CN208602702U - A kind of cable line inspection device - Google Patents
A kind of cable line inspection device Download PDFInfo
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- CN208602702U CN208602702U CN201821143725.6U CN201821143725U CN208602702U CN 208602702 U CN208602702 U CN 208602702U CN 201821143725 U CN201821143725 U CN 201821143725U CN 208602702 U CN208602702 U CN 208602702U
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- propeller
- face
- wing
- rotation axis
- empennage
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The utility model relates to a kind of cable line inspection devices, including wing, propeller, empennage, rudder, fuselage, head, photoelectric nacelle and integrated gondola, the both sides of the fuselage are equipped with for providing the wing of lift, the upper surface of the wing is equipped with solar panel, the front end face of the wing is equipped with propeller runing rest, the end face of the propeller runing rest is disposed with for providing the propeller of lift, the tail portion of the fuselage is provided with empennage, the end face of empennage is equipped with solar panel, rudder for controlling heading is installed in the middle part of empennage, the left and right end face of the empennage is mounted on the fixed bracket of propeller, the support bracket fastened other end of the propeller is equipped with for providing the propeller of lift, total, the utility model has structure simple, it is easy to operate, it patrols The long advantage of ETS estimated time of sailing.
Description
Technical field
The utility model belongs to electrical circuitry equipment technical field, and in particular to a kind of cable line inspection device.
Background technique
Line inspection be track walker's more system and it is orderly check cable run and its equipment, route is installed when tour
The important link and content of machinery equipment management work are the most basic work for guaranteeing route and its equipment safety operation, purpose
Be check for defect or security risk to understand and grasp route health status, running environment in time, while for route and
The maintenance of its equipment, defect elimination plan provide the foundation of science, traditional artificial patrolling method not only heavy workload but also condition is difficult
Hardship, the especially inspection of the power transmission line to mountain area and across great rivers, and in the case where specific disaster occurs, manually patrol
Line needs take longer time there is unmanned plane line inspection device, but pass with the development of technology with higher cost now
The unmanned plane line inspection device of system has no idea effectively to make an inspection tour cable when haze item is more serious, when during line walking
It was found that processing mode traditional when thering is foreign matter to be suspended on cable be foreign matter is cleared up by flame device, but near forest or
It carries out cleaning to foreign matter using flame device when nearby combustible is more to be possible to cause fire, while foreign matter is during the burning process
Also it pollutes the environment.
Utility model content
The problem of purpose of the utility model is to solve proposed in background technique, and provide a kind of with structure letter
Single, easy to operate, the cruise time is long cable line inspection device.
A kind of cable line inspection device that the purpose of this utility model is realized in, including wing, propeller, empennage, side
To rudder, fuselage, head, photoelectric nacelle and integrated gondola, the both sides of the fuselage are equipped with for providing the wing of lift, institute
The upper surface for the wing stated is equipped with solar panel, and the front end face of the wing is equipped with propeller runing rest, institute
The end face for the propeller runing rest stated is disposed with for providing the propeller of lift,
The tail portion of the fuselage is provided with empennage, and the end face of empennage is equipped with solar panel, the middle part peace of empennage
Equipped with the rudder for controlling heading, the left and right end face of the empennage is mounted on the fixed bracket of propeller, described
The support bracket fastened other end of propeller be equipped with for providing the propeller of lift,
The front end face of the fuselage is equipped with head, and the one of the inside of the fuselage and the head inner space
Part is equipped with battery, and the top of the head is equipped with the protection shell for protecting internal electronic equipment, described
The inside of protection shell is equipped with communication module, and airborne computer is equipped between communication module and battery,
The lower end surface of the fuselage is equipped with the integrated gondola for making an inspection tour cable, integrates the lower end surface installation of gondola
There is photoelectric nacelle, the end face of the photoelectric nacelle is equipped with three-dimensional scanner, the end face peace of the three-dimensional scanner
Equipped with navigation module, the outer end face of the integrated gondola is equipped with the manipulator for clearing up sundries, one end peace of manipulator
Equipped with automatic scissors.
The wing is made of port wing and starboard wing, is equipped at the medium position of the front end face of the port wing
The propeller runing rest is equipped with the propeller rotation branch at the medium position of the front end face of the starboard wing
Frame, the propeller in the middle part of propeller runing rest and the starboard wing front end face in the middle part of the port wing front end face rotate
Bracket is symmetrical relative to the medium line of the wing.
The lower end of the propeller runing rest, which is provided with, is connected and fixed plate, it is described be connected and fixed plate by welding with
The wing is fixedly connected, and the lower end surface for being connected and fixed plate is flushed with the lower end surface of the wing, is connected and fixed the end of plate
Face is welded with two rotation axis fixing plates at a distance of 5cm-15cm, is equipped with rotation between two rotation axis fixing plates
Axis, the end face of the rotation axis fixing plate are provided with coaxially arranged with the rotation axis and are used to provide power for rotation axis
Electric rotating motivation, the other end for rotating axis fixing plate is provided with the decoder coaxially arranged with the rotation axis, described
Rotation axis end face on the promising propeller is installed the propeller motor of power, the propeller motor is provided
Diameter with the lower end surface from rotation axis being equidistant to the upper surface for being connected and fixed plate.
The fixed bracket of the propeller is fixedly connected by bolt with empennage, the support bracket fastened other end setting of propeller
Have for providing the propeller motor of power for the propeller.
The top of the rudder is equipped with the signal lamp for reminding other air equipments, signal lamp and the solar energy
Solar panel is electrically connected by electric installation, and signal lamp is connect with the airborne computer.
The inner surface of the fuselage and head is equipped with the shielded layer of anti-electromagnetic interference.
The communication module includes PCM remote-control receiver, data radio station, satellite communication module, GPRS module, 3G and 4G
Module, the airborne computer include control module, steering engine controller, gyroscope and accelerometer.
The navigation module includes GPS navigation module, Beidou navigation module, speed measuring module, barometertic altimeter, ranging dress
It sets.
The three-dimensional scanner is EH-MR3D 3 D laser scanning radar oblique photograph camera, and the photoelectricity is hung
Cabin is equipped with storage facilities, optical camera, infrared thermal imager and camera, and the camera is equipped with filter and SSD
Penetrating Fog module.
The manipulator is fixedly connected by bolt with the integrated gondola, and manipulator is mounted on the side of integrated gondola
The projection of line plane composed by the head and the wing at end face, manipulator and integrated gondola center and institute
The angle of the center line for the head stated is between 30 degree to 60 degree, and manipulator is sc-3601 electric shear, the maximum of automatic scissors
Shearing diameter is 30mm, openings of sizes 3cm.
The utility model has the beneficial effects that
It is bigger to make an inspection tour range, is not limited by landform, can fly to and manually be difficult to the comprehensive tower bar of the place arrived at progress
Inspection.
From the visible light and infrared equipment that unmanned plane carries are carried out from aerial angle, provided for defect analysis multi-faceted
Foundation.
The operating efficiency of unmanned plane is high, timeliness more like, nobody when return picture in real time, it is timely to facilitate electrical power line inspector
It finds the problem.
Solar panel can provide energy during unmanned plane during flying for unmanned plane, increase the boat of unmanned plane
Journey.
Unmanned plane is equipped with longer hang gliding, and unmanned plane can close engine dependence after the speed for reaching certain
Wing continues to slide longer distance under the action of inertia, increases the voyage of unmanned plane.
Unmanned plane installation manipulator the foreign matter on cable can be disposed, traditional foreign matter reset mode be mostly according to
By the mode of baked wheaten cake, fire is easily caused, manipulator removes foreign matter by electric shear, avoids the appearance of fire hazard.
The camera of unmanned plane installation has optics and algorithm handle except haze to image simultaneously, haze sky still more
Enough normal line walkings.
Non bearing structure, shell and the insignificant metal parts of unmanned plane are replaced using composite material and plastics,
The overall weight for mitigating unmanned plane, increases the voyage of unmanned plane, total, and the utility model has structure simple, easy to operate, patrol
The long advantage of ETS estimated time of sailing.
Detailed description of the invention
Fig. 1 is a kind of top view of cable line inspection device of the utility model.
Fig. 2 is a kind of schematic diagram of cable line inspection device of the utility model.
Fig. 3 is a kind of front view of cable line inspection device of the utility model.
Fig. 4 is a kind of front view of the propeller runing rest of cable line inspection device of the utility model.
Fig. 5 is a kind of side view of the propeller runing rest of cable line inspection device of the utility model.
Fig. 6 is a kind of schematic diagram of the integrated gondola of cable line inspection device of the utility model.
In figure: 1, wing 101, port wing 102, starboard wing 2, propeller runing rest 201, be connected and fixed plate
202, electric rotating motivation 203, decoder 204, rotation axis fixing plate 205, rotation axis 206, propeller motor 3, spiral
Paddle 4, propeller fixed bracket 5, solar panel 6, empennage 7, rudder 8, fuselage 9, head 10, battery
11, airborne computer 12, communication module 13, protection shell 14, integrated gondola 1401, automatic scissors 1402, manipulator
1403, three-dimensional scanner 1404, navigation module 15, photoelectric nacelle.
Specific embodiment
The technical solutions in the embodiments of the present invention are clearly and completely described with reference to the accompanying drawing, it is clear that institute
The embodiment of description is only the utility model a part of the embodiment, rather than whole embodiments, based in the utility model
Embodiment, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, all
Belong to the range of the utility model protection.
Embodiment 1
As shown in Figure 1, Figure 2, Fig. 3, Fig. 4, Fig. 5 and a kind of cable line inspection device shown in fig. 6, including wing 1, propeller 3, tail
The wing 6, rudder 7, fuselage 8, head 9, photoelectric nacelle 15 and integrated gondola 14, the both sides of fuselage 8 are equipped with for providing lift
Wing 1, the upper surface of wing 1 is equipped with solar panel 5, and the front end face of wing 1 is equipped with propeller runing rest 2,
The end face of propeller runing rest 2 is disposed with for providing the propeller 3 of lift, and the tail portion of fuselage 8 is provided with empennage 6, empennage 6
End face solar panel 5 is installed, the middle part of empennage 6 is equipped with the rudder 7 for controlling heading, empennage 6
Left and right end face is mounted on the fixed bracket 4 of propeller, and the other end of the fixed bracket 4 of propeller is equipped with for providing the spiral shell of lift
Paddle 3 is revolved, the front end face of fuselage 8 is equipped with head 9, and a part of 9 inner space of inside and head of fuselage 8 is equipped with battery
10, the top of head 9 is equipped with the protection shell 13 for protecting internal electronic equipment, and the inside of protection shell 13 is equipped with logical
Module 12 is interrogated, airborne computer 11 is installed between communication module 12 and battery 10,
The lower end surface of fuselage 8 is equipped with the integrated gondola 14 for making an inspection tour cable, integrates the lower end surface installation of gondola 14
There is photoelectric nacelle 15, the end face of photoelectric nacelle 15 is equipped with three-dimensional scanner 1403, the end face peace of three-dimensional scanner 1403
Equipped with navigation module 1404, the outer end face of integrated gondola 14 is equipped with the manipulator 1402 for clearing up sundries, manipulator 1402
One end automatic scissors 1401 are installed.
Wing 1 is made of port wing 101 and starboard wing 102, is equipped with spiral shell at the medium position of the front end face of port wing 101
Paddle runing rest 2 is revolved, propeller runing rest 2 is installed at the medium position of the front end face of starboard wing 102, before port wing 101
The propeller runing rest 2 in the middle part of propeller runing rest 2 and 102 front end face of starboard wing in the middle part of end face is relative to wing 1
Medium line is symmetrical；
The lower end of propeller runing rest 2, which is provided with, is connected and fixed plate 201, is connected and fixed plate 201 and passes through welding and wing 1
It is fixedly connected, the lower end surface for being connected and fixed plate 201 is flushed with the lower end surface of wing 1, and the end face for being connected and fixed plate 201 is welded with two
A rotation axis fixing plate 204 at a distance of 5cm-15cm is equipped with rotation axis 205, rotation axis between two rotation axis fixing plates 204
The end face of fixed plate 204 is provided with coaxially arranged with rotation axis 205 and is used to provide the electric rotating motivation of power for rotation axis 205
202, the other end of rotation axis fixing plate 204 is provided with the decoder 203 coaxially arranged with rotation axis 205, rotation axis 205
Promising propeller 3 is installed on end face, the propeller motor 206 of power is provided, the diameter of propeller motor 206 with from rotation
The lower end surface of axis 205 is equidistant to the upper surface for being connected and fixed plate 201；
The fixed bracket 4 of propeller is fixedly connected by bolt with empennage 6, and the other end of the fixed bracket 4 of propeller is provided with
For providing the propeller motor 206 of power for propeller 3；The top of rudder 7, which is equipped with, reminds other air equipments
Signal lamp, signal lamp are electrically connected with solar panel 5 by electric installation, and signal lamp is connect with airborne computer 11；Fuselage 8
The shielded layer of anti-electromagnetic interference is equipped with the inner surface of head 9；Communication module 12 include PCM remote-control receiver, data radio station,
Satellite communication module, GPRS module, 3G and 4G module, airborne computer 11 include control module, steering engine controller, gyroscope and
Accelerometer；Navigation module 1404 includes GPS navigation module, Beidou navigation module, speed measuring module, barometertic altimeter, ranging dress
It sets；Three-dimensional scanner 1403 is EH-MR3D 3 D laser scanning radar oblique photograph camera, and photoelectric nacelle 15 is equipped with storage
Equipment, optical camera, infrared thermal imager and camera, camera are equipped with filter and SSD Penetrating Fog module；Manipulator 1402
Be fixedly connected by bolt with integrated gondola 14, manipulator 1402 is mounted on the side end face of integrated gondola 14, manipulator 1402 with
The angle of the center line of the projection and head 9 of line plane composed by head 9 and wing 1 at integrated 14 center of gondola is 30
It spends between 60 degree, the automatic scissors 1401 of 1402 one end of manipulator installation are sc-3601 electric shear, automatic scissors 1401
Maximum shear diameter is 30mm, openings of sizes 3cm.
The utility model is equipped on the both sides of fuselage 8 for providing the wing 1 of lift, the upper surface of wing 1 when implementing
Solar panel 5 is installed, the front end face of wing 1 is equipped with propeller runing rest 2, the end face of propeller runing rest 2
It is disposed with for providing the propeller 3 of lift, the tail portion of fuselage 8 is provided with empennage 6, and the end face of empennage 6 is equipped with solar-electricity
Pond plate 5, the middle part of empennage 6 are equipped with the rudder 7 for controlling heading, and the left and right end face of empennage 6 is mounted on spiral
Paddle fixes bracket 4, and the other end of the fixed bracket 4 of propeller is equipped with for providing the propeller 3 of lift, the front end face of fuselage 8
Head 9 is installed, a part of 9 inner space of inside and head of fuselage 8 is equipped with battery 10, the top installation of head 9
There is the protection shell 13 for protecting internal electronic equipment, the inside of protection shell 13 is equipped with communication module 12, communication module
Airborne computer 11 is installed between 12 and battery 10,
The lower end surface of fuselage 8 is equipped with the integrated gondola 14 for making an inspection tour cable, integrates the lower end surface installation of gondola 14
There is photoelectric nacelle 15, the end face of photoelectric nacelle 15 is equipped with three-dimensional scanner 1403, the end face peace of three-dimensional scanner 1403
Equipped with navigation module 1404, the outer end face of integrated gondola 14 is equipped with the manipulator 1402 for clearing up sundries, manipulator 1402
One end automatic scissors 1401 are installed.
Wing 1 is made of port wing 101 and starboard wing 102, is equipped with spiral shell at the medium position of the front end face of port wing 101
Paddle runing rest 2 is revolved, propeller runing rest 2 is installed at the medium position of the front end face of starboard wing 102, before port wing 101
The propeller runing rest 2 in the middle part of propeller runing rest 2 and 102 front end face of starboard wing in the middle part of end face is relative to wing 1
Medium line is symmetrical；
The lower end of propeller runing rest 2, which is provided with, is connected and fixed plate 201, is connected and fixed plate 201 and passes through welding and wing 1
It is fixedly connected, the lower end surface for being connected and fixed plate 201 is flushed with the lower end surface of wing 1, and the end face for being connected and fixed plate 201 is welded with two
A rotation axis fixing plate 204 at a distance of 5cm-15cm is equipped with rotation axis 205, rotation axis between two rotation axis fixing plates 204
The end face of fixed plate 204 is provided with coaxially arranged with rotation axis 205 and is used to provide the electric rotating motivation of power for rotation axis 205
202, the other end of rotation axis fixing plate 204 is provided with the decoder 203 coaxially arranged with rotation axis 205, rotation axis 205
Promising propeller 3 is installed on end face, the propeller motor 206 of power is provided, the diameter of propeller motor 206 with from rotation
The lower end surface of axis 205 is equidistant to the upper surface for being connected and fixed plate 201；
The fixed bracket 4 of propeller is fixedly connected by bolt with empennage 6, and the other end of the fixed bracket 4 of propeller is provided with
For providing the propeller motor 206 of power for propeller 3；The top of rudder 7, which is equipped with, reminds other air equipments
Signal lamp, signal lamp are electrically connected with solar panel 5 by electric installation, and signal lamp is connect with airborne computer 11；Fuselage 8
The shielded layer of anti-electromagnetic interference is equipped with the inner surface of head 9；Communication module 12 include PCM remote-control receiver, data radio station,
Satellite communication module, GPRS module, 3G and 4G module, airborne computer 11 include control module, steering engine controller, gyroscope and
Accelerometer；Navigation module 1404 includes GPS navigation module, Beidou navigation module, speed measuring module, barometertic altimeter, ranging dress
It sets；Three-dimensional scanner 1403 is EH-MR3D 3 D laser scanning radar oblique photograph camera, and photoelectric nacelle 15 is equipped with storage
Equipment, optical camera, infrared thermal imager and camera, camera are equipped with filter and SSD Penetrating Fog module；Manipulator 1402
Be fixedly connected by bolt with integrated gondola 14, manipulator 1402 is mounted on the side end face of integrated gondola 14, manipulator 1402 with
The angle of the center line of the projection and head 9 of line plane composed by head 9 and wing 1 at integrated 14 center of gondola is 30
It spends between 60 degree, the automatic scissors 1401 of 1402 one end of manipulator installation are sc-3601 electric shear, automatic scissors 1401
Maximum shear diameter is 30mm, openings of sizes 3cm；
When work, ground control centre uploads flight plan to the communication module 12 of UAV flight, and communication module 12 connects
It receives flight plan and transmits data to airborne computer 11, while the solar panel 5 of 1 top of wing of unmanned plane later
It converts solar energy into electrical energy and is stored in battery 10, then airborne computer 11 is issued to propeller runing rest 2 and is ordered,
Decoder 203 will be sent to electric rotating motivation 202 after data processing, electric rotating motivation 202, which is started to work, drives rotary shaft 205
Propeller motor 206 is gone to vertical means by horizontality by rotation, and then airborne computer 11 is to propeller runing rest 2
Instruction is issued with the propeller motor 206 on the fixed bracket 4 of propeller, propeller motor 206 is started to work, propeller electricity
Motivation 206 drives propeller 3 to work, and with the raising of 3 revolving speed of propeller, unmanned plane starts to go up to the air, and unmanned plane rises to centainly
Airborne computer 11 is issued to propeller runing rest 2 and is instructed after height, and decoder 203 will be sent to rotation after data processing
Turn motor 202, electric rotating motivation 202, which is started to work, drives the rotation of rotary shaft 205 by propeller motor 206 by plumbness
Horizontal device is gone to, while airborne computer 11 issues to reduce and rotates speed to the propeller motor 206 of the fixed bracket 4 of propeller
The order of degree, then the propeller motor 206 of the fixed bracket 4 of propeller reduces rotation speed after receiving instruction, at this time
Unmanned plane switchs to horizontal flight, the location information that the 1404 real-time reception navigation satellite of navigation module of unmanned plane is sent, airborne meter
Calculation machine 11 controls rudder 7 to control the direction of unmanned plane during flying, and unmanned plane is made to fly to the starting point for starting line walking, navigation module
Estimate module and barometertic altimeter in 1404 send airborne computer 11 for speed and high-speed data in real time, and unmanned plane is flying
Airborne computer 11 is issued to integrated gondola 14 and is instructed when to line walking task segment starting point, and integrated gondola 14 receives photoelectricity after instruction
Gondola 15 is started to work, and the optical camera of photoelectric nacelle 15 and camera are started to work during the day, what photoelectric nacelle 15 was shot
Picture passes ground control centre back by communication module 12, and the staff of ground control centre is according to the image passed back to power grid
Operating status judged that, when unmanned plane flies to the top of steel tower, ground control centre is diversion instruction to unmanned plane sending,
After unmanned plane receives instruction by communication module 12, airborne computer 11 is issued to propeller runing rest 2 and is ordered, decoding
Device 203 will be sent to electric rotating motivation 202 after data processing, electric rotating motivation 202, which is started to work, drives rotary shaft 205 to rotate
Propeller motor 206 is gone into vertical means by horizontality, four propellers 3 are plumbness, then unmanned plane around
Steel tower does annular flight, and the optical camera and camera of photoelectric nacelle 15 shoot the key equipment on the top of steel tower, so
The image of shooting is returned by ground control centre by communication module 12 afterwards, the staff of ground control centre is according to shooting
The case where image viewing tower bar, insulator chain and wire clamp, whether observation tower bar deforms, airborne when needing to model tower bar
After computer 11 receives the modeling instruction of ground control centre sending by communication module 12, airborne computer 11 is to three-dimensional
Scanning means 1403 issues instruction, then three-dimensional scanner 1403, which is scanned tower bar, passes through communication mould the data of scanning
Block 12 passes back to ground control centre, and ground control centre receives after data and to carry out three to the tower bar of scanning on computer again
Dimension modeling, by the route three-dimensional visualization of tour, convenient for intuitively browsing and inquiring any tower bar basic information.
Embodiment 2
As shown in Figure 1, Figure 2, it is equipped on the both sides of fuselage 8 for providing the wing 1 of lift shown in Fig. 3, Fig. 4, Fig. 5 and Fig. 6,
The upper surface of wing 1 is equipped with solar panel 5, and the front end face of wing 1 is equipped with propeller runing rest 2, propeller rotation
The end face for turning bracket 2 is disposed with for providing the propeller 3 of lift, and the tail portion of fuselage 8 is provided with empennage 6, the end face peace of empennage 6
Equipped with solar panel 5, the middle part of empennage 6 is equipped with the rudder 7 for controlling heading, the left and right end face of empennage 6
It is mounted on the fixed bracket 4 of propeller, the other end of the fixed bracket 4 of propeller is equipped with for providing the propeller 3 of lift, machine
The front end face of body 8 is equipped with head 9, and a part of 9 inner space of inside and head of fuselage 8 is equipped with battery 10, head 9
Top the protection shell 13 for protecting internal electronic equipment is installed, the inside of protection shell 13 is equipped with communication module
12, airborne computer 11 is installed between communication module 12 and battery 10,
The lower end surface of fuselage 8 is equipped with the integrated gondola 14 for making an inspection tour cable, integrates the lower end surface installation of gondola 14
There is photoelectric nacelle 15, the end face of photoelectric nacelle 15 is equipped with three-dimensional scanner 1403, the end face peace of three-dimensional scanner 1403
Equipped with navigation module 1404, the outer end face of integrated gondola 14 is equipped with the manipulator 1402 for clearing up sundries, manipulator 1402
One end automatic scissors 1401 are installed.
Wing 1 is made of port wing 101 and starboard wing 102, is equipped with spiral shell at the medium position of the front end face of port wing 101
Paddle runing rest 2 is revolved, propeller runing rest 2 is installed at the medium position of the front end face of starboard wing 102, before port wing 101
The propeller runing rest 2 in the middle part of propeller runing rest 2 and 102 front end face of starboard wing in the middle part of end face is relative to wing 1
Medium line is symmetrical；
The lower end of propeller runing rest 2, which is provided with, is connected and fixed plate 201, is connected and fixed plate 201 and passes through welding and wing 1
It is fixedly connected, the lower end surface for being connected and fixed plate 201 is flushed with the lower end surface of wing 1, and the end face for being connected and fixed plate 201 is welded with two
A rotation axis fixing plate 204 at a distance of 5cm-15cm is equipped with rotation axis 205, rotation axis between two rotation axis fixing plates 204
The end face of fixed plate 204 is provided with coaxially arranged with rotation axis 205 and is used to provide the electric rotating motivation of power for rotation axis 205
202, the other end of rotation axis fixing plate 204 is provided with the decoder 203 coaxially arranged with rotation axis 205, rotation axis 205
Promising propeller 3 is installed on end face, the propeller motor 206 of power is provided, the diameter of propeller motor 206 with from rotation
The lower end surface of axis 205 is equidistant to the upper surface for being connected and fixed plate 201；
The fixed bracket 4 of propeller is fixedly connected by bolt with empennage 6, and the other end of the fixed bracket 4 of propeller is provided with
For providing the propeller motor 206 of power for propeller 3；The top of rudder 7, which is equipped with, reminds other air equipments
Signal lamp, signal lamp are electrically connected with solar panel 5 by electric installation, and signal lamp is connect with airborne computer 11；Fuselage 8
The shielded layer of anti-electromagnetic interference is equipped with the inner surface of head 9；Communication module 12 include PCM remote-control receiver, data radio station,
Satellite communication module, GPRS module, 3G and 4G module, airborne computer 11 include control module, steering engine controller, gyroscope and
Accelerometer；Navigation module 1404 includes GPS navigation module, Beidou navigation module, speed measuring module, barometertic altimeter, ranging dress
It sets；Three-dimensional scanner 1403 is EH-MR3D 3 D laser scanning radar oblique photograph camera, and photoelectric nacelle 15 is equipped with storage
Equipment, optical camera, infrared thermal imager and camera, camera are equipped with filter and SSD Penetrating Fog module；Manipulator 1402
Be fixedly connected by bolt with integrated gondola 14, manipulator 1402 is mounted on the side end face of integrated gondola 14, manipulator 1402 with
The angle of the center line of the projection and head 9 of line plane composed by head 9 and wing 1 at integrated 14 center of gondola is 30
It spends between 60 degree, the automatic scissors 1401 of 1402 one end of manipulator installation are sc-3601 electric shear, automatic scissors 1401
Maximum shear diameter is 30mm, openings of sizes 3cm.
When work, ground control centre uploads flight plan to the communication module 12 of UAV flight, and communication module 12 connects
It receives flight plan and transmits data to airborne computer 11, while the solar panel 5 of 1 top of wing of unmanned plane later
It converts solar energy into electrical energy and is stored in battery 10, then airborne computer 11 is issued to propeller runing rest 2 and is ordered,
Decoder 203 will be sent to electric rotating motivation 202 after data processing, electric rotating motivation 202, which is started to work, drives rotary shaft 205
Propeller motor 206 is gone to plumbness by horizontality by rotation, and then airborne computer 11 is to propeller runing rest 2
Instruction is issued with the propeller motor 206 on the fixed bracket 4 of propeller, propeller motor 206 is started to work, propeller electricity
Motivation 206 drives propeller 3 to work, and with the raising of 3 revolving speed of propeller, unmanned plane starts to go up to the air, and unmanned plane rises to centainly
Airborne computer 11 is issued to propeller runing rest 2 and is instructed after height, and decoder 203 will be sent to rotation after data processing
Turn motor 202, electric rotating motivation 202, which is started to work, drives the rotation of rotary shaft 205 by propeller motor 206 by plumbness
Horizontal device is gone to, while airborne computer 11 issues to reduce and rotates speed to the propeller motor 206 of the fixed bracket 4 of propeller
The order of degree, then the propeller motor 206 of the fixed bracket 4 of propeller reduces rotation speed after receiving instruction, at this time
Unmanned plane switchs to horizontal flight, the location information that the 1404 real-time reception navigation satellite of navigation module of unmanned plane is sent, airborne meter
Calculation machine 11 controls rudder 7 to control the direction of unmanned plane during flying, and unmanned plane is made to fly to the starting point for starting line walking, and unmanned plane exists
Airborne computer 11 is issued to integrated gondola 14 and is instructed when flying to line walking task segment starting point, and integrated gondola 14 receives light after instruction
Electric gondola 15 is started to work, and when daytime, haze was larger, the picture of shooting is carried out optics Penetrating Fog by the camera of photoelectric nacelle 15
With the processing of algorithm Penetrating Fog, treated picture by communication module 12 is then passed back into ground control centre, avoids mist
The problem of haze day can not be maked an inspection tour normally, when unmanned plane enters cruising condition, then airborne computer 11 is to propeller runing rest 2
The order to stop working is issued with the propeller motor 206 of the fixed bracket 4 of propeller, propeller motor 206 receives finger
It stopping working after order, unmanned plane continues to slide forward under the action of inertia by wing 1, and it is energy saving, when in the control of ground
The heart observes on cable when having foreign matter that ground control centre issues cleaning instruction, and airborne computer 11 is connect by communication module 12
After receiving instruction, airborne computer 11 issues the instruction of work to propeller motor 206, and propeller motor 206 drives spiral shell
Paddle 3 to be revolved to work, the state of flight that airborne computer 11 controls the change unmanned plane of rudder 7 is changed to vrille by horizontal flight,
Location information and range information are passed back to airborne computer 11 in real time by navigation module 1404 simultaneously, different when unmanned plane and cable
When the distance of object is less than 5 meters, airborne computer 11 controls propeller 3 and unmanned plane is adjusted to floating state by vrille, so
The position letter that computing computer 11 is passed back according to navigation module 1404 afterwards close and the rotation speed of range information adjustment propeller 3 and
Direction is when unmanned plane is 2 meters at a distance from foreign matter and airborne when being in sustained height by unmanned plane slowly close to foreign matter
Computer 11 controls propeller 3 and unmanned plane is in floating state, and then airborne computer 11 is issued to manipulator 1402 and instructed,
Manipulator 1402 receives slowly close to foreign matter, the distance-sensor of the automatic scissors 1401 on 1402 top of manipulator after instruction
Automatic scissors 1401 are uploaded into airborne computer 11 and ground control centre, while photoelectric nacelle 15 at a distance from foreign matter in real time
Camera real-time pictures are passed back into ground control centre, ground control centre is determined according to the picture that photoelectric nacelle 15 returns
Fixed specifically how to clean up foreign matter, the posture that then airborne computer 11 controls unmanned plane slowly reaches automatic scissors 1401
At foreign matter, then airborne computer 11 is issued to automatic scissors 1401 and is instructed, and automatic scissors 1401 are set out after receiving instruction
Make to remove foreign matter and cable, airborne computer 11 controls manipulator after automatic scissors 1401 remove foreign matter and cable
1402 withdraw, and then airborne computer 11 is issued to propeller motor 206 and ordered, and propeller motor 206 is reinforced nobody
The elevated height of machine, then airborne computer 11 control propeller motor 206 make unmanned plane enter average flight state after
The continuous work for carrying out cable tour, airborne computer 11 controls propeller motor 206 and mentions unmanned plane after line walking terminates
It is raised to higher height then, then airborne computer 11 is issued to propeller runing rest 2 and ordered, and decoder 203 is by data
Electric rotating motivation 202 is sent to after processing, electric rotating motivation 202, which is started to work, drives the rotation of rotary shaft 205 by propeller electricity
Motivation 206 goes to horizontality by plumbness, then propeller electricity of the airborne computer 11 to the fixed bracket 4 of two propellers
Motivation 206 issues the instruction that stops working, and the propeller motor 206 of the fixed bracket 4 of two propellers stops after receiving instruction
Work, so that unmanned plane obtains the power of horizontal flight, when the speed of unmanned plane reaches cruising speed, airborne computer 11 will
The propeller motor 206 of two propeller runing rests 2 is closed, and unmanned plane is slided by wing, nothing in taxiing procedures
The man-machine gliding state that unmanned plane is controlled by airborne computer 11 and navigation module 1404, when sliding into ground control centre
Propeller motor 206 is powered on by airborne computer 11, then controls propeller 3 and unmanned plane is made slowly to drop to ground
On, total, the utility model has structure simple, advantage easy to operate, the cruise time is long.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Any modification made in novel protection scope, equivalent replacement etc. should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of cable line inspection device, it is characterised in that: including wing (1), propeller (3), empennage (6), rudder (7), machine
Body (8), head (9), photoelectric nacelle (15) and integrated gondola (14), the both sides of the fuselage (8) are equipped with to rise for providing
The wing (1) of power, the upper surface of the wing (1) are equipped with solar panel (5), the front end face of the wing (1)
It is equipped with propeller runing rest (2), the end face of the propeller runing rest (2) is disposed with for providing the spiral of lift
Paddle (3),
The tail portion of the fuselage (8) is provided with empennage (6), and the end face of empennage (6) is equipped with solar panel (5), empennage
(6) rudder (7) for controlling heading is installed, the left and right end face of the empennage (6) is mounted on spiral shell in the middle part of
It revolving paddle and fixes bracket (4), the other end of the propeller fixed bracket (4) is equipped with the propeller (3) for providing lift,
The front end face of the fuselage (8) is equipped with head (9), and the inside of the fuselage (8) and the head (9) are internal
The a part in space is equipped with battery (10), and the top of the head (9) is equipped with for protecting internal electronic equipment
It protects shell (13), the inside of the protection shell (13) is equipped with communication module (12), communication module (12) and battery
(10) airborne computer (11) are installed between,
The lower end surface of the fuselage (8) is equipped with the integrated gondola (14) for making an inspection tour cable, integrates under gondola (14)
End face is equipped with photoelectric nacelle (15), and the end face of the photoelectric nacelle (15) is equipped with three-dimensional scanner (1403), described
The end face of three-dimensional scanner (1403) be equipped with navigation module (1404), the outer end face installation of the integrated gondola (14)
There is the manipulator (1402) for clearing up sundries, one end of manipulator (1402) is equipped with automatic scissors (1401).
2. a kind of cable line inspection device according to claim 1, it is characterised in that: the wing (1) is by port wing
(101) it is formed with starboard wing (102), the spiral is installed at the medium position of the front end face of the port wing (101)
Paddle runing rest (2) is equipped with the propeller runing rest at the medium position of the front end face of the starboard wing (102)
(2), in the propeller runing rest (2) in the middle part of the port wing (101) front end face and described starboard wing (102) front end face
The propeller runing rest (2) in portion is symmetrical relative to the medium line of the wing (1).
3. a kind of cable line inspection device according to claim 1, it is characterised in that: the propeller runing rest (2)
Lower end be provided with and be connected and fixed plate (201), it is described that be connected and fixed plate (201) fixed with the wing (1) by welding
Connection, the lower end surface for being connected and fixed plate (201) are flushed with the lower end surface of the wing (1), are connected and fixed the end face of plate (201)
Two rotation axis fixing plates (204) at a distance of 5cm-15cm are welded with, are installed between two rotation axis fixing plates (204)
Have rotation axis (205), the end face of the rotation axis fixing plate (204) is provided with coaxially arranged with the rotation axis (205)
And for providing the electric rotating motivation (202) of power, the other end setting of rotation axis fixing plate (204) for rotation axis (205)
There is the decoder (203) coaxially arranged with the rotation axis (205), is installed on the end face of the rotation axis (205) promising
The propeller (3) provides the propeller motor (206) of power, the diameter of the propeller motor (206) with from
The lower end surface of rotation axis (205) is equidistant to the upper surface for being connected and fixed plate (201).
4. a kind of cable line inspection device according to claim 1, it is characterised in that: the propeller is fixed bracket (4)
It is fixedly connected by bolt with empennage (6), the other end of propeller fixed bracket (4) is provided with for for the propeller
(3) the propeller motor (206) of power is provided.
5. a kind of cable line inspection device according to claim 1, it is characterised in that: pacify on the top of the rudder (7)
Equipped with the signal lamp for warning, signal lamp is electrically connected with the solar panel (5) by electric installation, signal lamp with
Airborne computer (11) connection.
6. a kind of cable line inspection device according to claim 1, it is characterised in that: the fuselage (8) and head (9)
Inner surface is equipped with the shielded layer of anti-electromagnetic interference.
7. a kind of cable line inspection device according to claim 1, it is characterised in that: the communication module (12) includes
PCM remote-control receiver, data radio station, satellite communication module, GPRS module, 3G and 4G module, the airborne computer (11)
Including control module, steering engine controller, gyroscope and accelerometer.
8. a kind of cable line inspection device according to claim 1, it is characterised in that: the navigation module (1404) includes
GPS navigation module, Beidou navigation module, speed measuring module, barometertic altimeter, range unit.
9. a kind of cable line inspection device according to claim 1, it is characterised in that: the three-dimensional scanner (1403)
For EH-MR3D 3 D laser scanning radar oblique photograph camera, the photoelectric nacelle (15) is equipped with storage facilities, optics phase
Machine, infrared thermal imager and camera, the camera are equipped with filter and SSD Penetrating Fog module.
10. a kind of cable line inspection device according to claim 1, it is characterised in that: the manipulator (1402) passes through
Bolt is fixedly connected with the integrated gondola (14), and manipulator (1402) is mounted on the side end face of integrated gondola (14), mechanical
Line plane composed by the head (9) and the wing (1) at hand (1402) and integrated gondola (14) center
The angle of the center line of projection and the head (9) is between 30 degree to 60 degree, and manipulator (1402) one end is installed automatic
Scissors (1401) is sc-3601 electric shear, and the maximum shear diameter of automatic scissors (1401) is 30mm, openings of sizes 3cm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821143725.6U CN208602702U (en) | 2018-07-19 | 2018-07-19 | A kind of cable line inspection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821143725.6U CN208602702U (en) | 2018-07-19 | 2018-07-19 | A kind of cable line inspection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208602702U true CN208602702U (en) | 2019-03-15 |
Family
ID=65669534
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821143725.6U Expired - Fee Related CN208602702U (en) | 2018-07-19 | 2018-07-19 | A kind of cable line inspection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208602702U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547239A (en) * | 2020-05-11 | 2020-08-18 | 安徽安凯汽车股份有限公司 | High-voltage transmission line inspection device and working method |
-
2018
- 2018-07-19 CN CN201821143725.6U patent/CN208602702U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111547239A (en) * | 2020-05-11 | 2020-08-18 | 安徽安凯汽车股份有限公司 | High-voltage transmission line inspection device and working method |
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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: 20190315 Termination date: 20190719 |