CN218537113U

CN218537113U - Straw decomposition agent spraying aircraft

Info

Publication number: CN218537113U
Application number: CN202223137333.8U
Authority: CN
Inventors: 陈钊; 魏德林; 陈喜强; 韦展堂; 杨梦芸; 吴定刚; 许永祥
Original assignee: Guangxi Chenhan Agricultural Development Co ltd
Current assignee: Guangxi Chenhan Agricultural Development Co ltd
Priority date: 2022-11-25
Filing date: 2022-11-25
Publication date: 2023-02-28
Anticipated expiration: 2032-11-25

Abstract

The utility model discloses a straw decomposing inoculant sprinkles aircraft belongs to and sprinkles aircraft technical field. An aircraft for spraying straw decomposition agent comprises a body, wherein the bottom end of the body is provided with two circular grooves. The utility model discloses be equipped with bounding wall, roof, round hole, stopper, use the spacing groove inner wall joint that fixed stopper outer wall in roof top and box bottom were seted up, use the top of bounding wall and the bottom mounting of roof, control pump extracts the inside medicament of box to the inner wall of connecting pipe, is equipped with connecting block, spout, shock attenuation pole, bonding board, and the outer wall that uses two bonding boards slides with the inner wall of spout respectively, uses the box top of filling with the medicament and bonds with the bottom of the ware body.

Description

Straw decomposition agent spraying aircraft

Technical Field

The utility model belongs to the technical field of scatter the aircraft, concretely relates to straw decomposition agent scatters aircraft.

Background

An aircraft for spraying straw decomposition agent is an aircraft device for spraying straw decomposition agent.

At present, a lot of straw decomposition agents are sprayed on the market, but in a common straw decomposition agent spraying aircraft, supporting legs of the aircraft are usually used for carrying a bucket loaded with a medicament to spray and irrigate, so that the joints of the supporting legs and the bucket are collided by external force, and the falling of the bucket is easily caused to influence the normal use of the device;

and the agent in the bucket is directly sprayed and irrigated, so that the agent for irrigating partial straws is too concentrated, the waste of straw surface irrigation is caused, and the using effect of the device is reduced.

Therefore, a straw decomposition agent spraying aircraft is needed, and the problem that in the prior art, a supporting leg of the aircraft is used for carrying a bucket loaded with a chemical to spray and irrigate, so that the joint of the supporting leg and the bucket is collided by external force, the bucket is easy to fall off, the chemical in the bucket is directly sprayed and irrigated, and partial chemical for watering the straw is too concentrated is solved.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a straw decomposing inoculant sprinkles aircraft to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme:

the utility model provides an aircraft is sprinkled to straw maturity agent, includes the ware body, two circular slots have been seted up to the bottom of the ware body, the bottom of the ware body bonds there is the box, the top of box is fixed with two cylinders, two the cylindrical outer wall all with the inner wall joint of circular slot, the inner wall bottom of box is equipped with the water pump, the play water end joint of water pump has the connecting pipe, the bottom of box is equipped with dispersion mechanism, dispersion mechanism includes the bounding wall, the top of bounding wall bonds there is the roof, the round hole has been seted up on the top of roof, the inner wall of round hole and the outer wall joint of connecting pipe, the top of roof is fixed with two stoppers, two spacing grooves have been seted up to the bottom of box, two the inner wall of spacing groove all with the outer wall joint of stopper, the inner wall joint of bounding wall has the orifice plate.

What need explain in the scheme is, the outer wall of the ware body is equipped with buffer gear, buffer gear includes two connecting blocks, two the one end of connecting block all is fixed with the outer wall of the ware body, two the other end of connecting block all slides with the outer wall of box, two the spout, two have all been seted up to one side of connecting block the inner wall one side of spout all is fixed with the shock attenuation pole, two the one end of shock attenuation pole all is fixed with bonding board, two one side of bonding board all bonds with the outer wall of box, two the outer wall of bonding board all slides with the inner wall of spout, two the outer wall of shock attenuation pole all is equipped with the spring, two the outer wall of spring all overlaps and is equipped with the ring cover.

It is further worth to explain that, the diameter size of the inner surface of the inner ring wall of the two circular grooves is matched with the diameter size of the outer surface of the outer ring wall of the cylinder, and the depth size of the inner wall of the two circular grooves is matched with the height size of the outer wall of the cylinder.

It should be further explained that, the height dimension of the outer wall of the two limiting blocks is matched with the depth dimension of the inner wall of the limiting groove, and the vertical cross-sectional area dimension of the outer wall of the two limiting blocks is matched with the vertical cross-sectional area dimension of the inner wall of the limiting groove.

Preferably, the size of the vertical cross-sectional area of the outer wall of the pore plate is matched with the size of the vertical cross-sectional area of the inner wall of the enclosing plate, and the diameter of the inner surface of the inner annular wall of the circular hole is matched with the diameter of the outer surface of the outer annular wall of the connecting pipe.

Preferably, the diameter of the outer surface of the outer ring wall of each of the two shock-absorbing rods is matched with the diameter of the inner surface of the inner ring wall of the spring.

Compared with the prior art, the utility model provides a straw maturity agent sprinkles aircraft has following beneficial effect:

(1) The utility model discloses a be equipped with the bounding wall, the roof, the round hole, the stopper, use the spacing groove inner wall joint that fixed stopper outer wall in roof top and box bottom were seted up, make the round hole inner wall joint that the roof top was seted up, use the top of bounding wall and the bottom mounting of roof, use the outer wall of orifice plate and the inner wall joint of bounding wall, the controller body flies appointed straw and sprinkles the region, the control water pump extracts the inside medicament of box to the inner wall of connecting pipe, be convenient for to the inside medicament extraction dispersion of box spout to the straw, avoid local straw to spout the medicine and concentrate.

(2) The utility model discloses a be equipped with the connecting block, the spout, the shock absorber pole, the bonding board, the outer wall that uses two bonding boards slides with the inner wall of spout respectively, make the outer wall extrusion shock absorber pole and the spring shrink of bonding board, use the box top of filling with the medicament and the bottom of the ware body to bond, loosen the spacing of bonding board, make one side of the reverse thrust drive bonding board of spring closely bond with the outer wall of box, the cushioning nature of improving means installation between to the box and the ware body, it leads to the junction not hard up to avoid the box to receive the collision, the practicality of improving means.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the separating structure of the case and the case body of the present invention;

fig. 3 is a schematic structural view of the dispersing mechanism of the present invention;

fig. 4 is a schematic view of the structure of the buffer mechanism of the present invention.

Description of the reference numerals:

1. a body; 11. a circular groove; 12. a box body; 13. a cylinder; 14. a water pump; 15. a connecting pipe; 2. a dispersing mechanism; 21. enclosing plates; 22. a top plate; 23. a circular hole; 24. a limiting block; 25. a limiting groove; 26. an orifice plate; 3. a buffer mechanism; 31. connecting blocks; 32. a chute; 33. a shock-absorbing lever; 34. bonding the board; 35. a spring; 36. a loop is provided.

Detailed Description

The present invention will be further described with reference to the following examples.

Please refer to fig. 1-4, the utility model provides a straw maturity agent sprinkle aircraft, including the ware body 1, two circular slots 11 have been seted up to the bottom of the ware body 1, the bottom of the ware body 1 bonds and has box 12, the top of box 12 is fixed with two cylinders 13, the outer wall of two cylinders 13 all is with the inner wall joint of circular slot 11, the inner wall bottom of box 12 is equipped with water pump 14, the play water outlet end joint of water pump 14 has connecting pipe 15, the bottom of box 12 is equipped with dispersion mechanism 2, the medicament that is convenient for take out water pump 14 spouts to the straw through the inner wall dispersion of orifice plate 26, avoid local spraying excessive, influence the normal use of device, dispersion mechanism 2 includes bounding wall 21, the top of bounding wall 21 bonds and has roof 22, round hole 23 has been seted up on the top of roof 22, the inner wall of round hole 23 and the outer wall joint of connecting pipe 15, the top of roof 22 is fixed with two stoppers 24, two spacing grooves 25 have been seted up to the bottom of box 12, the inner wall of two spacing grooves 25 all is in the joint with the outer wall joint of stopper 24, the inner wall joint of orifice plate 21 has 26.

Further as shown in fig. 1 and 4, it is worth specifically explaining that the outer wall of the container body 1 is provided with the buffer mechanism 3, the buffer mechanism 3 includes two connecting blocks 31, one end of each of the two connecting blocks 31 is fixed to the outer wall of the container body 1, the other end of each of the two connecting blocks 31 slides to the outer wall of the container body 12, one side of each of the two connecting blocks 31 is provided with a sliding groove 32, one side of the inner wall of each of the two sliding grooves 32 is fixed with a shock-absorbing rod 33, one end of each of the two shock-absorbing rods 33 is fixed with an adhesive plate 34, one side of each of the two adhesive plates 34 is adhered to the outer wall of the container body 12, the outer walls of the two adhesive plates 34 slide to the inner wall of the container body 32, the outer walls of the two adhesive plates 34 are sleeved with springs 35, the outer walls of the two springs 35 are sleeved with a ring 36, the outer walls of the two adhesive plates 34 slide to the inner walls of the sliding grooves 32 respectively, so that the outer walls of the adhesive plates 34 and the springs 35 shrink until the outer walls of the container body 12 slide to one end of the connecting block 31, so that the top end of the container body 12 is tightly adhered to the bottom of the container body 1, the container body 1 is loosened, and the container body 12 are prevented from being impacted by the impact on the container body 12.

Further as shown in fig. 2, it is worth specifically explaining that the inner surface diameters of the inner walls of the two circular grooves 11 are matched with the outer surface diameters of the outer walls of the cylinders 13, and the inner depth dimensions of the inner walls of the two circular grooves 11 are matched with the outer height dimensions of the cylinders 13, so that the outer walls of the cylinders 13 on the inner walls of the circular grooves 11 are tightly clamped, and the stability of the adhesion between the top end of the box body 12 and the bottom end of the box body 1 is improved.

The scheme has the following working processes: when the aircraft for spraying the straw decomposition agent is used, the outer walls of two bonding plates 34 slide with the inner wall of a sliding groove 32 respectively to enable the outer walls of the bonding plates 34 to extrude a shock absorption rod 33 and a spring 35 to shrink, then the top end of a box body 12 filled with the agent is bonded with the bottom end of the device body 1 to enable the outer wall of a cylinder 13 fixed at the top end of the box body 12 to be clamped with the inner wall of a circular groove 11 formed at the bottom end of the device body 1, the limiting of the bonding plates 34 is loosened to enable one side of the bonding plates 34 to be tightly bonded with the outer wall of the box body 12 through the driving of the reverse thrust of the spring 35, then the outer wall of a limiting block 24 fixed at the top end of a top plate 22 is clamped with the inner wall of a limiting groove 25 formed at the bottom end of the box body 12 to enable the inner wall of a circular hole 23 formed at the top end of a top plate 22 to be clamped, the top end of a surrounding plate 21 is fixed with the bottom end of the top plate 22, the outer wall of a hole plate 26 is clamped with the inner wall of the surrounding plate 21, finally the device body 1 is controlled to fly to a designated straw spraying area, a water pump 14 is controlled to pump the agent in the box body 12 to spray the inner wall of the connecting pipe 15, and the agent on the inner wall 26 clamped by the surrounding plate 21, and the straw is enabled to be sprayed to disperse the agent to be sprayed to the surrounding plate.

According to the working process, the following steps are known: the outer walls of the two bonding plates 34 respectively slide with the inner wall of the sliding groove 32 to enable the outer walls of the bonding plates 34 to extrude the shock absorption rod 33 and the spring 35 to contract, the top end of the box body 12 filled with the medicament is bonded with the bottom end of the box body 1, the outer wall of the cylinder 13 fixed at the top end of the box body 12 is clamped with the inner wall of the circular groove 11 arranged at the bottom end of the box body 1, the limit of the bonding plates 34 is loosened to enable one side of the bonding plates 34 driven by the reverse thrust of the spring 35 to be tightly bonded with the outer wall of the box body 12, the buffering performance of the device for mounting between the box body 12 and the box body 1 is improved, the situation that the joint of the box body 12 is loosened due to collision and the normal mounting of the box body 12 is influenced is avoided, use the spacing groove 25 inner wall joint that stopper 24 outer wall of roof 22 top fixed and box 12 bottom were seted up, make the round hole 23 inner wall joint that roof 22 top was seted up, use the top of bounding wall 21 and the bottom mounting of roof 22, use the outer wall of orifice plate 26 and the inner wall joint of bounding wall 21, controller body 1 flies appointed straw and spouts the region, control water pump 14 extracts the inside medicament of box 12 to the inner wall of connecting pipe 15, make the medicament spout via the orifice plate 26 inner wall of bounding wall 21 inner wall joint, make the medicament dispersion spout to the straw, be convenient for spout the inside medicament extraction dispersion of box 12 to the straw, avoid local straw to spout the medicine and concentrate, the practicality of the device is improved.

Further as shown in fig. 3, it is worth specifically explaining that the outer wall height dimension of the two limit blocks 24 is matched with the inner wall depth dimension of the limit groove 25, the outer wall vertical cross-sectional area dimension of the two limit blocks 24 is matched with the inner wall vertical cross-sectional area dimension of the limit groove 25, and the limit blocks 24 and the limit groove 25 are clamped and fixed conveniently.

As further shown in fig. 3, it should be specifically noted that the size of the vertical cross-sectional area of the outer wall of the orifice plate 26 matches the size of the vertical cross-sectional area of the inner wall of the surrounding plate 21, and the size of the diameter of the inner surface of the inner annular wall of the circular hole 23 matches the size of the diameter of the outer surface of the outer annular wall of the connecting pipe 15, so as to facilitate the normal use of the device.

As further shown in fig. 4, it should be specifically noted that the outer diameters of the outer walls of the two shock-absorbing rods 33 are matched with the inner diameter of the inner wall of the spring 35, so as to facilitate the normal extension and contraction of the spring 35.

To sum up: the outer walls of the two bonding plates 34 respectively slide with the inner wall of the sliding groove 32 to enable the outer walls of the bonding plates 34 to extrude the shock absorption rod 33 and the spring 35 to contract, the top end of the box body 12 filled with the chemical is used for being bonded with the bottom end of the device body 1, the limiting position of the bonding plates 34 is loosened, the reverse thrust of the spring 35 is enabled to drive one side of the bonding plates 34 to be tightly bonded with the outer wall of the box body 12, the buffering performance of the device for installation between the box body 12 and the device body 1 is improved, the situation that the joint of the box body 12 is loosened due to collision is avoided, the normal installation of the box body 12 is affected, the outer wall of the limiting block 24 fixed at the top end of the top plate 22 is clamped with the inner wall of the limiting groove 25 arranged at the bottom end of the box body 12, the inner wall of the round hole 23 arranged at the top end of the top plate 22 is clamped with the top end of the top plate 21, the outer wall of the hole plate 26 is clamped with the inner wall of the surrounding plate 21, the device body 1 flies to an appointed straw spraying area, the water pump 14 is controlled to pump extract and spray the chemical inside the box body 12 to the inner wall of the spraying pipe 15, the straw conveniently, the straw is extracted and dispersed and sprayed to the straw, the straw is avoided concentrating, and the local chemical is improved.

The water pump 14 is commercially available, and the water pump 14 is provided with a power supply, which belongs to the mature technology in the field and is fully disclosed, so the repeated description in the specification is omitted.

Claims

1. The utility model provides an aircraft is sprinkled to straw maturity agent, includes the ware body (1), its characterized in that, two circular slot (11) have been seted up to the bottom of the ware body (1), the bottom bonding of the ware body (1) has box (12), the top of box (12) is fixed with two cylinder (13), two the outer wall of cylinder (13) all with the inner wall joint of circular slot (11), the inner wall bottom of box (12) is equipped with water pump (14), the play water end joint of water pump (14) has connecting pipe (15), the bottom of box (12) is equipped with dispersion mechanism (2), dispersion mechanism (2) are including bounding wall (21), the top bonding of bounding wall (21) has roof (22), round hole (23) have been seted up on the top of roof (22), the inner wall and the outer wall joint of connecting pipe (15) of round hole (23), the top of roof (22) is fixed with two stopper (24), two spacing groove (25) have been seted up to the bottom of box (12) the inner wall of spacing groove (25) all with the joint of stopper (24), the joint of inner wall (21) has stopper (26).

2. The straw decomposition agent spraying aircraft according to claim 1, wherein: the outer wall of the device body (1) is equipped with buffer gear (3), buffer gear (3) include two connecting blocks (31), two the one end of connecting block (31) all is fixed with the outer wall of the device body (1), two the other end of connecting block (31) all slides with the outer wall of box (12), two spout (32), two have all been seted up to one side of connecting block (31) inner wall one side of spout (32) all is fixed with shock attenuation pole (33), two the one end of shock attenuation pole (33) all is fixed with bonding board (34), two one side of bonding board (34) all bonds with the outer wall of box (12), two the outer wall of bonding board (34) all slides with the inner wall of spout (32), two the outer wall of shock attenuation pole (33) all overlaps and is equipped with spring (35), two the outer wall of spring (35) all overlaps and is equipped with ring cover (36).

3. The straw decomposition agent spraying aircraft according to claim 1, characterized in that: the inner surfaces of the inner circular walls of the two circular grooves (11) are matched with the outer surface of the outer circular wall of the cylinder (13) in diameter, and the depth of the inner walls of the two circular grooves (11) is matched with the height of the outer wall of the cylinder (13).

4. The straw decomposition agent spraying aircraft according to claim 1, wherein: the height dimension of the outer wall of the limiting block (24) is matched with the depth dimension of the inner wall of the limiting groove (25), and the vertical cross-sectional area dimension of the outer wall of the limiting block (24) is matched with the vertical cross-sectional area dimension of the inner wall of the limiting groove (25).

5. The straw decomposition agent spraying aircraft according to claim 1, wherein: the size of the vertical cross section area of the outer wall of the pore plate (26) is matched with that of the vertical cross section area of the inner wall of the enclosing plate (21), and the diameter of the inner surface of the inner annular wall of the circular hole (23) is matched with that of the outer surface of the outer annular wall of the connecting pipe (15).

6. The straw decomposition agent spraying aircraft according to claim 2, wherein: the diameter of the outer surface of the outer ring wall of each shock absorption rod (33) is matched with the diameter of the inner surface of the inner ring wall of the spring (35).