CN109850144A - A kind of solar energy flapping wing bionic Aircraft - Google Patents
A kind of solar energy flapping wing bionic Aircraft Download PDFInfo
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- CN109850144A CN109850144A CN201910302505.6A CN201910302505A CN109850144A CN 109850144 A CN109850144 A CN 109850144A CN 201910302505 A CN201910302505 A CN 201910302505A CN 109850144 A CN109850144 A CN 109850144A
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Abstract
A kind of solar energy flapping wing bionic Aircraft category vehicle technology field, the present invention in flapping wing aircraft flapping wing structure is driven using the connection of miniature DC motor and secondary gear reducer；Bionic flapping-wing solar energy film wing plate provides the space of laying flexible thin-film solar cell plate；Flapping wing aircraft empennage respectively drives crank rotation by two steering engines, drives connecting rod swing to realize the rotation of the upper and lower of empennage, left and right four direction.The present invention is able to achieve the energy saving, efficient, sustainable of flapping wing aircraft, birds wing, the structure of empennage and motion mode simultaneously, it is emerged from bionic flapping-wing sporting flying of the invention, has the advantages that structure novel, transmission mechanism are simple and reliable, the energy is reproducible.
Description
Technical field
The invention belongs to vehicle technology fields, and in particular to a kind of solar energy flapping wing bionic Aircraft.
Background technique
Flapping wing aircraft is to imitate the forms of motion of bird or insect swatter wing and design, it has VTOL, hovering, respectively
To functions such as movements.Its not only light weight, at low cost, it is often more important that structure is simplified and high-efficient.Therefore, flapping wing aircraft
All will be very vast in the application distant view of national defence and civil field, while it is in the case where executing small space or MODEL OVER COMPLEX TOPOGRAPHY
With the advantage that other aircraft are incomparable when task.
Solar energy is the generally existing and easy a kind of energy being easy to get in nature, while having clean and environmental protection, renewable
Etc. advantages.The important utilization form of one of solar energy is solar photo-voltaic power generation station, and main dependence solar battery group is series-parallel
Component is formed, electric energy is converted by the solar energy of absorption and is used.
There are mainly three types of the solar battery types for occupying mainstream at present, i.e. monocrystaline silicon solar cell, the polysilicon sun
It can battery and non-crystal silicon solar cell.In recent years, as second generation solar battery, the production of thin-film solar cells
It develops and application technology is quickly grown.Amorphous silicon thin-film solar cell in thin-film solar cells is even more to have raw material
The advantages such as materials are few, low energy consumption for manufacturing process, energy payback period is short, and amorphous silicon thin-film solar cell plate is at present
The very light scale of construction can be reached, emerging organic thin film solar cell and dye sensitization technology etc. keep production cost further
It reduces, product is provided with better flexibility, can be bonded the wing shapes of flapping wing aircraft well, if can flutter miniature
It is applied on rotor aircraft, will greatly promote its flying quality.
Summary of the invention
The purpose of the present invention is to provide a kind of structure novel, transmission mechanism is simple and reliable, the reproducible solar energy of the energy
Flapping wing bionic Aircraft.
The present invention is proposed a kind of bionical solar energy flapping wing aircraft by the inspiration of Bird Flight.This flapping wing aircraft
With novel driving-gear mechanism, structure novel, transmission mechanism are simple and reliable；And pass through wing plate and tail in flight
The biomimetic features of the wing obtain the enough lift of flight, meet the flight demand of minute vehicle.The minute vehicle also has simultaneously
The flapping wing of flexible solar film battery plate fitting, can be converted to electric energy using solar energy in minute vehicle flight,
Realize energy compensating, make to fly efficient, sustainable that there is weight for the mobility and cruising ability that improve flapping-wing modal
Want meaning.
The present invention is by solar energy film right wing plate A, driving-transmission device B, solar energy film left wing plate C and bionical empennage D
Composition, in which: the solar energy film right wing plate A and solar energy film left wing plate C is about the symmetrical of the central axes fuselage a-a
Structure；In solar energy film right wing plate A in the hole a a of right connecting rod 2 and driving-transmission device B gag lever post on a15 the hole i i and
The hole n n on rocker arm a12 is flexibly connected；The hole the b b of right connecting rod 2 is affixed to the hole the m m on a12 through bolt and rocker arm.
In solar energy film left wing plate C in the hole the a1 a1 of left connecting rod 3 and driving-transmission device B gag lever post to the i1 on b36
Hole i1 and rocker arm are flexibly connected the hole the n1 n1 on b35；The hole the b1 b1 of left connecting rod 3 is through bolt and rocker arm to the hole the m1 m1 on b35
It is affixed；Bionical empennage D is articulated with the rear end of fuselage 1.
Q slot q, r slot r, s slot s of bionical empennage D middle fuselage 1 is affixed through the hole o o and driving-transmission device B fixed frame 20.
Driving-transmission device B solar charging controller 32 and battery 33 and side frame 18 are affixed；Solar recharging
4 circuit connection of solar panel of controller 32 and solar energy film right wing plate A and solar energy film left wing plate C, battery
33 one end connect solar charging controller 32, and 33 other end of battery connects driving-transmission device B brushless motor 7.
The solar energy film right wing plate A and solar energy film left wing plate C is the symmetrical junction about the central axes fuselage a-a
Structure, structure is identical, contrary, is made of solar panel 4, wing plate 5, skeleton 6, and middle skeleton 6 is equipped with the hole p p；
Right connecting rod 2 is additionally provided on solar energy film right wing plate A, 2 left end of right connecting rod is equipped with the hole a a and hole b b；Solar energy film left wing plate C
On be additionally provided with left connecting rod 3,3 right end of left connecting rod is equipped with the hole the a1 a1 and hole b1 b1；The skeleton 6 of solar energy film left wing plate C is through the hole p p
Affixed with left connecting rod 3, wing plate 5 is supported by skeleton 6；Solar panel 4 is adhered to above wing plate 5；Solar energy film right wing plate A
Skeleton it is affixed through the hole p and right connecting rod 2, wing plate is by skeletal support；Solar panel is adhered to above wing plate.
The driving-transmission device B is by brushless motor 7, right rack 8, level-one pinion gear 9, level-one gear wheel 10, second level
Pinion gear a11, rocker arm are to a12, yoke a13, drive rod to a14, gag lever post to a15, second level gear wheel a16, bolt group a17, side
Rack 18, second level pinion gear b19, fixed frame 20, left frame 21, primary axis 22, second level axis 23, second level gear wheel b24, yoke b34,
Rocker arm forms b35, gag lever post to b36, drive rod b37 and bolt group b38, in which: right rack 8 is about machine with left frame 21
The symmetrical structure of the central axes body a-a；Right rack 8 is equipped with the hole the c hole c, d hole d, e hole e, f hole f, g g and the hole h h；On left frame 21
Equipped with the hole the c1 hole c1, d1 hole d1, e1 hole e1, f1 hole f1, g1 g1 and the hole h1 h1；Gag lever post is equipped with the hole i i to a15；Rocker arm pair
A12 is equipped with the hole the j hole j, k hole k, m m and hole n n；Gag lever post is equipped with the hole i1 i1 to b36；Rocker arm to b35 be equipped with the hole j1 j1,
The hole the k1 hole k1, m1 m1 and hole n1 n1；Fixed frame 20 is equipped with the hole o o；Right rack 8 and left frame 21 are arranged in parallel, and through side frame
18 is affixed；Brushless motor 7 is affixed through the hole the c hole c, d hole d, e hole e, f f and right 8 bolt of rack；Brushless motor 7 is through the hole the c1 hole c1, d1
The hole d1, e1 hole e1, f1 f1 and 21 bolt of left frame are affixed；Level-one pinion gear 9 is fixed in 7 output end of brushless motor；Primary axis 22
With 23 parallel arrangement of second level axis；From right-to-left successively affixed second level pinion gear a11, level-one gear wheel 10 and second level on primary axis 22
Pinion gear b19, and 22 both ends of primary axis are movably connected on the hole the g g of right rack 8 and the hole the g1 g1 of left frame 21；Second level axis 23
Second level gear wheel a16 and second level gear wheel b24 is fixedly mounted in upper front and back, and 23 both ends of second level axis are movably connected on right rack 8
The hole h h and left frame 21 the hole h1 h1 on；Level-one pinion gear 9 is engaged with level-one gear wheel 10；Second level pinion gear a11 and second level
Gear wheel a16 engagement；Second level pinion gear b19 is engaged with second level gear wheel b24.
Gag lever post is fixed in right 8 right side of rack to a15；A hole a of the rocker arm to the hole the n n on a12 through pin shaft and connecting rod 1, limit
Position bar is flexibly connected the hole the i i of a15；Rocker arm is affixed through bolt group a17 and the both ends yoke a13 to the hole the j hole j, k k on a12；Driving
Bar a14 and the second level gear wheel a16 flank of tooth are affixed；The long hole width of yoke a13 is greater than drive rod a14 diameter.
Gag lever post is fixed in 21 left side of left frame to b36；A1 hole of the rocker arm to the hole the n1 n1 on b35 through pin shaft Yu connecting rod 1
A1, gag lever post are flexibly connected the hole the i1 i1 of b36；Rocker arm is to the hole the j1 hole j1, k1 k1 on b35 through bolt group b38 and yoke b34 two
It holds affixed；Drive rod b37 and the second level gear wheel a16 flank of tooth are affixed；The long hole width of yoke b34 is greater than drive rod b37 diameter；It is fixed
20 bottom end of frame and side frame 18 are affixed.
The bionical empennage D by fuselage 1, retaining ring 25, steering engine 26, universal joint 27, tailplane 28, vertical tail 29,
Fixed plate 30 and hinged rope are formed to 31, in which: fuselage 3 is equipped with q slot q, r slot r, s slot s, t slot t and u slot u；1 rear end of fuselage
It is affixed with 27 front of universal joint；Universal joint 27 and 30 center of fixed plate are hinged.
Hingedly rope is made of to 31 the hinged rope in left and right two, and two rear ends hingedly restricted are respectively and at left and right sides of fixed plate 30
It is affixed；Two front ends hingedly restricted are affixed with 26 left and right sides of steering engine respectively.
Steering engine 26 is fixed on the t slot t and u slot u of fuselage 1 through retaining ring 25；Tailplane 28 and 29 front end of vertical tail are affixed
Behind fixed plate 30.
The principle of the present invention and the course of work are as follows:
In the present invention, brushless motor 7 drives level-one pinion gear 9 to rotate, and passes through level-one pinion gear 9 and level-one gear wheel 10
Engagement, the axle center fixed hinge of level-one gear wheel 10, second level pinion gear a11, second level pinion gear b19, second level pinion gear a11 and two
Grade gear wheel a16 engagement, second level pinion gear b19 is engaged with second level gear wheel b24, to drive second level gear wheel a16, second level big
Gear b24 is rotated with identical revolving speed, and the rotation of second level gear wheel a16, second level gear wheel b24 drive the driving on respective gear
Bar a14 and drive rod b37 is rotated around gear centre, while drive rod a14 is slided in the long hole of yoke a13, to drive yoke
A13, which is realized, to move up and down, therefore realizes that rocker arm respectively surrounds rocker arm to a12 to a12 and gag lever post to the hinged center rotating of a15,
It is final that right connecting rod 2 is driven to flutter with solar energy film right wing plate A, left connecting rod 3 and solar energy film left wing plate C or more.
Flapping wing wing plate of the invention is by wing plate 5, solar panel 4, brushless motor 7, solar charging controller 32
It is formed with battery 33；The several piece amorphous silicon thin-film solar cell plate 4 being laid on wing plate 5 absorbs solar energy, passes through solar energy
Charge controller 32 protects battery 33, so that the electric energy that solar panel is converted by solar energy is steadily saved in battery
In, store electric energy in battery 33, by motor connect, energy be provided endlessly supplement for brushless motor 7, realize energy
The sustainable and high efficiency in source.
Bionical empennage D is connect with fuselage 3 using typed ball bearing pair universal joint 27 and realizes universal fortune by the bionical empennage D of flapping wing aircraft
It is dynamic, then hinged rope 31 is drawn by steering engine 26 and respectively drives rotation, it goes that fixed plate 30 is driven to swing to realize tailplane 28 and hang down
The rotation of the upper and lower of straight tail 29, left and right four direction.By the different cooperations turned to of control steering engine 26 can realize up and down,
The purpose of left and right turn.If steering engine 26 turns to identical, the left and right turn of tailplane 28 and vertical tail 29 may be implemented.If rudder
Machine 26 turns on the contrary, tailplane 28 then may be implemented and the upper and lower of vertical tail 29 swats, so that flapping-wing aircraft climbs or bows
Punching.
The beneficial effects of the present invention are:
The present invention is proposed a kind of bionical solar energy flapping wing aircraft by the inspiration of Bird Flight.This flapping wing aircraft
With novel driving-gear mechanism, structure novel, transmission mechanism are simple and reliable；And pass through wing plate and tail in flight
The biomimetic features of the wing obtain the enough lift of flight, meet the flight demand of minute vehicle.The minute vehicle also has simultaneously
The flapping wing of flexible solar film battery plate fitting, can be converted to electric energy using solar energy in minute vehicle flight,
It realizes energy compensating, to save the energy, promote flight performance, makes to fly efficient, sustainable, for improving flapping-wing modal
Mobility and cruising ability be of great significance.
Flapping wing aircraft rack of the invention is manufactured using ABS plastic, and connecting rod, rocking bar are all made of nylon manufacture, and axis is whole
It is manufactured using titanium alloy.Lighter weight and meet certain strength condition.
Second level expansion cylinder gear speed reducer two-stage gear pairing material of the invention is identical, removes axis and the outer institute of bearing
It is plastics with material, to mitigate total weight as far as possible, each gear tooth width coefficient is equal, so that contact strength of tooth surface is substantially
It is equal.
The present invention designs bionic flapping-wing structure from bionics, increases flight lift, reduces flight resistance, reduces and flies
Energy consumption when row.In addition the adhesive film solar panel on flapping wing aircraft wing plate supplements the energy and power for aircraft.
The solar battery plate material that the present invention uses uses amorphous silicon thin-film solar cell, lighter weight and can be any
Bending.Amorphous silicon thin-film solar cell plate has the characteristics of light quality, can also generate electricity under dim light, compensates for other sun
The short slab to discharge under energy solar panel specific light source, then charges to battery, so that the cruising ability of aircraft is enhanced.
Detailed description of the invention
Fig. 1 is the overall structure diagram of solar energy flapping wing bionic Aircraft
Fig. 2 is the axonometric drawing of solar energy film left wing plate and right wing plate
Fig. 3 is the part drawing of right connecting rod
Fig. 4 is the part drawing of left connecting rod
Fig. 5 is the part drawing of skeleton
Fig. 6 is part drawing of the rocker arm to a
Fig. 7 is part drawing of the rocker arm to b
Fig. 8 is driving-transmission structures schematic diagram right view of flapping wing aircraft
Fig. 9 is driving-transmission device axis and gear axonometric drawing
Figure 10 is the axonometric drawing of rack
Figure 11 is driving-transmission structures schematic diagram left view of flapping wing aircraft
Figure 12 is gear-driven schematic diagram
Figure 13 is the part drawing of right rack
Figure 14 is the part drawing of left frame
Figure 15 is part drawing of the gag lever post to a
Figure 16 is part drawing of the gag lever post to b
Figure 17 is the part drawing of fixed frame
Figure 18 is the skeleton structure schematic diagram of solar energy flapping wing bionic Aircraft
Figure 19 is the axonometric drawing of tail gear
Figure 20 is the axonometric drawing of fuselage device
Figure 21 is the schematic illustration of solar energy film wing plate
Wherein: the A. solar energy film right wing plate B. driving-bionical empennage of transmission device C. solar energy film left wing plate D.
1. the right rack 9. of 7. brushless motor of fuselage 2. right connecting rod, 3. left connecting rod, 4. solar panel, 5. wing plate, 6. skeleton 8.
10. level-one gear wheel of level-one pinion gear, 11. second level pinion gear a, 12. rocker arm limits 13. yoke a of a, 14. drive rod a 15.
Bar is to 16. second level gear wheel a of a, 17. 18. side frame of bolt group a, 19. 20. fixed frame of second level pinion gear b, 21. left frame
22. 23. second level axis of primary axis, 24. 27. universal joint of second level gear wheel b 25. retaining ring, 26. steering engine, 28. tailplane 29.
30. fixed plate 31. of vertical tail is hingedly restricted to 32. solar charging controller, 33. battery, 34. yoke b, 35. rocker arm pair
36. gag lever post of b is to 37. drive rod b of b, 38. bolt group b
Specific embodiment
The present invention is explained in detail with reference to the accompanying drawing:
As shown in Figure 1, the present invention is by solar energy film right wing plate A, driving-transmission device B, solar energy film left wing plate
C and bionical empennage D composition, in which: the solar energy film right wing plate A and solar energy film left wing plate C is about fuselage a-a
The symmetrical structure of central axes；Gag lever post pair in the hole a a of right connecting rod 2 and driving-transmission device B in solar energy film right wing plate A
The hole n n on the hole i i and rocker arm a12 on a15 is flexibly connected；The hole the b b of right connecting rod 2 is solid to the hole the m m on a12 through bolt and rocker arm
It connects.
In solar energy film left wing plate C in the hole the a1 a1 of left connecting rod 3 and driving-transmission device B gag lever post to the i1 on b36
Hole i1 and rocker arm are flexibly connected the hole the n1 n1 on b35；The hole the b1 b1 of left connecting rod 3 is through bolt and rocker arm to the hole the m1 m1 on b35
It is affixed；Bionical empennage D is articulated with the rear end of fuselage 1.
Q slot q, r slot r, s slot s of bionical empennage D middle fuselage 1 is affixed through the hole o o and driving-transmission device B fixed frame 20.
Driving-transmission device B solar charging controller 32 and battery 33 and side frame 18 are affixed；Solar recharging
4 circuit connection of solar panel of controller 32 and solar energy film right wing plate A and solar energy film left wing plate C, battery
33 one end connect solar charging controller 32, and 33 other end of battery connects driving-transmission device B brushless motor 7.
As shown in Figures 2 to 5, a kind of solar energy flapping wing bionic Aircraft, it is characterised in that: the solar energy
Film right wing plate A and solar energy film left wing plate C is the symmetrical structure about the central axes fuselage a-a, and structure is identical, direction phase
Instead, it is made of solar panel 4, wing plate 5, skeleton 6, middle skeleton 6 is equipped with the hole p p；On solar energy film right wing plate A
It is additionally provided with right connecting rod 2,2 left end of right connecting rod is equipped with the hole a a and hole b b；Left connecting rod 3, Zuo Lian is additionally provided on solar energy film left wing plate C
3 right end of bar is equipped with the hole the a1 a1 and hole b1 b1.
The skeleton 6 of solar energy film left wing plate C is affixed through the hole p p and left connecting rod 3, and wing plate 5 is supported by skeleton 6；Solar-electricity
Pond plate 4 is adhered to above wing plate 5；The skeleton of solar energy film right wing plate A is affixed through the hole p and right connecting rod 2, and wing plate is by skeleton branch
Support；Solar panel is adhered to above wing plate.
As shown in Fig. 6 to Figure 14, the driving-transmission device B by brushless motor 7, right rack 8, level-one pinion gear 9,
Level-one gear wheel 10, second level pinion gear a11, rocker arm are to a12, yoke a13, drive rod to a14, gag lever post to a15, second level gear wheel
A16, bolt group a17, side frame 18, second level pinion gear b19, fixed frame 20, left frame 21, primary axis 22, second level axis 23, second level
Gear wheel b24, yoke b34, rocker arm form b35, gag lever post to b36, drive rod b37 and bolt group b38, in which: right rack 8 with
Left frame 21 is the symmetrical structure about the central axes fuselage a-a；Right rack 8 be equipped with the hole the c hole c, d hole d, e hole e, f hole f, g g and
The hole h h；Left frame 21 is equipped with the hole the c1 hole c1, d1 hole d1, e1 hole e1, f1 hole f1, g1 g1 and the hole h1 h1；Gag lever post on a15 to setting
There is the hole i i；Rocker arm is equipped with the hole the j hole j, k hole k, m m and hole n n to a12；Gag lever post is equipped with the hole i1 i1 to b36；Rocker arm is to b35
It is equipped with the hole the j1 hole j1, k1 hole k1, m1 m1 and hole n1 n1；Fixed frame 20 is equipped with the hole o o；Right rack 8 and 21 parallel of left frame
Column, and it is affixed through side frame 18；Brushless motor 7 is affixed through the hole the c hole c, d hole d, e hole e, f f and right 8 bolt of rack；Brushless motor 7
It is affixed through the hole the c1 hole c1, d1 hole d1, e1 hole e1, f1 f1 and 21 bolt of left frame；It is defeated that level-one pinion gear 9 is fixed in brushless motor 7
Outlet；Primary axis 22 and 23 parallel arrangement of second level axis；From right-to-left successively affixed second level pinion gear a11, level-one on primary axis 22
Gear wheel 10 and second level pinion gear b19, and 22 both ends of primary axis are movably connected on the hole the g g of right rack 8 and the hole g1 of left frame 21
On g1；Second level gear wheel a16 and second level gear wheel b24, and the activity of 23 both ends of second level axis is fixedly mounted in front and back on second level axis 23
It is connected on the hole the h h of right rack 8 and the hole the h1 h1 of left frame 21；Level-one pinion gear 9 is engaged with level-one gear wheel 10；Second level is small
Gear a11 is engaged with second level gear wheel a16；Second level pinion gear b19 is engaged with second level gear wheel b24.
Gag lever post is fixed in right 8 right side of rack to a15；A hole a of the rocker arm to the hole the n n on a12 through pin shaft and connecting rod 1, limit
Position bar is flexibly connected the hole the i i of a15；Rocker arm is affixed through bolt group a17 and the both ends yoke a13 to the hole the j hole j, k k on a12；Driving
Bar a14 and the second level gear wheel a16 flank of tooth are affixed；The long hole width of yoke a13 is greater than drive rod a14 diameter.
Gag lever post is fixed in 21 left side of left frame to b36；A1 hole of the rocker arm to the hole the n1 n1 on b35 through pin shaft Yu connecting rod 1
A1, gag lever post are flexibly connected the hole the i1 i1 of b36；Rocker arm is to the hole the j1 hole j1, k1 k1 on b35 through bolt group b38 and yoke b34 two
It holds affixed；Drive rod b37 and the second level gear wheel a16 flank of tooth are affixed；The long hole width of yoke b34 is greater than drive rod b37 diameter；It is fixed
20 bottom end of frame and side frame 18 are affixed.
As shown in Figure 15 to Figure 17, the bionical empennage D is by fuselage 1, retaining ring 25, steering engine 26, universal joint 27, horizontal tail
The wing 28, vertical tail 29, fixed plate 30 and hinged rope are formed to 31, in which: fuselage 3 is equipped with q slot q, r slot r, s slot s, t slot t
With u slot u；1 rear end of fuselage and 27 front of universal joint are affixed；Universal joint 27 and 30 center of fixed plate are hinged.
Hingedly rope is made of to 31 the hinged rope in left and right two, and two rear ends hingedly restricted are respectively and at left and right sides of fixed plate 30
It is affixed；Two front ends hingedly restricted are affixed with 26 left and right sides of steering engine respectively.
Steering engine 26 is fixed on the t slot t and u slot u of fuselage 1 through retaining ring 25；Tailplane 28 and 29 front end of vertical tail are affixed
Behind fixed plate 30.
Claims (4)
1. a kind of solar energy flapping wing bionic Aircraft, it is characterised in that: by solar energy film right wing plate (A), driving-transmission device
(B), solar energy film left wing plate (C) and bionical empennage (D) composition, in which: the solar energy film right wing plate (A) and the sun
Energy film left wing plate (C) is the symmetrical structure about the central axes fuselage a-a；Right connecting rod (2) in solar energy film right wing plate (A)
The hole a (a) connects the hole n (n) activity on the hole i (i) and rocker arm a (12) on a (15) with gag lever post in driving-transmission device (B)
It connects；The hole b (b) of right connecting rod (2) is affixed to the hole m (m) on a (12) through bolt and rocker arm；It is left in solar energy film left wing plate (C)
In the hole a1 (a1) of connecting rod (3) and driving-transmission device (B) gag lever post on b (36) the hole i1 (i1) and rocker arm on b (35)
The hole n1 (n1) be flexibly connected；The hole b1 (b1) of left connecting rod (3) is affixed to the hole m1 (m1) on b (35) through bolt and rocker arm；It is imitative
Raw empennage (D) is articulated with the rear end of fuselage (1)；The q slot (q) of bionical empennage (D) middle fuselage (1), r slot (r), s slot (s) are through the hole o
(o) affixed with the fixed frame (20) of driving-transmission device (B)；The solar charging controller (32) of driving-transmission device (B)
It is affixed with battery (33) and side frame (18)；Solar charging controller (32) and solar energy film right wing plate (A) and the sun
Solar panel (4) circuit connection of energy film left wing plate (C), battery (33) one end connect solar charging controller
(32), the brushless motor (7) of battery (33) other end connection driving-transmission device (B).
2. a kind of solar energy flapping wing bionic Aircraft according to claim 1, it is characterised in that: the solar energy film is right
Wing plate (A) and solar energy film left wing plate (C) are the symmetrical structure about the central axes fuselage a-a, and structure is identical, direction phase
Instead, it is made of solar panel (4), wing plate (5), skeleton (6), middle skeleton (6) is equipped with the hole p (p)；Solar energy film
It is additionally provided on right wing plate (A) right connecting rod (2), right connecting rod (2) left end is equipped with the hole a (a) and the hole b (b)；Solar energy film left wing plate
(C) it is additionally provided on left connecting rod (3), left connecting rod (3) right end is equipped with the hole a1 (a1) and the hole b1 (b1)；Solar energy film left wing plate (C)
Skeleton (6) it is affixed through the hole p (p) and left connecting rod (3), wing plate (5) by skeleton (6) support；Solar panel (4) is adhered to the wing
Plate (5) is above；The skeleton of solar energy film right wing plate (A) is affixed through the hole p and right connecting rod (2), and wing plate is by skeletal support；Solar energy
Solar panel is adhered to above wing plate.
3. a kind of solar energy flapping wing bionic Aircraft according to claim 1, it is characterised in that: the driving-transmission dress
Set (B) by brushless motor (7), right rack (8), level-one pinion gear (9), level-one gear wheel (10), second level pinion gear a (11), shake
Arm is to a (12), yoke a (13), drive rod to a (14), gag lever post to a (15), second level gear wheel a (16), bolt group a (17), side
Rack (18), second level pinion gear b (19), fixed frame (20), left frame (21), primary axis (22), second level axis (23), second level canine tooth
B (24), yoke b (34), rocker arm are taken turns to b (35), gag lever post to b (36), drive rod b (37) and bolt group b (38) composition, in which:
Right rack (8) and left frame (21) are the symmetrical structure about the central axes fuselage a-a；Right rack (8) is equipped with the hole c (c), the hole d
(d), the hole e (e), the hole f (f), the hole g (g) and the hole h (h)；Left frame (21) be equipped with the hole c1 (c1), the hole d1 (d1), the hole e1 (e1),
The hole f1 (f1), the hole g1 (g1) and the hole h1 (h1)；Gag lever post is equipped with the hole i (i) to a (15)；Rocker arm is equipped with the hole j to a (12)
(j), the hole k (k), the hole m (m) and the hole n (n)；Gag lever post is equipped with the hole i1 (i1) to b (36)；Rocker arm is equipped with the hole j1 to b (35)
(j1), the hole k1 (k1), the hole m1 (m1) and the hole n1 (n1)；Fixed frame (20) is equipped with the hole o (o)；Right rack (8) and left frame (21)
It is arranged in parallel and affixed through side frame (18)；Brushless motor (7) is through the hole c (c), the hole d (d), the hole e (e), the hole f (f) and right rack
(8) bolt is affixed；Brushless motor (7) is through the hole c1 (c1), the hole d1 (d1), the hole e1 (e1), the hole f1 (f1) and left frame (21) bolt
It is affixed；Level-one pinion gear (9) is fixed in brushless motor (7) output end；Primary axis (22) and second level axis (23) parallel arrangement；Level-one
From right-to-left successively affixed second level pinion gear a (11), level-one gear wheel (10) and second level pinion gear b (19) on axis (22), and one
Grade axis (22) both ends are movably connected on the hole g (g) of right rack (8) and the hole g1 (g1) of left frame (21)；On second level axis (23)
Second level gear wheel a (16) and second level gear wheel b (24) is fixedly mounted in front and back, and second level axis (23) both ends are movably connected on right machine
On the hole h (h) of frame (8) and the hole h1 (h1) of left frame (21)；Level-one pinion gear (9) is engaged with level-one gear wheel (10)；Second level
Pinion gear a (11) is engaged with second level gear wheel a (16)；Second level pinion gear b (19) is engaged with second level gear wheel b (24)；Gag lever post
A (15) is fixed on the right side of right rack (8)；A hole (a) of the rocker arm to the hole n (n) on a (12) through pin shaft and connecting rod (1), limit
Bar is flexibly connected the hole i (i) of a (15)；Rocker arm on a (12) the hole j (j), the hole k (k) is through bolt group a (17) and yoke a (13)
Both ends are affixed；Drive rod a (14) and second level gear wheel a (16) flank of tooth are affixed；The long hole width of yoke a (13) is greater than drive rod a
(14) diameter；Gag lever post is fixed on the left of left frame (21) b (36)；Rocker arm is to the hole n1 (n1) on b (35) through pin shaft and company
The hole a1 (a1) of bar (1), gag lever post are flexibly connected the hole i1 (i1) of b (36)；Rocker arm is to the hole j1 (j1), the hole k1 on b (35)
(k1) affixed through bolt group b (38) and yoke b (34) both ends；Drive rod b (37) and second level gear wheel a (16) flank of tooth are affixed；Yoke b
(34) long hole width is greater than drive rod b (37) diameter；Fixed frame (20) bottom end and side frame (18) are affixed.
4. a kind of solar energy flapping wing bionic Aircraft according to claim 1, it is characterised in that: the bionical empennage (D)
By fuselage (1), retaining ring (25), steering engine (26), universal joint (27), tailplane (28), vertical tail (29), fixed plate (30) and
Hinged rope forms (31), in which: fuselage (3) is equipped with q slot (q), r slot (r), s slot (s), t slot (t) and u slot (u)；Fuselage
(1) rear end and universal joint (27) front are affixed；Universal joint (27) and fixed plate (30) center are hinged；Hinged rope is to (31) by left and right
Two hinged rope compositions, two rear ends hingedly restricted are affixed with fixed plate (30) left and right sides respectively；Two front ends hingedly restricted
It is affixed with steering engine (26) left and right sides respectively；Steering engine (26) is fixed on the t slot (t) and u slot (u) of fuselage (1) through retaining ring (25)；Water
The horizontal tail wing (28) and vertical tail (29) front end are fixed in fixed plate (30) below.
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| CN201910302505.6A CN109850144B (en) | 2019-04-16 | 2019-04-16 | Solar flapping wing bionic aircraft |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910302505.6A CN109850144B (en) | 2019-04-16 | 2019-04-16 | Solar flapping wing bionic aircraft |
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| CN109850144B CN109850144B (en) | 2023-08-22 |
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| CN112278267A (en) * | 2020-10-28 | 2021-01-29 | 北京航空航天大学 | Bionic flapping wing aircraft and control method thereof |
| CN112977850A (en) * | 2021-04-16 | 2021-06-18 | 北京航空航天大学 | Flapping wing aircraft thermal management system suitable for high and cold environment |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN109850144B (en) | 2023-08-22 |
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