CN203902839U - Electrified foreign object clearing unmanned aerial vehicle - Google Patents

Electrified foreign object clearing unmanned aerial vehicle Download PDF

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Publication number
CN203902839U
CN203902839U CN201420210493.7U CN201420210493U CN203902839U CN 203902839 U CN203902839 U CN 203902839U CN 201420210493 U CN201420210493 U CN 201420210493U CN 203902839 U CN203902839 U CN 203902839U
Authority
CN
China
Prior art keywords
support
hinged
foreign matter
handgrip
flexible motor
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
CN201420210493.7U
Other languages
Chinese (zh)
Inventor
娄磊
刘全宝
张新成
孙士年
刘加峰
王浩
冯迎春
尹国慧
刘玉海
王琳华
陈育淦
钮文彬
于宏志
亓海波
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.)
State Grid Corp of China SGCC
Maintenance Branch of State Grid Shandong Electric Power Co Ltd
Original Assignee
State Grid Corp of China SGCC
Maintenance Branch of State Grid Shandong Electric Power 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 State Grid Corp of China SGCC, Maintenance Branch of State Grid Shandong Electric Power Co Ltd filed Critical State Grid Corp of China SGCC
Priority to CN201420210493.7U priority Critical patent/CN203902839U/en
Application granted granted Critical
Publication of CN203902839U publication Critical patent/CN203902839U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

An electrified foreign object clearing unmanned aerial vehicle comprises a rotor wing aircraft; a first support is connected to the central position on the upper surface of the rotor wing aircraft; a fixing sleeve is connected to the top of the first support, and is connected with the lower end of a second support; a left gripper and a right gripper are hinged to the top of the second support; a left bracket and a right bracket are arranged on the second support respectively; a left telescopic motor is hinged to the left bracket; a right telescopic motor is hinged to the right bracket; the telescopic rod of the left telescopic motor is hinged to the middle of the left gripper; the telescopic rod of the right telescopic motor is hinged to the middle of the right gripper. A worker can operate the unmanned aerial vehicle while standing on the ground; the unmanned aerial vehicle can reach a position below a cable on which a foreign object is hung, and the left and right grippers are closed to grip the foreign object to clear the foreign object. As neither power failure nor climbing operation is needed during the whole process, the unmanned aerial vehicle can be used for clearing the foreign object hung on the cable safely, fast and conveniently; the safety of personnel and equipment is feasibly guaranteed; the work efficiency is greatly improved.

Description

Band electrical clean-up foreign matter unmanned plane
Technical field
The utility model relates to a kind of unmanned plane, specifically a kind of band electrical clean-up foreign matter unmanned plane.
Background technology
Grid equipment is exposed in natural environment, and foreign matter is suspended on wire, uses for a long time foreign matter may cause the damage of cable, and clearing up in time foreign matter is work important in electric power overhaul.At present, electrical equipment hangs the processing mode of foreign matter for passing through workman directly in cable on-line operation, this mode safety is low, the risk that has an accident is high, or adopt the equipment of walking on cable, weight of equipment is large, requires the weight capacity of cable to be eager to excel, and when operation, may cause damage to cable.Aforesaid way all needs ascend operation, and operating environment safety is low.
Utility model content
The purpose of this utility model is to provide a kind of band electrical clean-up foreign matter unmanned plane, can solve in the time that cleaning electrical equipment hangs foreign matter that hidden danger is serious, reliability reduces problem.
The utility model for achieving the above object, be achieved through the following technical solutions: band electrical clean-up foreign matter unmanned plane, comprise rotor craft, rotor craft upper surface center connects the first support, first top of the trellis is connected and fixed cover, fixed cover is connected with the lower end of the second support, the hinged left handgrip in top and the right handgrip of the second support, left socle and right support are set respectively on the second support, the flexible motor in a hinged left side on left socle, the flexible motor in the hinged right side on right support, the middle part of the hinged left handgrip of expansion link of left flexible motor, the middle part of the hinged right handgrip of expansion link of right flexible motor.
In order further to realize the purpose of this utility model, can also be by the following technical solutions: a side of described fixed cover arranges through hole, bottom one side of the second support arranges hold down groove, the first support bottom arranges L-type fixed block, L-type fixed block is made up of horizon bar and vertical plate, horizontal plate is fixedly mounted on the sidepiece of the first support, vertically bar is arranged on the end of horizon bar, lower flexible motor is set on the top of the vertical plate of L-type fixed block, the expansion link of lower flexible motor coordinates with hold down groove through through hole, the second support one side connects one end of insulating cord, the first support one side arranges twine carrier, the rope body of insulating cord is positioned in twine carrier.The end of described left handgrip arranges grapple.The end of described right handgrip arranges grapple.Cantilever one end connection metal ring of described rotor craft.
The utility model has the advantage of: face the utility model by staff on ground and operate on ground, the utility model is accurately arrived under the cable of foreign matter, by left handgrip and have the closure of handgrip that foreign matter is caught, thereby complete the work of cleaning foreign matter, whole process is without having a power failure and ascend operation, just can be safely, fast, easily the foreign matter hanging on wire is eliminated, conscientiously ensured the safety of personnel and equipment, greatly improved work efficiency.The utility model contacts with cable, avoids directly contact to the pressure of cable, can not damage cable.The utility model can as required, separate by remote control the second support with fixed cover, make handgrip depart from unmanned plane, emits insulating cord simultaneously, and staff can take off foreign matter by insulating cord.The utility model also has advantages of compactness simple for structure, cheap for manufacturing cost and easy to use.
Brief description of the drawings
Fig. 1 is main TV structure schematic diagram of the present utility model; Fig. 2 is the plan structure schematic diagram of Fig. 1; Fig. 3 is the I portion enlarged drawing of Fig. 2; Fig. 4 is the II portion enlarged drawing of Fig. 1; Fig. 5 is the III portion enlarged drawing of Fig. 1.
Mark explanation: right flexible 18 times flexible motor 19 through holes of motor 13 right support 14 left socle 15 second support 16 fixed cover 17 hold down grooves of the right handgrip 8 grapple 9L type fixed block left flexible motor 12 of 10 first support 11 of the left handgrip 7 of 1 rotor craft 2 cantilever 3 becket 4 twine carrier 5 insulating cord 6.
Detailed description of the invention
Band electrical clean-up foreign matter unmanned plane, as Fig. 1, shown in Fig. 2 and Fig. 4, comprise rotor craft 1, rotor craft 1 upper surface center connects the first support 10, the first support 10 tops are connected and fixed cover 16, fixed cover 16 is connected with the lower end of the second support 15, the hinged left handgrip 6 in top and the right handgrip 7 of the second support 15, left socle 14 and right support 13 are set respectively on the second support 15, the flexible motor 11 in a hinged left side on left socle 14, the flexible motor 12 in the hinged right side on right support 13, the middle part of the hinged left handgrip 6 of expansion link of left flexible motor 11, the middle part of the hinged right handgrip 7 of expansion link of right flexible motor 12.One side of described fixed cover 16 arranges through hole 19, bottom one side of the second support 15 arranges hold down groove 17, the first support 10 bottoms arrange L-type fixed block 9, L-type fixed block 9 is made up of horizon bar and vertical plate, horizontal plate is fixedly mounted on the sidepiece of the first support 10, vertically bar is arranged on the end of horizon bar, lower flexible motor 18 is set on the top of the vertical plate of L-type fixed block 9, the expansion link of lower flexible motor 18 coordinates with hold down groove 17 through through hole 19, the second support 15 1 sides connect one end of insulating cord 5, the first support 10 1 sides arrange twine carrier 4, the rope body of insulating cord 5 is positioned in twine carrier 4.As shown in Figure 3, the end of described left handgrip 6 arranges grapple 8.The end of described right handgrip 7 arranges grapple 8.Cantilever 2 one end connection metal rings 3 of described rotor craft 1.The utility model is in the time of work, flown to below, electric wire foreign matter place by rotor craft 1, the expansion link of left contracting motor 11 and right flexible motor 12 stretches out, controlling respectively left handgrip 6 and right handgrip 7 opens, within the crawl scope of electric wire foreign matter in left handgrip 6 and right handgrip 7 time, the expansion link of left contracting motor 11 and right flexible motor 12 is retracted, and controls respectively left handgrip 6 and right handgrip 7 and draws in, and electric wire foreign matter is captured by left handgrip 6 and right handgrip 7.Rotor craft 1 declines electric wire foreign matter is removed.When electric wire foreign matter is connected too firmly with electric wire, cannot take off by the strength of rotor craft 1 time, lower flexible motor 18 shrinks, and the expansion link of lower flexible motor 18 and hold down groove 17 are departed from, and now the second support 15 separates with fixed cover 16.Rotor craft 1 declines, and the insulating cord 5 in twine carrier 4 is released, and one end of insulating cord 5 connects second support 15 other ends is put to ground, can be by drawing insulating cord 5 that electric wire foreign matter is taken off the staff on ground.The end of described left handgrip 6 arranges grapple 8.The end of described right handgrip 7 arranges grapple 8.Make left handgrip 6 and right handgrip 7 can capture more easily electric wire foreign matter.Cantilever 2 one end connection metal rings 3 of described rotor craft 1, can shielding wire highfield around, make to be with electrical clean-up foreign matter unmanned plane under highfield, to work.The utility model is without having a power failure and ascend operation, just can be safely, fast, easily the foreign matter hanging on wire is eliminated, conscientiously ensure the safety of personnel and equipment, and greatly improve work efficiency.The utility model also has advantages of compactness simple for structure, cheap for manufacturing cost and easy to use.
The technical solution of the utility model is not restricted in the scope of embodiment described in the utility model.The utility model not technology contents of detailed description is known technology.

Claims (5)

1. band electrical clean-up foreign matter unmanned plane, it is characterized in that: comprise rotor craft (1), rotor craft (1) upper surface center connects the first support (10), the first support (10) top is connected and fixed cover (16), fixed cover (16) is connected with the lower end of the second support (15), the hinged left handgrip in top (6) of the second support (15) and right handgrip (7), left socle (14) and right support (13) are set respectively on the second support (15), the flexible motor (11) in the upper hinged left side of left socle (14), the flexible motor (12) in the upper hinged right side of right support (13), the middle part of the hinged left handgrip of expansion link (6) of left flexible motor (11), the middle part of the hinged right handgrip of expansion link (7) of right flexible motor (12).
2. band electrical clean-up foreign matter unmanned plane according to claim 1, it is characterized in that: a side of described fixed cover (16) arranges through hole (19), bottom one side of the second support (15) arranges hold down groove (17), the first support (10) bottom arranges L-type fixed block (9), L-type fixed block (9) is made up of horizon bar and vertical plate, horizontal plate is fixedly mounted on the sidepiece of the first support (10), vertically bar is arranged on the end of horizon bar, lower flexible motor (18) is set on the top of the vertical plate of L-type fixed block (9), the expansion link of lower flexible motor (18) coordinates with hold down groove (17) through through hole (19), the second support (15) one sides connect one end of insulating cord (5), the first support (10) one sides arrange twine carrier (4), the rope body of insulating cord (5) is positioned in twine carrier (4).
3. band electrical clean-up foreign matter unmanned plane according to claim 1, is characterized in that: the end of described left handgrip (6) arranges grapple (8).
4. band electrical clean-up foreign matter unmanned plane according to claim 1, is characterized in that: the end of described right handgrip (7) arranges grapple (8).
5. band electrical clean-up foreign matter unmanned plane according to claim 1, is characterized in that: cantilever (2) one end connection metal ring (3) of described rotor craft (1).
CN201420210493.7U 2014-04-28 2014-04-28 Electrified foreign object clearing unmanned aerial vehicle Expired - Fee Related CN203902839U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420210493.7U CN203902839U (en) 2014-04-28 2014-04-28 Electrified foreign object clearing unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420210493.7U CN203902839U (en) 2014-04-28 2014-04-28 Electrified foreign object clearing unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN203902839U true CN203902839U (en) 2014-10-29

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ID=51777126

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420210493.7U Expired - Fee Related CN203902839U (en) 2014-04-28 2014-04-28 Electrified foreign object clearing unmanned aerial vehicle

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CN (1) CN203902839U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106986027A (en) * 2017-05-10 2017-07-28 佛山市神风航空科技有限公司 A kind of aerial sports unmanned plane
US11368002B2 (en) 2016-11-22 2022-06-21 Hydro-Quebec Unmanned aerial vehicle for monitoring an electrical line

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11368002B2 (en) 2016-11-22 2022-06-21 Hydro-Quebec Unmanned aerial vehicle for monitoring an electrical line
CN106986027A (en) * 2017-05-10 2017-07-28 佛山市神风航空科技有限公司 A kind of aerial sports unmanned plane

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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: 20141029

Termination date: 20180428