CN214523368U

CN214523368U - A wisdom aircraft self-charging platform for electric power is patrolled and examined

Info

Publication number: CN214523368U
Application number: CN202022374475.0U
Authority: CN
Inventors: 杨雄; 杨永刚; 李锋涛; 王盛; 孙小宾; 赵隆; 彭海涛
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-10-23
Filing date: 2020-10-23
Publication date: 2021-10-29
Anticipated expiration: 2030-10-23

Abstract

The utility model discloses a wisdom aircraft self-charging platform for electric power patrols and examines, including descending platform, four bounding walls of last fixed surface of descending platform are connected with, four be provided with the aircraft body between the bounding wall, four one side that the bounding wall is close to the aircraft body all is provided with the mount, the first motor of lateral wall fixedly connected with of mount, the drive end of first motor extends to the inside fixedly connected with bidirectional threaded rod of mount, the one end of first motor and the inside wall fixed connection of mount are kept away from to bidirectional threaded rod. The utility model discloses can charge to the aircraft body automatically after the automatic back of navigating of aircraft body low-power, make the aircraft body also can charge when unmanned looking, make the charge mode more convenient, and more intelligent, can carry out automation to charging plug when not using simultaneously and accomodate, avoid the external environment to cause the pollution to charging plug, have certain practicality.

Description

A wisdom aircraft self-charging platform for electric power is patrolled and examined

Technical Field

The utility model relates to an electric power patrols and examines technical field, especially relates to a wisdom aircraft self-charging platform for electric power patrols and examines.

Background

Along with the development of science and technology, the progress of society, the wisdom aircraft can replace the manual work to carry out electric power and patrol and examine, current wisdom aircraft all has the automatic function that returns of low-power, in order to avoid taking place to drop when not having the electricity, but make the wisdom aircraft automatic landing on descending platform at low-power, charge through artifical inserting the socket inside of aircraft bottom with the plug, this kind of charging mode needs the manual work to operate, comparatively inconvenient, and when nobody looks at, can not charge its timely behind the aircraft body landing on the platform, influence the progress that electric power was patrolled and examined easily.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the wisdom aircraft that is used for electric power to patrol and examine that provides is from charging platform.

In order to achieve the above purpose, the utility model adopts the following technical scheme: a self-charging platform of a smart aircraft for electric power inspection comprises a landing platform, wherein four surrounding plates are fixedly connected to the upper surface of the landing platform, an aircraft body is arranged between the four surrounding plates, a fixing frame is arranged on one side, close to the aircraft body, of each surrounding plate, a first motor is fixedly connected to the outer side wall of each fixing frame, the driving end of each first motor extends to the inner portion of each fixing frame and is fixedly connected with a bidirectional threaded rod, one end, far away from the first motor, of each bidirectional threaded rod is fixedly connected with the inner side wall of each fixing frame, two threaded blocks are sleeved on the outer surface threads of each bidirectional threaded rod, one sides of the two threaded blocks are rotatably connected with two rotating rods, one ends, far away from the threaded blocks, of the two rotating rods are rotatably connected with a positioning plate together, a groove is formed in the surface of the landing platform, and an electric telescopic rod is fixedly connected to the inner portion of the groove, electric telescopic handle's drive end fixedly connected with charging plug, the inside of descending platform is provided with controller and battery, the inside of recess is provided with the switch board, the switch board is located the top of charging plug, the cavity has been seted up to the inside of descending platform, the cavity is located one side of switch board, the inside fixedly connected with second motor of cavity, the drive end fixedly connected with gear of second motor, the one end of switch board extends to the inside of cavity, the lower surface of switch board is provided with the rack, the wheel is connected with the rack toothing.

As a further description of the above technical solution:

the four enclosing plates are connected in an end-to-end mode to form a square-shaped structure.

As a further description of the above technical solution:

the upper surface of descending platform is provided with proximity switch, proximity switch and controller electric connection.

As a further description of the above technical solution:

the inside fixedly connected with guide arm of cavity, the surface of guide arm has cup jointed the slide, the lateral wall of slide and the one end fixed connection of switch plate.

As a further description of the above technical solution:

the thread block is connected with the sliding groove on the side wall of the enclosing plate in a sliding mode.

As a further description of the above technical solution:

the storage battery is connected with the charging plug through a lead.

The utility model discloses following beneficial effect has:

1. the utility model discloses a setting of locating plate, proximity switch, charging plug, controller, electric telescopic handle, battery can be adjusted the position of aircraft through the locating plate after the aircraft is automatic to return voyage to automatically, make charging plug insert the charging socket of aircraft body in charge, make the aircraft body also can charge when unmanned looking at, make the charge mode more convenient, and more intelligent.

2. The utility model discloses a setting of gear, rack, switch board, second motor, guide arm makes the flight body can spill charging plug with the automatic opening of switch board when needs charge, and the switch board is closed when need not charge and avoids causing the pollution to charging plug in external environment.

Drawings

Fig. 1 is a main sectional view of the self-charging platform of the smart aircraft for power inspection according to the present invention;

fig. 2 is a partial sectional view of the self-charging platform of the smart aircraft for power inspection according to the present invention;

fig. 3 is the utility model provides a wisdom aircraft self-charging platform's an enlarger for electric power patrols and examines.

Illustration of the drawings:

1. landing the platform; 2. an aircraft body; 3. enclosing plates; 4. positioning a plate; 5. a bidirectional threaded rod; 6. a controller; 7. a storage battery; 8. a groove; 9. an electric telescopic rod; 10. a charging plug; 11. a first motor; 12. a fixed mount; 13. a thread block; 14. rotating the rod; 15. a switch plate; 16. a rack; 17. a slide plate; 18. a second motor; 19. a guide bar; 20. a gear; 21. a cavity; 22. a proximity switch.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-3, the present invention provides an embodiment: a self-charging platform of a smart aircraft for electric power inspection comprises a landing platform 1, wherein four coamings 3 are fixedly connected to the upper surface of the landing platform 1, an aircraft body 2 is arranged between the four coamings 3, a fixing frame 12 is arranged on one sides of the four coamings 3 close to the aircraft body 2, a first motor 11 is fixedly connected to the outer side wall of the fixing frame 12, a driving end of the first motor 11 extends to the inner part of the fixing frame 12 and is fixedly connected with a bidirectional threaded rod 5, one end of the bidirectional threaded rod 5 far away from the first motor 11 is fixedly connected with the inner side wall of the fixing frame 12, two threaded blocks 13 are sleeved on the outer surface threads of the bidirectional threaded rod 5, two rotating rods 14 are rotatably connected to one sides of the two threaded blocks 13, one ends of the two rotating rods 14 far away from the threaded blocks 13 are rotatably connected with a positioning plate 4 together, a groove 8 is formed in the surface of the landing platform 1, and an electric telescopic rod 9 is fixedly connected to the inner part of the groove 8, electric telescopic handle 9's drive end fixedly connected with charging plug 10, the inside of descending platform 1 is provided with controller 6 and battery 7, the inside of recess 8 is provided with switch board 15, switch board 15 is located charging plug 10's top, cavity 21 has been seted up to the inside of descending platform 1, cavity 21 is located one side of switch board 15, the inside fixedly connected with second motor 18 of cavity 21, the drive end fixedly connected with gear 20 of second motor 18, the one end of switch board 15 extends to the inside of cavity 21, the lower surface of switch board 15 is provided with rack 16, gear 20 is connected with the meshing of rack 16.

The four coamings 3 are connected in an end-to-end manner to form a square structure so as to position the aircraft body 2 on four sides; the upper surface of the landing platform 1 is provided with a proximity switch 22, and the proximity switch 22 is electrically connected with the controller 6 so as to complete the automatic charging of the aircraft body 2 through the controller 6; a guide rod 19 is fixedly connected inside the cavity 21, a sliding plate 17 is sleeved on the surface of the guide rod 19, and the side wall of the sliding plate 17 is fixedly connected with one end of the switch plate 15, so that the moving stability of the switch plate 15 is improved conveniently; the thread block 13 is connected with the sliding groove on the side wall of the enclosing plate 3 in a sliding way so as to prevent the thread block 13 from rotating along with the bidirectional threaded rod 5 when the bidirectional threaded rod rotates; the storage battery 7 is connected with the charging plug 10 through a lead so as to be charged.

The working principle is as follows: when aircraft body 2 electric quantity is low excessively, automatically, return and fall on landing platform 1, proximity switch 22 senses behind aircraft body 2's the fall, start first motor 11 through controller 6, first motor 11 rotates electronic two-way threaded rod 5 and rotates, make two screw thread pieces 13 be close to, make the contained angle of dwang 14 diminish, make locating plate 4 stretch out, fix a position aircraft body 2 through these four locating plates 4, make the socket of its bottom aim at charging plug 10, later second motor 18 starts to make it drive gear 20 and rotate, gear 20 rotates and drives rack 16 and switch plate 15 and remove, make inside switch plate 15 withdrawal recess 8, electric telescopic handle 9 drives charging plug 10 ejecting, make charging plug 10 insert in the socket of aircraft body 2 bottoms can carry out automatic charging.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims

1. A wisdom aircraft self-charging platform for electric power is patrolled and examined, including descending platform (1), its characterized in that: the aircraft landing platform is characterized in that four enclosing plates (3) are fixedly connected to the upper surface of the landing platform (1), an aircraft body (2) is arranged between the four enclosing plates (3), a fixing frame (12) is arranged on one side, close to the aircraft body (2), of each of the four enclosing plates (3), a first motor (11) is fixedly connected to the outer side wall of each fixing frame (12), the driving end of each first motor (11) extends to a bidirectional threaded rod (5) fixedly connected to the inside of each fixing frame (12), one end, far away from the first motor (11), of each bidirectional threaded rod (5) is fixedly connected to the inner side wall of each fixing frame (12), two threaded blocks (13) are sleeved on the outer surface threads of each bidirectional threaded rod (5), two rotating rods (14) are rotatably connected to one side of each threaded block (13), and one ends, far away from the threaded blocks (13), of the two rotating rods (14) are rotatably connected to a positioning plate (4) together, the surface of the landing platform (1) is provided with a groove (8), the inner part of the groove (8) is fixedly connected with an electric telescopic rod (9), the driving end of the electric telescopic rod (9) is fixedly connected with a charging plug (10), the inner part of the landing platform (1) is provided with a controller (6) and a storage battery (7), the inner part of the groove (8) is provided with a switch board (15), the switch board (15) is positioned above the charging plug (10), the inner part of the landing platform (1) is provided with a cavity (21), the cavity (21) is positioned on one side of the switch board (15), the inner part of the cavity (21) is fixedly connected with a second motor (18), the driving end of the second motor (18) is fixedly connected with a gear (20), one end of the switch board (15) extends to the inner part of the cavity (21), the lower surface of the switch board (15) is provided with a rack (16), the gear (20) is meshed with the rack (16).

2. The smart aircraft self-charging platform for power inspection according to claim 1, wherein: the four enclosing plates (3) are connected in an end-to-end manner to form a square structure.

3. The smart aircraft self-charging platform for power inspection according to claim 1, wherein: the upper surface of descending platform (1) is provided with proximity switch (22), proximity switch (22) and controller (6) electric connection.

4. The smart aircraft self-charging platform for power inspection according to claim 1, wherein: the inside fixedly connected with guide arm (19) of cavity (21), slide (17) have been cup jointed on the surface of guide arm (19), the lateral wall and the one end fixed connection of switch board (15) of slide (17).

5. The smart aircraft self-charging platform for power inspection according to claim 1, wherein: the thread block (13) is in sliding connection with a sliding groove in the side wall of the enclosing plate (3).

6. The smart aircraft self-charging platform for power inspection according to claim 1, wherein: the storage battery (7) is connected with the charging plug (10) through a lead.