CN209396044U - A kind of unmanned plane sowing apparatus - Google Patents
A kind of unmanned plane sowing apparatus Download PDFInfo
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- CN209396044U CN209396044U CN201821997279.5U CN201821997279U CN209396044U CN 209396044 U CN209396044 U CN 209396044U CN 201821997279 U CN201821997279 U CN 201821997279U CN 209396044 U CN209396044 U CN 209396044U
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Abstract
The utility model discloses a kind of unmanned plane sowing apparatus, including unmanned plane and it is mounted in sowing on unmanned plane and component and sows component；Component of sowing includes kind of a case lid, carries plants case, diversion pipe and flow restriction baffle, kind of box top is carried to be fixedly connected with kind case lid, and it is fixed below the rotor rack of unmanned plane by kind of case lid, diversion pipe is connected to the bottom for carrying plants case, it is equipped with electronic flow restriction baffle at diversion pipe and load plants case docking, the flow of sowing that the adjustment of water conservancy diversion tube section carries plants case is controlled by flow restriction baffle；Sowing component includes sowing mounting plate and motor-driven sowing disk by sowing, mounting plate is sowed to be fixed on by dismountable pipe clamp on the rod piece of unmanned plane support frame, it sows motor and is fixed on and sow on mounting plate, and be sequentially connected with relative to the disk of sowing for sowing mounting plate rotation setting, the diversion pipe for component of sowing, which is located at, to be sowed above disk.Utility model device is structurally reasonable, can carry out corresponding adjusting for the effect of sowing of different seeds, guarantee the optimization for sowing effect.
Description
Technical field
The utility model belongs to agricultural seeder equipment, and in particular to a kind of unmanned plane sowing apparatus.
Background technique
Agricultural mechanization development is the necessary condition of modern agricultural development.It is a more difficult technology that seed, which is sowed, because
More difficult to control to sow density, if it is excessive to sow density, it is too poor to will lead to ontogeny, easily lodges；If density is too low,
It will lead to Severe Reduction.It sows to be broadly divided into manpower and sow at present and be sowed with machinery, manpower sows not only large labor intensity, work
Time is long, and the assurance of certain experiences is needed for the control for sowing density, and new hand, which be easy to cause, sows non-uniform phenomenon.
Machinery, which is sowed, is broadly divided into man-hour manually hand-held formula machinery and land machinery, and hand-held machine needs manually to bear to be sowed under seed,
Large labor intensity, while inefficient, land machinery is suitble to sow with large area, high-efficient, but in the presence of it is difficult, to broadcasting
Kind landform requires strictly, and weight is big, is easy the disadvantages of damaging to soil reclamation.
With the progress of science and technology, emerging unmanned plane starts to be applied in mechanization of agriculture, it is powerful nobody
Machine has the characteristics that structure is simple, small in size, light-weight, load-carrying is big, easy to operate, and application is very extensive, such as application No. is
201410455577.1 Chinese patent disclose a kind of precise sowing operating system and method based on unmanned aerial vehicle platform, use
Single rotor unmanned plane has carried out wind field sowing as platform；Application No. is 201521123128.3 Chinese patents to disclose one kind
Unmanned seeder combined with fertilising apparatus designs the sowing structure of UAV flight, but when mouth of sowing is smaller, and leakage kind effect is not
Good, while mouth of sowing is fixed relative to the position for sowing disk, falling within seed, to sow disk position immutable, and seed is fallen within
The position of disk has a significant impact for finally sowing effect, will cause sow away seed distribution it is substantially stationary, parameter can
Tonality is not high.
Utility model content
The technical issues of the utility model solves is: for existing unmanned plane in the technical drawbacks described above of agricultural seeder,
A kind of novel unmanned plane sowing apparatus is provided, promotes to can change while the even drop down of seed and sows mouth relative to sowing
The position of component, wide adaptability is good to terrain adaptability, high-efficient.
The utility model adopts the following technical solution realizes:
A kind of unmanned plane sowing apparatus including unmanned plane 1 and is mounted in sowing on unmanned plane 1 and component 2 and sows group
Part 3；
The component 2 of sowing includes kind of a case lid 21, carries plants case 22, diversion pipe 28 and flow restriction baffle 210, the load plants case
22 tops are fixedly connected with kind case lid 21, and are fixed below the rotor rack of unmanned plane 1 by kind of case lid 21, the diversion pipe
28 are connected to the bottom for carrying plants case 22, are equipped with electronic flow restriction baffle 210 at the diversion pipe 28 and load 22 docking of plants case, pass through
Flow restriction baffle 210 controls the flow of sowing that the adjustment of water conservancy diversion tube section carries plants case；
The component 3 of sowing includes sowing mounting plate 32 and sowing disk 37 by sow that motor 31 drives, described to sow
Mounting plate 32 is fixed on the rod piece of unmanned plane support frame 4 by dismountable pipe clamp, it is described sow motor 31 and be fixed on sow
On mounting plate 32, and it is sequentially connected with relative to the disk 37 of sowing for sowing the rotation setting of mounting plate 32, the water conservancy diversion of the component 2 of sowing
Pipe 28, which is located at, sows 37 top of disk.
Further, the unmanned plane support frame 4 includes strut 41 and cross bar 42, the rotation of the strut 41 and unmanned plane 1
Wing rack is fixedly connected, and is used to support entire unmanned plane 1, the cross bar 42 by the first pipe clamp 43 be connected horizontally on strut 41 it
Between, the mounting plate 32 of sowing is fixed on cross bar 42 by the second pipe clamp 44.
Further, it is described sow mounting plate 32 be equipped with adjust the fixed position of the second pipe clamp 44 sow component mounting groove
311, the axially staggered setting for sowing component mounting groove 311 Yu cross bar 42, second pipe clamp 44 is fixed by connector
In sowing component mounting groove 311.
Further, the component 3 of sowing further includes sowing platform 36, it is described sow platform 36 and be fixed on sow mounting plate
It 32 and sows between disk 37, which is provided with around the baffle of disk 37 circumferentially is sowed, the baffle is equipped with and sows opening, described
It sows disk 37 and is radially disposed with and sow blade 38.
Further, described sow is connected with positioning cover plate 314 on platform 36, and the lid of positioning cover plate 314, which is mounted in, to be sowed
On platform 36, and with sow between platform 36 at least two turned positions positioning connection structure；The diversion pipe 28
End is docked in the hole location on positioning cover plate 314 by the fixation of flexible steel in flat section tubing 220, is docked with the disk 37 of sowing of lower section.
Further, it is described sow on mounting plate 32 that setting fine tuning sows 36 position of platform sow stage+module slot 310.
In a kind of unmanned plane sowing apparatus of the utility model, the component 2 of sowing further includes stirring shaft 26, described to stir
In the load plants case 22 of 210 top of the rotation setting of moving axis 26 flow restriction baffle, the stirring shaft 26 is sequentially connected with stirring motor 24, leads to
Cross adjustment seed fall within 26 velocity of rotation of relative position and stirring shaft, 210 opening width of flow restriction baffle sowed on disk 37 can
To realize that the uniformity of variable grain seed is sowed.
Further, the outlet at bottom fixed sleeves that the load plants case 22 is docked with diversion pipe 28 are connected to latch segment 27, institute
It states and fixes stirring motor mounting plate 23 and servo motor mounting plate 211 on latch segment 27 respectively, drive the agitation electricity of stirring shaft 26
Machine 24 is fixedly mounted on stirring motor mounting plate 23, and the servo motor 212 of driving flow restriction baffle 210 is fixedly mounted on servo electricity
On machine mounting plate 211.
Further, the swing of flow restriction baffle 210 is mounted on latch segment 27, passes through swing arm 218 and servo motor 212
Transmission connection, the flow restriction baffle 210 is using the motor shaft of servo motor 212 as oscillation center.
Further, 27 bottom of latch segment is fixed with the mounting cylinder being coaxial docking with load 22 outlet at bottom of plants case
29, the diversion pipe 28 is fixedly attached with mounting cylinder 29.
Further, the plants case 22 that carries is equipped with the seed inlet 213 for adding seed.
The utility model uses multi-rotor unmanned aerial vehicle, will sow and component and sows the rotor that component is separately fixed at unmanned plane
In rack and support frame, whole device is structurally reasonable, and setting stirring shaft and flow restriction baffle, can be effectively prevented card in device of sowing
Kind, and item adjusting can be carried out to flow of sowing；Mouthful position of sowing for sowing the opposite component of sowing of disk for sowing component can be with
It is adjusted, can be adjusted according to the parameter of sowing of different seeds, be conducive to sow effect progress for different seeds
It is corresponding to adjust, guarantee the optimization for sowing effect.
In addition, the utility model is also applied for sowing for granular solid fertilizer simultaneously.
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Detailed description of the invention
Fig. 1 is the unmanned plane sowing apparatus overall structure diagram in embodiment.
Fig. 2 is the component structure diagram of sowing in embodiment.
Fig. 3 is the load plants case structural schematic diagram in embodiment.
Fig. 4 is the kind case lid structural schematic diagram in embodiment.
Fig. 5 is the flow restriction baffle structural schematic diagram in embodiment.
Fig. 6 is to sow component structure diagram in embodiment.
Fig. 7 is to sow dish structure schematic diagram in embodiment.
Fig. 8 is to sow unit installing board structural schematic diagram in embodiment.
Fig. 9 is that the position of sowing sowed on disk in embodiment adjusts schematic diagram.
Figure label:
1- unmanned plane,
2- sows component,
21- kind case lid, 22- load plants case, 23- stirring motor mounting plate, 24- stirring motor, 25- stir shaft coupling, and 26- is stirred
Moving axis, 27- latch segment, 28- diversion pipe, 29- mounting cylinder, 210- flow restriction baffle, 211- servo motor mounting plate, 212- servo electricity
Machine, 213- seed inlet, the first connecting column of 214-, 215- stirring shaft entrance, 216- kind case lid fixation hole, 217- carry plants case and fix
Hole, 218- swing arm, 219- splined hole, 220- flexible steel in flat section tubing；
3- sows component,
31- sows motor, and 32- sows mounting plate, and 33- sows shaft coupling, the second connecting column of 34-, 35- output shaft, and 36- is broadcast
Platform is spread, 37- sows disk, and 38- sows blade, 39- tack hole, and 310- sows stage+module slot, and 311- sows component mounting groove,
312- sows motor installing hole, and 313- sows motor delivery outlet, 314- positioning cover plate, 315- positioning screw, 316- regulating tank；
4- unmanned plane support frame,
41- strut, 42- cross bar, the first pipe clamp of 43-, the second pipe clamp of 44-.
Specific embodiment
Embodiment
Referring to Fig. 1, the unmanned plane sowing apparatus in diagram is the preferred embodiment of the utility model, specifically include unmanned plane 1,
Sow component 2, sow 4 four parts of component 3 and unmanned plane support frame, wherein unmanned plane 1 use six rotor wing unmanned aerial vehicles, provide whole
The flying power of a sowing apparatus can also require the multi-rotor unmanned aerial vehicle for using different parameters according to the load-carrying of practical application；
Component 2 of sowing is fixed below the rotor rack of unmanned plane 1, for storing the seed sowed and by seed water conservancy diversion to sowing group
Part 3；Unmanned plane support frame 4 is fixed on the bottom of unmanned plane rotor rack, symmetrically connect including the rotor rack with unmanned plane
Two groups of struts 41, the setting of strut 41 is identical as existing unmanned plane support frame structure, and unmanned plane, this implementation are supported when for landing
Example two parallel cross bars 42 of connection setting also between two groups of struts 41, sow component 3 and are fixedly mounted on cross bar 42, be used for
It receives to sow and seed that component 2 is fallen and sow seed by rotation centrifugal force.
It is fixedly connected between cross bar 42 and strut 41 by the first pipe clamp 43, it is fixed by the second pipe clamp 44 to sow component 3
On cross bar 42, pipe clamp 43 using screw locking detachable pipe clamp, using to adjust group can be sowed by disassembly pipe clamp
Position of the part 3 on unmanned plane support frame 4, and then realize the relative position adjustment for sowing component 3 between component 2 of sowing.
The organization plan and control principle of unmanned plane 1 can refer to existing multi-rotor unmanned aerial vehicle, and the present embodiment is not done herein
It repeats.
The specific structural features for component 2 of sowing are described in detail below in conjunction with Fig. 2 to Fig. 5.
Component 2 of sowing specifically includes kind of case lid 21, carries plants case 22, stirring motor mounting plate 23, stirring motor 24, agitation connection
Axis device 25, stirring shaft 26, latch segment 27, diversion pipe 28, mounting cylinder 29, flow restriction baffle 210, servo motor mounting plate 211, servo
Motor 212, seed inlet 213, the first connecting column 214.
As shown in Figures 2 and 3, it carries 22 top of plants case to be fixedly connected with kind case lid 21, and is fixed on by kind of a case lid 21
Below the rotor rack of unmanned plane 1, the rotor rack center that unmanned plane 1 is arranged in plants case 22 as far as possible is carried, keeps group of sowing
The center of gravity of part and the center of unmanned plane 1 are conducive to unmanned plane in the gesture stability of control sowing flight on same vertical direction.
As shown in connection with fig. 4, it plants and is provided with kind of case lid fixation hole 216 on case lid 21 and carries plants case fixation hole 217, kind case lid 21 uses screw thread
Connector is fixedly connected by kind of case lid fixation hole 216 with the rotor bottom of the frame of unmanned plane 1, carries plants case 22 using the first connection
Column 214 is fixedly connected by carrying plants case fixation hole 217 with kind case lid 21.
It is provided with and communicated with seed inlet 213 in the side for carrying plants case 22, can not have to remove kind of case lid or carry the feelings of plants case
Under condition to carry plants case 22 inside add seed.
It is funnel-shaped to carry the setting of 22 bottom of plants case, funnel bottom opening is docked with diversion pipe 28, will be carried by diversion pipe 28
Seed drainage inside plants case 22, which drops into, sows on component 3.Current limiting is set with the place of docking for carrying plants case 22 in diversion pipe 28
Baffle 210, the flow restriction baffle 210 are driven by servo motor 212, are swung between diversion pipe 28 and load plants case 22, are adjusted kind
Son enters the flow area inside diversion pipe 28 from plants case 22 is carried, and can control the opening and closing for component 2 of sowing, simultaneously also
The quantity control that seed is sowed can be realized by adjusting seed circulation section.
Specifically, being connected to a latch segment carrying the funnel bottom outlet fixed sleeves that plants case 22 is docked with diversion pipe 28
27,27 bottom of latch segment, which is connected through a screw thread, fixes a mounting cylinder 29, and mounting cylinder 29 and load 22 outlet at bottom of plants case are coaxially right
It connects, diversion pipe 28 is socketed in 29 bottom of mounting cylinder, and limits by the way that bolt is fixed.Servo electricity is fixed in the side of latch segment 27
Machine mounting plate 211, servo motor 212 are fixedly mounted on servo motor mounting plate 211, as shown in connection with fig. 5, flow restriction baffle 210
With a circular portion identical with 22 outlet at bottom section of plants case is carried, it is provided with the receiving part on latch segment 27 and is carrying
The slot position swung laterally at 22 outlet at bottom of plants case, the part connect a swing arm 218, and swing arm 218 extends to 27 outside of latch segment
211 bottom of servo motor mounting plate, and with servo motor 212 be sequentially connected, utilize the rotate driving current limliting of servo motor 212
The swing of baffle 210, which is mounted on, carries 22 outlet at bottom of plants case.Splined hole 219, the motor of servo motor 212 are machined in swing arm 218
Matched spline is processed on axis, is directly sequentially connected with swing arm 218 by spline fitted, so that flow restriction baffle 210 is to watch
It takes and is swung centered on the motor shaft of motor 212.
Load plants case 22 above flow restriction baffle 210 is internally provided with stirring shaft 26, and the rotation setting current limliting of stirring shaft 26 is kept off
In the load plants case 22 of 210 top of plate, bending thereon forms the agitation blades that agitation carries 22 internal seeds of plants case, and the other end, which passes through, to be carried
The stirring shaft entrance 215 and external stirring motor 24 being arranged on inside plants case are sequentially connected, and the uniformity sowed is effectively ensured.
Stirring motor mounting plate 23 is fixedly connected on the other side of latch segment 27, stirring motor 24 is fixedly mounted on stirring motor peace
In loading board 23, the motor shaft of stirring motor 24 is sequentially connected by agitation shaft coupling 25 and stirring shaft 26, and will stir shaft coupling
25 both ends are locked with the motor shaft of stirring motor and stirring shaft by screw respectively.
The specific structural features for sowing component 3 are described in detail below in conjunction with Fig. 6 to Fig. 8.
It sows component 3 and specifically includes and sow motor 31, sow mounting plate 32, sow shaft coupling 33, is the second connecting column 34, defeated
Shaft 35 sows platform 36, sows disk 37, sows blade 38.It wherein sows 32 bottom of mounting plate and the second pipe clamp 44 is fixedly installed,
And be fixed on the cross bar 42 of unmanned plane support frame 4 by the second pipe clamp 44, sowing disk 37 is disk, is provided with several groups
Radially distributed sows blade 38, as shown in fig. 7, sowing disk 37 and sowing the transmission connection of motor 31, rotational installation is in sowing
The top of mounting plate 32 is sowed motor 31 and is mounted on and sows 32 bottom of mounting plate, and is connected through a screw thread part and is fixed on and sow installation
Sowing in motor installing hole 312 on plate 32, the motor shaft for sowing motor 31 pass through sow on mounting plate 32 to sow motor defeated
Portal 313, and be sequentially connected by sowing shaft coupling 33 and output shaft 35, the center location for sowing disk 37 is machined with a tack
Hole 39 is sowed disk 37 and is mounted on the corresponding flush configuration of output shaft 35 by 39 turning set of tack hole, sows motor 31 and pass through
The driving of tack drive mechanism is sowed disk 37 and is rotated.
It sows platform 36 and is fixed on and sow mounting plate 32 and sow between disk 37, have around sowing disk 37 circumferentially
Baffle, baffle is equipped with and sows opening, falls in the seed sowed on disk 37 of rotation under the action of the centrifugal force along sowing blade
38 are displaced outwardly, sow platform 36 baffle guarantee rotation sow disk 37 by thereon sow opening in the same direction into
Row seed is sowed.
28 top of diversion pipe is docked along the vertical direction with plants case 22 is carried, and the other end exports transitional slope in the horizontal direction, this
Sample is avoided falling on vertically from the seed of diversion pipe 28 out and be sowed on component, causes excessively to bounce and jump out and sow disk.Meanwhile
It sows and is connected with positioning cover plate 314 on platform 36, the circumferential size phase that positioning cover plate 314 is surrounded with the baffle for sowing platform 36
Together, it can just cover on the baffle for sowing platform 36, sow platform 36 equipped with a connection hole location, the end of diversion pipe 28
End is docked in the hole location on positioning cover plate 314 by the fixation of flexible steel in flat section tubing 220, and the seed in diversion pipe 28 is drained docking
It is sowed on disk 37 to lower section, the bellows of plastic material can be used in flexible steel in flat section tubing 220.Positioning cover plate 314 can sow it is flat
Rotation adjustment is carried out on platform 36 to be provided on positioning cover plate 314 in conjunction with shown in Fig. 9 with the relative angle for sowing platform 36
Arc regulating tank 316 identical with the baffle top arc of platform 36 is sowed, is equipped in the top corresponding position for sowing platform 36
Threaded hole passes through regulating tank 316 by positioning screw 315 and connect with the threaded hole for sowing 36 top of platform, can be by locating cover
Plate 314 is located by connecting on the multiple turned positions sowed on platform 36 within the scope of the curved angle of regulating tank 316, has adjusted kind
Son falls in the position of sowing sowed on disk 37, and the flexible steel in flat section tubing 220 between diversion pipe 28 and positioning cover plate 314 can adapt to fixed
The rotation adjustment of position cover board 314.
Flexible steel in flat section tubing nozzle (mouth of sowing) ordinary circumstance that diversion pipe 28 extends is rotated clockwise according to disk 37 is sowed,
Mouth right upper half of XY coordinate system in Fig. 9 of sowing of diversion pipe 28, at coordinate points (5,6), mouth of sowing is relative to sowing disk 37
Position can be fixed by sowing positioning cover plate 314 on platform 36 and positioning screw 315.It is fallen within by adjusting seed and sows disk
Any grain seed may be implemented in 26 velocity of rotation of relative position and stirring shaft, 210 opening width of flow restriction baffle on 37
Uniformity is sowed.
In the present embodiment sow component 3 can adjust and sow component 2 diversion pipe 28 relative position.It is specific to adjust
Whole structure is as follows: as shown in figure 8, processing sows stage+module slot 310 equipped with two groups and sows component on sowing mounting plate 32
Mounting groove 311 is strip kidney slot, is fixed on wherein the second pipe clamp 44 is connected through a screw thread part and sows component mounting groove 311
In, part adjusting can be connected through a screw thread and be mounted on any position sowed on component mounting groove 311, while passing through the second pipe clamp
44 are fixed on mounting plate 32 is entirely sowed on the cross bar 42 of unmanned plane support frame 4, wherein sowing component mounting groove 311 and cross bar
Be mutually perpendicular between 42, so respectively the clip position by adjusting the second pipe clamp 44 on cross bar 42 and adjustment the second pipe clamp
44 adjust in the plan-position that the fixation position for sowing component mounting groove 311 may be implemented to sow mounting plate 32.It sows simultaneously flat
The bottom plate of platform 36 is supported and fixed on and is sowed on stage+module slot 310 by the second connecting column 34, can finely tune sow platform 36 with
It sows existing to position between disk 37.
Motor control mode in the present embodiment, including stirring motor 24, servo motor 212 and to sow motor 31 logical
The power module and remote control module crossed on unmanned plane 1 are powered and control, power supply and wireless controlled particularly with regard to motor
System is conventional electric machines control technology, and those skilled in the art can carry out conventional design according to the parameter of electric machine of selection, this
Embodiment is herein without repeating.
The specific work process sowed through this embodiment the following steps are included:
A, to carrying in plants case after loading seed, control unmanned plane 1 keeps certain height and hovers after taking off；
B, motor 31 is sowed by being remotely controlled the stirring motor 24 started in component 2 of sowing and sowing in component；
C, the servo motor 212 started in component 2 of sowing goes to certain angle, enters material according to certain flow and broadcasts
Sowing in disk 37 in component is spread, is adjusted to suitably sow motor speed, seed, which is sowed, to be sowed blade 38 and dish out on disk 37；
D, unmanned plane flies automatically according to setting path parameter, realizes sowing for seed；
E, unmanned plane returns to takeoff point hovering after completing appointed task, and the servo motor 212 in component of sowing is resetted, is closed
It the stirring motor 24 that closes in component of sowing and sows in component and sows motor 31；
F, the landing of control unmanned plane, work terminate.
The advantages of embodiment above describes the basic principles and main features of the utility model and the utility model, current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the concrete operating principle of the utility model, on the premise of not departing from the spirit and scope of the utility model, this reality
It will also have various changes and improvements with novel, these various changes and improvements fall within the scope of the claimed invention, this
Utility model is claimed range and is defined by the appending claims and its equivalent thereof.
Claims (10)
1. a kind of unmanned plane sowing apparatus, it is characterised in that: including unmanned plane (1) and be mounted in sowing on unmanned plane (1)
It component (2) and sows component (3)；
The component of sowing (2) includes kind of case lid (21), carries plants case (22), diversion pipe (28) and flow restriction baffle (210), described
It carries and is fixedly connected at the top of plants case (22) with kind case lid (21), and be fixed on the rotor rack of unmanned plane (1) by kind of case lid (21)
Lower section, the diversion pipe (28) are connected to the bottom for carrying plants case (22), set at the diversion pipe (28) and load plants case (22) docking
There are electronic flow restriction baffle (210), controls the flow of sowing that the adjustment of water conservancy diversion tube section carries plants case by flow restriction baffle (210)；
It is described sow component (3) include sow mounting plate (32) and by sow motor (31) driving sow disk (37), it is described
Mounting plate (32) is sowed to be fixed on by dismountable pipe clamp on the rod piece of unmanned plane support frame (4), it is described to sow motor (31)
It is fixed on and sows on mounting plate (32), and be sequentially connected with relative to sow disk (37) for sowing mounting plate (32) rotation setting, institute
The diversion pipe (28) for stating component of sowing (2), which is located at, to be sowed above disk (37).
2. a kind of unmanned plane sowing apparatus according to claim 1, it is characterised in that: unmanned plane support frame (4) packet
Strut (41) and cross bar (42) are included, the strut (41) is fixedly connected with the rotor rack of unmanned plane (1), is used to support entire nothing
Man-machine (1), the cross bar (42) is connected horizontally between strut (41) by the first pipe clamp (43), described to sow mounting plate (32)
It is fixed on cross bar (42) by the second pipe clamp (44).
3. a kind of unmanned plane sowing apparatus according to claim 2, it is characterised in that: described sow sets on mounting plate (32)
Have and adjusts sowing component mounting groove (311) for the second pipe clamp (44) fixed position, it is described to sow component mounting groove (311) and cross bar
(42) axially staggered setting, second pipe clamp (44) is fixed on by connector sows in component mounting groove (311).
4. a kind of unmanned plane sowing apparatus according to claim 3, it is characterised in that: the component (3) of sowing further includes
Sow platform (36), it is described sow platform (36) and be fixed on sow mounting plate (32) and sow between disk (37), which is provided with and enclose
Around the baffle of disk (37) circumferentially is sowed, the baffle is equipped with and sows opening, and the disk (37) of sowing radially is arranged
Sow blade (38).
5. unmanned plane sowing apparatus according to claim 4, it is characterised in that: described sow is connected with calmly on platform (36)
Position cover board (314), positioning cover plate (314) lid, which is mounted in, to be sowed on platform (36), and is had extremely with sowing between platform (36)
The positioning connection structure of few two turned positions；The end of the diversion pipe (28) passes through flexible steel in flat section tubing (220) fixed docking
In the hole location on positioning cover plate (314), docked with the disk (37) of sowing of lower section.
6. a kind of unmanned plane sowing apparatus according to claim 5, it is characterised in that: described sow sets on mounting plate (32)
That sets that fine tuning sows platform (36) position sows stage+module slot (310).
7. a kind of unmanned plane sowing apparatus according to claim 1 to 6, it is characterised in that: the component of sowing
It (2) further include stirring shaft (26), in the load plants case (22) above stirring shaft (26) rotation setting flow restriction baffle (210), institute
Stirring shaft (26) and stirring motor (24) are stated to be sequentially connected, fallen within by adjusting seed the relative position sowed on disk (37), with
And stirring shaft (26) velocity of rotation, flow restriction baffle (210) opening width may be implemented the uniformity of variable grain seed and sow.
8. a kind of unmanned plane sowing apparatus according to claim 7, it is characterised in that: the load plants case (22) and diversion pipe
(28) the outlet at bottom fixed sleeves docked are connected to latch segment (27), fix stirring motor installation on the latch segment (27) respectively
Plate (23) and servo motor mounting plate (211), the stirring motor (24) of driving stirring shaft (26) are fixedly mounted on stirring motor peace
In loading board (23), the servo motor (212) of driving flow restriction baffle (210) is fixedly mounted on servo motor mounting plate (211).
9. a kind of unmanned plane sowing apparatus according to claim 8, it is characterised in that: the flow restriction baffle (210) swings
It is mounted on latch segment (27), is sequentially connected by swing arm (218) and servo motor (212), the flow restriction baffle (210) is to watch
The motor shaft for taking motor (212) is oscillation center.
10. a kind of unmanned plane sowing apparatus according to claim 9, it is characterised in that: latch segment (27) bottom is solid
Fixed to be equipped with the mounting cylinder (29) being coaxial docking with load plants case (22) outlet at bottom, the diversion pipe (28) and mounting cylinder (29) are fixed
Socket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821997279.5U CN209396044U (en) | 2018-11-30 | 2018-11-30 | A kind of unmanned plane sowing apparatus |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821997279.5U CN209396044U (en) | 2018-11-30 | 2018-11-30 | A kind of unmanned plane sowing apparatus |
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| CN209396044U true CN209396044U (en) | 2019-09-17 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113460304A (en) * | 2021-07-20 | 2021-10-01 | 江苏大学 | Unmanned aerial vehicle rice device of flewing |
| CN113859546A (en) * | 2021-10-21 | 2021-12-31 | 四川农业大学 | Seed and fertilizer dual-purpose broadcasting device of multi-rotor-wing plant protection unmanned aerial vehicle |
-
2018
- 2018-11-30 CN CN201821997279.5U patent/CN209396044U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113460304A (en) * | 2021-07-20 | 2021-10-01 | 江苏大学 | Unmanned aerial vehicle rice device of flewing |
| CN113859546A (en) * | 2021-10-21 | 2021-12-31 | 四川农业大学 | Seed and fertilizer dual-purpose broadcasting device of multi-rotor-wing plant protection unmanned aerial vehicle |
| CN113859546B (en) * | 2021-10-21 | 2023-05-09 | 四川农业大学 | Seed and fertilizer dual-purpose sowing device of multi-rotor plant protection unmanned aerial vehicle |
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Address after: 410000 room 603, building 4, Xingwei Chuangxin garden, Changsha Economic and Technological Development Zone, Changsha City, Hunan Province Co-patentee after: Hunan Agricultural University Patentee after: Hunan star Sol science and technology of aviation company limited Address before: 410100 Wufeng Mechanical and Electrical Industrial Park Complex Building 315, No. 9 East 11 Road, Changsha Economic Development Zone, Yuelu District, Changsha City, Hunan Province Co-patentee before: Hunan Agricultural University Patentee before: Hunan star Sol science and technology of aviation company limited |