CN204688418U - Aircraft spray structure - Google Patents
Aircraft spray structure Download PDFInfo
- Publication number
- CN204688418U CN204688418U CN201520169348.3U CN201520169348U CN204688418U CN 204688418 U CN204688418 U CN 204688418U CN 201520169348 U CN201520169348 U CN 201520169348U CN 204688418 U CN204688418 U CN 204688418U
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- CN
- China
- Prior art keywords
- spray boom
- fixed
- spray
- permanent seat
- fixed sturcture
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model belongs to agricultural machinery technological field, specifically disclose a kind of aircraft spray structure, comprise spraying fixed sturcture, spray boom, be located at the medicine-chest of spraying on fixed sturcture and the Teat pipette be located at below spraying fixed sturcture, spray boom is fixed with shower nozzle, and pencil connects medicine-chest, Teat pipette and shower nozzle successively.The utility model structure is simple, convenient disassembly and spray effect is good.
Description
Technical field
The utility model belongs to agricultural machinery technological field, relates to a kind of aircraft spray structure.
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 spray structure is comparatively firm, disassembling operations is loaded down with trivial details, and must by instrument, not only time-consuming but also require great effort.
Utility model content
The purpose of this utility model is to provide that a kind of structure is simple, convenient disassembly and the good aircraft spray structure of spray effect.
For achieving the above object, the utility model is by the following technical solutions: aircraft spray structure, comprise spraying fixed sturcture, spray boom, be located at the medicine-chest of spraying on fixed sturcture and the Teat pipette be located at below spraying fixed sturcture, spray boom is fixed with shower nozzle, pencil connects medicine-chest, Teat pipette and shower nozzle successively, and 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.
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, and 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, the beneficial effects of the utility model are as follows:
1, 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, permanent seat center is provided with spray boom mounting hole, 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 utility model;
Fig. 2 is the structural representation of base plate;
Fig. 3 is the structural representation of baffle plate;
Fig. 4 is the structural representation of connecting panel;
Fig. 5 is the structural representation of C-type clamp;
Fig. 6 is the structural representation of geometrical clamp;
Fig. 7 is the structural representation of shower nozzle fixed sturcture;
Fig. 8 is the structural representation of spray boom fixed sturcture.
Detailed description of the invention
Aircraft spray structure, as shown in figures 1-8, comprise spraying fixed sturcture, spray boom 18, be located at the medicine-chest 30 of spraying on fixed sturcture and the Teat pipette 31 be located at below spraying fixed sturcture, 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 and spray boom fixed sturcture; Shower nozzle fixed sturcture 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 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 32 and locating clip 34, and strut bar 32 two ends are provided with propclip 33; Propclip 33 and the locating clip 34 of strut bar 32 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, is fixed on the support arranged below aircraft by spray boom fixed sturcture in connecting bore 23 and through hole 24.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 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.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 is fixed on support.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 drive spray boom 18 to be that axle rotates with support, again screw or pin are tightened after turning to correct position.When adjusting the direction of spray boom 18, the propclip 33 be slidably located on spray boom 18, when adjusting to required direction, the position of propclip 33 is fixed by side locating clip 34 being slided into propclip 33, and then the direction of fixing spray boom 18.
Spraying fixed sturcture, comprise base plate, baffle plate and connecting panel, 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 this structure is fixed on the support arranged 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 spray structure, comprise spraying fixed sturcture, Teat pipette that spray boom, strut bar are located at the medicine-chest on spraying fixed sturcture and are located at below spraying fixed sturcture, spray boom is fixed with shower nozzle, pencil connects medicine-chest, Teat pipette and shower nozzle successively, it is characterized in that: 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.
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 spray structure 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 spray structure as claimed in claim 3, is characterized in that: described anchor ear is the sheet-like flexible structure of arc.
5. aircraft spray structure 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 spray structure 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 spray structure 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 spray structure 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 |
|---|---|---|---|
| CN201520169348.3U CN204688418U (en) | 2015-03-25 | 2015-03-25 | Aircraft spray structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520169348.3U CN204688418U (en) | 2015-03-25 | 2015-03-25 | Aircraft spray structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204688418U true CN204688418U (en) | 2015-10-07 |
Family
ID=54228736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520169348.3U Expired - Fee Related CN204688418U (en) | 2015-03-25 | 2015-03-25 | Aircraft spray structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204688418U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104709466A (en) * | 2015-03-25 | 2015-06-17 | 赵红英 | Spraying system for aircraft |
-
2015
- 2015-03-25 CN CN201520169348.3U patent/CN204688418U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104709466A (en) * | 2015-03-25 | 2015-06-17 | 赵红英 | Spraying system for aircraft |
| CN104709466B (en) * | 2015-03-25 | 2016-08-17 | 河南展翼航空科技有限公司 | Aircraft sprinkling system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20151007 Termination date: 20180325 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |