CN206914644U - Unmanned plane normal pressure shower nozzle - Google Patents

Unmanned plane normal pressure shower nozzle Download PDF

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Publication number
CN206914644U
CN206914644U CN201720368245.9U CN201720368245U CN206914644U CN 206914644 U CN206914644 U CN 206914644U CN 201720368245 U CN201720368245 U CN 201720368245U CN 206914644 U CN206914644 U CN 206914644U
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CN
China
Prior art keywords
upper body
shower nozzle
lower body
unmanned plane
normal pressure
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Application number
CN201720368245.9U
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Chinese (zh)
Inventor
阮波
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Shandong Falcon Science And Technology Of Aviation Co Ltd
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Shandong Falcon Science And Technology Of Aviation Co Ltd
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Priority to CN201720368245.9U priority Critical patent/CN206914644U/en
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Abstract

It the utility model is related to unmanned plane shower nozzle, unmanned plane normal pressure shower nozzle, including the truncated cone-shaped upper body and lower body to interfix are provided, upper body and lower body are thin-wall construction and one end open, Open Side Down and middle part connection machine shaft for upper body, and pencil is provided with above upper body;Lower body opening upwards, lower body edge are located on the inside of upper body edge, and teeth groove is uniformly provided with the inside of upper body and lower body.The utility model unitary construction is simple, and compared to the shower nozzle of pressure type, its atomizing particle is small, and general up to 50 80 microns, atomizing effect is good;Decoction need not pressurize, and can prepare the highly enriched decoction of higher concentration, avoid the defects of pressure type shower nozzle is not suitable for the decoction of configuration higher concentration, simplify structure, improve carrier fluid amount.

Description

Unmanned plane normal pressure shower nozzle
Technical field
It the utility model is related to unmanned plane shower nozzle, and in particular to a kind of unmanned plane normal pressure shower nozzle.
Background technology
The use of unmanned plane at present is quite extensive, especially in plant protection field, the unmanned plane spray big efficiency high of scope. But the shower nozzle of existing sprinkling decoction, generally require and decoction pressure is improved into 0.5-2Mpa, then by shower nozzle by medicine liquid spray Go out that the requirement for requiring atomization could be met, this mode of pressure of decoction is improved using hydraulic pump, hydraulic test can increase weight Amount, reduces effective carrier fluid amount, and when being sprayed using unmanned plane, traditional sprinkler heads operation influences very big on its efficiency.
The content of the invention
The utility model is to solve the above problems, provide one kind without pressurized equipment, the good nothing of atomizing effect simple in construction Man-machine normal pressure shower nozzle.
The utility model realized using following technical scheme, unmanned plane normal pressure shower nozzle, including in the truncated cone-shaped to interfix Body portion and lower body, upper body and lower body are thin-wall construction and one end open, and Open Side Down and middle part connection motor for upper body Rotating shaft, upper body top are provided with pencil;Lower body opening upwards, lower body edge are located on the inside of upper body edge, upper body and Teeth groove is uniformly provided with the inside of lower body.
Preferably, groove is provided with the middle part of the upper body, motor is located in groove, and pencil is located at the both sides of groove respectively.
Further, the shaft end of the motor is provided with connector, upper body and lower body and is fixed on company by screw column On junctor.
Further, the teeth groove of the lower body and the angled setting of bus.
Of the present utility model to be beneficial in that, unitary construction is simple, and compared to the shower nozzle of pressure type, its atomizing particle is small, It is general good up to 50-80 microns, atomizing effect;Decoction need not pressurize, and can prepare the highly enriched decoction of higher concentration, improve Operating efficiency, the defects of pressure type shower nozzle is not suitable for the decoction of configuration higher concentration is avoided, simplifies structure, improves carrier fluid amount.
Brief description of the drawings
Fig. 1 the utility model structure diagrams;
Fig. 2 the utility model lower body internal structure schematic diagrams;
1. lower body in figure, 11. lower body edge teeths, 2. upper bodies, 21. upper body edge teeths, 3. pencils, 4. motors, 5. connector, 6. screw columns.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings.
As depicted in figs. 1 and 2, the utility model provides a kind of unmanned plane normal pressure shower nozzle, including truncated cone-shaped upper body 2 is with Body portion 1, upper body and lower body are the thin-wall construction of truncated conical shape, big to hold a side opening to set, the side seal of small end one.Upper body Open Side Down and the middle part connection rotating shaft of motor 4, and upper body is provided with pencil 3, and pencil is that decoction is injected on the inside of upper body.Under The big end opening in body portion 2 is upward, and lower body edge is located on the inside of upper body edge, and tooth is uniformly provided with the inside of upper body and lower body Groove, upper body and lower body are fixedly connected by screw column 6, the small end sealed end of pencil face lower body.
In order to increase overall stability, make structure compacter, be provided with groove in the middle part of upper body, motor is located at groove Interior, pencil 3 is located at the both sides of groove respectively.The shaft end of motor is provided with connector 5, and upper body and lower body pass through screw column 6 are fixed on connector.
When implementing, motor is fixed on nozzle rod the utility model, and motor driven connector rotates at a high speed during work, even Junctor is simultaneously fixed together shower nozzle upper body and lower body by screw column, thus the high speed rotation of motor drives upper body Rotated at a high speed with lower body.
Decoction enters shower nozzle lower body from top to bottom by pencil, and under the influence of centrifugal force, decoction can be along lower body Groove on inner surface continues to accelerate movement, and when reaching lower body edge, one is carried out to decoction by lower body edge teeth Secondary refinement, the liquor granule after refinement carry out secondary refinement, work of the final decoction in centrifugal force again by upper body edge teeth Thrown away under, realize spray.
In order that atomizing effect is more preferable, teeth groove and the angled setting of bus of lower body, incline direction and motor rotation side To being oppositely arranged.

Claims (4)

1. unmanned plane normal pressure shower nozzle, it is characterised in that including the truncated cone-shaped upper body to interfix and lower body, upper body is with Body portion is thin-wall construction and one end open, and Open Side Down and middle part connection machine shaft for upper body, and pencil is provided with above upper body; Lower body opening upwards, lower body edge are located on the inside of upper body edge, and teeth groove is uniformly provided with the inside of upper body and lower body.
2. unmanned plane normal pressure shower nozzle according to claim 1, it is characterised in that be provided with groove in the middle part of the upper body, electricity Machine is located in groove, and pencil is located at the both sides of groove respectively.
3. unmanned plane normal pressure shower nozzle according to claim 2, it is characterised in that the shaft end of the motor is provided with connection Body, upper body and lower body are fixed on connector by screw column.
4. unmanned plane normal pressure shower nozzle according to claim 3, it is characterised in that the teeth groove of the lower body and bus are in angle Degree is set.
CN201720368245.9U 2017-04-10 2017-04-10 Unmanned plane normal pressure shower nozzle Active CN206914644U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720368245.9U CN206914644U (en) 2017-04-10 2017-04-10 Unmanned plane normal pressure shower nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720368245.9U CN206914644U (en) 2017-04-10 2017-04-10 Unmanned plane normal pressure shower nozzle

Publications (1)

Publication Number Publication Date
CN206914644U true CN206914644U (en) 2018-01-23

Family

ID=61307058

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720368245.9U Active CN206914644U (en) 2017-04-10 2017-04-10 Unmanned plane normal pressure shower nozzle

Country Status (1)

Country Link
CN (1) CN206914644U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110754461A (en) * 2019-12-10 2020-02-07 山东猎鹰航空科技有限公司 Charged atomizing and spraying system for forming wind-drug integration of rotor unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110754461A (en) * 2019-12-10 2020-02-07 山东猎鹰航空科技有限公司 Charged atomizing and spraying system for forming wind-drug integration of rotor unmanned aerial vehicle

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