CN205738112U - A kind of foldable spray rod on Multi-axis aircraft - Google Patents
A kind of foldable spray rod on Multi-axis aircraft Download PDFInfo
- Publication number
- CN205738112U CN205738112U CN201620713413.9U CN201620713413U CN205738112U CN 205738112 U CN205738112 U CN 205738112U CN 201620713413 U CN201620713413 U CN 201620713413U CN 205738112 U CN205738112 U CN 205738112U
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- CN
- China
- Prior art keywords
- rotating seat
- shower nozzle
- axis aircraft
- fixing seat
- spray rod
- 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
This utility model belongs to agricultural Multi-axis aircraft technical field, it is specifically related to a kind of foldable spray rod on Multi-axis aircraft, including fixing seat, rotating seat, connecting rod, shower nozzle connector, shower nozzle, fixing seat is provided with centre bore, fixing seat is provided with the chute of the arc-shaped structure with centre bore as the center of circle, it is provided with central shaft in described centre bore, described rotating seat is connected with central shaft, central axis is in rotating seat, rotating seat is provided with the clamping screw running through the upper and lower two ends of rotating seat, is arranged in chute bottom clamping screw；Connecting rod one end is connected with rotating seat, and the connecting rod other end is connected with shower nozzle connector, and shower nozzle is hinged with shower nozzle connector.This utility model can regulate the Multi-axis aircraft spraying scope to pesticide according to demand, and connecting rod can be folded by chute, then locks with clamping screw, convenient for collecting.
Description
Technical field
This utility model belong to agricultural Multi-axis aircraft technical field, be specifically related to a kind of on Multi-axis aircraft can
Folding spray rod.
Background technology
Multi-axis aircraft, the most rotor wing unmanned aerial vehicles, it is provided with multiple propeller, controls multiple propellers by multiple motors and come
Realize flight, be widely used in take photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural, have that volume is little, lightweight, expense
With low, flexible operation and safety high.The Multi-axis aircraft being currently used for agriculture field spray spraying pesticide needs at horn
On spray boom is set, and the setting of spray boom determines the scope of spray spraying pesticide, and in prior art, spray boom is the most all integrally fixed at horn
On, spray boom position cannot be carried out regulation, so the scope sprayed and angle are all fixing, it is impossible to according to the reality in farmland
Situation carries out the regulation of spraying scope and angle, because spray boom position cannot regulate, so storage is the most inconvenient.
Summary of the invention
This utility model is for being used for what spray boom position on the Multi-axis aircraft of spray spraying pesticide can not regulate in prior art
Drawback, it is provided that a kind of foldable spray rod on Multi-axis aircraft, because the nozzle position of spray boom can be adjusted, so can adjust
The spraying scope of joint pesticide, and the design of foldable spray rod, also can make Multi-axis aircraft storage more convenient.
Goal of the invention of the present utility model is achieved through the following technical solutions: a kind of on Multi-axis aircraft can
Folding spray rod, including fixing seat, rotating seat, connecting rod, shower nozzle connector, shower nozzle, fixing seat is provided with centre bore, on fixing seat
Be provided with the chute of arc-shaped structure with centre bore as the center of circle, in described centre bore, be provided with central shaft, described rotating seat with
Central shaft connects, and central axis is in rotating seat, and rotating seat is provided with the clamping screw running through the upper and lower two ends of rotating seat, locking screw
It is arranged in chute bottom bolt；Connecting rod one end is connected with rotating seat, and the connecting rod other end is connected with shower nozzle connector, shower nozzle with
Shower nozzle connector is hinged.
As preferably, fixing seat downside is arc-shaped structure, the center of circle of the fixing seat downside of arc-shaped structure with in
Central hole is overlapping.
As preferably, rotating seat is provided with projection towards the lower end of fixing seat side, and projection upper side is positioned on the downside of rotating seat
Below face.
As preferably, projection upper side is arc-shaped structure, the projection upper side of arc-shaped structure and rotating seat downside
Parallel.
As preferably, rotating seat upper end is provided with and turns hole, and rotating seat connects on center shaft by turning borehole jack.
As preferably, rotating seat is provided with groove A towards the side of fixing seat.
As preferably, rotating seat lower end is provided with locking hole, and rotating seat side is provided with fluting, and fluting connects with locking hole, opens
Groove both sides are respectively provided with one piece of clamping plate, and clamping plate are provided with locking hole.
As preferably, described connecting rod is hollow tubular structure, and the upper and lower two ends of connecting rod of hollow tubular structure respectively set
There is a pipeline connecting hole.
As preferably, fixing seat is provided with installing hole.
As preferably, shower nozzle connector side is provided with groove B, groove B and is positioned in the plane at rotary motion trace place of shower nozzle.
Compared with prior art, this utility model has the advantages that this utility model can multiple be combined making
With, it being respectively distributed to the diverse location of horn, fixing seat is fixed on horn, by the anglec of rotation of regulation rotating seat with fixing seat
Degree, can regulate shower nozzle position, and be locked on chute by rotating seat with clamping screw, it is thus possible to regulation spraying scope；
And shower nozzle and shower nozzle connector are hinged, shower nozzle can rotate around articulated position, so the spraying angle of shower nozzle can be regulated.
In sum, this utility model can regulate the Multi-axis aircraft spraying scope to pesticide according to demand, and can pass through
Connecting rod is folded by chute, then locks with clamping screw, convenient for collecting.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation；
Fig. 2 is fixed seat structure schematic diagram；
Fig. 3 is rotating seat structure schematic diagram；
Fig. 4 is that this utility model is applied in combination structural representation；
Labelling in figure: 1, fixing seat, 2, rotating seat, 3, connecting rod, 4, shower nozzle connector, 5, shower nozzle, 6, centre bore, 7, sliding
Groove, 8, central shaft, 9, clamping screw, 10, projection, 11, turn hole, 12, groove A, 13, locking hole, 14, fluting, 15, clamping plate, 16,
Locking hole, 17, pipeline connecting hole, 18, groove B, 19, installing hole.
Detailed description of the invention
This utility model is further described by the embodiment represented by 1-4 below in conjunction with the accompanying drawings:
Embodiment 1
As Figure 1-4, a kind of foldable spray rod on Multi-axis aircraft, including fixing seat 1, rotating seat 2, connect
Bar 3, shower nozzle connector 4, shower nozzle 5, fixing seat 1 is provided with centre bore 6, and fixing seat 1 is provided with the circular arc with centre bore 6 as the center of circle
The chute 7 of shape structure, is provided with central shaft 8 in described centre bore 6, rotating seat 2 upper end is provided with and turns hole 11, and rotating seat 2 is by turning
Hole 11 is socketed on central shaft 8, and rotating seat 2 can rotate around central shaft 8, and central shaft 8 is perpendicular to rotating seat 2, and rotating seat 2 sets
There is the clamping screw 9 running through rotating seat about 2 two ends, be arranged on bottom clamping screw 9 in chute 7；Rotating seat 2 lower end is provided with lock
Tieholen 13, rotating seat 2 side is provided with fluting 14, and fluting 14 connects with locking hole 13, and 14 both sides of slotting are respectively provided with one piece of clamping plate 15,
Clamping plate 15 are provided with locking hole 16, and connecting rod 3 upper end is arranged in locking hole 13, and arranging bolt in locking hole 13 can will connect
Bar 3 clamps, and connecting rod 3 lower end is connected with shower nozzle connector 4, and shower nozzle 5 is hinged with shower nozzle connector 4, and shower nozzle 5 can be around hinged place
Rotating, shower nozzle 5 connector side is provided with groove B18, groove B18 and is positioned in the plane at rotary motion trace place of shower nozzle 5.
Fixing seat 1 downside is arc-shaped structure, the center of circle of fixing seat 1 downside of arc-shaped structure and centre bore 6 weight
Folded.Rotating seat 2 is provided with projection 10 towards the lower end of fixing seat 1 side, and projection 10 upper side is positioned at below rotating seat 2 downside,
Projection 10 upper side is arc-shaped structure, and projection 10 upper side of arc-shaped structure is parallel with rotating seat 2 downside.Rotating seat 2
It is provided with groove A12, groove A12 to be arranged on turn between hole 11 and projection 10 towards the side of fixing seat 1.It is additionally provided with on fixing seat 1
Two installing holes 19, fixing seat 1 is arranged on horn by installing hole 19.
Described connecting rod 3 is hollow tubular structure, and the connecting rod about 3 of hollow tubular structure is respectively arranged at the two ends with a pipe
Road connecting hole 17, when using this utility model, needs to connect flexible pipe, the flexible pipe pipeline by connecting rod 3 lower end on shower nozzle 5
Connecting hole 17 is arranged in connecting rod 3, and flexible pipe upper end is arranged on Multi-axis aircraft through the pipeline connecting hole 17 of connecting rod 3 upper end
Horn in, can play the effect of hiding flexible pipe, and be easy to storage.
Specific embodiment described in literary composition is only to this utility model spirit explanation for example.Belonging to this utility model
Described specific embodiment can be made various amendment or supplements or use similar by those skilled in the art
Mode substitutes, but without departing from spirit of the present utility model or surmount scope defined in appended claims.
Claims (10)
1. the foldable spray rod on Multi-axis aircraft, including fixing seat (1), rotating seat (2), connecting rod (3), shower nozzle
Connector (4), shower nozzle (5), it is characterised in that fixing seat is provided with centre bore (6), fixing seat is provided with centre bore as the center of circle
The chute (7) of arc-shaped structure, be provided with central shaft (8) in described centre bore, described rotating seat is connected with central shaft, in
Mandrel is perpendicular to rotating seat, and rotating seat is provided with the clamping screw (9) running through the upper and lower two ends of rotating seat, arranges bottom clamping screw
In chute；Connecting rod one end is connected with rotating seat, and the connecting rod other end is connected with shower nozzle connector, shower nozzle and shower nozzle connector
Hinged.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that under fixing seat
Side is arc-shaped structure, and the center of circle of the fixing seat downside of arc-shaped structure is overlapping with centre bore.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 2, it is characterised in that rotating seat court
Being provided with projection (10) to the lower end of fixing seat side, projection upper side is positioned at below rotating seat downside.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 3, it is characterised in that on the upside of projection
Face is arc-shaped structure, and the projection upper side of arc-shaped structure is parallel with rotating seat downside.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that on rotating seat
End is provided with and turns hole (11), and rotating seat connects on center shaft by turning borehole jack.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that rotating seat court
It is provided with groove A(12) to the side of fixing seat.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that under rotating seat
End is provided with locking hole (13), and rotating seat side is provided with fluting (14), and fluting connects with locking hole, and fluting both sides are respectively provided with one piece of folder
Plate (15), clamping plate are provided with locking hole (16).
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that described company
Extension bar is hollow tubular structure, and the connecting rod of hollow tubular structure is respectively arranged at the two ends with a pipeline connecting hole (17) up and down.
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that on fixing seat
It is provided with installing hole (19).
A kind of foldable spray rod on Multi-axis aircraft the most according to claim 1, it is characterised in that shower nozzle is even
Fitting side is provided with groove B(18), groove B is positioned in the plane at rotary motion trace place of shower nozzle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620713413.9U CN205738112U (en) | 2016-07-08 | 2016-07-08 | A kind of foldable spray rod on Multi-axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620713413.9U CN205738112U (en) | 2016-07-08 | 2016-07-08 | A kind of foldable spray rod on Multi-axis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205738112U true CN205738112U (en) | 2016-11-30 |
Family
ID=57377578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620713413.9U Expired - Fee Related CN205738112U (en) | 2016-07-08 | 2016-07-08 | A kind of foldable spray rod on Multi-axis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205738112U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106423695A (en) * | 2016-12-14 | 2017-02-22 | 菏泽锅炉厂有限公司 | Spraying type acid washing device |
| CN107088486A (en) * | 2017-04-21 | 2017-08-25 | 成都大漠石油技术有限公司 | Antirust solution is sprayed on to the mechanism of oil drum inwall |
-
2016
- 2016-07-08 CN CN201620713413.9U patent/CN205738112U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106423695A (en) * | 2016-12-14 | 2017-02-22 | 菏泽锅炉厂有限公司 | Spraying type acid washing device |
| CN106423695B (en) * | 2016-12-14 | 2022-06-17 | 山东中杰特种装备股份有限公司 | Spraying type pickling device |
| CN107088486A (en) * | 2017-04-21 | 2017-08-25 | 成都大漠石油技术有限公司 | Antirust solution is sprayed on to the mechanism of oil drum inwall |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161130 Termination date: 20210708 |