CN108791908A - A kind of agricultural aircraft for being convenient for changing battery - Google Patents
A kind of agricultural aircraft for being convenient for changing battery Download PDFInfo
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- CN108791908A CN108791908A CN201810523331.1A CN201810523331A CN108791908A CN 108791908 A CN108791908 A CN 108791908A CN 201810523331 A CN201810523331 A CN 201810523331A CN 108791908 A CN108791908 A CN 108791908A
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- fixedly connected
- shell
- aircraft
- threaded post
- convenient
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 8
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000779 depleting effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of agricultural aircraft for being convenient for changing battery, including aircraft fuselage, the left and right sides of the aircraft fuselage are fixedly connected with two opposite one end of telescopic device respectively, the left end of telescopic device is fixedly connected with the right side of the first block, and the upper surface of telescopic device is fixedly connected with the lower surface of fixed plate.The agricultural aircraft for being convenient for changing battery, by the way that the first slide bar is arranged, second slide bar, first fixture block, second fixture block, handle, first block, bearing and the first threaded post, when battery is fixed, peasant makes the second connecting plate move down downwardly against briquetting, last peasant opens shell and replaces the accumulator inside aircraft fuselage, without peasant using tool unscrew aircraft fuselage shell replace inside accumulator, the operation of peasant is not only facilitated in this way, and the certain convenience brought for the operation of peasant, so that the operating efficiency of peasant improves.
Description
Technical field
The present invention relates to unmanned vehicle technical field, specially a kind of agricultural aircraft for being convenient for changing battery.
Background technology
Miniature unmanned vehicle is a kind of new concept weapon, tackles traditional weapon with microminiature weapon, will lead to the following war
There is " the unbalanced war of scale " in field, thus exerts far reaching influence to future military operation.They can be not attractive
Aerial reconnaissance activity, shooting country are carried out, and is passed back ground
The fields, such as aircraft of agricultural such as existing aircraft is widely used in taking photo by plane, agricultural and forestry, it can help agriculture
The people are more convenient for the state of observation wheatland, but since the battery capacity of existing agriculture aircraft is smaller, due to outdoors
It can not directly charge when use, therefore use for a long time can not be then continuing with after depleting electric power outdoors, therefore peasant
It needs to replace accumulator to aircraft, however accumulator is located at aircraft interior, and accumulator could be replaced by needing to dismantle shell, from
And peasant is needed to unscrew the shell of aircraft using tool, the accumulator of aircraft interior is then replaced, peasant inconvenient in this way
Operation, and be certain trouble for bringing of operation of peasant so that the operating efficiency of peasant reduces.
Invention content
（One）The technical issues of solution
In view of the deficiencies of the prior art, the present invention provides a kind of agricultural aircraft for being convenient for changing battery, needs are solved
Peasant uses tool changing accumulator, the operation of peasant inconvenient in this way, and the certain trouble brought for the operation of peasant, makes
The problem of obtaining the operating efficiency of peasant reduces.
（Two）Technical solution
To achieve the above object, the present invention provides the following technical solutions：A kind of agricultural aircraft for being convenient for changing battery, including
The left and right sides of aircraft fuselage, the aircraft fuselage are fixedly connected with two opposite one end of telescopic device respectively, institute
The left end for stating telescopic device is fixedly connected with the right side of the first block, the upper surface of the telescopic device and the following table of fixed plate
Face is fixedly connected, and the telescopic device includes the first slide bar, the left and right ends of first slide bar right side with the first block respectively
Side is fixedly connected with the left side of aircraft fuselage.
The outer surface of first slide bar is socketed with the first spring and the first sliding sleeve, the right side of first sliding sleeve with fly
The left side of row device fuselage overlaps, the left and right ends of first spring respectively with the right side of the first block and the first sliding sleeve
Left side is fixedly connected, and the upper surface of first sliding sleeve is fixedly connected with the lower surface of fixed plate, the left side of the fixed plate
Face is fixedly connected with handle, and the right side of the fixed plate is fixedly connected with the left side of the first fixture block, and first fixture block is set
It sets in the first card slot, first card slot is opened in the left side of shell, the lower surface of the shell and aircraft fuselage
Upper surface overlaps, and the upper surface of first fixture block offers the second card slot, the second fixture block, institute are provided in second card slot
The upper surface for stating the second fixture block is fixedly connected with the bottom end of connecting rod, and the setting of the connecting rod is in first through hole, and described
One through-hole is opened in the upper surface of shell.
The top of the connecting rod is fixedly connected with the lower surface of the first connecting plate, the upper surface card of first connecting plate
It is connected to the first thread cap, the first thread cap internal thread is connected with the first threaded post, the top of first threaded post and the
The bottom end of one stubborn ring is fixedly connected.
Preferably, the bottom end of first threaded post is fixedly connected with the top of rotating device, the rotating device clamping
It is fixedly connected with the top of telescopic rod in the lower surface of the upper surface of shell, first connecting plate, the bottom end of the telescopic rod
It is fixedly connected with the upper surface of shell, the telescopic rod is located at the right side of rotating device.
Preferably, the rotating device includes bearing, and the bearing is connected to the upper surface of shell, and the bearing inner sleeve connects
There are shaft, the top of the shaft to be fixedly connected with the bottom end of the first threaded post.
Preferably, the upper surface of the shell is fixedly connected there are two carriage, and the carriage is connected to second
The lower surface of connecting plate, the top of the carriage are fixedly connected with the lower surface of the second block, and the carriage includes
The top of second slide bar, second slide bar is fixedly connected with the lower surface of the second block, the bottom end of second slide bar with it is outer
The upper surface of shell is fixedly connected, and the outer surface of second slide bar is socketed with the second sliding sleeve, and second sliding sleeve is connected to second
The lower surface of connecting plate.
Preferably, the upper surface of second connecting plate is fixedly connected with the lower surface of briquetting, and the briquetting is located at two
Between second sliding sleeve, the lower surface of second connecting plate is fixedly connected with the top of supporting rod, the bottom end of the supporting rod with
The upper surface of second thread cap is fixedly connected.
Preferably, the second thread cap internal thread is connected with the second threaded post, described positive one end of second threaded post
It is fixedly connected with the one end at the second stubborn ring back side, the front of the aircraft fuselage opens up fluted, is provided in the groove
Third thread cap, the third thread cap is identical as the diameter of the second thread cap inner ring, and the quantity of the third thread cap is two
It is a, and two third thread caps are located at the front and back of aircraft fuselage.
Preferably, the four corners of the aircraft fuselage outer surface have been fixedly connected with support plate, the support plate it is upper
Surface is provided with propeller, and the lower surface of the aircraft fuselage is fixedly connected with the upper surface of pedestal, the shape of the pedestal
Four corners for hemispherical, the base lower surface have been fixedly connected with support leg.
Preferably, the telescopic rod includes shell, and the upper surface of the shell offers the second through-hole, second through-hole
It is inside provided with support column, the bottom end of the support column is fixedly connected with the upper surface of slide plate, the left and right ends difference of the slide plate
It is slidably connected in two sliding slots, and two sliding slots are opened in the left and right sides of inner walls, the top of the support column respectively
It is fixedly connected with the lower surface of the first connecting plate, the lower surface of the shell is fixedly connected with the upper surface of shell.
（Three）Advantageous effect
The present invention provides a kind of agricultural aircraft for being convenient for changing battery, have following advantageous effect：
1, the agricultural aircraft for being convenient for changing battery, by the way that the first slide bar, the second slide bar, the first fixture block, the second card is arranged
Block, handle, the first block, bearing and the first threaded post, when battery is fixed, peasant makes second downwardly against briquetting
Connecting plate moves down so that supporting rod drives the second thread cap to be moved to the front of third thread cap, then rotates second
Twist ring rotate forward so that the second stubborn annulus move the second threaded post rotate forward so that the second threaded post move backward and with third thread cap spiral shell
Line connects so that shell is fixed more to be stablized, and when needing to replace accumulator, peasant turns the first stubborn ring reversion
So that the reversion of the first threaded post so that the first threaded post moves up so that the first threaded post drives the second fixture block to move up,
So that the second fixture block is no longer stuck in the second card slot, then turns the second stubborn ring and invert so that the forward movement of the second threaded post, makes
It obtains the second threaded post to be no longer threadedly coupled with third thread cap, while second spring drives the second connecting plate to move up so that
Second connecting plate drives the second threaded post to move up by supporting rod, while peasant pulls two one or two palmistrys separate respectively, makes
It obtains two the first fixture blocks to be no longer stuck in two the first card slots, last peasant opens shell and simultaneously replaces the storage inside aircraft fuselage
Battery unscrews the accumulator inside the shell replacement of aircraft fuselage, so not only without peasant using tool
Facilitate the operation of peasant, and the certain convenience brought for the operation of peasant so that the operating efficiency of peasant improves.
2, the agricultural aircraft for being convenient for changing battery, by the first slide bar and the first sliding sleeve, so that fixed plate
The first sliding sleeve can be driven to move left and right when moving left and right so that the first sliding sleeve is moved left and right along the first slide bar, to make
Fixed plate will not shake when moving left and right and more stablize so that the first fixture block of drive that fixed plate can be stablized sticks into the
In one card slot, by the way that the first spring is arranged, so that the first spring can drive the first sliding sleeve to move right when extending so that
First sliding sleeve drives fixed plate to move right so that and fixed plate can drive the first fixture block to move right and stick into the first card slot,
So that shell is fixed, by the way that the first fixture block and the first card slot is arranged, so that the first fixture block sticks into the first card slot
When interior, shell, which is fixed, to be shaken, and more stablized so that internal accumulator is fixed, and the second card of setting is passed through
Slot and the second fixture block, so that when the second fixture block is sticked into the second card slot, the first fixture block, which is fixed, to be loosened, to make
It is fixed more stable to obtain shell.
3, the agricultural aircraft for being convenient for changing battery, by the way that bearing and shaft is arranged, so that the first threaded post
Shaft can be driven to rotate when rotated so that shaft rotates in bearing, so that the first threaded post when rotated will not
Shake and more stablize so that the first thread cap can stablize moving up and down and will not shake, by be arranged telescopic rod,
So that the first thread cap can drive the second connecting plate to move up and down when moving up and down so that the second connecting plate drives flexible
Bar is extended or is shunk, so that the first thread cap will not rotate when moving up and down and more stablize, is slided by setting second
Set and the second slide bar, so that the second connecting plate can drive the second sliding sleeve to move up and down when moving up and down so that second slides
Set can be moved up and down along the second slide bar, so that the second connecting plate will not shake moving up and down and more stablize, from
And it will not be shaken when making supporting rod that the second threaded post be driven to move down so that can be located at when the second threaded post moves down
The front of third thread cap so that the second threaded post can be threadedly coupled when rotating with third thread cap, by the way that second gear is arranged
Block, so that the second sliding sleeve will not move upward out the second slide bar, by the way that the second thread cap is arranged, so that the second screw thread
Column can be moved forward and backward when rotating so that the second threaded post can move backward and connect with third screw thread cap thread when rotated
It connects, and structure of the invention is compact, reasonable design is highly practical.
Description of the drawings
Fig. 1 is the cross-sectional view that the present invention faces；
Fig. 2 is the structural schematic diagram that the present invention overlooks；
Fig. 3 is the structural schematic diagram that the present invention faces；
Fig. 4 is the enlarged structure schematic diagram at A of the present invention；
Fig. 5 is the cross-sectional view of telescopic rod of the present invention.
In figure：1 aircraft fuselage, 2 telescopic devices, 201 first sliding sleeves, 202 first slide bars, 203 first springs, 3 first
Block, 4 fixed plates, 5 handles, 6 shells, 7 first fixture blocks, 8 first card slots, 9 second card slots, 10 second fixture blocks, 11 connecting rods, 12
First through hole, 13 first connecting plates, 14 first thread caps, 15 pedestals, 16 first threaded posts, 17 first stubborn rings, 18 telescopic rods,
1801 shells, 1802 slide plates, 1803 sliding slots, 1804 support columns, 1,805 second through-holes, 19 rotating devices, 191 shafts, 192 axis
Hold, 20 second connecting plates, 21 carriages, 211 second slide bars, 212 second sliding sleeves, 22 support legs, 23 second springs, 24 second
It is block, 25 briquettings, 26 supporting rods, 27 second thread caps, 28 second stubborn rings, 29 second threaded posts, 30 third thread caps, 31 recessed
Slot, 32 support plates, 33 propellers.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As shown in Figs. 1-5, the present invention provides a kind of technical solution：A kind of agricultural aircraft for being convenient for changing battery, packet
Aircraft fuselage 1 is included, the left and right sides of aircraft fuselage 1 are fixedly connected with two opposite one end of telescopic device 2, stretch respectively
The left end of compression apparatus 2 is fixedly connected with the right side of the first block 3, and the upper surface of telescopic device 2 is solid with the lower surface of fixed plate 4
Fixed connection, by the way that fixed plate 4 is arranged, so that the first fixture block 7 will not shake and more stablize, telescopic device 2 at work
Including the first slide bar 202, the left and right ends of the first slide bar 202 left side with the right side and aircraft fuselage 1 of the first block 3 respectively
Side is fixedly connected, by the way that the first block 3 is arranged, so as to avoid worker that the first sliding sleeve 201 is pulled away from first to the left
Slide bar 202.
The outer surface of first slide bar 202 is socketed with the first spring 203 and the first sliding sleeve 201, passes through the first slide bar 202 and
One sliding sleeve 201, so that fixed plate 4 can drive the first sliding sleeve 201 to move left and right when moving left and right so that the first sliding sleeve
201 move left and right along the first slide bar 202, so that fixed plate 4 will not shake when moving left and right and more stablize so that
The first fixture block of drive 7 that fixed plate 4 can be stablized sticks into the first card slot 8, the right side of the first sliding sleeve 201 and aircraft fuselage
1 left side overlap joint, the left and right ends of the first spring 203 left side with the right side of the first block 3 and the first sliding sleeve 201 respectively
Face is fixedly connected, by be arranged the first spring 203 so that the first spring 203 extend when can drive the first sliding sleeve 201 to
It moves right so that the first sliding sleeve 201 drives fixed plate 4 to move right so that fixed plate 4 can drive the first fixture block 7 to move right
It is dynamic to stick into the first card slot 8, so that shell 6 is fixed, the lower surface of the upper surface and fixed plate 4 of the first sliding sleeve 201
It is fixedly connected, the left side of fixed plate 4 is fixedly connected with handle 5, and the right side of fixed plate 4 and the left side of the first fixture block 7 are solid
Fixed connection, the first fixture block 7 are arranged in the first card slot 8, by the way that the first fixture block 7 and the first card slot 8 is arranged, so that the first card
When block 7 is sticked into the first card slot 8, shell 6, which is fixed, to be shaken, so that internal accumulator is fixed more steady
It is fixed, by the way that the second card slot 9 and the second fixture block 10 is arranged, so that when the second fixture block 10 is sticked into the second card slot 9, the first fixture block
7 are fixed and cannot loosen, and more stablize so that shell 6 is fixed, and the first card slot 8 is opened in the left side of shell 6,
The lower surface of shell 6 and the upper surface of aircraft fuselage 1 overlap, and the upper surface of the first fixture block 7 offers the second card slot 9, and second
The second fixture block 10 is provided in card slot 9, the upper surface of the second fixture block 10 is fixedly connected with the bottom end of connecting rod 11, connecting rod 11
It is arranged in first through hole 12, by the way that first through hole 12 is arranged, so that connecting rod 11 will not be hindered when moving up and down
Hinder and more convenient, first through hole 12 is opened in the upper surface of shell 6.
The top of connecting rod 11 is fixedly connected with the lower surface of the first connecting plate 13, the upper surface clamping of the first connecting plate 13
There are the first thread cap 14,14 internal thread of the first thread cap to be connected with the first threaded post 16, the top and first of the first threaded post 16
The bottom end for twisting ring 17 is fixedly connected, by the way that the first stubborn ring 17 is arranged, so that worker is when turning the rotation of the first threaded post 16
More convenient, the bottom end of the first threaded post 16 is fixedly connected with the top of rotating device 19, and rotating device 19 is connected to shell 6
The lower surface of upper surface, the first connecting plate 13 is fixedly connected with the top of telescopic rod 18, by the way that telescopic rod 18 is arranged, so that
First thread cap 14 can drive the second connecting plate 20 to move up and down when moving up and down so that the second connecting plate 20 drives telescopic rod
18 elongations are shunk, so that the first thread cap 14 will not rotate when moving up and down and more stablize, the bottom of telescopic rod 18
End is fixedly connected with the upper surface of shell 6, and telescopic rod 18 is located at the right side of rotating device 19, and rotating device 19 includes bearing 192,
Bearing 192 is connected to the upper surface of shell 6, and shaft 191 is socketed in bearing 192, by the way that bearing 192 and shaft 191 is arranged, from
And make the first threaded post 16 that shaft 191 can be driven to rotate when rotated so that the rotation in bearing 192 of shaft 191, to
So that the first threaded post 16 will not shake when rotated and more stablize so that the first thread cap 14 can stablize up and down
It moves and will not shake, the top of shaft 191 is fixedly connected with the bottom end of the first threaded post 16, and the upper surface of shell 6, which is fixed, to be connected
It connects there are two carriage 21, carriage 21 is connected to the lower surface of the second connecting plate 20, the top of carriage 21 and the
The lower surface of two blocks 24 is fixedly connected, by the way that the second block 24 is arranged, so that the second sliding sleeve 212 will not move upward out
Second slide bar 211, by the way that the second thread cap 27 is arranged, so that the second threaded post 29 can be moved forward and backward when rotating so that
Second threaded post 29 can be moved backward and is threadedly coupled with third thread cap 30 when rotated, and carriage 21 includes the second cunning
Bar 211, the top of the second slide bar 211 are fixedly connected with the lower surface of the second block 24, bottom end and the shell 6 of the second slide bar 211
Upper surface be fixedly connected, the outer surface of the second slide bar 211 is socketed with the second sliding sleeve 212, by the way that the second sliding sleeve 212 and the is arranged
Two slide bars 211, so that the second connecting plate 20 can drive the second sliding sleeve 212 to move up and down when moving up and down so that second
Sliding sleeve 212 can be moved up and down along the second slide bar 211, so that the second connecting plate 20 will not shake and more moving up and down
Add stabilization, so that supporting rod 26 drives the second threaded post 29 not shake when moving down so that the second threaded post 29 to
The front of third thread cap 30 can be located at when lower mobile so that the second threaded post 29 can be with 30 spiral shell of third thread cap when rotating
Line connects, and the second sliding sleeve 212 is connected to the lower surface of the second connecting plate 20, the upper surface of the second connecting plate 20 under briquetting 25
Surface is fixedly connected, and briquetting 25 is located between two the second sliding sleeves 212, by the way that briquetting 25 is arranged, so that worker is passing through
Briquetting 25 presses more convenient when the second connecting plate 20 moves down, the top of the lower surface and supporting rod 26 of the second connecting plate 20
It is fixedly connected, the bottom end of supporting rod 26 is fixedly connected with the upper surface of the second thread cap 27, by the way that supporting rod 26 is arranged, to make
Obtaining will not shake and more stablize when the second thread cap 27 moves down, and 27 internal thread of the second thread cap is connected with the second threaded post
29,29 positive one end of the second threaded post is fixedly connected with the one end at 28 back side of the second stubborn ring, and the front of aircraft fuselage 1 opens up
Fluted 31, by the way that groove 31 is arranged, more stablize so that third thread cap 30 is fixed so that the second threaded post 29
When being threaded in third thread cap 30, shell 6 can be stably fixed on aircraft fuselage 1, setting in groove 31
There is third thread cap 30, third thread cap 30 is identical as the diameter of 27 inner ring of the second thread cap, by the way that third thread cap 30 is arranged
It is identical with the diameter of 27 inner ring of the second thread cap, so that the second threaded post 29 can normally be threaded in third screw thread
The quantity of cap 30, third thread cap 30 is two, and two third thread caps 30 are located at front and the back of the body of aircraft fuselage 1
The four corners in face, 1 outer surface of aircraft fuselage have been fixedly connected with support plate 32, and the upper surface of support plate 32 is provided with propeller
33, the lower surface of aircraft fuselage 1 is fixedly connected with the upper surface of pedestal 15, and the shape of pedestal 15 is hemispherical, under pedestal 15
The four corners on surface have been fixedly connected with support leg 22, by the way that support leg 22 is arranged, so that aircraft fuselage 1 is placed on
More stablize when on ground, and will not overturn, telescopic rod 18 includes shell 1801, and the upper surface of shell 1801 offers second and leads to
Hole 1805 is provided with support column 1804 in second through-hole 1805, by the way that the second through-hole 1805 is arranged, so that support column 1804
Will not be hindered when moving up and down, the bottom end of support column 1804 is fixedly connected with the upper surface of slide plate 1802, slide plate 1802
Left and right ends be slidably connected at respectively in two sliding slots 1803, by the way that slide plate 1802 and sliding slot 1803 is arranged, so that branch
Dagger 1804 can drive slide plate 1802 to move up and down when moving up and down so that slide plate 1802 moves down on sliding slot 1803 is interior
Dynamic, so that support column 1804 will not shake when moving up and down and more stablize, and two sliding slots 1803 are opened in respectively
The left and right sides of 1801 inner wall of shell, the top of support column 1804 are fixedly connected with the lower surface of the first connecting plate 13, shell
1801 lower surface is fixedly connected with the upper surface of shell 6.
In use, peasant downwardly against briquetting 25 so that the second connecting plate 20 moves down so that supporting rod 26 drives the
Two thread caps 27 are moved to the front of third thread cap 30, then rotate the second stubborn ring 28 and rotate forward so that the second stubborn ring 28 drives
Second threaded post 29 rotates forward so that the second threaded post 29 is moved backward and is threadedly coupled with third thread cap 30 so that 6 quilt of shell
Fixed more to stablize, when needing to replace accumulator, peasant turns the first stubborn ring 17 and inverts so that the first threaded post
16 reversions so that the first threaded post 16 moves up so that the first threaded post 16 drives the second fixture block 10 to move up so that the
Two fixture blocks 10 are no longer stuck in the second card slot 9, are then turned the second stubborn ring 28 and are inverted so that the forward movement of the second threaded post 29, makes
The second threaded post 29 is no longer threadedly coupled with third thread cap 30, while the second connecting plate 20 of drive of second spring 23 is to moving up
It is dynamic so that the second connecting plate 20 drives the second threaded post 29 to move up by supporting rod 26, while peasant pulls two respectively
Handle 5 is mutually separate so that two the first fixture blocks 7 are no longer stuck in two the first card slots 8, and last peasant opens shell 6 and replaces
Accumulator inside aircraft fuselage 1, after battery altering, peasant pulls two handles 5 mutually separate respectively, simultaneously
Shell 6 is placed on aircraft fuselage 1, unclamps handle 5 so that the first spring 203 extends so that the drive of the first sliding sleeve 201 is solid
Fixed board 4 moves right so that fixed plate 4 drives the first fixture block 7 to move right and sticks into the first card slot 8, then turns first and twists
Ring 17 rotates forward so that the first thread cap 14 drives the first connecting plate 13 to move down so that the second fixture block 10, which moves down, to be sticked into
In second card slot 9, then worker is again downwardly against briquetting 25 so that and the second connecting plate 20 drives supporting rod 26 to move down,
So that the second threaded post 29 is moved to the front of third thread cap 30, last worker turns the rotation of the second stubborn ring 28 so that second
Threaded post 29, which moves backward, to be threaded in third thread cap 30, so that shell 6 is stably fixed to aircraft machine
On body 1.
Can to sum up obtain, 1, the agricultural with the aircraft of battery is convenient for changing, pass through and the first slide bar 202, the second slide bar be set
211, the first fixture block 7, the second fixture block 10, handle 5, the first block 3, bearing 192 and the first threaded post 16, consolidate when to battery
Periodically, peasant makes the second connecting plate 20 move down downwardly against briquetting 25 so that supporting rod 26 drives the second thread cap 27
It is moved to the front of third thread cap 30, the second stubborn ring 28 is then rotated and rotates forward so that the second stubborn ring 28 drives the second threaded post
29 rotate forward so that the second threaded post 29 is moved backward and is threadedly coupled with third thread cap 30 so that shell 6 is fixed more
Stablize, when needing to replace accumulator, peasant turns the first stubborn ring 17 and inverts so that the reversion of the first threaded post 16 so that
First threaded post 16 moves up so that the first threaded post 16 drives the second fixture block 10 to move up so that the second fixture block 10 is not
It is stuck in again in the second card slot 9, then turns the second stubborn ring 28 and invert so that the second threaded post 29 moves forward so that the second screw thread
Column 29 is no longer threadedly coupled with third thread cap 30, while second spring 23 drives the second connecting plate 20 to move up so that the
Two connecting plates 20 drive the second threaded post 29 to move up by supporting rod 26, while peasant pulls two handles 5 mutually remote respectively
From so that two the first fixture blocks 7 are no longer stuck in two the first card slots 8, and last peasant opens shell 6 and replaces aircraft fuselage
Accumulator inside 1, the shell 6 for unscrewing aircraft fuselage 1 using tool without peasant replace internal electric power storage
Pond not only facilitates the operation of peasant, and the certain convenience brought for the operation of peasant so that the operating efficiency of peasant in this way
It improves.
2, the agricultural aircraft for being convenient for changing battery, by the first slide bar 202 and the first sliding sleeve 201, so that
Fixed plate 4 can drive the first sliding sleeve 201 to move left and right when moving left and right so that the first sliding sleeve 201 is along the first slide bar 202
It moves left and right, so that fixed plate 4 will not shake when moving left and right and more stablize so that fixed plate 4 can be stablized
The first fixture block 7 is driven to stick into the first card slot 8, by the way that the first spring 203 is arranged, so that the first spring 203 can when extending
To drive the first sliding sleeve 201 to move right so that the first sliding sleeve 201 drives fixed plate 4 to move right so that fixed plate 4 can be with
It drives the first fixture block 7 to move right to stick into the first card slot 8, so that shell 6 is fixed, by the way that the first fixture block 7 is arranged
With the first card slot 8, so that when the first fixture block 7 is sticked into the first card slot 8, shell 6, which is fixed, to be shaken, so that
Internal accumulator is fixed more to be stablized, by the way that the second card slot 9 and the second fixture block 10 is arranged, so that the second fixture block 10
When sticking into the second card slot 9, the first fixture block 7 is fixed and cannot loosen, and more stablizes so that shell 6 is fixed.
3, the agricultural aircraft for being convenient for changing battery, by the way that bearing 192 and shaft 191 is arranged, so that first
Threaded post 16 can drive shaft 191 to rotate when rotated so that the rotation in bearing 192 of shaft 191, so that the first spiral shell
Line column 16 will not shake and more stablize when rotated, so that moving up and down of can stablizing of the first thread cap 14 and will not
It shakes, by the way that telescopic rod 18 is arranged, so that the first thread cap 14 can drive the second about 20 connecting plate when moving up and down
It is mobile so that the second connecting plate 20 drives the elongation of telescopic rod 18 or shrinks, so that the first thread cap 14 is when moving up and down
It will not rotate and more stablize, by the way that the second sliding sleeve 212 and the second slide bar 211 is arranged, so that the second about 20 connecting plate
The second sliding sleeve 212 can be driven to move up and down when mobile so that the second sliding sleeve 212 can be moved up and down along the second slide bar 211,
So that the second connecting plate 20 will not shake moving up and down and more stablize, so that supporting rod 26 drives the second screw thread
Column 29 will not shake when moving down so that the front of third thread cap 30 can be located at when the second threaded post 29 moves down,
It is threadedly coupled with third thread cap 30 when second threaded post 29 is rotated, by the way that the second block 24 is arranged, so that
Second sliding sleeve 212 will not move upward out the second slide bar 211, by the way that the second thread cap 27 is arranged, so that the second threaded post
29 rotation when can be moved forward and backward so that the second threaded post 29 can move backward when rotated and with 30 screw thread of third thread cap
Connection, and structure of the invention is compact, reasonable design, it is highly practical.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. a kind of agricultural aircraft for being convenient for changing battery, including aircraft fuselage（1）, it is characterised in that：The aircraft
Fuselage（1）Left and right sides respectively with two telescopic devices（2）Opposite one end is fixedly connected, the telescopic device（2）'s
Left end and the first block（3）Right side be fixedly connected, the telescopic device（2）Upper surface and fixed plate（4）Lower surface
It is fixedly connected, the telescopic device（2）Including the first slide bar（202）, first slide bar（202）Left and right ends respectively with
One block（3）Right side and aircraft fuselage（1）Left side be fixedly connected；
First slide bar（202）Outer surface be socketed with the first spring（203）With the first sliding sleeve（201）, first sliding sleeve
（201）Right side and aircraft fuselage（1）Left side overlap joint, first spring（203）Left and right ends respectively with
One block（3）Right side and the first sliding sleeve（201）Left side be fixedly connected, first sliding sleeve（201）Upper surface with
Fixed plate（4）Lower surface be fixedly connected, the fixed plate（4）Left side be fixedly connected with handle（5）, the fixed plate
（4）Right side and the first fixture block（7）Left side be fixedly connected, first fixture block（7）It is arranged in the first card slot（8）It is interior,
First card slot（8）It is opened in shell（6）Left side, the shell（6）Lower surface and aircraft fuselage（1）Upper table
Face overlaps, first fixture block（7）Upper surface offer the second card slot（9）, second card slot（9）Inside it is provided with the second card
Block（10）, second fixture block（10）Upper surface and connecting rod（11）Bottom end be fixedly connected, the connecting rod（11）Set
It sets in first through hole（12）It is interior, the first through hole（12）It is opened in shell（6）Upper surface；
The connecting rod（11）Top and the first connecting plate（13）Lower surface be fixedly connected, first connecting plate（13）'s
Upper surface is connected with the first thread cap（14）, first thread cap（14）Internal thread is connected with the first threaded post（16）, described
First threaded post（16）Top and the first stubborn ring（17）Bottom end be fixedly connected.
2. a kind of agricultural aircraft for being convenient for changing battery according to claim 1, it is characterised in that：First spiral shell
Line column（16）Bottom end and rotating device（19）Top be fixedly connected, the rotating device（19）It is connected to shell（6）It is upper
Surface, first connecting plate（13）Lower surface and telescopic rod（18）Top be fixedly connected, the telescopic rod（18）Bottom
End and shell（6）Upper surface be fixedly connected, the telescopic rod（18）Positioned at rotating device（19）Right side.
3. a kind of agricultural aircraft for being convenient for changing battery according to claim 2, it is characterised in that：The rotating dress
It sets（19）Including bearing（192）, the bearing（192）It is connected to shell（6）Upper surface, the bearing（192）Inside it is socketed with
Shaft（191）, the shaft（191）Top and the first threaded post（16）Bottom end be fixedly connected.
4. a kind of agricultural aircraft for being convenient for changing battery according to claim 3, it is characterised in that：The shell
（6）Upper surface be fixedly connected there are two carriage（21）, the carriage（21）It is connected to the second connecting plate（20）'s
Lower surface, the carriage（21）Top and the second block（24）Lower surface be fixedly connected, the carriage（21）
Including the second slide bar（211）, second slide bar（211）Top and the second block（24）Lower surface be fixedly connected, it is described
Second slide bar（211）Bottom end and shell（6）Upper surface be fixedly connected, second slide bar（211）Outer surface be socketed with
Second sliding sleeve（212）, second sliding sleeve（212）It is connected to the second connecting plate（20）Lower surface.
5. a kind of agricultural aircraft for being convenient for changing battery according to claim 4, it is characterised in that：Described second connects
Fishplate bar（20）Upper surface and briquetting（25）Lower surface be fixedly connected, the briquetting（25）Positioned at two the second sliding sleeves（212）
Between, second connecting plate（20）Lower surface and supporting rod（26）Top be fixedly connected, the supporting rod（26）Bottom
End and the second thread cap（27）Upper surface be fixedly connected.
6. a kind of agricultural aircraft for being convenient for changing battery according to claim 5, it is characterised in that：Second spiral shell
Line cap（27）Internal thread is connected with the second threaded post（29）, second threaded post（29）Positive one end and the second stubborn ring（28）
The one end at the back side is fixedly connected, the aircraft fuselage（1）Front open up it is fluted（31）, the groove（31）Inside it is provided with
Third thread cap（30）, the third thread cap（30）With the second thread cap（27）The diameter of inner ring is identical, the third screw thread
Cap（30）Quantity be two, and two third thread caps（30）It is located at aircraft fuselage（1）Front and back.
7. a kind of agricultural aircraft for being convenient for changing battery according to claim 1, it is characterised in that：The aircraft
Fuselage（1）The four corners of outer surface have been fixedly connected with support plate（32）, the support plate（32）Upper surface be provided with spiral
Paddle（33）, the aircraft fuselage（1）Lower surface and pedestal（15）Upper surface be fixedly connected, the pedestal（15）Shape
For hemispherical, the pedestal（15）The four corners of lower surface have been fixedly connected with support leg（22）.
8. a kind of agricultural aircraft for being convenient for changing battery according to claim 1, it is characterised in that：The telescopic rod
（18）Including shell（1801）, the shell（1801）Upper surface offer the second through-hole（1805）, second through-hole
（1805）Inside it is provided with support column（1804）, the support column（1804）Bottom end and slide plate（1802）Upper surface fix connect
It connects, the slide plate（1802）Left and right ends be slidably connected at two sliding slots respectively（1803）It is interior, and two sliding slots（1803）Point
Shell is not opened in it（1801）The left and right sides of inner wall, the support column（1804）Top and the first connecting plate（13）Following table
Face is fixedly connected, the shell（1801）Lower surface and shell（6）Upper surface be fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810523331.1A CN108791908A (en) | 2018-05-28 | 2018-05-28 | A kind of agricultural aircraft for being convenient for changing battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810523331.1A CN108791908A (en) | 2018-05-28 | 2018-05-28 | A kind of agricultural aircraft for being convenient for changing battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108791908A true CN108791908A (en) | 2018-11-13 |
Family
ID=64090502
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810523331.1A Pending CN108791908A (en) | 2018-05-28 | 2018-05-28 | A kind of agricultural aircraft for being convenient for changing battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108791908A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771855A (en) * | 2022-06-22 | 2022-07-22 | 江苏云端智能科技有限公司 | Unmanned aerial vehicle multi-degree-of-freedom aerial photography device and aerial photography method |
-
2018
- 2018-05-28 CN CN201810523331.1A patent/CN108791908A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114771855A (en) * | 2022-06-22 | 2022-07-22 | 江苏云端智能科技有限公司 | Unmanned aerial vehicle multi-degree-of-freedom aerial photography device and aerial photography method |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20181113 |
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| WD01 | Invention patent application deemed withdrawn after publication |