fuselage is the plane tabular of non-uniform thickness, upper side is arcuation, downside is concavity, and tail adopts fish tail structure, the body of the downside of head is installed with left engine and the support of independent setting, left engine and left gear mechanical power are in transmission connection, and left gear is connected with left outside connecting rod and left inside connecting rod mechanical type; Right gear is fixedly connected with body by support, and right gear is connected with right outside connecting rod and right inside connecting rod mechanical type; Left gear and right gear are mutually meshing, and left gear promotes right gear and rotates, and the left wing of arcuate structure symmetrical expression and right wing are separately positioned on the left and right sides of fuselage about body axis symmetry; Left wing and right wing are connected by main framing, plumage bar and accessory pinna respectively and form; The right part of the main framing of left wing is provided with left pipe link, and left wing is connected with left outside connecting rod and left inside connecting rod mechanical type by left pipe link; The left part of the main framing of right wing is provided with right pipe link, and right wing is connected with right outside connecting rod and right inside connecting rod mechanical type by right pipe link.

Compared with prior art, the resistance difference formed when swatting up and down based on birds wing is the principle providing raising force of flying to the utility model, and research and development make a kind of flapping-wing aircraft device; Its structure is simple, scientific in principle, and cost of manufacture is low, and be easy to regulation and control, flight effect is good, has a extensive future.

Accompanying drawing illustrates:

Fig. 1 is agent structure principle schematic of the present utility model.

Fig. 2 is the agent structure principle schematic of the wing that the utility model relates to.

Detailed description of the invention:

Also by reference to the accompanying drawings the utility model is described further below by embodiment.

Embodiment:

The agent structure of the flapping-wing aircraft device of the two four-bar linkage structure of the specular formula that the present embodiment relates to comprises left gear 1, left outside connecting rod 2, left engine 3, left wing 4, left inside connecting rod 5, main framing 6, plumage bar 7, accessory pinna 8, right gear 9, right outside connecting rod 10, support 11, right wing 12, right inside connecting rod 13, body 14, head 15, fuselage 16, tail 17, left pipe link 18 and right pipe link 19; The body 14 of fish shape framed structure is made up of head 15, fuselage 16 and tail 17 integral type, head 15 is pointed arcuate structure, be beneficial to minimizing advance resistance, fuselage 16 is the plane tabular of non-uniform thickness, upper side is arcuation, downside is concavity, tail 17 adopts fish tail structure, be beneficial to adjustment heading, the body 14 of the downside of head 15 is installed with left engine 3 and the support 11 of independent setting, left engine 3 is in transmission connection with left gear 1 mechanical power, and left gear 1 is connected with left outside connecting rod 2 and left inside connecting rod 5 mechanical type; Right gear 9 is fixedly connected with body 14 by support 11, and right gear 9 is connected with right outside connecting rod 10 and right inside connecting rod 13 mechanical type; Left gear 1 is mutually meshing with right gear 9, and left gear 1 promotes right gear 9 and rotates, and the left wing 4 of arcuate structure symmetrical expression and right wing 12 are separately positioned on the left and right sides of fuselage 16 about body 14 axis symmetry; Left wing 4 and right wing 12 are connected by main framing 6, plumage bar 7 and accessory pinna 8 respectively and form; The right part of the main framing 6 of left wing 4 is provided with left pipe link 18, and left wing 4 is connected with left outside connecting rod 2 and left inside connecting rod 5 mechanical type by left pipe link 18; The left part of the main framing 6 of right wing 12 is provided with right pipe link 19, and right wing 12 is connected with right outside connecting rod 10 and right inside connecting rod 13 mechanical type by right pipe link 19; Each part fits forms the flapping-wing aircraft device of the two four-bar linkage structure of specular formula, realizes the fly mechanics of Bird Flight state.

The main framing 6 of the left outside connecting rod 2 that the present embodiment relates to, left inside connecting rod 5, left pipe link 18 and left wing 4 and the main framing 6 of right outside connecting rod 10, right inside connecting rod 13, right pipe link 19 and right wing 12 are formed the two four-bar linkage structure of specular formula centered by the axis of body 14, swat power for left wing 4 and right wing 12 provide symmetrical; Described left engine 3 is slowdown type engine, comprises combustion engine, electrical motor and powered by nuclear energy machine; The double dynamical export structure of left engine 3 or employing single power machine.

When the present embodiment uses, left engine 3 provides power for left gear 1 and drives left wing about 4 to swat by the main framing 6 of left outside connecting rod 2, left inside connecting rod 5, left pipe link 18 and left wing 4, left gear 1 promotes right gear 9 and rotates and provide power and drive swatting up and down of right wing 12 by the main framing 6 of right outside connecting rod 10, right inside connecting rod 13, right pipe link 19 and right wing 12, and mutually meshing left gear 1 and right gear 9 make left wing 4 and right wing 12 is synchronous swats up and down; Make left gear 1 controlled with the rotating speed of right gear 9 by the setting of left engine 3, thus realize the regulation and control of the speed of swatting up and down of left wing 4 and right wing 12, and make the speed of flutterring slow, under to flutter speed fast, for left wing 4 and right wing 12 provide asymmetric speed of fluttering up and down, produce different raising forces, realize lifting, turn to and adjust effect.

The resistance difference that the flight theory of the flapping-wing aircraft device of the specular formula that the present embodiment relates to two four-bar linkage structure is formed when being and fluttering based on left wing 4 and right wing about 12 provides lifting force for the flapping-wing aircraft device of the two four-bar linkage structure of specular formula, resistance when flutterring under resistance when left wing 4 and right wing 12 are flutterred is less than is little, the antagonistic force that resistance when flutterring is produced is greater than the antagonistic force that when flutterring, resistance produces, act on left wing 4 and right wing 12 power is upwards greater than downward power, produce raising force, formula due to air resistance is F=ASV ², A is effective resistance area, S is a coefficient relevant with the shape of drag area, if cross section is fleetline, S is just little, it is spill, S is just large, V is kinematic velocity, the upper plane of left wing 4 and right wing 12 is arcs, the lower plane of left wing 4 and right wing 12 is spills, when left wing 4 and right wing 12 are flutterred, the little F of S is also little, under when flutterring the large F of S also large, when left wing 4 and right wing 12 carry out swatting action, speed is swatted up and down by what arrange that left engine 3 converts that left gear 1 and the rotating speed of right gear 9 control left wing 4 and right wing 12, make down to flutter faster than on flutter, under flutter V and be greater than and flutter V, F when below flutterring is greater than F when flutterring, the antagonistic force of air is also like this, comprehensive application affects several factors of resistance when left wing 4 and right wing about 12 are fluttered, resistance when flutterring under raising, resistance when minimizing is flutterred, thus improve air antagonistic force upwards, for the flapping-wing aircraft device of the two four-bar linkage structure of specular formula provides maximum raising force, left wing 4 and right wing about 12 to be fluttered in process as fish tail swing for the flapping-wing aircraft device of the two four-bar linkage structure of specular formula provides ahead power, and realize direction controlling.

Claims

1. a flapping-wing aircraft device for the two four-bar linkage structure of specular formula, is characterized in that agent structure comprises left gear, left outside connecting rod, left engine, left wing, left inside connecting rod, main framing, plumage bar, accessory pinna, right gear, right outside connecting rod, support, right wing, right inside connecting rod, body, head, fuselage, tail, left pipe link and right pipe link; The body of fish shape framed structure is made up of head, fuselage and tail integral type, head is pointed arcuate structure, fuselage is the plane tabular of non-uniform thickness, upper side is arcuation, downside is concavity, and tail adopts fish tail structure, the body of the downside of head is installed with left engine and the support of independent setting, left engine and left gear mechanical power are in transmission connection, and left gear is connected with left outside connecting rod and left inside connecting rod mechanical type; Right gear is fixedly connected with body by support, and right gear is connected with right outside connecting rod and right inside connecting rod mechanical type; Left gear and right gear are mutually meshing, and left gear promotes right gear and rotates, and the left wing of arcuate structure symmetrical expression and right wing are separately positioned on the left and right sides of fuselage about body axis symmetry; Left wing and right wing are connected by main framing, plumage bar and accessory pinna respectively and form; The right part of the main framing of left wing is provided with left pipe link, and left wing is connected with left outside connecting rod and left inside connecting rod mechanical type by left pipe link; The left part of the main framing of right wing is provided with right pipe link, and right wing is connected with right outside connecting rod and right inside connecting rod mechanical type by right pipe link.