CN206125426U - Wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing - Google Patents
Wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing Download PDFInfo
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- CN206125426U CN206125426U CN201620805975.6U CN201620805975U CN206125426U CN 206125426 U CN206125426 U CN 206125426U CN 201620805975 U CN201620805975 U CN 201620805975U CN 206125426 U CN206125426 U CN 206125426U
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Abstract
The utility model relates to an aircraft technical field especially relates to a wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing, has characteristics such as body a small amount of is light, convenient operation, safe and reliable. The wing that this flapping -wing aircraft was used includes bracket component and wing cabin, and the bracket component sets up in the inside in wing cabin to it makes a round trip to flutter from top to bottom to drive the wing cabin, the front and the back in wing cabin are equipped with inlet port and exhaust hole respectively, the diameter of inlet port is greater than the diameter in the hole of exhausting, when making a round trip to flutter from top to bottom in the wing cabin, has the pressure differential between the air convection that the front in wing cabin and the inside and outside air at the back formed respectively, thereby provide sufficient lifting force for this wing, when the wing of controing this manpower flapping -wing aircraft as the user in original place or run -up is fluttered from top to bottom, the pressure differential lifting force that produces and the lifting force that the resistance difference produced that are become manifold by the air combine together, it goes up to the air to make this manpower flapping -wing aircraft can utilize sufficient lifting force to drive the user, thereby realize the flight of manpower flapping wing formula.
Description
Technical field
This utility model is related to vehicle technology field, more particularly to a kind of flapping-wing aircraft wing and with the wing
Manpower ornithopter.
Background technology
All the time, people thirst for have as bird and wing are freely circled in the air, and then various aircraft should
Transport and give birth to.Wherein fixed wing airplane, gyroplane are obtained successfully already, and are applied in the life of people.However, flapping flight
It is considered as flying method in hgher efficiency, and nearly all flying creature all seems also to print using flapping wings type flight in the Nature
This point is demonstrate,proved.But, people have studied so flapping-wing aircraft for many years, but never real to realize.
Flapping-wing aircraft refers to the airborne vehicle for overweighting air that wing can be fluttered as bird and insect wing up and down, also known as flutter
Machine.The wing fluttered not only produces lift, also produces motive force forward.At present, existing flapping-wing aircraft is enough in order to ensure
Lifting force, generally too busy to get away mechanokinetic auxiliary；The flight of extremely indivedual pure man powers, though there has also been take off, can again because of machine
Wing super large is heavy, adds the human body physical agility limit, also can't bear the heavy load eventually.
Utility model content
(1) technical problem to be solved
The technical problems to be solved in the utility model there is provided a kind of wing of flapping-wing aircraft and the people with the wing
Power flapping-wing aircraft, body are light, easy to operate, safe and reliable in a small amount, can provide sufficiently large motive force for the lift-off of flapping-wing aircraft, make flapping wing
Machine realizes that flapping wings type flies.
(2) technical scheme
In order to solve above-mentioned technical problem, this utility model provides a kind of wing of flapping-wing aircraft, including carriage assembly
With wing cabin, the carriage assembly is arranged at the inside in wing cabin, to drive the wing cabin to flutter back and forth up and down；The wing
The front and back in cabin is respectively equipped with air inlet and steam vent, the diameter with diameter greater than steam vent of the air inlet.
Further, also including multiple ducted fans, multiple ducted fans are fixed on carriage assembly, and run through institute
State at least one side in the front and back in wing cabin；Connected by carriage assembly between each described ducted fan.
Further, length direction and short transverse of multiple ducted fans along wing cabin is linearly uniformly distributed.
Further, the air outlet of each ducted fan to wing cabin on be uniformly provided with multiple air intakes respectively
Hole.
Further, the ducted fan includes fan shaft and connecting line, and the fan shaft is provided with back power apparatus, described
Connecting line is connected with fan shaft, to pull the fan shaft to rotate which.
Further, also including multiple buoyancy bags, multiple buoyancy bags are individually fixed on carriage assembly.
Further, the carriage assembly includes supporting mobile jib, cabin frame and manipulates clue, and the support mobile jib is used for band
Motivation wing tank is fluttered up and down back and forth, and the cabin is put up truss structure and is laid in around support mobile jib；The manipulation clue is led to
Cross zipper ring to fix along the length direction for supporting mobile jib.
Further, the carriage assembly also includes supporting one end of secondary bar, the support mobile jib and support secondary bar to fix
Connection, the other end sequentially pass through multiple elastic spring connections.
Further, the material of the wing is lightweight structural material, and the lightweight structural material includes plastics, timber or gold
One or more combination in category.
This utility model additionally provides a kind of Manpower ornithopter, including symmetrically arranged two flapping-wing aircrafts as above are used
Wing, removably connected by brace bag between two wings.
(3) beneficial effect
Above-mentioned technical proposal of the present utility model has the advantages that：The wing bag of flapping-wing aircraft of the present utility model
Carriage assembly and wing cabin are included, carriage assembly is arranged at the inside in wing cabin, to drive wing cabin to flutter back and forth up and down；Wing cabin
Front and back be respectively equipped with air inlet and steam vent, the diameter with diameter greater than steam vent of air inlet.The flapping-wing aircraft
The features such as wing and the Manpower ornithopter with the wing have body light, easy to operate, safe and reliable in a small amount, it is upper and lower in wing cabin
When fluttering back and forth, there is between the cross-ventilation that the inner air and outer air of the front and back in wing cabin is formed respectively pressure differential, so as to
Enough lifting forces are provided for the wing, when user manipulates in situ or in run-up the wing of the Manpower ornithopter and flutters up and down
When, the lifting force that the lifting force produced by the pressure differential that cross-ventilation is formed is produced with resistance difference combines so that the manpower is flutterred
Wing function drives user lift-off using enough lifting forces, so as to realize that manpower flapping wings type flies；Also, the wing and brace
Between bag, and each component of wing between be detachable connection, therefore can in order to quick assembly and disassembly, in order to
Carry and transport；Additionally, the manufacturing cost of the wing of the flapping-wing aircraft and the Manpower ornithopter with the wing is relatively low, it is economical real
Favour, it is adaptable to different crowd, is a kind of flight chess that can be used as trip instrument or movement entertainment, and which has wide application
Prospect.
Description of the drawings
Positive structural representations of the Fig. 1 for the artificial flapping-wing aircraft of this utility model embodiment；
Structural representations of the Fig. 2 for the back side of the artificial flapping-wing aircraft of this utility model embodiment；
Positive structural representations of the Fig. 3 for the wing of the flapping-wing aircraft of this utility model embodiment；
Structural representations of the Fig. 4 for the back side of the wing of the flapping-wing aircraft of this utility model embodiment；
Structural representations of the Fig. 5 for the ducted fan of this utility model embodiment；
Structural representations of the Fig. 6 for the frame structure of this utility model embodiment；
Partition schematic diagrams of the Fig. 7 for the support mobile jib of this utility model embodiment；
Assembling schematic diagrams of the Fig. 8 for the support mobile jib of this utility model embodiment；
A kind of assembling schematic diagrams of the Fig. 9 for the support secondary bar of this utility model embodiment；
Another kind of assembling schematic diagrams of the Figure 10 for the support secondary bar of this utility model embodiment；
Scheme of installations of the Figure 11 for the fixing lock of this utility model embodiment.
Wherein, 1, wing cabin；2nd, cabin frame；3rd, support mobile jib；4th, ducted fan；5th, brace bag；6th, buoyancy bag；7th, manipulate
Clue；8th, arm retainer ring；9th, connecting line；10th, body anchor band；11st, support secondary bar；12nd, elastic spring；13rd, kayser；14、
Drag-line ring；15th, gim peg；16th, air inlet；17th, ornament；18th, transfer port；19th, tape retainer ring；20th, tape；21st, cabling
Pipe；22nd, fresh air inlet；23rd, wiring holes；24th, power apparatus are returned；25th, steam vent；26th, fixing lock；27th, screw hole；28th, sealing gasket；
29th, fixed screw；30th, fixed edge；31st, installing port；32nd, it is fixedly connected control device；33rd, retainer ring band；34th, fixed annular distance；
35 buoyancy bag Zhan Xi areas；36th, thread head；37th, screwed hole.
Specific embodiment
With reference to the accompanying drawings and examples embodiment of the present utility model is described in further detail.Following examples
For illustrating this utility model, but can not be used for limiting scope of the present utility model.
In description of the present utility model, unless otherwise stated, " multiple " are meant that two or more.Term
" on ", D score, "left", "right", " interior ", " outward ", " front end ", " rear end ", " head ", the orientation of the instruction such as " afterbody " or position close
System is, based on orientation shown in the drawings or position relationship, to be for only for ease of description this utility model and simplify description, rather than
The device or element for indicating or implying indication must have specific orientation, with specific azimuth configuration and operation, therefore can not
It is interpreted as to restriction of the present utility model.
Each component of the wing of the flapping-wing aircraft described in the present embodiment and artificial flapping-wing aircraft is demountable structure, so as to
In dismounting and transport, the wing can be pulled down after folding from artificial flapping-wing aircraft during transport, be put into transport in family-sized car.
As shown in figure 1, the wing of the flapping-wing aircraft includes carriage assembly and wing cabin 1, carriage assembly is arranged at wing cabin 1
Inside, to drive wing cabin to be fluttered about 1 back and forth, in the present embodiment, when dressing the Manpower ornithopter with user, user
Towards direction be front, then wing and user front in the same direction for wing cabin 1, is reversed the back side in wing cabin 1；Wing cabin
1 front and back is respectively equipped with air inlet 16 and steam vent 25, the diameter with diameter greater than steam vent 25 of air inlet 16, in machine
When wing tank is fluttered about 1 back and forth, there is between the cross-ventilation that the inner air and outer air of the front and back in wing cabin 1 is formed respectively pressure
Power is poor, so as to provide enough lifting forces for the wing, when user manipulates in situ or in run-up the wing of the Manpower ornithopter
When wing is fluttered up and down, the lifting force that the lifting force produced by the pressure differential that cross-ventilation is formed is produced with resistance difference combines, and makes
Obtaining the Manpower ornithopter can utilize enough lifting forces to drive user lift-off, so as to realize that manpower flapping wings type flies.
In order to ensure have suitable space to produce cross-ventilation, the front and back in preferred wing cabin 1 inside wing cabin 1
The distance between be 10～20cm, more preferably 12cm.The wing cabin 1 of the present embodiment for inverted trapezoidal, the length of side thereon
More than the lower length of side, all parts being beneficial on wing cabin 1 arrange simultaneously the effectively front and back of enlarger wing tank 1 and air
Contact area；In addition to trapezoidal, wing cabin 1 can also be other shapes, as long as meet being close to wing shape, can reduce sky
Atmidometer.In order to attractive in appearance, with wing cabin 1 near the side of user body as inner side, otherwise be outside, in wing cabin 1
Outboard end and wing cabin 1 be respectively arranged below with ornament 17 so that the wing generally triangle Vespertilio shape, it is also possible to set
Other profiles are calculated as, the configuration design should also be as reducing based on air drag.It is preferred that the greatest length in the wing cabin 1 and maximum
The ratio of height is 6:5～9:5, in the present embodiment, the greatest length in the wing cabin 1 is preferably 1.2～1.8m, more preferably
1.5m；The maximum height in the wing cabin 1 is 1.0m～1.4m, more preferably 1.1m.
In the present embodiment, the front in wing cabin 1 is uniformly distributed with multiple air inlets 16, and the back side is uniformly distributed with multiple
Steam vent 25, the diameter of air inlet 16 are preferably 5～20mm, and the diameter of steam vent 25 is preferably 2～8mm, should meet wing cabin 1
Air inlet 16 the diameter with diameter greater than steam vent 25 so that into wing cabin 1 air than discharge air it is many, in machine
The formation resistance difference up and down of wing tank 1, and due to air inlet 16 it is different with the diameter of steam vent 25, when by being fixed on support mobile jib
When manipulation clue 7 on 3 pulls carriage assembly, wing cabin 1 can be fluttered up and down back and forth by manpower control, can cause when fluttering
There is pressure differential, so as to carry for the wing between the cross-ventilation that the inner air and outer air of the front and back in wing cabin 1 is formed respectively
For enough lifting forces, the lifting force produced with the resistance difference that wing cabin is formed about 1 is combined, and can cause Manpower ornithopter
It is more easy to lift-off.
As shown in Fig. 2 in order to ensure the Manpower ornithopter with the wing is obtained in that the bigger lifting needed for lift-off
Power, the preferably wing also include multiple ducted fans 4, and multiple ducted fans 4 are fixed on carriage assembly, and run through wing cabin 1
Front and back at least one side, i other words, multiple ducted fans 4 can be installed on the front in wing cabin 1, it is also possible to pacify
The back side loaded on wing cabin 1, or the front and back in wing cabin 1 is mounted on multiple ducted fans 4, using ducted fan
4 fast turn-around can form propulsive thrust, make wing cabin 1 obtain more lifting forces.
As shown in Figure 3 and Figure 4, connected by carriage assembly between each ducted fan 4, preferably multiple ducted fans 4
Length direction and short transverse along wing cabin 1 is linearly uniformly distributed, to ensure that the wing rises the balance and reliability of space-time
Property, in the present embodiment, is from top to bottom laid with two row's ducted fans 4 on carriage assembly, by having three ducts in upper several first rows
Fan 4, second row have two ducted fans 4, and two row's ducted fans 4 linearly uniformly divide with vertical direction respectively in the horizontal direction
Cloth；The air outlet of each ducted fan 4 to wing cabin 1 on be uniformly provided with multiple fresh air inlets 22 respectively so that fan
Two sides is respectively formed cross-ventilation, as the upper and lower blast of ducted fan 4 is different, causes the front and back shape of ducted fan 4
Into cross-ventilation formed pressure differential, when wing cabin 1 is fluttered forward, ducted fan 4 rotate to wing cabin 1 produce propulsive thrust,
Which is helped to go up to the air, when wing cabin 1 is fluttered backward, which forward rotates to die down and even stop ducted fan 4 due to inertia, but wing
Fluttering forward next time for cabin 1 is arrived quickly, so as to promote ducted fan 4 constantly to produce propulsive thrust.
As shown in figure 5, ducted fan 4 includes fan shaft and connecting line 9, fan shaft is provided with back power apparatus 24, connecting line 9
It is connected with fan shaft, to pull fan shaft to rotate which, one end of preferred connecting line 9 is connected with fan shaft, and the other end is fixed on
In the manipulation clue 7 of carriage assembly, user, can also be while logical when being fluttered about 1 by manipulation 7 control machine wing tank of clue
Cross pulling connecting line 9 and multiple ducted fans 4 are made while rotating, so as to the pressure differential generation by 1 front and back of wing cabin
Lifting force is rotated the propulsive thrust for producing and is combined with ducted fan 4 so that the Manpower ornithopter has more sufficient lifting
Power.It is preferred that ducted fan 4 is cone so that ducted fan 4 can form bigger propulsive thrust in rotation, and its maximum outside diameter is excellent
Choosing is less than 25cm, highly less than 18cm.
Further, it is also possible to increase by one group of Luo rotating plasma blade at the back side in wing cabin 1, propeller blade is connected with connecting line 9,
Propeller blade can be pulled when pulling connecting line 9 to rotate, so as to further lift the climbing power of flapping-wing aircraft.
In order to further increase the lift-off lifting force of the Manpower ornithopter, the preferably wing also includes multiple buoyancy bags 6, many
Individual buoyancy bag 6 is individually fixed on carriage assembly so that when fluttering back and forth up and down, its front and back can be produced in wing cabin 1
Buoyancy difference, is that the lift-off of artificial flapping-wing aircraft fills into more climbing powers so as to be easier to lift-off；Further preferred multiple buoyancy bags
6 are separately fixed between any two ducted fan 4.Filled with sufficient light gas, such as hydrogen in each buoyancy bag 6
Deng can be stained with the front and/or the back side for tie up to wing cabin 1 with its buoyancy of further service hoisting, the size of buoyancy bag 6, rule
Lattice and installation site be not affecting air inlet 16 and steam vent 25 on wing cabin 1, and operate with hindering miscellaneous equipment
It is advisable, the quantity for being stained with the buoyancy bag 6 for being is usually each wing and is provided with 3～5, it is also possible to do not install buoyancy bag 6, buoyancy bag additional
6 more a lot of leap easily.Buoyancy bag 6 is provided with 6 transfer port 1818 of buoyancy bag, to install light gas additional.
As shown in Fig. 6, Fig. 7 and Fig. 8, in order to ensure the action of fluttering of wing it is smooth, and can be wing cabin 1 in liter space-time
Reliable supporting role is provided, preferred carriage assembly includes supporting mobile jib 3 and cabin frame 2, support mobile jib 3 to be used to drive wing cabin
About 1 flutters back and forth, and 2 one-tenth truss structures of cabin frame are laid in around support mobile jib 3；Support being respectively arranged at two ends with for mobile jib 3
Zipper ring 14, manipulates clue 7 for fixed, and user can control the amplitude of fluttering of wing by pulling manipulation clue 7, when
When two wings are combined, as the structure of two wings is to be symmetrical arranged, particularly on the carriage assembly of two wings
The position of fixed ducted fan 4 and quantity are symmetrical arranged, and pass through between two ducted fans 4 in preferred symmetric position
Connecting line 9 connects, and further preferably between two wings is provided with away spool 21 by wiring holes 23, and connecting line 9 is arranged at away
In spool 21, the two ends of connecting line 9 connect the ducted fan 4 of correspondence position on two wings respectively.Therefore, user is by behaviour
Ordinate rope 7 can pull connecting line 9 simultaneously so that user both can pull simultaneously two wings do same frequency up and down back and forth
Flutter, it is also possible to while the distance between two ducted fans 4 changed in the symmetric position of two wings are poor, make two symmetrically
The fan of position is opposed respectively to rotation, promotes wing to go up to the air upwards so as to form propulsive thrust respectively, its operation principle and birds
The principle that wing is agitated during flight is similar to.It is preferred that the connecting line 9 for manipulating clue 7 with ducted fan 4 is seizing wire, to ensure
Its solid reliability.
In the present embodiment, screw hole 27 is provided with and fixed along 30 at the middle part of ducted fan 4 and bottom outer, this is solid
It is fixed that sealing gasket 28 is fixed with by fixed screw 29 along 30, and utilize fixed screw 29 and the locking of screw hole 27 to coordinate so that containing
It is tightly connected between the edge and wing cabin 1 of road fan 4.Be provided with the wing cabin 1 relative with the bottom of ducted fan 4 into
Air holes 22 and the screw hole 27 for fixing with cabin frame 2, to ensure that the thrust of ducted fan 4 is played and safe operation.Except
Outside from the ducted fan 4 of the present embodiment, it is possible to use turbocharging fan or other class fans, as long as by pulling with strong
Strength ground propulsive thrust and lightweight fan can be used as preferred.Additionally, the wing of the present embodiment is applied with mechanical force source or
Power supply is also applicable on the flapping-wing aircraft of power, it is only necessary to be connected the rotating shaft of ducted fan 4 with mechanical force source or power supply.
As shown in figure 9, the carriage assembly of the present embodiment also includes supporting secondary bar 11, support mobile jib 3 and support secondary bar 11
One end is fixedly connected, and the other end sequentially passes through multiple elastic springs 12 and connects, and user supports secondary bar 11 to drive support by pulling
Mobile jib is fluttered about 3 back and forth, can effectively save manpower.The end of the support mobile jib 3 of the present embodiment is provided with screwed hole 37, can be with
Support mobile jib 3 on another wing is threadedly coupled, the spiral shell respectively with connecting rod of screwed hole 37 of the support mobile jib 3 of two wings
The locking connection of stricture of vagina head 36, the weight that mobile jib 3 is capable of shared both sides wing cabin 1 that supports of two after combination wing make which
Balance, and it is bent downwardly wing cabin 1 by user is slightly pulled, the flexibility of two support mobile jibs 3 when user is pulled
Parallel lines should be not less than lower 45 °.In the present embodiment, the length after preferably two wing combinations should be less than the wing of two wings
The total length of cabin 1 and the width sum of human body, two after the combination of the present embodiment support mobile jib 3 and connecting rod is 3.4m, its
In, it is 1.4 meters that each supports the length of mobile jib 3, and connecting rod is 0.6m, on mobile jib 3 is supported is provided with multiple along its length
Arm retainer ring 8, each arm retainer ring 8 are vertically arranged with mobile jib 3 is supported, and the arm in order to user is extended there through,
The body anchor band 10 for regular user's body is fixed with connecting rod.
Support mobile jib 3 be the stiff rod without flexibility, be connected use with elastic spring 12 with secondary bar 11 is supported, so pass through
Manipulate clue 7 to pull support secondary bar 11 and drive and support mobile jib 3 effectively save artificial force.Using support mobile jib 3 or hard
The support secondary bar 11 of matter can also increase the degree of facing upward of pole, more effectively to ensure quickly taking off for artificial flapping-wing aircraft.Above-mentioned is upper
Typically not greater than 45 degree of degree of facing upward, it is to avoid the performance for affecting wing cabin 1, ducted fan 4 to act on buoyancy bag 6.Increase degree of facing upward to exist
Can directly formulate during bar processed, also mobile jib 3 can supported control device 32 to be fixedly connected by what human body end position increase had a degree of facing upward, such as
Shown in Figure 10, this is fixedly connected retaining collar of the control device 32 similar to opening upwards, and therefore not to repeat here.Support mobile jib 3,
The two ends for supporting secondary bar 11 and manipulating a part or several parts in clue 7 are equipped with drag-line ring, solid by zipper ring 14
Surely clue 7 is manipulated, and both sides wing cabin 1 is manipulated in order to by the pulling to manipulating clue 7 and is completed fluttering for wing.
As shown in fig. 6, cabin frame 2 and the frame structure for supporting the composition of mobile jib 3 can be that wing cabin 1 and ducted fan 4 are provided
Reliable support supports, and the frame structure that this combines increases with the quantity of the ducted fan 4 installed and increases.In the support body
In structure, any one cross junction may be incorporated for fixedly mounting a ducted fan 4, and each ducted fan 4
Preferably made by the cross connecting plate to reinforce support, the structure of the connecting plate is circular or deltiod.Cabin frame 2 is each
Individual cross junction is provided with screw hole 27, with make itself reinforce, and the frame structure respectively with wing cabin 1 and duct
Reinforce between fan 4 and use, glue may also be employed, is stained with and the mode such as connects and bundle and reinforce.
The edge of cabin frame 2 inner (near user) is provided with gim peg 15, using as with brace bag 5 and tape 20
Be connected use.Retainer ring band 33 is additionally provided with cabin frame 2, can be used to connect arm retainer ring 8, and can be with manipulation clue
7 replace use, to realize multi-functional operation.
As shown in Fig. 3, Fig. 4 and Fig. 6, in order to ensure reliable installation of the ducted fan 4 on carriage assembly, preferably in wing
At least one side in cabin 1 is provided with installing port 31, it is preferable that wing cabin 1 is equal with the junction of cabin frame 2 and ducted fan 4 respectively
Screw hole 27 is provided with, and wing cabin 1 is respectively between cabin frame 2 and ducted fan 4 by fixed along 30, sealing gasket 28 and fixed
One or more combination airtight connection in screw 29, provides good be tightly connected for the place of being tightly connected using screw hole 27
Power.Airtight connection between wing cabin 1, cabin frame 2 and ducted fan 4 may also be employed glue or be stained with that the mode such as to connect in addition closed.
The front and back in wing cabin 1 is provided with fixed annular distance 34 simultaneously, extends there through and fixes with arm in order to retainer ring band 33
Ring 8 connects, and the front and back in wing cabin 1 further respectively has multiple buoyancy bag Zhan Xi areas 35, so that buoyancy bag 6 is stained with the machine of tying up to
On the outer surface of wing tank 1.
As shown in figure 11, for the ease of assembling the wing, preferred wing cabin 1 for can opening-closing structure, in the front in wing cabin 1
Multiple fixing locks 26 are respectively equipped with the junction at the back side, so as to lock between the front and back in wing cabin 1 closed.
It should be noted that ducted fan 4 can not be installed additional when wing cabin 1 can undertake and fast take off, when wing cabin 1 and culvert
Road fan 4 can undertake；Can undertake when both sides wing cabin 1 respectively installs a ducted fan 4 additional
Second ducted fan 4 can not be installed when fast taking off additional, quick rising can be undertaken when both sides wing cabin 1 respectively installs a buoyancy bag 6 additional
Second buoyancy bag 6 can not be installed when winged additional, because the body weight of people is not quite similar, typically both sides wing cabin 1 respectively installs five culverts additional
Road fan 4, does not install buoyancy bag 6 additional and is advisable.
In the present embodiment, preferably the material of the wing be lightweight structural material, lightweight structural material include plastics, timber or
In one or more combination in metal, such as the present embodiment, the material in wing cabin 1 can adopt PV force-bearing plates, its thickness to be less than
2mm, supports mobile jib 3 combine using high-toughness glass fibre or carbon material or both；Fixed screw 29 and gim peg 15 can
Using plastic material.The gross weight maximum of the Manpower ornithopter for assembling is advisable less than 20kg, usually 8～15kg.
The Manpower ornithopter that the present embodiment is provided includes the wing of symmetrically arranged two flapping-wing aircrafts as above, two
Connect by brace bag 5 is dismountable between individual wing.Load carrier of the brace bag 5 for the Manpower ornithopter, with cabin frame 2
Gim peg 15 connects, and is demountable structure, similar to common brace bag 5, so here is not excessively repeated.Except adopting
Brace bag 5 is fixedly connected outside two wings, body anchor band 10 may also be employed and makees simple connection load-bearing with kayser 13, or without mistake
Cross and directly be directly connected to carry out load-bearing by the support mobile jib 3 of two wings.Foot is respectively equipped with the bottom in the wing cabin 1 of two wings
Band retainer ring 19 or tape 20, so that the lower limb of user are easy to place in flight, so as to reduce air drag during flight,
Beneficial to efficiently flight.The similar car belt of the principle of the tape retainer ring 19 or tape 20, so here is not excessively repeated.
It is pointed out that the restriction of the profile of above-mentioned man power flapping-wing aircraft, material, specification is simply preferred square
Formula, here, not being limited.
In sum, the wing of the flapping-wing aircraft of the present embodiment includes carriage assembly and wing cabin 1, and carriage assembly is arranged at
The inside in wing cabin 1, to drive wing cabin to be fluttered about 1 back and forth；The front and back in wing cabin 1 is respectively equipped with 16 He of air inlet
Steam vent 25, the diameter with diameter greater than steam vent 25 of air inlet 16.The wing of the flapping-wing aircraft and the manpower with the wing
The features such as flapping-wing aircraft has body light, easy to operate, safe and reliable in a small amount, when wing cabin is fluttered about 1 back and forth, wing cabin 1
There is pressure differential, so that enough carrying is provided for the wing between the cross-ventilation that the inner air and outer air of front and back is formed respectively
Lift, when user is in situ or when manipulating the wing of the Manpower ornithopter and fluttering up and down in run-up, is formed by cross-ventilation
The lifting force that the lifting force that pressure differential is produced is produced with resistance difference combines so that the Manpower ornithopter can utilize enough liftings
Power drives user lift-off, so as to realize that manpower flapping wings type flies；Also, between the wing and brace bag 5, and wing is each
Detachable connection is between component, therefore can be in order to quick assembly and disassembly, in order to carrying and transporting；Additionally, should
The manufacturing cost of the wing of flapping-wing aircraft and the Manpower ornithopter with the wing is relatively low, economical and practical, it is adaptable to different crowd,
It is a kind of flight chess that can be used as trip instrument or movement entertainment, which has broad application prospects.
Embodiment of the present utility model in order to example and description for the sake of and be given, and be not exhaustively or will
This utility model is limited to disclosed form.Many modifications and variations are aobvious and easy for the ordinary skill in the art
See.It is, in order to more preferably illustrate principle of the present utility model and practical application, and to make this area to select and describe embodiment
Those of ordinary skill is it will be appreciated that this utility model is so as to designing the various embodiments with various modifications for being suitable to special-purpose.
Claims (10)
1. a kind of wing of flapping-wing aircraft, it is characterised in that including carriage assembly and wing cabin, the carriage assembly is arranged at machine
The inside of wing tank, to drive the wing cabin to flutter back and forth up and down by supporting mobile jib；The front and back in the wing cabin point
Air inlet and steam vent, the diameter with diameter greater than steam vent of the air inlet are not provided with.
2. wing according to claim 1, it is characterised in that also including multiple ducted fans, multiple ducted fans
It is fixed on carriage assembly, and at least one side in the front and back in the wing cabin；Each described ducted fan it
Between by carriage assembly connect.
3. wing according to claim 2, it is characterised in that multiple ducted fans along wing cabin length direction and
Short transverse is linearly uniformly distributed.
4. wing according to claim 2, it is characterised in that the air outlet of each ducted fan to wing cabin
It is upper to be uniformly provided with multiple fresh air inlets respectively.
5. wing according to claim 2, it is characterised in that the ducted fan includes fan shaft and connecting line, described
Fan shaft is provided with back power apparatus, and the connecting line is connected with fan shaft, to pull the fan shaft to rotate which.
6. wing according to claim 1, it is characterised in that also including multiple buoyancy bags, multiple buoyancy bags difference
It is fixed on carriage assembly.
7. wing according to claim 1, it is characterised in that the carriage assembly includes cabin frame and manipulates clue, institute
State cabin put up truss structure be laid in support mobile jib around；It is described to manipulate clue by zipper ring along the length for supporting mobile jib
Direction is fixed.
8. wing according to claim 7, it is characterised in that the carriage assembly also includes supporting secondary bar, the support
Mobile jib is fixedly connected with the one end for supporting secondary bar, and the other end sequentially passes through multiple elastic spring connections.
9. the wing according to any one of claim 1-8, it is characterised in that the material of the wing is lightweight construction material
Material, the lightweight structural material include the one or more combination in plastics, timber or metal.
10. a kind of Manpower ornithopter, it is characterised in that including symmetrically arranged two as any one of claim 1-9
Flapping-wing aircraft wing, removably connected by brace bag between two wings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620805975.6U CN206125426U (en) | 2016-07-27 | 2016-07-27 | Wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620805975.6U CN206125426U (en) | 2016-07-27 | 2016-07-27 | Wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206125426U true CN206125426U (en) | 2017-04-26 |
Family
ID=58563986
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620805975.6U Expired - Fee Related CN206125426U (en) | 2016-07-27 | 2016-07-27 | Wing that flapping -wing aircraft was used and have manpower flapping -wing aircraft of this wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206125426U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148143A (en) * | 2021-04-28 | 2021-07-23 | 中国矿业大学 | Flapping-wing robot with adjustable wingspan area |
| CN113212748A (en) * | 2021-04-28 | 2021-08-06 | 中国矿业大学 | Flapping-wing robot with adjustable breathing window wings |
| CN116674747A (en) * | 2023-08-03 | 2023-09-01 | 西南石油大学 | Flexible flapping wing and ducted propeller hybrid-driven simulated baton floating aircraft |
-
2016
- 2016-07-27 CN CN201620805975.6U patent/CN206125426U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148143A (en) * | 2021-04-28 | 2021-07-23 | 中国矿业大学 | Flapping-wing robot with adjustable wingspan area |
| CN113212748A (en) * | 2021-04-28 | 2021-08-06 | 中国矿业大学 | Flapping-wing robot with adjustable breathing window wings |
| CN113212748B (en) * | 2021-04-28 | 2022-12-02 | 中国矿业大学 | Flapping-wing robot with adjustable breathing window wings |
| CN113148143B (en) * | 2021-04-28 | 2022-12-30 | 中国矿业大学 | Flapping-wing robot with adjustable wingspan area |
| CN116674747A (en) * | 2023-08-03 | 2023-09-01 | 西南石油大学 | Flexible flapping wing and ducted propeller hybrid-driven simulated baton floating aircraft |
| CN116674747B (en) * | 2023-08-03 | 2023-10-20 | 西南石油大学 | Flexible flapping wing and ducted propeller hybrid-driven simulated baton floating aircraft |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170426 |