CN112550742A - Rotary unmanned aerial vehicle electroscope - Google Patents
Rotary unmanned aerial vehicle electroscope Download PDFInfo
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- CN112550742A CN112550742A CN202011454216.7A CN202011454216A CN112550742A CN 112550742 A CN112550742 A CN 112550742A CN 202011454216 A CN202011454216 A CN 202011454216A CN 112550742 A CN112550742 A CN 112550742A
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- 230000005611 electricity Effects 0.000 claims abstract description 62
- 238000012360 testing method Methods 0.000 claims abstract description 54
- 238000009434 installation Methods 0.000 claims abstract description 25
- 230000001360 synchronised effect Effects 0.000 claims description 13
- 230000009471 action Effects 0.000 claims description 3
- 238000007689 inspection Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 21
- 239000004020 conductor Substances 0.000 description 14
- 230000008569 process Effects 0.000 description 6
- 230000008859 change Effects 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000002337 anti-port Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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Abstract
The invention discloses a rotary type unmanned aerial vehicle electricity testing device, and aims to provide a rotary type unmanned aerial vehicle electricity testing device which is high in electricity testing efficiency and good in electricity testing safety; and can effectively improve and test the electric in-process, unmanned aerial vehicle's stability to effectively solve unmanned aerial vehicle and test electric device because of the rotary type unmanned aerial vehicle of the unbalanced problem of external force interference. The unmanned aerial vehicle comprises an unmanned aerial vehicle, wherein the unmanned aerial vehicle comprises a frame; the rotating device comprises a first rotating seat positioned above the rack and a torque steering engine arranged on the rack and used for driving the first rotating seat to rotate, and a rotating shaft of the first rotating seat is perpendicular to a rotating shaft of a propeller of the unmanned aerial vehicle; electroscope device, electroscope device are including fixing the installation pole on first rotation seat and fixing the electroscope on the installation pole.
Description
Technical Field
The invention relates to an electricity testing device, in particular to a rotary type unmanned aerial vehicle electricity testing device.
Background
In the maintenance of the distribution overhead line, electricity inspection is the first step of maintenance, and the line maintenance work can be started after the fact that the line has no voltage is proved. The traditional electricity testing method is that an operator climbs a pole for operation, an electricity testing pen is used for testing electricity of a circuit at a safe distance, and the circuit is judged to be in maintenance work after no voltage is determined. This kind of traditional pole-climbing electroscope operation not only the operating efficiency is low, and the operation risk is high moreover.
In order to solve the problems of the traditional pole climbing electricity testing operation, some inventors design an unmanned aerial vehicle electricity testing device, and an electricity tester is carried by an unmanned aerial vehicle to test electricity of a power distribution overhead line, so that the safety and reliability of electricity testing are ensured, and the labor intensity is reduced; but electroscope among present unmanned aerial vehicle electroscope generally all is direct fixed mounting on unmanned aerial vehicle, and this makes when unmanned aerial vehicle drives the electroscope's electroscope probe contact distribution overhead line, because unmanned aerial vehicle is in the mobile state, and the electroscope's electroscope probe takes place the rigid contact with distribution overhead line, leads to unmanned aerial vehicle unbalance because of external force interference easily, influences unmanned aerial vehicle electroscope efficiency of electroscope device, leads to unmanned aerial vehicle unbalance even and drops the problem of damage.
Disclosure of Invention
The invention aims to overcome the defects that the electricity testing efficiency is high, and the electricity testing safety is good; and can effectively improve and test the electric in-process, unmanned aerial vehicle's stability to effectively solve unmanned aerial vehicle and test electric device because of the rotary type unmanned aerial vehicle of the unbalanced problem of external force interference.
The technical scheme of the invention is as follows:
a rotary type unmanned aerial vehicle electroscope, includes:
the unmanned aerial vehicle comprises a frame;
the rotating device comprises a first rotating seat positioned above the rack and a torque steering engine arranged on the rack and used for driving the first rotating seat to rotate, and a rotating shaft of the first rotating seat is perpendicular to a rotating shaft of a propeller of the unmanned aerial vehicle;
electroscope device, electroscope device are including fixing the installation pole on first rotation seat and fixing the electroscope on the installation pole.
The rotary type unmanned aerial vehicle electricity testing device specifically works as follows, after the unmanned aerial vehicle approaches an electricity testing ring on an overhead conductor to be tested, the hovering characteristic of the unmanned aerial vehicle is utilized, and after the unmanned aerial vehicle hovers, the first rotating seat, the mounting rod and the electricity tester are driven to rotate through the torque steering engine, so that the spatial position change of the electricity tester is realized, and an electricity testing contact of the electricity tester is in a proper position; then, the position of the unmanned aerial vehicle is further adjusted, so that the unmanned aerial vehicle can be driven to hover after an electricity testing contact of an electricity tester is driven to contact an electricity testing ring on the overhead conductor through rotation of the mounting rod; then, the torque steering engine drives the first rotating seat, the mounting rod and the electroscope to rotate, so that an electroscope contact contacts an electroscope ring on the overhead conductor, thereby realizing contact electroscope for the overhead conductor, and having high electroscope efficiency and good electroscope safety. On the other hand, the rotary type unmanned aerial vehicle electricity testing device utilizes the hovering characteristic of the unmanned aerial vehicle, meanwhile, the torque steering engine is utilized to realize the change of the space position of the electricity tester after the unmanned aerial vehicle hovers, and after the unmanned aerial vehicle hovers, the electricity testing contact of the electricity tester is made to contact with an electricity testing ring on the overhead conductor through the rotation of the mounting rod; so, at the in-process of the test ring on the electroscope's the contact overhead conductor that tests electricity, unmanned aerial vehicle is in the state of hovering, can effectively improve and test the electric in-process, unmanned aerial vehicle's stability to effectively solve unmanned aerial vehicle and disturb the unbalanced problem because of external force.
Preferably, the balance adjusting device comprises a synchronous gear set, a second rotating seat positioned above the rack and a balance rod arranged on the second rotating seat, the second rotating seat is rotatably arranged on the rack, a rotating shaft of the second rotating seat is parallel to a rotating shaft of the first rotating seat, a first gear and a second gear which are meshed with each other through the synchronous gear set are arranged, the outer diameters of the first gear and the second gear are the same, the first gear is fixed on the rotating shaft of the first rotating seat, and the second gear is fixed on the rotating shaft of the second rotating seat; when the mounting rod is in a vertical state, the balance rod is also in a vertical state; when the torque steering engine drives the first rotating seat and the mounting rod to rotate, the second rotating seat and the balance rod synchronously and reversely rotate under the action of the synchronous gear set.
In the application, the unmanned aerial vehicle is in a hovering state in the process that the electricity testing contact of the electricity tester is in contact with the electricity testing ring on the overhead conductor, so that the stability of the unmanned aerial vehicle in the electricity testing process can be effectively improved; but installation pole and electroscope rotate the in-process, still can cause centrobaric skew, influence unmanned aerial vehicle's stability, when installation pole length is longer, the unbalanced problem of unmanned aerial vehicle still can appear. In order to solve this problem, this scheme has set up balance adjustment device, it rotates the seat and installs pole pivoted in-process at the first rotation of torque steering wheel drive, the second rotates seat and balancing pole and will be at synchronous gear train's effect synchronous antiport down, thereby offset through the balancing pole, rotate because of installation pole and electroscope, and the problem of the focus skew that causes, in order to guarantee installation pole and electroscope rotation in-process, unmanned aerial vehicle's stability, thereby further improvement electricity testing in-process, unmanned aerial vehicle's stability, in order to effectively solve unmanned aerial vehicle because of the unbalanced problem of external force interference.
Preferably, the first rotating seat and the second rotating seat are symmetrically distributed on two opposite sides of the center of the frame.
Preferably, the mounting bar and the balancing bar are symmetrically arranged on two opposite sides of the center of the frame.
Preferably, the first rotating seat and the second rotating seat are close to the center of the frame.
Preferably, the first rotating seat is further provided with a camera, and the camera is used for shooting the positions of the mounting rod and the electroscope. So, can shoot the position of installation pole and electroscope through the camera to make the person of controlling observe the position state of installation pole and electroscope in real time, be used for adjusting the gesture of electroscope, so that carry out high altitude contact electroscope, simultaneously, can also save the process that electroscope contact electroscope encircles in real time.
Preferably, the electroscope is fixed to the upper end of the mounting rod.
Preferably, the mounting rod is a hollow rod, and the inner hole of the mounting rod forms a wire passing hole.
Preferably, the mounting rod is an insulated plastic rod.
Preferably, the torque steering engine is mounted on the frame by bolts.
The invention has the beneficial effects that: the electricity testing efficiency is high, and the electricity testing safety is good; and can effectively improve and test the electric in-process, unmanned aerial vehicle's stability to effectively solve unmanned aerial vehicle and disturb unbalanced problem because of external force interference.
Drawings
Fig. 1 is a schematic structural diagram of a rotary drone electroscope apparatus according to a first embodiment of the present invention.
Fig. 2 is a schematic structural diagram of a rotary unmanned aerial vehicle electroscope apparatus according to a second embodiment of the present invention, in which a mounting rod is in a vertical state.
Fig. 3 is a schematic structural diagram of a rotary drone electroscope according to a second embodiment of the present invention, when a mounting rod is in an inclined state.
In the figure:
a frame 1;
the device comprises a rotating device 2, a first rotating seat 2.1 and a torque steering engine 2.2;
the electroscope comprises an electroscope device 3, an installation rod 3.1 and an electroscope 3.2;
a camera 4;
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions of the embodiments of the present invention are clearly explained and illustrated below with reference to the accompanying drawings, but the following embodiments are only preferred embodiments of the present invention, and not all embodiments. Based on the embodiments in the implementation, other embodiments obtained by those skilled in the art without any creative effort belong to the protection scope of the present invention.
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below by referring to the drawings are exemplary only for explaining the present scheme, and are not construed as limiting the scheme of the present invention.
These and other aspects of embodiments of the invention will be apparent with reference to the following description and attached drawings. In the description and drawings, particular embodiments of the invention have been disclosed in detail as being indicative of some of the ways in which the principles of the embodiments of the invention may be practiced, but it is understood that the scope of the embodiments of the invention is not limited thereby. On the contrary, the embodiments of the invention include all changes, modifications and equivalents coming within the spirit and terms of the claims appended hereto.
In the description of the present invention, it is to be understood that the terms "thickness", "upper", "lower", "horizontal", "top", "bottom", "inner", "outer", "circumferential", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., and "several" means one or more unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; may be mechanically coupled, may be electrically coupled or may be in communication with each other; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
The first embodiment is as follows: as shown in fig. 1, a rotary type unmanned aerial vehicle electroscope device, includes unmanned aerial vehicle, rotary device 2 and electroscope device 3. Unmanned aerial vehicle includes frame 1 and sets up the screw in the frame.
The rotating device 2 comprises a first rotating seat 2.1 positioned above the rack and a torque steering engine 2.2 arranged on the rack and used for driving the first rotating seat to rotate. The rotation axis of first rotation seat is mutually perpendicular with the rotation axis of unmanned aerial vehicle's screw. In this embodiment, the torque steering engine is mounted on the frame through a bolt.
The electroscope device 3 comprises a mounting rod 3.1 fixed on the first rotating seat and an electroscope 3.2 fixed on the mounting rod. The electroscope is provided with an electroscope contact. In this embodiment, the electroscope is fixed in the upper end of installation pole, and of course, the electroscope can also be fixed in other positions of installation pole.
In this embodiment, the installation pole is hollow pole, and the hole formation of installation pole crosses the line hole. The signal line of the electroscope can be arranged in the wire through hole. The mounting rod is an insulating plastic rod.
The rotary type unmanned aerial vehicle electricity testing device of the embodiment specifically works as follows, after the unmanned aerial vehicle approaches an electricity testing ring on an overhead conductor to be tested, the hovering characteristic of the unmanned aerial vehicle is utilized, and after the unmanned aerial vehicle hovers, the first rotating seat, the mounting rod and the electricity tester are driven to rotate through the torque steering engine, so that the spatial position change of the electricity tester is realized, and an electricity testing contact of the electricity tester is in a proper position; then, the position of the unmanned aerial vehicle is further adjusted, so that the unmanned aerial vehicle can be driven to hover after an electricity testing contact of an electricity tester is driven to contact an electricity testing ring on the overhead conductor through rotation of the mounting rod; then, the torque steering engine drives the first rotating seat, the mounting rod and the electroscope to rotate, so that an electroscope contact contacts an electroscope ring on the overhead conductor, thereby realizing contact electroscope for the overhead conductor, and having high electroscope efficiency and good electroscope safety. On the other hand, the rotary type unmanned aerial vehicle electricity testing device utilizes the hovering characteristic of the unmanned aerial vehicle, meanwhile, the torque steering engine is utilized to realize the change of the space position of the electricity tester after the unmanned aerial vehicle hovers, and after the unmanned aerial vehicle hovers, the electricity testing contact of the electricity tester is made to contact with an electricity testing ring on the overhead conductor through the rotation of the mounting rod; so, at the in-process of the test ring on the electroscope's the contact overhead conductor that tests electricity, unmanned aerial vehicle is in the state of hovering, can effectively improve and test the electric in-process, unmanned aerial vehicle's stability to effectively solve unmanned aerial vehicle and disturb the unbalanced problem because of external force.
Further, as shown in fig. 1, a camera 4 is further arranged on the first rotating seat, and the camera is used for shooting the positions of the mounting rod and the electroscope. So, can shoot the position of installation pole and electroscope through the camera to make the person of controlling observe the position state of installation pole and electroscope in real time, be used for adjusting the gesture of electroscope, so that carry out high altitude contact electroscope, simultaneously, can also save the process that electroscope contact electroscope encircles in real time.
In a second embodiment, the remaining structure of the present embodiment refers to the first embodiment, and the difference therebetween is that:
as shown in fig. 2 and 3, the rotary drone electroscope further includes a balance adjusting device 5. The balance adjusting device comprises a synchronous gear set, a second rotating seat 5.1 positioned above the rack and a balance rod 5.2 arranged on the second rotating seat. The second rotating seat is rotatably arranged on the rack, and a rotating shaft of the second rotating seat is parallel to a rotating shaft of the first rotating seat. The first gear 5.3 and the second gear 5.4 are meshed with the synchronous gear set, and the outer diameters of the first gear and the second gear are the same. The first gear is fixed on the rotating shaft of the first rotating seat, and the second gear is fixed on the rotating shaft of the second rotating seat.
As shown in fig. 2, when the mounting bar is in the vertical state, the stabilizer bar is also in the vertical state.
As shown in FIG. 3, when the torque steering engine drives the first rotating seat and the mounting rod to rotate, the second rotating seat and the balance rod synchronously and reversely rotate under the action of the synchronous gear set.
In this embodiment, the first rotating base and the second rotating base are symmetrically distributed on two opposite sides of the center of the rack. The mounting rods and the balancing rods are symmetrically distributed on two opposite sides of the center of the rack. The first rotating seat and the second rotating seat are close to the center of the rack.
In the application, the unmanned aerial vehicle is in a hovering state in the process that the electricity testing contact of the electricity tester is in contact with the electricity testing ring on the overhead conductor, so that the stability of the unmanned aerial vehicle in the electricity testing process can be effectively improved; but installation pole and electroscope rotate the in-process, still can cause centrobaric skew, influence unmanned aerial vehicle's stability, when installation pole length is longer, the unbalanced problem of unmanned aerial vehicle still can appear. In order to solve this problem, this scheme has set up balance adjustment device, it rotates the seat and installs pole pivoted in-process at the first rotation of torque steering wheel drive, the second rotates seat and balancing pole and will be at synchronous gear train's effect synchronous antiport down, thereby offset through the balancing pole, rotate because of installation pole and electroscope, and the problem of the focus skew that causes, in order to guarantee installation pole and electroscope rotation in-process, unmanned aerial vehicle's stability, thereby further improvement electricity testing in-process, unmanned aerial vehicle's stability, in order to effectively solve unmanned aerial vehicle because of the unbalanced problem of external force interference.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and all simple modifications, alterations and equivalents of the above embodiments according to the technical spirit of the present invention are still within the protection scope of the technical solution of the present invention.
Claims (9)
1. The utility model provides a rotary type unmanned aerial vehicle tests electric installation, characterized by includes:
the unmanned aerial vehicle comprises a frame;
the rotating device comprises a first rotating seat positioned above the rack and a torque steering engine arranged on the rack and used for driving the first rotating seat to rotate, and a rotating shaft of the first rotating seat is perpendicular to a rotating shaft of a propeller of the unmanned aerial vehicle;
electroscope device, electroscope device are including fixing the installation pole on first rotation seat and fixing the electroscope on the installation pole.
2. The rotary type unmanned aerial vehicle electricity testing device of claim 1, further comprising a balance adjusting device, wherein the balance adjusting device comprises a synchronous gear set, a second rotating seat located above the rack, and a balance rod arranged on the second rotating seat, the second rotating seat is rotatably arranged on the rack, a rotating shaft of the second rotating seat is parallel to a rotating shaft of the first rotating seat, a first gear and a second gear meshed with the synchronous gear set are arranged, the outer diameters of the first gear and the second gear are the same, the first gear is fixed on the rotating shaft of the first rotating seat, and the second gear is fixed on the rotating shaft of the second rotating seat;
when the mounting rod is in a vertical state, the balance rod is also in a vertical state;
when the torque steering engine drives the first rotating seat and the mounting rod to rotate, the second rotating seat and the balance rod synchronously and reversely rotate under the action of the synchronous gear set.
3. The rotary unmanned aerial vehicle electroscope of claim 2, wherein the first and second rotating bases are symmetrically disposed on opposite sides of a center of the frame.
4. A rotary unmanned aerial vehicle electricity inspection device of claim 2 or 3, wherein the mounting bar and the balancing bar are symmetrically distributed on opposite sides of the center of the frame.
5. The rotary unmanned aerial vehicle electroscope of claim 2 or 3, wherein the first and second rotary seats are near the center of the frame.
6. The rotary type unmanned aerial vehicle electroscope of claim 1, wherein still be equipped with the camera on the first rotation seat, the camera is used for shooing the position of installation pole and electroscope.
7. A rotary unmanned aerial vehicle electroscope apparatus as claimed in claim 1, wherein the electroscope is fixed at an upper end of the mounting rod.
8. The rotary unmanned aerial vehicle electricity inspection device of claim 1, wherein the mounting rod is a hollow rod, and the inner bore of the mounting rod forms a wire passing hole.
9. A rotary unmanned aerial vehicle electroscope apparatus as claimed in claim 1, wherein the torque steering engine is mounted on the frame by bolts.
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| CN202011454216.7A CN112550742B (en) | 2020-12-10 | 2020-12-10 | Rotary unmanned aerial vehicle electroscope |
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| CN202011454216.7A CN112550742B (en) | 2020-12-10 | 2020-12-10 | Rotary unmanned aerial vehicle electroscope |
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