CN207235412U - UAV system seeder - Google Patents

UAV system seeder Download PDF

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Publication number
CN207235412U
CN207235412U CN201721287329.6U CN201721287329U CN207235412U CN 207235412 U CN207235412 U CN 207235412U CN 201721287329 U CN201721287329 U CN 201721287329U CN 207235412 U CN207235412 U CN 207235412U
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CN
China
Prior art keywords
seeder
demarcation strip
sowing
rotation axis
uav system
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Active
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CN201721287329.6U
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Chinese (zh)
Inventor
卓士远
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Ocean Foundation Electronic Engineering Co Ltd
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Tianjin Ocean Foundation Electronic Engineering Co Ltd
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Priority to CN201721287329.6U priority Critical patent/CN207235412U/en
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Publication of CN207235412U publication Critical patent/CN207235412U/en
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Abstract

The utility model is created and provides a kind of UAV system seeder, and the seeder includes:Storage box, demarcation strip, retainer ring, sowing mechanism and transport mechanism, the demarcation strip is fixed on the inner wall of storage box, the retainer ring is fixed on the outer wall of storage box, and the sowing mechanism is located at the lower section of demarcation strip, and the transport mechanism is located at the top of demarcation strip;The sowing mechanism includes:Roller, the first rotation axis and some load kind plates, the load kind plate, which is uniformly distributed, to be fixed on roller, and the roller is fixedly connected with the first rotation axis.The utility model creates the UAV system seeder, not only reduces the labor intensity of work personnel, and improves speed of drilling and sowing stability, so as to improve sowing efficiency, reduces sowing cost.Meanwhile by controlling the speed of drilling of seeder and the flying speed of unmanned plane, additionally it is possible to realize the automation sowing of a variety of cropping patterns.

Description

UAV system seeder
Technical field
The invention belongs to unmanned plane apparatus field, more particularly, to a kind of UAV system seeder.
Background technology
The seeder of commercial type is mostly manually-operated equipment at present, and operating personnel need to have certain physical efficiency It could be sowed with strength using these seeders, limited to the use scope of seeder, while the work of operating personnel is strong Degree is also bigger, so as to influence to sow the efficiency and cost of work.
The content of the invention
In view of this, the invention is directed to a kind of UAV system seeder, to expand the use scope of sowing, drop The labor intensity of low operating personnel, improves the efficiency of sowing work, so as to reduce the cost of sowing work.
To reach above-mentioned purpose, what the technical solution of the invention was realized in:
A kind of UAV system seeder, the seeder include:Storage box, demarcation strip, retainer ring, sowing mechanism and biography Mechanism is sent, the demarcation strip is fixed on the inner wall of storage box, and the retainer ring is fixed on the outer wall of storage box, described Sowing mechanism be located at the lower section of demarcation strip, the transport mechanism is located at the top of demarcation strip;
The sowing mechanism includes:Roller, the first rotation axis and some load kind plates, the load kind plate are uniformly distributed It is fixed on roller, the roller is fixedly connected with the first rotation axis;
The transport mechanism includes:Sleeve, the second rotation axis and some transmission blades, the transmission blade are uniform Distribution is fixed on sleeve, and the sleeve is fixedly connected with the second rotation axis.
Further, the demarcation strip is the structure of intermediate recess.
Further, the demarcation strip is equipped with point kind of a mouth, and point kind of the mouth is located at the minimum point of demarcation strip.
Further, the center of point kind of the mouth is located on same plumb line with the second rotation axis, point kind of the mouth Center and the first rotation axis be located on same plumb line.
Further, the plane where the load kind plate and roller are tangent.
Further, the angle between transmission blade and the sleeve is acute angle.
Relative to the prior art, the UAV system seeder described in the invention has the advantage that:
UAV system seeder described in the invention, not only reduces the labor intensity of work personnel, and improves Speed of drilling and sowing stability, so as to improve sowing efficiency, reduce sowing cost.Meanwhile by controlling seeder Speed of drilling and unmanned plane flying speed, additionally it is possible to realize a variety of cropping patterns automation sowing.
Brief description of the drawings
The attached drawing for forming the part of the invention is used for providing further understanding the invention, present invention wound The schematic description and description made is used to explain the invention, does not form the improper restriction to the invention. In attached drawing:
Fig. 1 is the structure diagram of the UAV system seeder described in the invention embodiment.
Description of reference numerals:
1- storage boxes;11- stores mouth;2- demarcation strips;21- points of kind of mouths;3- sowing mechanisms;31- carries kind of a plate;32- rollers; The first rotation axis of 33-;4- transport mechanisms;41- transmits blade;42- sleeves;The second rotation axis of 43-;5- retainer rings.
Embodiment
The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments creates.
As shown in Figure 1, a kind of UAV system seeder, the seeder include:Storage box 1, demarcation strip 2, retainer ring 5th, sowing mechanism 3 and transport mechanism 4, the demarcation strip 2 are fixed on the inner wall of storage box 1, and the retainer ring 5 is fixed on On the outer wall of storage box 1, the sowing mechanism 3 is located at the lower section of demarcation strip 2, and the transport mechanism 4 is located at demarcation strip 2 Top;The seeder is fixed on unmanned plane by retainer ring 5.
The sowing mechanism 3 includes:Roller 32, the first rotation axis 33 and some load kind plates 31, the load kind plate 31 are uniformly distributed and are fixed on roller 32, and the roller 32 is fixedly connected with the first rotation axis 33;First rotation axis 33 are fixedly connected with motor, and motor drives roller 32 to rotate by the first rotation axis 33.The structure can be by controlling motor Rotating speed controls the purpose of seeder speed of drilling to realize.
The transport mechanism 4 includes:Sleeve 42, the second rotation axis 43 and some transmission blades 41, the transmission Blade 41, which is uniformly distributed, to be fixed on the sleeve 42, and the sleeve 42 is fixedly connected with the second rotation axis 43.Second rotation Shaft 43 is fixedly connected with motor, and motor is rotated by the second rotation axis 43 with moving sleeve 42.Transmission blade 41, which plays, constantly to be dialled The effect of dynamic seed, enables seed constantly to be fallen by point kind of a mouth 21.
The demarcation strip 2 is the structure of intermediate recess.The seed that the structure can make to be stored in storage box 1 is in itself weight Point kind of a mouth 21 is slided under the action of power.
The demarcation strip 2 is equipped with point kind of a mouth 21, and point kind of the mouth 21 is located at the minimum point of demarcation strip 2.The knot Structure can make the seed in storage box 1 to skid off storage box 1 by point kind of a mouth 21, seed will not be caused to accumulate.
The center of point kind of the mouth 21 is located on same plumb line with the second rotation axis 43, in point kind of the mouth 21 The heart and the first rotation axis 33 are located on same plumb line.The structure ensure that seed can smoothly leave storage box 1, then be carried Kind plate 31 is carried out seeder, realizes the purpose of sowing.
Plane and roller 32 where the load kind plate 31 is tangent.The structure can make the transmission kind that load kind plate 31 is stablized Son, will not cause seed arbitrarily to slide, it is uncontrolled so as to avoid the speed of drilling of seeder the problem of.
Angle between transmission blade 41 and the sleeve 42 is acute angle.
Seed is put into storage box 1 by storage mouth 11, seed is fallen by point kind of a mouth 21 under self gravitation effect, transmitted Blade 41 constantly stirs seed as the second rotation axis 43 rotates, and prevents seed from accumulating, and seed is carried after being fallen from point kind of a mouth 21 Kind plate 31 carries, and carries kind of plate 31 as the first rotation axis 33 rotates, and then seed slides from load kind plate 31, so as to depart from storage Case 1 completes sowing work.
The motor is connected by the controller of circuit and unmanned plane, it is achieved thereby that the sowing by controlling seeder The automation sowing that speed and the flying speed of unmanned plane are combined to realize a variety of cropping patterns.
The foregoing is merely the preferred embodiment of the invention, is not intended to limit the invention creation, all at this Within the spirit and principle of innovation and creation, any modification, equivalent replacement, improvement and so on, should be included in the invention Protection domain within.

Claims (6)

  1. A kind of 1. UAV system seeder, it is characterised in that:The seeder includes:Storage box (1), demarcation strip (2), fix Ring (5), sowing mechanism (3) and transport mechanism (4), the demarcation strip (2) is fixed on the inner wall of storage box (1), described Retainer ring (5) is fixed on the outer wall of storage box (1), and the sowing mechanism (3) is located at the lower section of demarcation strip (2), described Transport mechanism (4) is located at the top of demarcation strip (2);
    The sowing mechanism (3) includes:Roller (32), the first rotation axis (33) and some load kind plates (31), the load Kind plate (31), which is uniformly distributed, to be fixed on roller (32), and the roller (32) is fixedly connected with the first rotation axis (33);
    The transport mechanism (4) includes:Sleeve (42), the second rotation axis (43) and some transmission blades (41), it is described Transmission blade (41), which is uniformly distributed, to be fixed on sleeve (42), and the sleeve (42) is fixedly connected with the second rotation axis (43).
  2. 2. UAV system seeder according to claim 1, it is characterised in that:The demarcation strip (2) is intermediate recess Structure.
  3. 3. UAV system seeder according to claim 2, it is characterised in that:The demarcation strip (2) is equipped with a point kind Mouth (21), and point kind of the mouth (21) is located at the minimum point of demarcation strip (2).
  4. 4. UAV system seeder according to claim 3, it is characterised in that:The center of described point kind of mouth (21) and the Two rotation axis (43) are located on same plumb line, and the center of point kind of the mouth (21) is located at same lead with the first rotation axis (33) On vertical line.
  5. 5. UAV system seeder according to claim 1, it is characterised in that:Plane where the load kind plate (31) It is tangent with roller (32).
  6. 6. UAV system seeder according to claim 1, it is characterised in that:The transmission blade (41) and sleeve (42) angle between is acute angle.
CN201721287329.6U 2017-09-30 2017-09-30 UAV system seeder Active CN207235412U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721287329.6U CN207235412U (en) 2017-09-30 2017-09-30 UAV system seeder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721287329.6U CN207235412U (en) 2017-09-30 2017-09-30 UAV system seeder

Publications (1)

Publication Number Publication Date
CN207235412U true CN207235412U (en) 2018-04-17

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721287329.6U Active CN207235412U (en) 2017-09-30 2017-09-30 UAV system seeder

Country Status (1)

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CN (1) CN207235412U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112273029A (en) * 2020-10-28 2021-01-29 贵州理工学院 Outdoor cultivation device and cultivation method for artificial morchella

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112273029A (en) * 2020-10-28 2021-01-29 贵州理工学院 Outdoor cultivation device and cultivation method for artificial morchella

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