CN104709466B - Aircraft sprinkling system - Google Patents

Aircraft sprinkling system Download PDF

Info

Publication number
CN104709466B
CN104709466B CN201510132337.2A CN201510132337A CN104709466B CN 104709466 B CN104709466 B CN 104709466B CN 201510132337 A CN201510132337 A CN 201510132337A CN 104709466 B CN104709466 B CN 104709466B
Authority
CN
China
Prior art keywords
plate
hole
spray boom
aircraft
spray
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
Application number
CN201510132337.2A
Other languages
Chinese (zh)
Other versions
CN104709466A (en
Inventor
张伟
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.)
HENAN ZHANYI AVIATION TECHNOLOGY CO., LTD.
Original Assignee
Henan Zhanyi Aviation Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Henan Zhanyi Aviation Technology Co Ltd filed Critical Henan Zhanyi Aviation Technology Co Ltd
Priority to CN201510132337.2A priority Critical patent/CN104709466B/en
Publication of CN104709466A publication Critical patent/CN104709466A/en
Application granted granted Critical
Publication of CN104709466B publication Critical patent/CN104709466B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
  • Catching Or Destruction (AREA)

Abstract

The invention belongs to agricultural machinery technological field, specifically disclose a kind of aircraft sprinkling system, including support, aircraft spray structure it is provided with in support, aircraft spray structure includes spray fixed structure, spray boom, connecting on spraying fixed structure and have medicine-chest and Teat pipette, spray boom is fixed with shower nozzle, pencil is sequentially connected with medicine-chest, Teat pipette and shower nozzle;Present configuration is simple, convenient disassembly and spray effect good.

Description

Aircraft sprinkling system
Technical field
The invention belongs to agricultural machinery technological field, relate to a kind of aircraft sprinkling 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 is progressively completed by unmanned vehicle.Existing agricultural unmanned vehicle structure is complicated, bulky, heavier-weight, seriously constrains its popularization and application on a large scale.As a example by medicine liquid spray system, medicine liquid spray system is agricultural carry-on important component part, is mainly used in containing and spray liquid, but existing medicine liquid spray system not only structure is complicated, assemble loaded down with trivial details, volume is relatively big, Heavy Weight, and production cost is high, and the amplitude of spraying medicine is little, narrow range, sprays uneven, and spray effect is poor.In addition, although the attachment structure between the existing each parts of aircraft sprinkling system is the most firm, but disassembling operations is loaded down with trivial details, and have to be cumbersome and time consuming by instrument.
Summary of the invention
It is an object of the invention to provide the aircraft sprinkling system that a kind of simple in construction, convenient disassembly and spray effect are good.
For achieving the above object, the present invention is by the following technical solutions: aircraft sprinkling system, including support, aircraft spray structure it is provided with in support, aircraft spray structure includes spray fixed structure, spray boom, connecting on spraying fixed structure and have medicine-chest and Teat pipette, spray boom is fixed with shower nozzle, pencil is sequentially connected with medicine-chest, Teat pipette and shower nozzle;Spraying fixed structure includes base plate, baffle plate and connecting plate;Spray boom is provided with shower nozzle fixed structure and spray boom fixed structure, and shower nozzle fixed structure includes C-type clamp and fixation clamp, and C-type clamp includes connecting plate and c-type plate, and connecting plate is provided with hole, location;Fixation clamp includes that two ends are provided with the anchor ear of fixing post, and fixing post has the screw corresponding with positioning hole;Spray boom fixed structure includes the fixing seat of band base and is located at the fixed plate below fixing seat, and fixing seat center is provided with spray boom installing hole, and fixing seat top is provided with the groove connected with spray boom installing hole;Fixed plate includes two platy structures being provided with the circular arc opening that matches, and fixed plate is connected with the base of fixing seat;Frame bottom is provided with shock absorber part.
Spray boom is provided with supporting construction, and supporting construction includes that support bar and locating clip, support bar two ends are provided with propclip;Propclip and the positioning jacket of support bar one end are located on spray boom.
Base plate is strip board, and bottom end is provided with the first connecting hole, is provided with fixing hole and installing hole, fixing hole and installing hole and is respectively symmetrically the centrage both sides being distributed in the long limit of base plate in the middle part of base plate;Baffle plate is Qian template, and baffle plate includes two-arm and connects the connecting portion of two-arm, and the two-arm of baffle plate matches with base plate, and two-arm is provided with the second connecting hole;Connecting plate is the lamellar plate along the downward 90-degree bent of centrage, and broken line both sides are provided with the connecting hole matched with first and second connecting hole.
Anchor ear is the sheet-like flexible structure of arc.
C-type clamp is a pair, and the opening direction of c-type plate is relative, and the opening of c-type plate is Contraband shape.
The base of fixing seat is provided with connecting hole, and fixed plate is provided with the through hole matched with connecting hole;Fixing seat top is provided with fixing hole.
The center of base plate is provided with the elongated hole along floor length direction.
Fixing band installing hole it is equipped with in the two-arm of baffle plate and connecting portion.
Compared with prior art, beneficial effects of the present invention is as follows:
1, in shower nozzle fixed structure, C-type clamp includes connecting plate and c-type plate, and c-type plate has Contraband shape opening, during use a pair C-type clamp with the use of, opening direction is relative, can clamp shower nozzle, and clamping degree is high;Having hole, location on connecting plate, fixation clamp includes anchor ear and fixing post, and anchor ear is located at shower nozzle to be needed on fixing spray boom, have the screw corresponding with positioning hole on fixing post, by screw through screw and hole, location during use, shower nozzle is fixed on spray boom, screw, convenient disassembly is screwed off during dismounting.
2, spray boom is provided with supporting construction, supporting construction includes support bar and locating clip, support bar two ends are provided with propclip, the propclip of support 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 support bar, propclip can slide on spray boom, it is arranged with locating clip on spray boom simultaneously, the angle of support bar and spray boom can be fixed, be conducive to sprinkling direction is adjusted.
3, in spray boom fixed structure, fixing seat center is provided with spray boom installing hole, and fixing seat top is provided with the groove connected with spray boom installing hole, convenient clamping spray boom;Fixed plate includes two platy structures being provided with the circular arc opening that matches, fixed plate is connected with the base of fixing seat, being fixed on the support below aircraft by spray boom, the screw worn in the connecting hole be provided with by the base of fixing seat is convenient after unclamping rotates the spray boom fixed structure direction with adjustment spray boom.
4, base plate, baffle plate and connecting plate in spraying fixed structure cooperate, simple in construction;Base plate and baffle plate are fixed together by connecting plate, form a cubical receiving district in order to install medicine-chest;The fixing hole being provided with in the middle part of base plate, is conveniently fixed on this fixed structure on the support below aircraft, and installing hole is in order to install Teat pipette;Fixing band installing 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 the 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 plate;
Fig. 7 is the structural representation of C-type clamp;
Fig. 8 is the structural representation of fixation clamp;
Fig. 9 is the structural representation of shower nozzle fixed structure;
Figure 10 is the structural representation of spray boom fixed structure.
Detailed description of the invention
Aircraft sprinkling system, as Figure 1-10 shows, including support 32, it is provided with shock absorber part 35 bottom support 32, in support 32, is provided with aircraft spray structure, aircraft spray structure includes spray fixed structure 36, spray boom 18, connecting on spraying fixed structure 36 and have medicine-chest 30 and Teat pipette 31, medicine-chest 30 is located at above spraying fixed structure 36, and Teat pipette 31 is located at below spraying fixed structure 36, being fixed with shower nozzle 29 on spray boom 18, pencil 28 is sequentially connected with medicine-chest 30, Teat pipette 31 and shower nozzle 29.
Spray boom 18 is provided with shower nozzle fixed structure 33 and spray boom fixed structure 34;Shower nozzle fixed structure 33 includes C-type clamp and fixation clamp, and C-type clamp includes connecting plate 14 and c-type plate 13, and connecting plate 14 is provided with hole 15, location;Fixation clamp includes that two ends are provided with the anchor ear 16 of fixing post 17, and fixing post 17 has the screw corresponding with positioning hole 15;Spray boom fixed structure 34 includes the fixing seat 19 of band base 27 and is located at the fixed plate 26 below fixing seat 19, and fixing seat 19 center is provided with spray boom installing hole, and fixing seat 19 top is provided with the groove 21 connected with spray boom installing hole;Fixed plate 26 includes two platy structures being provided with the circular arc opening 25 that matches, and fixed plate 26 is connected with the base 27 of fixing seat 19.Spray boom 18 is provided with supporting construction, and supporting construction includes that support bar 37 and locating clip 39, support bar 37 two ends are provided with propclip 38;Propclip 38 and the locating clip 39 of support bar 37 one end are set on spray boom 18.Anchor ear is the sheet-like flexible structure of arc.The opening of c-type plate 13 is Contraband shape.C-type clamp is a pair, and the opening direction of c-type plate 13 is relative.The base 27 of fixing seat 19 is provided with connecting hole 23, and fixed plate 26 is provided with in the through hole 24 matched with connecting hole 23, connecting hole 23 and through hole 24 and is equipped with pin or screw, is fixed on by spray boom fixed structure 34 on the support 32 arranged below aircraft.Fixing seat 19 top is provided with fixing hole 22, is equipped with screw or pin in order to connect two parts of the fixing seat 19 of groove 21 both sides in fixing hole 22.
During use, a pair C-type clamp coordinates, the opening of c-type plate 13 is relative, clamping shower nozzle 29, now the hole, location 15 on the connecting plate 14 of two C-type clamp overlaps, anchor ear 16 is set on spray boom 18, and the screw on fixing post 17 overlaps with hole 15, location, screw is located in screw and is fixed on spray boom 18 by shower nozzle fixed structure 33 in hole 15, location.Spray boom 18 other end is located in the spray boom installing hole that fixing seat 19 center is arranged, and screw or pin is arranged in the fixing hole 22 that fixing seat 19 top is arranged so that fixing seat 19 clamps spray boom 18;The circular arc opening 25 that in fixed plate 26, two are matched is set on the support below aircraft, screw or pin is arranged on base 27 on the connecting hole 23 and fixed plate 26 arranged in the through hole 24 arranged, is fixed on support 32 by spray boom fixed structure 34.When needing the direction adjusting spray boom 18, unscrew the screw or pin being located in connecting hole 23 and through hole 24 so that spray boom fixed structure 34 drives spray boom 18 to rotate with support 32 for axle, screw or pin is tightened after turning to correct position again.When adjusting the direction of spray boom 18, the propclip 38 being slidably located on spray boom 18, when being adjusted to required direction, the position of propclip 38 is fixed by the side that locating clip 39 slides into propclip 38, and then the direction of fixing spray boom 18.
Spraying fixed structure 36, including base plate 1, baffle plate 6 and connecting plate 10, base plate 1 is strip board, and base plate 1 end is provided with the first connecting hole 4, is provided with fixing hole 2 and installing hole 3 in the middle part of base plate 1;Fixing hole 2 and installing hole 3 are respectively symmetrically the centrage both sides being distributed in the long limit of base plate 1;Baffle plate 6 is Qian template, and baffle plate 6 includes two-arm and connects the connecting portion of two-arm, and the two-arm of baffle plate 6 matches with base plate 1, and two-arm is provided with the second connecting hole 8;Connecting plate 10 is the lamellar plate along the downward 90-degree bent of centrage, and broken line both sides are provided with the connecting hole 12 matched with the first connecting hole and the connecting hole 11 matched with the second connecting hole.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 installing hole 9, and the connecting portion of baffle plate is provided with longitudinally fixed band installing hole 7.
Base plate 1, baffle plate 6 are a pair, connecting plate 10 is two right, connecting plate 10 is respectively provided at two-arm and base plate 1 joint of baffle plate 6, screw or pin is used base plate 1, connecting plate 10 and baffle plate 6 to be linked together, by the fixing hole 2 on base plate 1, spraying fixed structure 36 is fixed on the support 32 arranged below aircraft, installing hole 3 is in order to install Teat pipette, and the elongated hole 5 on base plate 1 fixes Teat pipette 31 further in order to wear fixing bringing;The longitudinally fixed band installing hole 7 arranged on the horizontal strap installing hole 9 arranged in the two-arm of baffle plate 6 and connecting portion fixes medicine-chest 30 further in order to wear fixing bringing.

Claims (8)

1. aircraft sprinkling system, including support, it is characterized in that: in described support, be provided with aircraft spray structure, aircraft spray structure includes spray fixed structure, spray boom, connect on spraying fixed structure and have medicine-chest and Teat pipette, being fixed with shower nozzle on spray boom, pencil is sequentially connected with medicine-chest, Teat pipette and shower nozzle;Described spraying fixed structure includes base plate, baffle plate and connecting plate;Described spray boom is provided with shower nozzle fixed structure and spray boom fixed structure, and described shower nozzle fixed structure includes that C-type clamp and fixation clamp, described C-type clamp include connecting plate and c-type plate, and connecting plate is provided with hole, location;Described fixation clamp includes that two ends are provided with the anchor ear of fixing post, and described fixing post has the screw corresponding with positioning hole;Described spray boom fixed structure includes the fixing seat of band base and is located at the fixed plate below fixing seat, and fixing seat center is provided with spray boom installing hole, and fixing seat top is provided with the groove connected with spray boom installing hole;Described fixed plate includes two platy structures being provided with the circular arc opening that matches, and fixed plate is connected with the base of fixing seat;Described frame bottom is provided with shock absorber part.
2. aircraft sprinkling system as claimed in claim 1, it is characterised in that: described spray boom is provided with supporting construction, and supporting construction includes that support bar and locating clip, support bar two ends are provided with propclip;Propclip and the positioning jacket of described support bar one end are located on spray boom.
3. aircraft sprinkling 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 hole, is provided with fixing hole and installing hole, fixing hole and installing hole and is respectively symmetrically the centrage both sides being distributed in the long limit of base plate in the middle part of base plate;Described baffle plate is Qian template, and baffle plate includes two-arm and connects the connecting portion of two-arm, and the two-arm of baffle plate matches with base plate, and two-arm is provided with the second connecting hole;Described connecting plate is the lamellar plate along the downward 90-degree bent of centrage, and broken line both sides are provided with the connecting hole matched with first and second connecting hole.
4. aircraft sprinkling system as claimed in claim 3, it is characterised in that: described anchor ear is the sheet-like flexible structure of arc.
5. aircraft sprinkling system as claimed in claim 4, it is characterised in that: described C-type clamp is a pair, and the opening direction of c-type plate is relative, and the opening of c-type plate is Contraband shape.
6. aircraft sprinkling system as claimed in claim 5, it is characterised in that: the base of described fixing seat is provided with connecting hole, and fixed plate is provided with the through hole matched with connecting hole;Described fixing seat top is provided with fixing hole.
7. aircraft sprinkling system as claimed in claim 6, it is characterised in that: the center of described base plate is provided with the elongated hole along floor length direction.
8. aircraft sprinkling system as claimed in claim 7, it is characterised in that: it is equipped with fixing band installing hole in the two-arm of described baffle plate and connecting portion.
CN201510132337.2A 2015-03-25 2015-03-25 Aircraft sprinkling system Expired - Fee Related CN104709466B (en)

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 CN104709466A (en) 2015-06-17
CN104709466B true 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)

* Cited by examiner, † Cited by third party
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
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
CN104709466A (en) 2015-06-17

Similar Documents

Publication Publication Date Title
CN104743120B (en) agricultural Multi-rotor aerocraft
CN205404794U (en) Radar corner reflector with adjustable an angle for detecting radar product signal
CN103526907B (en) A kind of inclination stone material dry suspending structure and construction method thereof
CN207512615U (en) A kind of positioning device used for construction of bridge T steel welding of peg
CN204674834U (en) Aircraft sprinkler system
CN204194181U (en) A kind of compartment paint line
CN204674836U (en) agricultural Multi-rotor aerocraft
CN104709466B (en) Aircraft sprinkling system
CN204688418U (en) Aircraft spray structure
CN208423130U (en) A kind of base station antenna mounting clamp
KR101464170B1 (en) Carrier for distance measuring instrument in geodetic survey
CN206646785U (en) A kind of wall tile fixed structure of interior decoration
CN209315159U (en) A kind of portable multi-function artistic picture holder
CN207405757U (en) A kind of fabricated lightweight steel construction claustra modelled after an antique
CN204822087U (en) Spray lance for aircraft
CN203227958U (en) Fixing device for welding connecting pipe assemblies of vibrating screens
CN202793346U (en) Positioner for body-in-white three-coordinate measuring support
CN104960479A (en) Vehicle-mounted support device for mobile terminal
CN206128658U (en) Mount with adjustable height
CN205175710U (en) Portable four -wheel positioner
CN206550563U (en) A kind of horizontal plane pin adjusting apparatus
CN207259970U (en) A kind of new road science of bridge building protective frame
CN207343072U (en) A kind of stable type auxiliary hanging part for painting line
CN206123507U (en) Contact net cantilever pre -prepared device
CN206568011U (en) A kind of center caliberating device of milling tools

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160817

Termination date: 20180325