CN207262449U - A kind of safety-type unmanned plane flame defect elimination device - Google Patents
A kind of safety-type unmanned plane flame defect elimination device Download PDFInfo
- Publication number
- CN207262449U CN207262449U CN201721173601.8U CN201721173601U CN207262449U CN 207262449 U CN207262449 U CN 207262449U CN 201721173601 U CN201721173601 U CN 201721173601U CN 207262449 U CN207262449 U CN 207262449U
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- supporting rod
- oil
- pump
- water
- oil plant
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Abstract
A kind of safety-type unmanned plane flame defect elimination device, including oil plant case, oil pump, igniter, supporting rod a and bocca, further include carry case, water tank, water pump, supporting rod b and driving motor, carry case is internally provided with two storage chambers, water tank and oil plant case are individually fixed in storage chamber, the capping plate of carry case is equipped with key seat and driving motor, driving motor is connected with axis pin, supporting rod a and supporting rod b is individually fixed on the axis pin between adjacent key seat, igniter is fixed with directly over supporting rod a, oil plant orifice and water atomization hole are provided with the front end face of bocca, the pump oil pipe of oil pump and the harness of igniter bury respectively with supporting rod a, the front of oil plant orifice is equipped with igniter head.The spray angle of the flame defect elimination device adjusts, and flame region is without dead angle, while the flame defect elimination device carries extinguishing device, and the hanger that can be come off to burning is put out a fire, and causes fire incident after preventing the random landing of hanger that burning comes off.
Description
Technical field
It the utility model is related to unmanned plane field, and in particular to a kind of safety-type unmanned plane flame defect elimination device.
Background technology
In recent years, the hanging wire foreign matter on transmission line wire has become the great threat of electric power netting safe running, at present, operation
Department is passed through frequently with being purged processing under power down mode, but this method is by foreign matter position, circuit surrounding geographical environmental restrictions
It is larger, and power failure processing can also influence transmission reliability.Peace is such as faced with using operating personnel again into electric field equipotential live line work
The unfavorable situation that full blast danger is big, operating efficiency is low.To solve the above-mentioned problems, the more flames that loaded on unmanned plane of researcher disappear
Lack device and burning disposal is carried out to inflammable hanger, instead of the way of operating personnel's manual removal hanger well.So
And existing unmanned plane flame defect elimination device still has problems with：First, flame device angle after fixation is difficult to adjust,
Hanger could be burned completely by needing operating personnel to carry out complicated posture changing to unmanned plane, and operating efficiency is relatively low；It is second, existing
Some unmanned planes are difficult to carry out fire extinguishing processing to burning the hanger to come off, and the hanger arbitrarily to drop easily causes fire
Calamity, particularly with the more demanding mountain area of fire-protection rating.
Utility model content
The utility model to solve the above-mentioned problems, devises a kind of safety-type unmanned plane flame defect elimination device, the flame
The spray angle of defect elimination device adjusts, and flame region need not carry out unmanned plane complicated gesture stability without dead angle, at the same time
The flame defect elimination device carries extinguishing device, and the hanger to come off to burning is put out a fire in time, the suspension for preventing burning from coming off
Thing causes fire incident after arbitrarily landing.
In order to realize above-mentioned technical purpose, reach above-mentioned technique effect, the utility model is real by the following technical programs
Existing：
A kind of safety-type unmanned plane flame defect elimination device, including oil plant case, oil pump, igniter, supporting rod a and bocca,
Further include carry case, water tank, water pump, supporting rod b and drive motor, inner space is divided into two by the partition plate inside the carry case
A storage chamber, water tank and oil plant case are individually fixed in storage chamber, and the bottom of carry case, which is equipped with, supplies infusion tube and oil hose
The duct of installation, the capping plate of carry case are equipped with three key seats, and the side of key seat is fixed with driving motor, and driving motor passes through
Shaft coupling is connected with axis pin, and axis pin sequentially passes through key seat, and supporting rod a and supporting rod b are individually fixed in the axis pin between adjacent key seat
On, the water pump and oil pump are individually fixed in the left and right sides below capping plate, and supporting rod a and supporting rod b are fixed on capping plate
Middle part and be fixed with igniter directly over the surface of oil pump and water pump, supporting rod a respectively, the bocca is in
Air admission hole is provided with seedpod of the lotus shape and side wall, oil plant orifice and water atomization hole are provided with the front end face of bocca, oil plant case goes out
Oil pipe is connected with oil hose, and oil hose is connected with oil pump, and the pump oil pipe of oil pump and the harness of igniter are buried respectively
In supporting rod a, the end of pump oil pipe is connected with oil plant orifice, and the front of oil plant orifice is equipped with the spark type ignition stretched out
Head, the outlet pipe of water tank are connected with infusion tube, and infusion tube is connected with water pump, and the water pumping pipe of water pump is embedded in supporting rod b
And the end of water pumping pipe is connected with water atomization hole.
Further, the flowline of the oil plant case is equipped with the first solenoid valve, and the outlet pipe of water tank is equipped with the second electricity
Magnet valve.
Further, the storage battery and control of first solenoid valve, second solenoid valve and driving motor with unmanned plane
Chip connects.
The beneficial effects of the utility model are：The spray angle of the flame defect elimination device adjusts, flame region without dead angle,
And without carrying out complicated gesture stability to unmanned plane, while the flame defect elimination device carries extinguishing device, comes off to burning
Hanger is put out a fire in time, causes fire incident after preventing the random landing of hanger that burning comes off.
Brief description of the drawings
In order to illustrate more clearly of the technical solution of the utility model embodiment, make required for being described below to embodiment
Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the utility model,
For those of ordinary skill in the art, without creative efforts, can also be obtained according to these attached drawings
Other attached drawings.
Fig. 1 is the overall structure diagram of safety-type unmanned plane flame defect elimination device；
Fig. 2 is the composition structure diagram of safety-type unmanned plane flame defect elimination device.
In attached drawing, parts list represented by the reference numerals is as follows：
1- carry casees, 11- storage chambers, 12- fixed discs, 13- capping plates, 14- key seats, 2- water tanks, 21- outlet pipes, 22-
Second solenoid valve, 3- oil plant casees, 4- igniters, 41- harness, 42- igniter head, 5- oil pumps, 51- oil hoses, 52- supports
Bar a, 521- oil plant orifice, 6- water pumps, 61- infusion tubes, 62- supporting rods b, 621- water atomization hole, 7- driving motors, 8- sprays
Nozzles.
Embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without creative efforts
The all other embodiment obtained, shall fall within the protection scope of the present invention.
Refering to shown in Fig. 1-2, a kind of safety-type unmanned plane flame defect elimination device, including oil plant case (3), oil pump (5), igniting
Device (4), supporting rod a (52) and bocca (8), further include carry case (1), water tank (2), water pump (6), supporting rod b (62) and drive
Inner space is divided into two storage chambers (11), is set at the top of carry case by dynamic motor (7), the internal partition plate of the carry case (1)
There is fixed disc (12) to be fixed on the holder of unmanned plane, water tank (2) and oil plant case (3) are individually fixed in storage chamber (11)
In, the bottom of carry case (1) is equipped with the duct installed for infusion tube (61) and oil hose (51), the capping of carry case (1)
Plate (13) is equipped with three key seats (14), and the side of key seat (14) is fixed with driving motor (7), and driving motor (7) passes through shaft coupling
Device is connected with axis pin, and axis pin sequentially passes through key seat (14), and supporting rod a (52) and supporting rod b (62) are individually fixed in adjacent key seat
(14) on the axis pin between, water pump (2) and oil pump (3) are individually fixed in the left and right sides below capping plate (13), supporting rod a (52) and
Supporting rod b (62) is fixed on the middle part of capping plate (13) and respectively positioned at the surface of oil pump (5) and water pump (6), supporting rod a
(52) igniter (4) is fixed with directly over, the bocca (8) is in be provided with air admission hole, bocca on seedpod of the lotus shape and side wall
Front end face on be provided with oil plant orifice (521) and water atomization hole (621), the flowline of oil plant case (3) is connected with oil hose
(51), oil hose (51) is connected with oil pump (3), and the pump oil pipe of oil pump and the harness (41) of igniter are buried and propped up respectively
In strut a (52), the end of pump oil pipe is connected with oil plant orifice (521), and the front of oil plant orifice (521) is equipped with what is stretched out
Spark type ignition head (42), the outlet pipe (21) of water tank are connected with infusion tube (61), and infusion tube (61) connects with water pump (6)
Connect, the water pumping pipe of water pump (6) is embedded in supporting rod b (62) and the end of water pumping pipe is connected with water atomization hole (621).
The flowline of oil plant case (5) is equipped with the first solenoid valve, and the outlet pipe of water tank (2) is equipped with second solenoid valve
(22), the first solenoid valve, second solenoid valve (22) and driving motor (7) are connected with the storage battery and control chip of unmanned plane,
Earth station's remote control driving motor (7), driving motor drive axis pin to rotate, and axis pin drives supporting rod a (52) and supporting rod b (62) to do
Elevating movement eliminates the dead angle of flame and water spray, avoids excessively multiple to change the pitch angle of supporting rod a and supporting rod b
Unmanned plane is operated miscellaneously to change spray angle.
The first solenoid valve and oil pump (3) or water pump (2) are opened in remote control makes oil plant orifice (521) oil plant, remote controlled point
Firearm carries out the oil plant of atomization igniting so as to eliminate the combustible for hanging on transmission line of electricity；After the completion of flame, the electricity of remote control second
Pond valve (22) and person's water pump (2) make water atomization hole (621) spray atomized water, and it is water atomization hole (621) to adjust supporting rod b (62)
It is directed at comburant and carries out sprinkling fire, prevents comburant landing from causing fire.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
At least one of the utility model is contained in reference to the embodiment or example particular features, structures, materials, or characteristics described
In embodiment or example.In the present specification, schematic expression of the above terms be not necessarily referring to identical embodiment or
Example.
The preferred embodiment in the utility model disclosed above is only intended to help and illustrates the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, it is only the embodiment also not limit the utility model.Obviously, according to this theory
The content of bright book, can make many modifications and variations.This specification is chosen and specifically describes these embodiments, is in order to preferably
The principle and practical application of the utility model is explained, so that skilled artisan can be best understood by and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (3)
1. a kind of safety-type unmanned plane flame defect elimination device, including oil plant case, oil pump, igniter, supporting rod a and bocca, its
It is characterized in that：Carry case, water tank, water pump, supporting rod b and driving motor are further included, the partition plate inside the carry case is by inside
Space is divided into two storage chambers, and water tank and oil plant case are individually fixed in storage chamber, and the bottom of carry case, which is equipped with, supplies infusion tube
With the duct of oil hose installation, the capping plate of carry case is equipped with three key seats, and the side of key seat is fixed with driving motor, drives
Dynamic motor is connected by shaft coupling with axis pin, and axis pin sequentially passes through key seat, and supporting rod a and supporting rod b are individually fixed in adjacent pin
On axis pin between seat, the water pump and oil pump are individually fixed in the left and right sides below capping plate, and supporting rod a and supporting rod b consolidate
Due to the middle part for covering plate and igniter is fixed with directly over the surface of oil pump and water pump, supporting rod a respectively, it is described
Bocca in air admission hole is provided with seedpod of the lotus shape and side wall, oil plant orifice and water atomization hole are provided with the front end face of bocca,
The flowline of oil plant case is connected with oil hose, and oil hose is connected with oil pump, and the igniting of the pump oil pipe and igniter of oil pump is led
Respectively in embedded and supporting rod a, the end of pump oil pipe is connected line with oil plant orifice, and the front of oil plant orifice is equipped with what is stretched out
Spark type ignition head, the outlet pipe of water tank are connected with infusion tube, and infusion tube is connected with water pump, and the water pumping pipe of water pump is embedded in
Supporting rod b is interior and the end of water pumping pipe is connected with water atomization hole.
A kind of 2. safety-type unmanned plane flame defect elimination device according to claim 1, it is characterised in that：The oil plant case
Flowline is equipped with the first solenoid valve, and the outlet pipe of water tank is equipped with second solenoid valve.
A kind of 3. safety-type unmanned plane flame defect elimination device according to claim 2, it is characterised in that：First electromagnetism
Valve, second solenoid valve and driving motor are connected with the storage battery and control chip of unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721173601.8U CN207262449U (en) | 2017-09-13 | 2017-09-13 | A kind of safety-type unmanned plane flame defect elimination device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721173601.8U CN207262449U (en) | 2017-09-13 | 2017-09-13 | A kind of safety-type unmanned plane flame defect elimination device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207262449U true CN207262449U (en) | 2018-04-20 |
Family
ID=61920779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721173601.8U Expired - Fee Related CN207262449U (en) | 2017-09-13 | 2017-09-13 | A kind of safety-type unmanned plane flame defect elimination device |
Country Status (1)
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|---|---|
| CN (1) | CN207262449U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109751597A (en) * | 2019-03-19 | 2019-05-14 | 攀枝花学院 | Unmanned plane hanging power grid is removed obstacles flame device |
| CN110645593A (en) * | 2019-09-16 | 2020-01-03 | 上海煤气第二管线工程有限公司 | Unmanned aerial vehicle ignition method for diffusing torch |
| CN111572792A (en) * | 2020-05-20 | 2020-08-25 | 广东电网有限责任公司 | Unmanned aerial vehicle carries flame projecting device and clearance unmanned aerial vehicle with adjustable injection direction |
| CN112290451A (en) * | 2020-10-23 | 2021-01-29 | 广东电网有限责任公司广州供电局 | Power transmission line clamp heating detection cooling system and method |
| CN115626286A (en) * | 2022-12-20 | 2023-01-20 | 北京卓翼智能科技有限公司 | Flame projecting unmanned aerial vehicle |
-
2017
- 2017-09-13 CN CN201721173601.8U patent/CN207262449U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109751597A (en) * | 2019-03-19 | 2019-05-14 | 攀枝花学院 | Unmanned plane hanging power grid is removed obstacles flame device |
| CN110645593A (en) * | 2019-09-16 | 2020-01-03 | 上海煤气第二管线工程有限公司 | Unmanned aerial vehicle ignition method for diffusing torch |
| CN111572792A (en) * | 2020-05-20 | 2020-08-25 | 广东电网有限责任公司 | Unmanned aerial vehicle carries flame projecting device and clearance unmanned aerial vehicle with adjustable injection direction |
| CN112290451A (en) * | 2020-10-23 | 2021-01-29 | 广东电网有限责任公司广州供电局 | Power transmission line clamp heating detection cooling system and method |
| CN112290451B (en) * | 2020-10-23 | 2021-11-05 | 广东电网有限责任公司广州供电局 | Power transmission line clamp heating detection cooling system and method |
| CN115626286A (en) * | 2022-12-20 | 2023-01-20 | 北京卓翼智能科技有限公司 | Flame projecting unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180420 Termination date: 20210913 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |