CN208272587U

CN208272587U - A kind of high altitude operation cable deicing unmanned plane

Info

Publication number: CN208272587U
Application number: CN201820633682.3U
Authority: CN
Inventors: 张景熙
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-04-29
Filing date: 2018-04-29
Publication date: 2018-12-21
Anticipated expiration: 2028-04-29

Abstract

The utility model relates to deicing air vehicle technique fields, especially a kind of high altitude operation cable deicing unmanned plane, including controlling box, finder is equipped in the middle part of the lower end of the suspending rod, the middle part of the suspending rod is connected separately with the first movable plate and the second movable plate by the first pin shaft, the upper end side of the bottom plate is equipped with bottom bearing corresponding with one of movable axis, and the upper end other side of the bottom plate is equipped with the ice-breaking stick motor with another activity axis connection.Using the heat fusing ice-melt design of full freedom degree, ice and snow can completely be cleared up again, using Gyroscopic stabilization mechanism, enhance unmanned plane in high aerial stability, increase Automatic Track Finding principle, nobody is allowed to realize the tracking that tracks along cable self-control angle in high-altitude, the recycling for increasing trash ice melts, prevents trash ice from falling down and hurt operator, ice and snow completely can be cleared up again simultaneously, prevent cable surface from having overboard Cheng Bing again, it is very useful, it is promoted the use of after being worth.

Description

A kind of high altitude operation cable deicing unmanned plane

Technical field

The utility model relates to deicing air vehicle technique field more particularly to a kind of high altitude operation cable deicing unmanned planes.

Background technique

It is especially more frequently regional in some snowfall ratios as long as annual into winter, on cable the removing of accumulated snow just at One allow all staff on board's headache the problem of because the serious cable of icing snowberg, which may can't bear the heavy load, directly to be broken, All communicating interrupts for leading to area, so after snowing in winter, it is necessary to which maintenance personnel constantly clears the snow to cable The work of deicing, but also exactly general low cable can be purged it by the bar that clears the snow, however for Some overhead cables, it is necessary to which maintenance personnel climbs to high-altitude and carries out operation, at this time often not only to overcome the problems, such as cold, also It needs to overcome the smooth of snowy day cable, is easy to cause very big influence to the safety of dimension personnel in this way；Country is for the winter at present The most common mode that mostly uses greatly of deicing mode that season overhead cable icing serious situation uses is exactly artificial deicing, and second It is exactly one kind is exactly using unmanned plane deicing mode, but general is exactly by using unmanned plane as carrier, carrying deicing work Tool carries out cable deicing, and very single by the way of, does not have various ways cooperation, it is easy to de-icing work be caused just to be completed Icing is had with that, will lead to the halfway problem of deicing in this way.For this purpose, it is proposed that a kind of high altitude operation cable deicing Unmanned plane.

Utility model content

Purpose of the utility model is to solve disadvantages existing in the prior art, and a kind of high altitude operation electricity proposed Cable deicing unmanned plane.

To achieve the goals above, the utility model adopts the technical scheme that

A kind of high altitude operation cable deicing unmanned plane, including control box are designed, the outside of the control box is equidistantly equipped with three The intersection of a wing and multiple solar panels, the solar panels and wing is described there are the notch to match with wing It is all provided with fluted on wing, the center bottom of the groove is mounted on propeller motor, and the propeller motor is far from groove A middle side part pass through shaft and be connected with propeller blade, and the tail end of the wing passes through connection frame and is connected with propeller Protective cover, the propeller protective cover are located at the surface of propeller blade, and the upper center of the control box is equipped with gyroscope, It is equipped with suspending rod in the middle part of the lower end of the control box, is equipped with finder in the middle part of the lower end of the suspending rod, in the suspending rod Portion is connected separately with the first movable plate and the second movable plate by the first pin shaft, and the lower end of first movable plate is equipped with camera shooting Head, and first movable plate and the second movable plate are hinged, first movable plate and the second movable plate far from suspending rod one End is hinged with first angle adjusting bracket by the second pin shaft, and the lower end of first movable plate and the second movable plate is symmetrically set Angled adjusting cylinder, the described one end of angular adjustment cylinder far from the first movable plate and the second movable plate are handed over by third pin shaft It is connected to second angle adjusting bracket, the second angle adjusting bracket and first angle adjusting bracket are hinged, the second angle adjusting bracket Inner wall side angular adjustment motor is installed, the angular adjustment motor passes through angular adjustment bearing and second angle adjusting bracket The connection of the inner wall other side, the outside of the angular adjustment bearing is equipped with hollow electric motor protecting shell, the hollow electric motor protecting shell Bottom end be equipped with heating wire, the inner cavity bottom end of the hollow electric motor protecting shell is equipped with motor stabilizing bracket, the motor stabilizing bracket Upper end is equipped with motor, and the motor is connected with fan blades of motor by output shaft, two second angle adjusting brackets it is opposite Side is respectively connected with bottom plate, and the lower end two sides of the control box are symmetrically arranged with load-bearing cylinder, and first movable plate and second live The lower end of movable plate is symmetrically arranged with top bearing, is equipped with movable axis in the middle part of the top bearing, one of them described activity The second ice-breaking stick and the first sheave are respectively equipped on the outside of axis, first sheave is located at the lower section of the second ice-breaking stick, another The first ice-breaking stick and the second sheave are respectively equipped on the outside of the movable axis, second sheave is located under the first ice-breaking stick Side, first sheave and the second sheave are connected by belt, and the upper end side of the bottom plate is equipped with and one of movable axis Corresponding bottom bearing, the upper end other side of the bottom plate are equipped with the ice-breaking stick motor with another activity axis connection；

The bottom plate lower end is equipped with defrosting plate cylinder, one end be connected with ice of the defrosting plate cylinder far from bottom plate Plate, the defrosting plate is in L font, and the vertical plane opposite side of two defrosting plates is equipped with solar panel, the defrosting plate Upper end be equipped with change ice heating wire, the control box includes battery, singlechip controller and signal projector, the electric power storage Pond, signal projector, camera are connected with singlechip controller, and describedization ice heating wire, battery are connected with solar panels, institute Propeller motor is stated, motor, heating wire, angular adjustment motor, ice-breaking stick motor, load-bearing cylinder, cylinder is adjusted, gyroscope, seeks Mark device, defrosting plate cylinder are connected with singlechip controller.

Preferably, describedization ice heating wire is placed equidistant with, and the distance between every group of heating wire for changing ice heating wire is three To five millimeters.

Preferably, the finder is infrared sensor.

Preferably, the gyroscope is sensing gyroscope instrument.

The utility model proposes a kind of high altitude operation cable deicing unmanned plane, beneficial effect is: being designed using plate The unmanned machine modeling of type, makes fuselage body more flexible, and adjustment angle is more ingenious, squeezes ice-breaking design using tooth form, can allow and remove Ice is more thorough, using the heat fusing ice-melt design of full freedom degree, can completely be cleared up ice and snow again, steady using gyroscope Determine mechanism, enhancing unmanned plane increases Automatic Track Finding principle in high aerial stability, allows nobody to track in high-altitude realization and tracks edge Cable self-control angle, increase trash ice recycling melt, prevent trash ice from falling down and hurt operator, while can be again Ice and snow is completely cleared up, prevents cable surface from having overboard Cheng Bing again, it is very useful, it is promoted the use of after being worth.

Detailed description of the invention

Fig. 1 be the utility model proposes the ice-breaking stick external structure of high altitude operation cable deicing unmanned plane a kind of face knot Structure schematic diagram；

Fig. 2 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane C at enlarged structure schematic diagram；

Fig. 3 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane hot melt ice-breaking modular structure it is left tiltedly Depending on structural schematic diagram；

Fig. 4 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane hot melt ice-breaking module-external structure Partial enlargement structural representation at left oblique view B；

Fig. 5 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane suspention beam external structure backsight knot Structure schematic diagram；

Fig. 6 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane active plate external structure backsight Oblique two survey view structural schematic diagram；

Fig. 7 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane active plate external structure it is left tiltedly Depending on structural schematic diagram；

Fig. 8 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane finder and gyroscope installation knot The positive oblique view of structural diagram of structure；

Fig. 9 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane the external knot of solar energy plate installation Structural schematic diagram is regarded under structure；

Figure 10 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane trash ice recycle plate external structure Positive oblique view of structural diagram；

Figure 11 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane trash ice recycle plate external structure Right oblique view of structural diagram；

Figure 12 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane hollow electric motor protecting shell structure Schematic diagram；

Figure 13 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane movable plate structural schematic diagram；

Figure 14 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane angular adjustment frame structural representation Figure；

Figure 15 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane ice-breaking stick structural schematic diagram；

Figure 16 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane defrosting plate structural schematic diagram；

Figure 17 be the utility model proposes a kind of high altitude operation cable deicing unmanned plane ice-breaking ice-melt and structure tune Throttle journey structural schematic diagram.

In figure: control box 1, wing 2, propeller motor 3, propeller blade 4, motor 5, fan blades of motor 6, angular adjustment axis Hold 7, motor stabilizing bracket 8, angular adjustment motor 9, top bearing 10, the first ice-breaking stick 11, the second ice-breaking stick 12, the first sheave 13, bottom bearing 14, belt 15, the second sheave 16, ice-breaking stick motor 17, the first movable plate 18,19, first jiaos of the second movable plate Spend adjusting bracket 20, second angle adjusting bracket 21, hollow electric motor protecting shell 22, heating wire 23, angular adjustment cylinder 24, suspending rod 25, load-bearing cylinder 26, camera 27, gyroscope 28, finder 29, defrosting plate cylinder 30, defrosting plate 31, solar panel 32, change ice Heating wire 33, solar panels 34, propeller protective cover 35.

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.

Referring to Fig.1-17, a kind of high altitude operation cable deicing unmanned plane, including control box 1, the outside of control box 1 are equidistantly set There are three wing 2 and multiple solar panels 34, there are lack with what wing 2 matched for the intersection of solar panels 34 and wing 2 Mouthful, it is all provided on wing 2 fluted, the center bottom of groove is mounted on propeller motor 3, and propeller motor 3 is far from groove One middle side part passes through shaft and is connected with propeller blade 4, and the tail end of wing 2 passes through connection frame and is connected with propeller protection Cover 35, propeller protective cover 35 are located at the surface of propeller blade 4, and the upper center of control box 1 is equipped with gyroscope 28, gyro Instrument 28 is sensing gyroscope instrument, and effect is more preferable, and more practical, the direction that its rotary shaft is pointing to is not by the influence of external force When, it and is exactly that certain direction is kept with it using this remote principle as foundation that it, which is not have any change, 's.

It controls and is equipped with suspending rod 25 in the middle part of the lower end of box 1, be equipped with finder 29, finder 29 in the middle part of the lower end of suspending rod 25 For infrared sensor, more universalness, practicability is stronger, and is conveniently replaceable, and will not be come not because of bad when due to rareness And replacement, and influence the practical of equipment.

The middle part of suspending rod 25 is connected separately with the first movable plate 18 and the second movable plate 19 by the first pin shaft, and first is living The lower end of movable plate 18 is equipped with camera 27, and the first movable plate 18 and the second movable plate 19 are hinged, the first movable plate 18 and the Two one end of movable plate 19 far from suspending rod 25 pass through the second pin shaft and are hinged with first angle adjusting bracket 20, the first movable plate 18 It is symmetrically arranged with angular adjustment cylinder 24 with the lower end of the second movable plate 19, angular adjustment cylinder 24 is far from 18 He of the first movable plate There is a second angle adjusting bracket 21 in one end of second movable plate 19 by the handover of third pin shaft, second angle adjusting bracket 21 and first jiao It is hinged to spend adjusting bracket 20, the inner wall side of second angle adjusting bracket 21 is equipped with angular adjustment motor 9, and angular adjustment motor 9 is logical Over-angle adjusts bearing 7 and connects with the inner wall other side of second angle adjusting bracket 21, and the outside of angular adjustment bearing 7 is equipped with hollow The bottom end of electric motor protecting shell 22, hollow electric motor protecting shell 22 is equipped with heating wire 23, and the inner cavity bottom end of hollow electric motor protecting shell 22 is set There is a motor stabilizing bracket 8, the upper end of motor stabilizing bracket 8 is equipped with motor 5, and motor 5 is connected with fan blades of motor 6 by output shaft, and two The opposite side of a second angle adjusting bracket 21 is respectively connected with bottom plate, and the lower end two sides of control box 1 are symmetrically arranged with load-bearing cylinder 26, The lower end of first movable plate 18 and the second movable plate 19 is symmetrically arranged with top bearing 10, and the middle part of top bearing 10 is equipped with work Moving axis, the second ice-breaking stick 12 and the first sheave 13 are respectively equipped on the outside of one of movable axis, and the first sheave 13 is located at second The lower section of ice-breaking stick 12 is respectively equipped with the first ice-breaking stick 11 and the second sheave 16, the second sheave 16 on the outside of another movable axis Positioned at the lower section of the first ice-breaking stick 11, the first sheave 13 and the second sheave 16 are connected by belt 15, and the upper end side of bottom plate is set There is bottom bearing 14 corresponding with one of movable axis, the upper end other side of bottom plate is equipped with broken with another activity axis connection Ice lolly motor 17；

Bottom plate lower end is equipped with defrosting plate cylinder 30, and defrosting plate cylinder 30 is connected with defrosting plate 31 far from one end of bottom plate, Defrosting plate 31 is in L font, and the vertical plane opposite side of two defrosting plates 31 is equipped with solar panel 32, and the upper end of defrosting plate 31 is set Having ice heating wire 33, changing the distance between every group of heating wire that ice heating wire 33 is placed equidistant with, and changes ice heating wire 33 is three To five millimeters, ice cube preferably can be melted into water, avoided in falling from high altitude good fortune security risk, and be easily installed manufacture.

Controlling box 1 includes battery, singlechip controller and signal projector, battery, signal projector, camera 27 connect with singlechip controller, change ice heating wire 33, battery and solar panels 34 and connect, propeller motor 3, motor 5, electricity Heated filament 23, ice-breaking stick motor 17, load-bearing cylinder 26, adjusts cylinder 24, gyroscope 28, finder 29, changes angular adjustment motor 9 Slab cylinder 30 is connected with singlechip controller.

Working principle: the battery for including in control box 1 provides electric energy supply for each electrical appliance of unmanned plane, internal single Piece machine controller and signal projector can control each movement flight of unmanned plane, camera under the operation of operator 27 can provide the visual field for the operation of operator, avoid various obstacles, at work, the propeller electricity being mounted on wing 2 Machine 3 drives the rotation of propeller blade 4, allows entire unmanned plane climb to altitude, is observing overhead cable by camera 27 After icing situation, operator can be adjusted by control load-bearing cylinder 26 first to be hinged and hinged with suspention beam 25 The first movable plate 18 and the second movable plate 19 opening and closing degree, when needing to carry out the de-icing work of cable, operator is first First control unmanned plane is tilted along cable extending direction, and then control is mounted on the first movable plate 18 and the second movable plate 19 Ice-breaking stick motor 17 rotate, first be mounted on ice-breaking stick motor 17 sheave 13 and be mounted on the second ice-breaking stick 12 second Sheave 16 can drive the second ice-breaking stick 12 to rotate under the transmission of belt 15, and unmanned plane inclination is then allowed to allow cable from two first The big opening part that first ice-breaking stick 11 is formed enters, and zigzag first ice-breaking stick 11 can slowly bite icing and worm directly Enter the osculum that two the second ice-breaking sticks 12 are formed to cable, the icing on such cable can be broken in the first ice-breaking stick 11 and second Icing is crushed under the crunch and rotation of ice lolly 12, at this moment adjusts unmanned plane, makes fuselage and cable holding horizontal, this When close two ice-breaking stick motors 17, pass through angular adjustment cylinder 24 and adjust first angle adjusting bracket 20 and second angle adjusting bracket Then 21 height and distance between the two adjust hollow electric motor protecting box 22 by control angular adjustment motor 9, allow hollow 22 osculum of electric motor protecting box is directed at cable, and the rotary electric machine flabellum 6 for then controlling motor 5 can blow the heat that heating wire 23 issues To cable, to melt again to the sleet layer on cable, to make cleaning more thorough, then by adjusting defrosting plate gas Cylinder 30 is flexible to allow the intermeshing of defrosting plate 31 formation one to connect trash ice groove with engaged gap, can catch by the first ice-breaking Stick 11 and the second ice-breaking stick 12 squeeze the trash ice to fall, at this moment change ice heating wire 33 for the luminous energy of solar panels 34 and are converted into heat Can, it the trash ice caught melt is processed into the trash ice slag of water or very little and is fallen from engaged gap, at the same time solar panel 32 can also concentrate on luminous energy on trash ice, the thawing processing of rubble ice be carried out, when cable is completely into the broken Machine for making ice-sucker of unmanned plane After all mechanisms of structure all regulate, the gyroscope 28 of connection control box 1 will help operator independently to stablize to unmanned plane It is controlled, finder 29 will start to work, and along the direction that cable extends, the heading for constantly adjusting unmanned plane is not necessarily to Manual control；After the completion of work, the work of motor 5 and heating wire 23 and ice-breaking stick motor 17 is closed by control box 1, so 19 opening and closing of extension and contraction control the first movable plate 18 and the second movable plate for passing through load-bearing cylinder 26 afterwards, allow unmanned plane to come out from cable ?.

The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model Within enclosing.

Claims

1. the outside of a kind of high altitude operation cable deicing unmanned plane, including control box (1), control box (1) is equidistantly equipped with three The intersection of a wing (2) and multiple solar panels (34), the solar panels (34) and wing (2) there are with wing (2) The notch to match, is all provided on the wing (2) fluted, and the center bottom of the groove is mounted on propeller motor (3), The propeller motor (3) passes through shaft far from a middle side part of groove and is connected with propeller blade (4), and the wing (2) tail end passes through connection frame and is connected with propeller protective cover (35), which is characterized in that in the upper end of control box (1) Portion is equipped with gyroscope (28), suspending rod (25) is equipped in the middle part of the lower end of control box (1), in the lower end of the suspending rod (25) Portion is equipped with finder (29), and the middle part of the suspending rod (25) is connected separately with the first movable plate (18) and the by the first pin shaft The lower end of two movable plates (19), first movable plate (18) is equipped with camera (27), and first movable plate (18) and Hingedly, the one end of first movable plate (18) and the second movable plate (19) far from suspending rod (25) is logical for second movable plate (19) It crosses the second pin shaft to be hinged with first angle adjusting bracket (20), the lower end of first movable plate (18) and the second movable plate (19) is equal It is symmetrically arranged with angular adjustment cylinder (24), the angular adjustment cylinder (24) is far from the first movable plate (18) and the second movable plate (19) one end has second angle adjusting bracket (21) by the handover of third pin shaft, the inner wall one of the second angle adjusting bracket (21) Side is equipped with angular adjustment motor (9), and the angular adjustment motor (9) is adjusted by angular adjustment bearing (7) and second angle The inner wall other side of frame (21) connects, and the outside of the angular adjustment bearing (7) is equipped with hollow electric motor protecting shell (22), and described time The bottom end of type electric motor protecting shell (22) is equipped with heating wire (23), and the inner cavity bottom end of the hollow electric motor protecting shell (22) is equipped with motor The upper end of stabilizing bracket (8), the motor stabilizing bracket (8) is equipped with motor (5), and the motor (5) is connected with electricity by output shaft Machine flabellum (6), the opposite side of two second angle adjusting brackets (21) are respectively connected with bottom plate, under the control box (1) Two sides are held to be equipped with load-bearing cylinder (26), the lower end of first movable plate (18) and the second movable plate (19) is symmetrically arranged with top Bearing (10) is equipped with movable axis in the middle part of the top bearing (10), is respectively equipped on the outside of one of them described movable axis Second ice-breaking stick (12) and the first sheave (13), first sheave (13) are located at the lower section of the second ice-breaking stick (12), another The first ice-breaking stick (11) and the second sheave (16) are respectively equipped on the outside of the movable axis, second sheave (16) is located at first The lower section of ice-breaking stick (11), first sheave (13) and the second sheave (16) by belt (15) connect, the bottom plate it is upper Side is held to be equipped with bottom bearing (14) corresponding with one of movable axis, the upper end other side of the bottom plate is equipped with and another The ice-breaking stick motor (17) of activity axis connection；

The bottom plate lower end is equipped with defrosting plate cylinder (30), one end be connected with of the defrosting plate cylinder (30) far from bottom plate Slab (31), and the vertical plane opposite side of two defrosting plates (31) is equipped with solar panel (32), the defrosting plate (31) Upper end be equipped with and change ice heating wire (33), the control box (1) includes battery, singlechip controller and signal projector, The battery, signal projector, camera (27) are connected with singlechip controller, describedization ice heating wire (33), battery It is connected with solar panels (34), the propeller motor (3), motor (5), heating wire (23), angular adjustment motor (9), ice-breaking Stick motor (17), load-bearing cylinder (26) adjust cylinder (24), gyroscope (28), finder (29), defrosting plate cylinder (30) and list The connection of piece machine controller.

2. a kind of high altitude operation cable deicing unmanned plane according to claim 1, which is characterized in that describedization ice heating wire (33) the distance between every group of heating wire for being placed equidistant with, and changing ice heating wire (33) is three to five millimeters.

3. a kind of high altitude operation cable deicing unmanned plane according to claim 1, which is characterized in that the finder (29) For infrared sensor.

4. a kind of high altitude operation cable deicing unmanned plane according to claim 1, which is characterized in that the gyroscope It (28) is sensing gyroscope instrument.