CN209516459U - A kind of unmanned plane electrification cleaning wire foreign matter device - Google Patents
A kind of unmanned plane electrification cleaning wire foreign matter device Download PDFInfo
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- CN209516459U CN209516459U CN201920187991.7U CN201920187991U CN209516459U CN 209516459 U CN209516459 U CN 209516459U CN 201920187991 U CN201920187991 U CN 201920187991U CN 209516459 U CN209516459 U CN 209516459U
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- fixedly installed
- motor
- foreign matter
- impact
- unmanned plane
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Abstract
The utility model discloses a kind of unmanned planes to charge cleaning wire foreign matter device, including drone body, and the wing that quantity is four and is symmetric is fixedly installed on the outside of drone body.Unmanned plane electrification cleaning wire foreign matter device, remote controlled drone ontology is flown near the conducting wire for needing to clear up, make the arc groove and conductive contact of T-type angle by the camera in drone body, without manually climbing, at this moment starting first motor rotates the output end of first motor with cam, when the farthest both ends of cam contact the push rod being located at left and right sides of first motor respectively and squeeze push rod, push rod is caused to squeeze u-bracket, so that u-bracket is with spiral arm, brush plate and the second motor do movement in a curve as the center of circle using the axle center of connecting shaft, starting the second motor simultaneously rotates the output shaft band movable knife disc of the second motor and blade, whole process has the cleaning of foreign matter at low cost, risk bottom and high-efficient advantage.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane electrification cleaning wire foreign matter device.
Background technique
Long distance delivery electric energy needs to carry out by cable, and existing cable is aerial cable, and aerial cable is usually by wind
The winding extension of zither, polybag and other wire bodies or sundries stays, and above-mentioned object is the hidden danger of safety power transmission, needs to carry out in time clear
Reason.
Traditional manner of cleaning up is usually manual cleaning, walks and is carried out on the line clearly after needing staff to climb up shaft tower
Reason, for the route in urban district, then can be cleared up with electric power operation car, and above-mentioned manner of cleaning up is that the high-altitude in the case of electrification is made
Industry, dangerous property is high, the high problem low with cleaning efficiency of disposal costs, so propose that a kind of unmanned plane electrification cleaning conducting wire is different
Object device solves the problems, such as above-mentioned propose.
Utility model content
The purpose of this utility model is to provide a kind of unmanned planes to charge cleaning wire foreign matter device, has at low cost, danger
Dangerous bottom and high-efficient advantage, with solve the dangerous property of traditional manner of cleaning up mentioned above in the background art it is high,
Disposal costs height and the low problem of cleaning efficiency.
To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane electrification cleaning wire foreign matter
Device, a kind of unmanned plane electrification cleaning wire foreign matter device, including drone body are fixedly installed on the outside of drone body
Quantity is four and the wing that is symmetric, is fixedly installed with propeller at the top of wing, the bottom of drone body is fixed
The under-chassis that quantity is four and is symmetric, the bottom of drone body and the intermediate fixed peace for being located at four under-chassis are installed
Equipped with camera holder, the bottom of camera holder is fixedly installed with camera, and the under-chassis side opposite with the rear side under-chassis in front side is equal
It is fixedly connected with pedestal, the bottom of pedestal is fixedly installed with the first impact-absorbing shell that quantity is two and is symmetric, and first is slow
The inner cavity of punching cover slidably connects the first sliding block, and the inner cavity of the first impact-absorbing shell is fixedly installed with one end and is fixedly connected with the first sliding block
The first spring, the bottom of the first sliding block is fixedly installed with the T-type angle that one end is run through and extends to the first impact-absorbing shell bottom,
The second impact-absorbing shell that quantity is two and is symmetric is fixedly installed at the top of pedestal, the inner cavity of the second impact-absorbing shell, which is slided, to be connected
It is connected to the second sliding block, the inner cavity of the second impact-absorbing shell is fixedly installed with the second spring that one end is fixedly connected with the second sliding block, pedestal
Top and be located at the centres of two the second impact-absorbing shells and be fixedly installed with first motor, be fixedly mounted at the output shaft of first motor
Have a cam, the bottom of wing is fixedly installed with connecting rod, between the connecting rod of two, left side with two, the right side connecting rod
Between be fixedly installed with connecting shaft, spiral arm is movably installed on the outside of connecting shaft, the bottom of spiral arm is fixedly installed with brush plate,
Two opposite sides of spiral arm are fixedly installed with the second motor, and cutterhead is fixedly installed at the output shaft of the second motor, cutterhead
Outside is fixedly installed with blade, and two opposite sides of spiral arm are fixedly installed with u-bracket, two the second impact-absorbing shells it is opposite one
Side is movably installed with one end and runs through and extend to the push rod on the inside of u-bracket, and the inside of u-bracket is living by shaft and push rod
Dynamic connection.
Preferably, the T-type angle is made of cylindrical rod piece and rectangle block part, the top of cylindrical rod piece and first
Sliding block is fixedly connected, and the bottom of cylindrical rod piece is fixedly connected with rectangle block part, and rectangle block part bottom offers arc groove, arc
The inside of slot is fixedly installed with electro-insulating rubber.
Preferably, when the distance at the farthest both ends of the cam is greater than second spring nature two push rod opposite sides it
Between distance.
Preferably, the spiral arm is made of annulus set and rectangle rod piece, and the internal diameter of annulus set and the diameter of connecting shaft are mutually fitted
Match and annulus set is flexibly connected with connecting shaft, the outside of annulus set is fixedly connected with rectangle rod piece.
Preferably, the quantity of the blade is ten, and blade is distributed in a ring.
Preferably, the push rod ecto-entad sequentially passes through the second impact-absorbing shell, the second sliding block and second spring, push rod and
Two sliding blocks are fixedly connected.
Compared with prior art, the utility model has the beneficial effects that unmanned plane electrification cleaning wire foreign matter device, distant
Control drone body is flown near the conducting wire for needing to clear up, and the arc of T-type angle is made by the camera in drone body
Slot and conductive contact, due to having electro-insulating rubber in arc groove, will not damage drone body without artificial climbing, this
When can be located in and need the near sites cleared up, at this moment start first motor and make the output end of first motor with cam
Rotation makes when the farthest both ends of cam contact the push rod being located at left and right sides of first motor respectively and squeeze push rod
It obtains direction of the push rod with the second sliding block compression second spring away from first motor to move, push rod is caused to squeeze u-bracket
Pressure, so that u-bracket does movement in a curve by the center of circle of the axle center of connecting shaft with spiral arm, brush plate and the second motor, is opened simultaneously
Dynamic second motor rotates the output shaft band movable knife disc of the second motor and blade, and brush plate can be to the winding near conducting wire at this time
Foreign matter clean, blade can cut the foreign matter of the winding near conducting wire, whole process to the cleaning of foreign matter have it is at low cost,
Risk bottom and high-efficient advantage.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is the utility model structure top view;
Fig. 3 is the utility model cutterhead and blade connection schematic diagram.
In figure: 1- drone body;2- wing;3- propeller;4- under-chassis;5- camera holder;6- camera;7- pedestal;8-
One impact-absorbing shell;The first sliding block of 9-;The first spring of 10-;11-T type angle;The second impact-absorbing shell of 12-;The second sliding block of 13-;14-
Two springs;15- first motor;16- cam;17- connecting rod;18- connecting shaft;19- spiral arm;20- brush plate;The second motor of 21-;
22- cutterhead;23- blade;24-U type bracket;25 push rods.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
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 embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, a kind of embodiment provided by the utility model: a kind of unmanned plane electrification cleaning wire foreign matter dress
It sets, including drone body 1, the outside of drone body 1 is fixedly installed with the wing 2 that quantity is four and is symmetric,
The top of wing 2 is fixedly installed with propeller 3, and it is four and in symmetrical point that the bottom of drone body 1, which is fixedly installed with quantity,
The under-chassis 4 of cloth, the bottom of drone body 1 and the centre for being located at four under-chassis 4 are fixedly installed with camera holder 5, the bottom of camera holder 5
Portion is fixedly installed with camera 6, and the side opposite with rear side under-chassis 4 of front side under-chassis 4 is fixedly connected with pedestal 7, the bottom of pedestal 7
It is fixedly installed with the first impact-absorbing shell 8 that quantity is two and is symmetric, the inner cavity of the first impact-absorbing shell 8 slidably connects first
Sliding block 9, the inner cavity of the first impact-absorbing shell 8 are fixedly installed with the first spring 10 that one end is fixedly connected with the first sliding block 9, the first sliding block
9 bottom is fixedly installed with the T-type angle 11 that one end is run through and extends to 8 bottom of the first impact-absorbing shell, and T-type angle 11 is by justifying
Cylindricality rod piece and rectangle block part composition, the top of cylindrical rod piece is fixedly connected with the first sliding block 9, the bottom of cylindrical rod piece and
Rectangle block part is fixedly connected, and rectangle block part bottom offers arc groove, and the inside of arc groove is fixedly installed with electro-insulating rubber, pedestal
7 top is fixedly installed with the second impact-absorbing shell 12 that quantity is two and is symmetric, the inner cavity sliding of the second impact-absorbing shell 12
It is connected with the second sliding block 13, the inner cavity of the second impact-absorbing shell 12 is fixedly installed with the second bullet that one end is fixedly connected with the second sliding block 13
Spring 14, the top of pedestal 7 and the centre for being located at two the second impact-absorbing shells 12 are fixedly installed with first motor 15, first motor 15
Model can be 42BYG250C-0151, be fixedly installed with cam 16 at the output shaft of first motor 15, the farthest both ends of cam 16
The bottom of the distance between two 25 opposite sides of push rod when distance is greater than 14 nature of second spring, wing 2 is fixedly mounted
There is connecting rod 17, be fixedly installed with connecting shaft 18 between the connecting rod 17 of two, right side between the connecting rod 17 of two, left side, even
The outside of spindle 18 is movably installed with spiral arm 19, and spiral arm 19 is made of annulus set and rectangle rod piece, the internal diameter of annulus set and connection
The diameter of axis 18 is adapted and annulus set is flexibly connected with connecting shaft 18, and the outside of annulus set is fixedly connected with rectangle rod piece, is revolved
The bottom of arm 19 is fixedly installed with brush plate 20, and two opposite sides of spiral arm 19 are fixedly installed with the second motor 21, the second electricity
The model of machine 21 can be 42BYG250C-0151, be fixedly installed with cutterhead 22 at the output shaft of the second motor 21, cutterhead 22 it is outer
Side is fixedly installed with blade 23, and the quantity of blade 23 is ten, and blade 23 is distributed in a ring, and the opposite side of two spiral arms 19 is solid
Dingan County is equipped with u-bracket 24, and two opposite sides of the second impact-absorbing shell 12 are movably installed with one end and run through and extend to U-shaped branch
The push rod 25 of 24 inside of frame, 25 ecto-entad of push rod sequentially pass through the second impact-absorbing shell 12, the second sliding block 13 and second spring 14, push away
Bar 25 is fixedly connected with the second sliding block 13, and the inside of u-bracket 24 is flexibly connected by shaft with push rod 25, unmanned plane electrification
Wire foreign matter device is cleared up, remote controlled drone ontology 1 is flown near the conducting wire for needing to clear up, and passes through the phase in drone body 1
Machine 6 makes the arc groove and conductive contact of T-type angle 11,, will not due to having electro-insulating rubber in arc groove without artificial climbing
Drone body 1 is damaged, the near sites for needing to clear up can be located at this time, at this moment starting first motor 15 makes
The output end for obtaining first motor 15 is rotated with cam 16, is located at 15 left side of first motor when the farthest both ends of cam 16 contact respectively
The push rod 25 of right two sides and when squeezing push rod 25 so that push rod 25 with the second sliding block 13 compress second spring 14 towards
Direction far from first motor 15 moves, and causes push rod 25 to squeeze u-bracket 24, so that u-bracket 24 is with spiral arm 19, hair
Brush 20 and the second motor 21 do movement in a curve by the center of circle of the axle center of connecting shaft 18, while starting the second motor 21 and making second
The output shaft band movable knife disc 22 and blade 23 of motor 21 rotate, and brush plate 20 can be clear to the foreign matter of the winding near conducting wire at this time
It sweeps, blade 23 can cut the foreign matter of the winding near conducting wire, and whole process has at low cost, risk to the cleaning of foreign matter
Bottom and high-efficient advantage.
In summary: unmanned plane electrification cleaning wire foreign matter device, remote controlled drone ontology 1, which is flown to, needs that clears up to lead
Near line, the arc groove and conductive contact of T-type angle 11 are made by the camera 6 in drone body 1, without manually climbing
It climbs, due to having electro-insulating rubber in arc groove, drone body 1 will not be damaged, can be located in need to clear up at this time
Near sites, at this moment start first motor 15 make the output end of first motor 15 with cam 16 rotate, when cam 16
When farthest both ends contact the push rod 25 for being located at 15 left and right sides of first motor respectively and squeeze push rod 25, so that push rod 25
Direction with the second sliding block 13 compression second spring 14 away from first motor 15 moves, and causes push rod 25 to u-bracket
24 squeeze, so that u-bracket 24 does arc as the center of circle using the axle center of connecting shaft 18 with spiral arm 19, brush plate 20 and the second motor 21
Line moves, while starting the second motor 21 and the output shaft band movable knife disc 22 of second motor 21 and blade 23 are rotated, at this time hair
Brush 20 can clean the foreign matter of the winding near conducting wire, and blade 23 can cut the foreign matter of the winding near conducting wire, entire mistake
Journey has at low cost, risk bottom and high-efficient advantage to the cleaning of foreign matter, solves and proposes in above-mentioned background technique
The dangerous property of traditional manner of cleaning up is high, the high problem low with cleaning efficiency of disposal costs.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (6)
1. a kind of unmanned plane electrification cleaning wire foreign matter device, including drone body (1), it is characterised in that: the unmanned plane
The wing (2) that quantity is four and is symmetric is fixedly installed on the outside of ontology (1), the top of wing (2) is fixedly mounted
Having propeller (3), the bottom of drone body (1) is fixedly installed with the under-chassis (4) that quantity is four and is symmetric, nobody
The bottom of machine ontology (1) and be located at four under-chassis (4) centre be fixedly installed with camera holder (5), the bottom of camera holder (5) is fixed
It being equipped with camera (6), the front side under-chassis (4) side opposite with the rear side under-chassis (4) is fixedly connected with pedestal (7),
The bottom of pedestal (7) is fixedly installed with the first impact-absorbing shell (8) that quantity is two and is symmetric, the first impact-absorbing shell (8)
Inner cavity slidably connects the first sliding block (9), and the inner cavity of the first impact-absorbing shell (8) is fixedly installed with one end and the first sliding block (9) are fixed
The first spring (10) of connection, the bottom of the first sliding block (9) is fixedly installed with one end and runs through and extend to the first impact-absorbing shell (8) bottom
The T-type angle (11) in portion is fixedly installed with the second impact-absorbing shell that quantity is two and is symmetric at the top of pedestal (7)
(12), the inner cavity of the second impact-absorbing shell (12) slidably connects the second sliding block (13), and the inner cavity of the second impact-absorbing shell (12) is fixedly mounted
The second spring (14) for thering is one end to be fixedly connected with the second sliding block (13), the top of pedestal (7) and be located at two the second impact-absorbing shells
(12) centre is fixedly installed with first motor (15), and cam (16), machine are fixedly installed at the output shaft of first motor (15)
The bottom of the wing (2) is fixedly installed with connecting rod (17), between the connecting rod (17) of two, left side with the connection of two, right side
It is fixedly installed with connecting shaft (18), is movably installed on the outside of connecting shaft (18) spiral arm (19) between bar (17), spiral arm (19)
Bottom be fixedly installed with brush plate (20), two opposite sides of spiral arm (19) are fixedly installed with the second motor (21), second
It is fixedly installed with cutterhead (22), is fixedly installed on the outside of cutterhead (22) blade (23) at the output shaft of motor (21), two rotations
The opposite side of arm (19) is fixedly installed with u-bracket (24), the activity installation of the opposite side of two the second impact-absorbing shells (12)
There is one end to run through and extend to the push rod (25) on the inside of u-bracket (24), the inside of u-bracket (24) passes through shaft and push rod
(25) it is flexibly connected.
2. a kind of unmanned plane electrification cleaning wire foreign matter device according to claim 1, it is characterised in that: the T-type is fixed
Position foot (11) is made of cylindrical rod piece and rectangle block part, and the top of cylindrical rod piece is fixedly connected with the first sliding block (9), cylinder
The bottom of shape rod piece is fixedly connected with rectangle block part, and rectangle block part bottom offers arc groove, and the inside of arc groove is fixedly mounted
There is electro-insulating rubber.
3. a kind of unmanned plane electrification cleaning wire foreign matter device according to claim 1, it is characterised in that: the cam
(16) the distance between two push rod (25) opposite sides when distance at farthest both ends is greater than second spring (14) nature.
4. a kind of unmanned plane electrification cleaning wire foreign matter device according to claim 1, it is characterised in that: the spiral arm
(19) it is made of annulus set and rectangle rod piece, the internal diameter of annulus set is adapted with the diameter of connecting shaft (18) and annulus is covered and connect
Axis (18) is flexibly connected, and the outside of annulus set is fixedly connected with rectangle rod piece.
5. a kind of unmanned plane electrification cleaning wire foreign matter device according to claim 1, it is characterised in that: the blade
(23) quantity is ten, and blade (23) is distributed in a ring.
6. a kind of unmanned plane electrification cleaning wire foreign matter device according to claim 1, it is characterised in that: the push rod
(25) ecto-entad sequentially passes through the second impact-absorbing shell (12), the second sliding block (13) and second spring (14), push rod (25) and second
Sliding block (13) is fixedly connected.
Priority Applications (1)
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CN201920187991.7U CN209516459U (en) | 2019-01-18 | 2019-01-18 | A kind of unmanned plane electrification cleaning wire foreign matter device |
Applications Claiming Priority (1)
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CN201920187991.7U CN209516459U (en) | 2019-01-18 | 2019-01-18 | A kind of unmanned plane electrification cleaning wire foreign matter device |
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CN209516459U true CN209516459U (en) | 2019-10-18 |
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CN201920187991.7U Expired - Fee Related CN209516459U (en) | 2019-01-18 | 2019-01-18 | A kind of unmanned plane electrification cleaning wire foreign matter device |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112217142A (en) * | 2020-10-27 | 2021-01-12 | 国网山东省电力公司济南供电公司 | High altitude cable foreign matter cleaning device that unmanned aerial vehicle carried on |
CN115036847A (en) * | 2022-07-25 | 2022-09-09 | 广东电网有限责任公司 | Power grid high-altitude obstacle clearing robot |
-
2019
- 2019-01-18 CN CN201920187991.7U patent/CN209516459U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112217142A (en) * | 2020-10-27 | 2021-01-12 | 国网山东省电力公司济南供电公司 | High altitude cable foreign matter cleaning device that unmanned aerial vehicle carried on |
CN115036847A (en) * | 2022-07-25 | 2022-09-09 | 广东电网有限责任公司 | Power grid high-altitude obstacle clearing robot |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
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: 20191018 Termination date: 20200118 |