CN104709466A - Spraying system for aircraft - Google Patents
Spraying system for aircraft Download PDFInfo
- Publication number
- CN104709466A CN104709466A CN201510132337.2A CN201510132337A CN104709466A CN 104709466 A CN104709466 A CN 104709466A CN 201510132337 A CN201510132337 A CN 201510132337A CN 104709466 A CN104709466 A CN 104709466A
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- Prior art keywords
- aircraft
- spray boom
- fixed
- permanent seat
- spraying
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Abstract
The invention belongs to the technical field of agricultural machines, and particularly discloses a spraying system for an aircraft. The spraying system comprises a support. A spraying structure for the aircraft is arranged in the support and comprises a spraying fixing structure and a spraying rod. A pesticide box and a pesticide pump are connected to the spraying fixing structure. A spraying head is fixed to the spraying rod. A pesticide pipe is connected with the pesticide box, the pesticide pump and the spraying head in sequence. The spraying system is simple in structure, convenient to disassemble and good in spraying effect.
Description
Technical field
The invention belongs to agricultural machinery technological field, relate to a kind of aircraft sprinkler system.
Background technology
Along with the development of society, the progress of science and technology, the work sprayed insecticide on a large scale in farmland has progressively been come by unmanned vehicle.Existing agricultural unmanned vehicle complex structure, bulky, heavier-weight, seriously constrain it and apply on a large scale.For medicine liquid spray system, medicine liquid spray system is agricultural carry-on important component part, is mainly used in splendid attire and spray liquid, but existing medicine liquid spray system not only complex structure, assemble loaded down with trivial details, volume is comparatively large, Heavy Weight, and productive costs is high, and the amplitude of spray medicine is little, narrow range, spray uneven, spray effect is poor.In addition, although the connection structure between each parts of existing aircraft sprinkler system is comparatively firm, disassembling operations is loaded down with trivial details, and must by instrument, not only time-consuming but also require great effort.
Summary of the invention
The object of this invention is to provide that a kind of structure is simple, convenient disassembly and the good aircraft sprinkler system of spray effect.
For achieving the above object, the present invention is by the following technical solutions: aircraft sprinkler system, comprise support, aircraft spray structure is provided with in support, aircraft spray structure comprises spraying fixed sturcture, spray boom, spraying fixed sturcture is connected with medicine-chest and Teat pipette, and spray boom is fixed with shower nozzle, and pencil connects medicine-chest, Teat pipette and shower nozzle successively; Spraying fixed sturcture comprises base plate, baffle plate and connecting panel; Spray boom is provided with shower nozzle fixed sturcture and spray boom fixed sturcture, and shower nozzle fixed sturcture comprises C-type clamp and geometrical clamp, and C-type clamp comprises connecting panel and C template, and connecting panel is provided with knock hole; Geometrical clamp comprises the anchor ear that two ends are provided with fixed leg, fixed leg has the screw corresponding with knock hole; The permanent seat that spray boom fixed sturcture comprises band base and the adapter plate be located at below permanent seat, permanent seat center is provided with spray boom mounting hole, the groove that permanent seat top is communicated with spray boom mounting hole; Adapter plate comprises the platy structure that two are provided with the circular arc opening that matches, and adapter plate is connected with the base of permanent seat; Frame bottom is provided with shock absorber part.
Spray boom is provided with supporting construction, and supporting construction comprises strut bar and locating clip, and strut bar two ends are provided with propclip; Propclip and the positioning jacket of strut bar one end are located on spray boom.
Base plate is strip board, and bottom end is provided with the first connecting bore, is provided with fixed orifice and mounting hole in the middle part of base plate, and fixed orifice and mounting hole are symmetrically distributed in the line of centers both sides on the long limit of base plate respectively; Baffle plate is Qian template, and baffle plate comprises two-arm and the connecting portion being connected two-arm, and the two-arm of baffle plate matches with base plate, and two-arm is provided with the second connecting bore; Connecting panel is the sheet plate of centrally 90-degree bent under alignment, and broken line both sides are provided with the connecting bore matched with first and second connecting bore.
Anchor ear is the sheet-like flexible structure of arc.
C-type clamp is that the opening direction of a pair, C template is relative, and the opening of C template is Contraband shape.
The base of permanent seat is provided with connecting bore, and adapter plate is provided with the through hole matched with connecting bore; Permanent seat top is provided with fixed orifice.
The center of base plate is provided with the elongated hole along floor length direction.
The two-arm of baffle plate and connecting portion are equipped with clamping band mounting hole.
Compared with prior art, beneficial effect of the present invention is as follows:
1, in shower nozzle fixed sturcture, C-type clamp comprises connecting panel and C template, C template has Contraband shape opening, during use a pair C-type clamp with the use of, opening direction is relative, and can clamp shower nozzle, clamping degree is high; Connecting panel has knock hole, and geometrical clamp comprises anchor ear and fixed leg, and anchor ear is located at shower nozzle to be needed on fixing spray boom, fixed leg has the screw corresponding with knock hole, during use, screw is passed screw and knock hole, shower nozzle is fixed on spray boom, screw is screwed off, convenient disassembly during dismounting.
2, spray boom is provided with supporting construction, supporting construction comprises strut bar and locating clip, strut bar two ends are provided with propclip, the propclip of strut bar one end and positioning jacket are located on spray boom, and the propclip of the other end is connected with the support below aircraft, when lifting or fall strut bar, propclip can slide on spray boom, spray boom is arranged with locating clip simultaneously, the angle of strut bar and spray boom can be fixed, be conducive to adjusting sprinkling direction.
3, in spray boom fixed sturcture, permanent seat center is provided with spray boom mounting hole, and the groove that permanent seat top is communicated with spray boom mounting hole conveniently clamps spray boom; Adapter plate comprises the platy structure that two are provided with the circular arc opening that matches, adapter plate is connected with the base of permanent seat, be fixed on by spray boom on the support below aircraft, the screw worn in the connecting bore be provided with by the base of permanent seat unclamps the rear convenient spray boom fixed sturcture that rotates to adjust the direction of spray boom.
4, base plate, baffle plate and the connecting panel of spraying in fixed sturcture cooperatively interacts, and structure is simple; Base plate and baffle plate are fixed together by connecting panel, form a cubical accommodation district in order to install medicine-chest; The fixed orifice be provided with in the middle part of base plate, be conveniently fixed on the support below aircraft by this fixed sturcture, mounting hole is in order to install Teat pipette; Clamping band mounting hole on baffle plate is in order to install restraint zone with fixing medicine-chest; Elongated hole on base plate is in order to install restraint zone in order to strengthen the fixed effect of Teat pipette.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is the structural representation of support;
Fig. 3 is the structural representation of aircraft spray structure;
Fig. 4 is the structural representation of base plate;
Fig. 5 is the structural representation of baffle plate;
Fig. 6 is the structural representation of connecting panel;
Fig. 7 is the structural representation of C-type clamp;
Fig. 8 is the structural representation of geometrical clamp;
Fig. 9 is the structural representation of shower nozzle fixed sturcture;
Figure 10 is the structural representation of spray boom fixed sturcture.
Detailed description of the invention
Aircraft sprinkler system, as Figure 1-10 shows, comprise support 32, bottom support 32, be provided with shock absorber part 35, in support 32, be provided with aircraft spray structure, aircraft spray structure comprises spraying fixed sturcture 36, spray boom 18, spraying fixed sturcture 36 is connected with medicine-chest 30 and Teat pipette 31, and medicine-chest 30 is located at above spraying fixed sturcture 36, and Teat pipette 31 is located at below spraying fixed sturcture 36, spray boom 18 is fixed with shower nozzle 29, pencil 28 connects medicine-chest 30, Teat pipette 31 and shower nozzle 29 successively.
Spray boom 18 is provided with shower nozzle fixed sturcture 33 and spray boom fixed sturcture 34; Shower nozzle fixed sturcture 33 comprises C-type clamp and geometrical clamp, and C-type clamp comprises connecting panel 14 and C template 13, and connecting panel 14 is provided with knock hole 15; Geometrical clamp comprises the anchor ear 16 that two ends are provided with fixed leg 17, and fixed leg 17 has the screw corresponding with knock hole 15; The permanent seat 19 that spray boom fixed sturcture 34 comprises band base 27 and the adapter plate 26 be located at below permanent seat 19, permanent seat 19 center is provided with spray boom mounting hole, the groove 21 that permanent seat 19 top is communicated with spray boom mounting hole; Adapter plate 26 comprises the platy structure that two are provided with the circular arc opening 25 that matches, and adapter plate 26 is connected with the base 27 of permanent seat 19.Spray boom 18 is provided with supporting construction, and supporting construction comprises strut bar 37 and locating clip 39, and strut bar 37 two ends are provided with propclip 38; Propclip 38 and the locating clip 39 of strut bar 37 one end are set on spray boom 18.Anchor ear is the sheet-like flexible structure of arc.The opening of C template 13 is Contraband shape.C-type clamp is that the opening direction of a pair, C template 13 is relative.The base 27 of permanent seat 19 is provided with connecting bore 23, and adapter plate 26 is provided with the through hole 24 matched with connecting bore 23, is equipped with pin or screw in connecting bore 23 and through hole 24, is fixed on the support 32 arranged below aircraft by spray boom fixed sturcture 34.Permanent seat 19 top is provided with fixed orifice 22, is equipped with screw or pin in order to connect two parts of the permanent seat 19 of groove 21 both sides in fixed orifice 22.
During use, a pair C-type clamp coordinates, the opening of C template 13 is relative, clamping shower nozzle 29, knock hole 15 on the connecting panel 14 of now two C-type clamp overlaps, anchor ear 16 is set on spray boom 18, and the screw on fixed leg 17 overlaps with knock hole 15, is located in by screw in screw and knock hole 15 and is fixed on spray boom 18 by shower nozzle fixed sturcture 33.Spray boom 18 other end is located in the spray boom mounting hole of permanent seat 19 center setting, screw or pin is arranged in the fixed orifice 22 of permanent seat 19 top setting, makes permanent seat 19 clamp spray boom 18; The circular arc opening 25 that on adapter plate 26, two are matched is set on the support below aircraft, screw or pin are arranged on base 27 arrange connecting bore 23 and adapter plate 26 on arrange through hole 24 in, spray boom fixed sturcture 34 is fixed on support 32.When needing to adjust the direction of spray boom 18, unscrew and be located in screw in connecting bore 23 and through hole 24 or pin, make spray boom fixed sturcture 34 drive spray boom 18 with support 32 for axle rotation, again screw or pin are tightened after turning to correct position.When adjusting the direction of spray boom 18, the propclip 38 be slidably located on spray boom 18, when adjusting to required direction, the position of propclip 38 is fixed by side locating clip 39 being slided into propclip 38, and then the direction of fixing spray boom 18.
Spraying fixed sturcture 36, comprise base plate 1, baffle plate 6 and connecting panel 10, base plate 1 is strip board, and base plate 1 end is provided with the first connecting bore 4, is provided with fixed orifice 2 and mounting hole 3 in the middle part of base plate 1; Fixed orifice 2 and mounting hole 3 are symmetrically distributed in the line of centers both sides on the long limit of base plate 1 respectively; Baffle plate 6 is Qian template, and baffle plate 6 comprises two-arm and the connecting portion being connected two-arm, and the two-arm of baffle plate 6 matches with base plate 1, and two-arm is provided with the second connecting bore 8; Connecting panel 10 is the sheet plate of centrally 90-degree bent under alignment, and broken line both sides are provided with the connecting bore 12 matched with the first connecting bore and the connecting bore 11 matched with the second connecting bore.The center of base plate 1 is provided with the elongated hole 5 along strip board length direction.The two-arm of baffle plate 6 is provided with horizontal strap mounting hole 9, and the connecting portion of baffle plate is provided with longitudinal clamping band mounting hole 7.
Base plate 1, baffle plate 6 are a pair, connecting panel 10 is two right, connecting panel 10 is located at two-arm and base plate 1 joint of baffle plate 6 respectively, screw or pin is used base plate 1, connecting panel 10 and baffle plate 6 to be linked together, by the fixed orifice 2 on base plate 1, spraying fixed sturcture 36 is fixed on the support 32 that arranges below aircraft, mounting hole 3 is in order to install Teat pipette, and the elongated hole 5 on base plate 1 fixedly brings fixing Teat pipette 31 further in order to wear; Longitudinal clamping band mounting hole 7 that the horizontal strap mounting hole 9 that the two-arm of baffle plate 6 is arranged and connecting portion are arranged fixedly brings fixing medicine-chest 30 further in order to wear.
Claims (8)
1. aircraft sprinkler system, comprise support, it is characterized in that: in described support, be provided with aircraft spray structure, aircraft spray structure comprises spraying fixed sturcture, spray boom, spraying fixed sturcture is connected with medicine-chest and Teat pipette, spray boom is fixed with shower nozzle, and pencil connects medicine-chest, Teat pipette and shower nozzle successively; Described spraying fixed sturcture comprises base plate, baffle plate and connecting panel; Described spray boom is provided with shower nozzle fixed sturcture and spray boom fixed sturcture, and described shower nozzle fixed sturcture comprises C-type clamp and geometrical clamp, and described C-type clamp comprises connecting panel and C template, and connecting panel is provided with knock hole; Described geometrical clamp comprises the anchor ear that two ends are provided with fixed leg, and described fixed leg has the screw corresponding with knock hole; The permanent seat that described spray boom fixed sturcture comprises band base and the adapter plate be located at below permanent seat, permanent seat center is provided with spray boom mounting hole, the groove that permanent seat top is communicated with spray boom mounting hole; Described adapter plate comprises the platy structure that two are provided with the circular arc opening that matches, and adapter plate is connected with the base of permanent seat; Described frame bottom is provided with shock absorber part.
2. aircraft spray structure as claimed in claim 1, it is characterized in that: described spray boom is provided with supporting construction, supporting construction comprises strut bar and locating clip, and strut bar two ends are provided with propclip; Propclip and the positioning jacket of described strut bar one end are located on spray boom.
3. aircraft sprinkler system as claimed in claim 1 or 2, it is characterized in that: described base plate is strip board, bottom end is provided with the first connecting bore, is provided with fixed orifice and mounting hole in the middle part of base plate, and fixed orifice and mounting hole are symmetrically distributed in the line of centers both sides on the long limit of base plate respectively; Described baffle plate is Qian template, and baffle plate comprises two-arm and the connecting portion being connected two-arm, and the two-arm of baffle plate matches with base plate, and two-arm is provided with the second connecting bore; Described connecting panel is the sheet plate of centrally 90-degree bent under alignment, and broken line both sides are provided with the connecting bore matched with first and second connecting bore.
4. aircraft sprinkler system as claimed in claim 3, is characterized in that: described anchor ear is the sheet-like flexible structure of arc.
5. aircraft sprinkler system as claimed in claim 4, is characterized in that: described C-type clamp is that the opening direction of a pair, C template is relative, and the opening of C template is Contraband shape.
6. aircraft sprinkler system as claimed in claim 5, it is characterized in that: the base of described permanent seat is provided with connecting bore, adapter plate is provided with the through hole matched with connecting bore; Described permanent seat top is provided with fixed orifice.
7. aircraft sprinkler system as claimed in claim 6, is characterized in that: the center of described base plate is provided with the elongated hole along floor length direction.
8. aircraft sprinkler system as claimed in claim 7, is characterized in that: the two-arm of described baffle plate and connecting portion are equipped with clamping band mounting hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510132337.2A CN104709466B (en) | 2015-03-25 | 2015-03-25 | Aircraft sprinkling system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510132337.2A CN104709466B (en) | 2015-03-25 | 2015-03-25 | Aircraft sprinkling system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104709466A true CN104709466A (en) | 2015-06-17 |
| CN104709466B CN104709466B (en) | 2016-08-17 |
Family
ID=53409300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510132337.2A Expired - Fee Related CN104709466B (en) | 2015-03-25 | 2015-03-25 | Aircraft sprinkling system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104709466B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5589201A (en) * | 1978-12-28 | 1980-07-05 | Nakanihon Koku Kk | Vermin extermination and its device with aerial application or release of attractant and aerial dusting of insecticide |
| JPH0691059A (en) * | 1992-09-17 | 1994-04-05 | Yamaha Motor Co Ltd | Remote control type helicopter |
| JPH09140314A (en) * | 1995-11-24 | 1997-06-03 | Chuichi Nakamura | Aerial applicator for radio-controlled helicopter |
| CN104743120A (en) * | 2015-03-25 | 2015-07-01 | 赵红英 | Agricultural multi-rotor aircraft |
| CN204674834U (en) * | 2015-03-25 | 2015-09-30 | 赵红英 | Aircraft sprinkler system |
| CN204688418U (en) * | 2015-03-25 | 2015-10-07 | 河南展翼航空科技有限公司 | Aircraft spray structure |
-
2015
- 2015-03-25 CN CN201510132337.2A patent/CN104709466B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5589201A (en) * | 1978-12-28 | 1980-07-05 | Nakanihon Koku Kk | Vermin extermination and its device with aerial application or release of attractant and aerial dusting of insecticide |
| JPH0691059A (en) * | 1992-09-17 | 1994-04-05 | Yamaha Motor Co Ltd | Remote control type helicopter |
| JPH09140314A (en) * | 1995-11-24 | 1997-06-03 | Chuichi Nakamura | Aerial applicator for radio-controlled helicopter |
| CN104743120A (en) * | 2015-03-25 | 2015-07-01 | 赵红英 | Agricultural multi-rotor aircraft |
| CN204674834U (en) * | 2015-03-25 | 2015-09-30 | 赵红英 | Aircraft sprinkler system |
| CN204688418U (en) * | 2015-03-25 | 2015-10-07 | 河南展翼航空科技有限公司 | Aircraft spray structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104709466B (en) | 2016-08-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| CB03 | Change of inventor or designer information |
Inventor after: Zhang Wei Inventor before: Zhao Hongying |
|
| COR | Change of bibliographic data | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20160708 Address after: The new Zheng Dong 450000 in Henan province Zhengzhou City Station Road West, No. 1 Fu Lu Bei (Henan chamber of Commerce Building 26 floor No. 2604) Applicant after: HENAN ZHANYI AVIATION TECHNOLOGY CO., LTD. Address before: 450000 No. 63, agricultural road, Henan, Zhengzhou Applicant before: Zhao Hongying |
|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 Termination date: 20180325 |
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| CF01 | Termination of patent right due to non-payment of annual fee |