CN213677190U

CN213677190U - Unmanned aerial vehicle flight control monitoring sensor

Info

Publication number: CN213677190U
Application number: CN202022271733.2U
Authority: CN
Inventors: 郭竟翔; 张前
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-10-13
Filing date: 2020-10-13
Publication date: 2021-07-13
Anticipated expiration: 2030-10-13

Abstract

The utility model discloses an unmanned aerial vehicle flight control monitoring sensor, including the sensor body, the bottom cover of sensor body is equipped with the set casing, the bottom fixedly connected with mount pad of set casing, the equal fixedly connected with picture peg in both sides of sensor body bottom, the slot that uses with the picture peg cooperation is all seted up to the both sides at mount pad top, the bottom of picture peg extends to the bottom of slot inner chamber, the both sides of mount pad inner chamber all are provided with the baffle, the surface of baffle and the inner wall fixed connection of mount pad. The utility model discloses a set up sensor body, set casing, mount pad, picture peg, slot, baffle, movable plate, fixture block, draw-in groove, carriage release lever, first spring, slide bar, sliding sleeve, second spring, connecting strip and operation panel, solved the problem that current unmanned aerial vehicle flight control monitoring sensor is not convenient for dismantle, this unmanned aerial vehicle flight control monitoring sensor possesses convenient to detach's advantage.

Description

Unmanned aerial vehicle flight control monitoring sensor

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle flight control monitoring sensor.

Background

Unmanned aerial vehicle is unmanned aerial vehicle for short, and is the unmanned aerial vehicle who utilizes radio remote control equipment and self-contained program control device to control, or by the vehicle-mounted computer completely or intermittently independently operate, compares with unmanned aerial vehicle, and unmanned aerial vehicle often is more suitable for those tasks of being insipid, dirty or dangerous, and unmanned aerial vehicle according to the application, can divide into military use and civilian use.

At present, the unmanned aerial vehicle flight control monitoring sensor is usually fixed through bolts, when the sensor is required to be disassembled for maintenance, a special tool is required to be used for operating a plurality of bolts, a large amount of time of workers is wasted, the practicability of the unmanned aerial vehicle flight control monitoring sensor is reduced, and the unmanned aerial vehicle flight control monitoring sensor is not beneficial to use.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle flight control monitoring sensor possesses convenient to detach's advantage, has solved the problem that current unmanned aerial vehicle flight control monitoring sensor is not convenient for dismantle.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle flight control monitoring sensor comprises a sensor body, wherein a fixed shell is sleeved at the bottom of the sensor body, a mounting seat is fixedly connected at the bottom of the fixed shell, inserting plates are fixedly connected at two sides of the bottom of the sensor body, inserting grooves matched with the inserting plates are formed in two sides of the top of the mounting seat, the bottoms of the inserting plates extend to the bottoms of inner cavities of the inserting grooves, partition plates are arranged at two sides of the inner cavity of the mounting seat, the surfaces of the partition plates are fixedly connected with the inner wall of the mounting seat, movable plates are arranged at one sides opposite to the two partition plates, clamping blocks are fixedly connected at one sides opposite to the two movable plates, clamping grooves matched with the clamping blocks are formed in one sides opposite to the two inserting plates, the sides opposite to the two clamping blocks penetrate through the mounting seat and extend to inner cavities of the clamping grooves, the utility model discloses a sliding sleeve, including the carriage release lever, the carriage release lever is equipped with the front side of mount pad, the surface cover of carriage release lever is equipped with first spring, and two relative one sides of carriage release lever all run through to the outside of baffle, are provided with the slide bar between two baffles, the top and the bottom of slide bar all with the inner wall fixed connection of mount pad, the surface of slide bar is from last to overlapping in proper order down and is equipped with sliding sleeve and second spring, the equal swing joint in both sides of sliding sleeve has the connecting strip, the one end and the carriage release lever swing joint of sliding sleeve are kept away from to the connecting strip, the front side fixedly connected with operation.

Preferably, the bottom of the two sides of the mounting seat is fixedly connected with a mounting block, mounting holes are formed in the front side and the rear side of the top of the mounting block, and the surface of the sensor body is in contact with the fixed shell.

Preferably, the top and the bottom of the moving plate are both fixedly connected with sliding blocks, and sliding grooves matched with the sliding blocks for use are formed in the top and the bottom of the inner cavity of the mounting seat.

Preferably, one side of the sliding block, which is far away from the moving plate, extends to the inner cavity of the sliding groove, and the surface of the sliding block is in sliding connection with the inner wall of the sliding groove.

Preferably, the top of the mounting seat is provided with a groove, and the top of the inner cavity of the groove is provided with a push plate.

Preferably, a third spring is fixedly connected between the bottom of the push plate and the inner wall of the groove, and an opening matched with the operating plate for use is formed in the front side of the mounting seat.

Preferably, the joints of the two ends of the connecting bar, the sliding sleeve and the moving rod are movably connected through a rotating shaft.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a set up sensor body, set casing, mount pad, picture peg, slot, baffle, movable plate, fixture block, draw-in groove, carriage release lever, first spring, slide bar, sliding sleeve, second spring, connecting strip and operation panel, solved the problem that current unmanned aerial vehicle flight control monitoring sensor is not convenient for dismantle, this unmanned aerial vehicle flight control monitoring sensor possesses convenient to detach's advantage, is worth promoting.

2. The utility model discloses a set up installation piece and mounting hole, the fixed of mount pad of can being convenient for, through setting up slider and spout, the removal of movable plate of can being convenient for, through setting up recess, push pedal and third spring, the sensor body rebound of can being convenient for, through setting up the opening, the use of operation panel of can being convenient for, through setting up the pivot, the use of connecting strip of can being convenient for.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a front view of the structure of the present invention;

fig. 3 is a partially enlarged view of a in fig. 1 according to the present invention.

In the figure: 1. a sensor body; 2. a stationary case; 3. a mounting seat; 4. inserting plates; 5. a slot; 6. a partition plate; 7. moving the plate; 8. a clamping block; 9. a card slot; 10. a travel bar; 11. a first spring; 12. a slide bar; 13. a sliding sleeve; 14. a second spring; 15. a connecting strip; 16. an operation panel; 17. a slider; 18. a chute; 19. a groove; 20. pushing the plate; 21. and a third spring.

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 "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end", 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 to be referred must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "provided", "connected", and the like are to be construed broadly, such as "connected", which may be 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, an unmanned aerial vehicle flight control monitoring sensor comprises a sensor body 1, a fixed shell 2 is sleeved at the bottom of the sensor body 1, a mounting seat 3 is fixedly connected to the bottom of the fixed shell 2, plug boards 4 are fixedly connected to both sides of the bottom of the sensor body 1, slots 5 matched with the plug boards 4 are formed in both sides of the top of the mounting seat 3, the bottom of the plug boards 4 extends to the bottom of the inner cavity of the slots 5, partition boards 6 are arranged on both sides of the inner cavity of the mounting seat 3, the surface of each partition board 6 is fixedly connected with the inner wall of the mounting seat 3, moving boards 7 are arranged on opposite sides of the two partition boards 6, clamping blocks 8 are fixedly connected to opposite sides of the two moving boards 7, clamping grooves 9 matched with the clamping blocks 8 are formed in opposite sides of the two plug boards 4, and opposite sides of the two clamping blocks 8 extend through, the opposite sides of the two moving plates 7 are fixedly connected with moving rods 10, the surface of each moving rod 10 is sleeved with a first spring 11, the opposite sides of the two moving rods 10 penetrate through the outer sides of the partition plates 6, a slide rod 12 is arranged between the two partition plates 6, the top and the bottom of the slide rod 12 are fixedly connected with the inner wall of the mounting seat 3, the surface of the slide rod 12 is sequentially sleeved with a slide sleeve 13 and a second spring 14 from top to bottom, the two sides of the slide sleeve 13 are movably connected with connecting strips 15, one ends of the connecting strips 15, far away from the slide sleeve 13, are movably connected with the moving rods 10, the front side of the slide sleeve 13 is fixedly connected with an operating plate 16, the front side of the operating plate 16 penetrates through the front side of the mounting seat 3, the bottoms of the two sides of the mounting seat 3 are fixedly connected with mounting blocks, the front side and the rear side of the top of the mounting blocks are respectively provided with mounting holes, the surface of the, the top and the bottom of the inner cavity of the mounting seat 3 are both provided with sliding grooves 18 matched with the sliding block 17 for use, one side of the sliding block 17 far away from the movable plate 7 extends to the inner cavity of the sliding groove 18, the surface of the sliding block 17 is in sliding connection with the inner wall of the sliding groove 18, the top of the mounting seat 3 is provided with a groove 19, the top of the inner cavity of the groove 19 is provided with a push plate 20, a third spring 21 is fixedly connected between the bottom of the push plate 20 and the inner wall of the groove 19, the front side of the mounting seat 3 is provided with an opening matched with the operating plate 16 for use, the two ends of the connecting strip 15 are movably connected with the joints of the sliding sleeve 13 and the moving rod 10 through rotating shafts, the mounting block and the mounting hole are arranged for facilitating the fixing of the mounting seat 3, the sliding block 17 and the sliding groove 18 are arranged for facilitating the moving of the movable plate, through setting up the opening, the use of operation panel 16 of can being convenient for, through setting up the pivot, the use of connecting strip 15 of being convenient for, through setting up sensor body 1, set casing 2, mount pad 3, picture peg 4, slot 5, baffle 6, movable plate 7, fixture block 8, draw-in groove 9, carriage release lever 10, first spring 11, slide bar 12, sliding sleeve 13, second spring 14, connecting strip 15 and operation panel 16, the problem of current unmanned aerial vehicle flight control monitoring sensor be not convenient for dismantle has been solved, this unmanned aerial vehicle flight control monitoring sensor, possess convenient to detach's advantage, be worth promoting.

During the use, the sliding sleeve 13 is moved downwards through the cooperation of the operating panel 16, the sliding sleeve 13 drives the two moving rods 10 to move towards the middle through the cooperation of the connecting strip 15, the moving rods 10 drive the two moving plates 7 to move towards the middle, the moving plates 7 drive the clamping blocks 8 to move out from the clamping grooves 9, the sensor body 1 can be moved upwards to be detached later, when the installation is needed, the inserting plates 4 are moved to enter the slots 5, the inserting plates 4 continue to move downwards to extrude the clamping blocks 8, the two clamping blocks 8 are driven to be kept away from each other, the clamping blocks 8 drive the two moving plates 7 to be kept away from each other to extrude the first spring 11, until the clamping grooves 9 correspond to the clamping blocks 8, the first spring 11 resets and drives the clamping blocks 8 to enter the clamping grooves 9 through the cooperation.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle flight control monitoring sensor, includes sensor body (1), its characterized in that: the sensor comprises a sensor body (1), wherein a fixed shell (2) is sleeved at the bottom of the sensor body (1), a mounting seat (3) is fixedly connected to the bottom of the fixed shell (2), inserting plates (4) are fixedly connected to the two sides of the bottom of the sensor body (1), inserting grooves (5) matched with the inserting plates (4) for use are formed in the two sides of the top of the mounting seat (3), the bottoms of the inserting plates (4) extend to the bottoms of inner cavities of the inserting grooves (5), partition plates (6) are arranged on the two sides of the inner cavity of the mounting seat (3), the surfaces of the partition plates (6) are fixedly connected with the inner wall of the mounting seat (3), movable plates (7) are arranged on the opposite sides of the two partition plates (6), fixture blocks (8) are fixedly connected to the opposite sides of the two movable plates (7), and clamping grooves (9) matched with the fixture blocks, one side opposite to each clamping block (8) penetrates through the mounting seat (3) and extends to an inner cavity of the clamping groove (9), one side opposite to each moving plate (7) is fixedly connected with a moving rod (10), the surface of each moving rod (10) is sleeved with a first spring (11), one side opposite to each moving rod (10) penetrates through the outer side of the partition plate (6), a sliding rod (12) is arranged between the two partition plates (6), the top and the bottom of each sliding rod (12) are fixedly connected with the inner wall of the mounting seat (3), the surface of each sliding rod (12) is sequentially sleeved with a sliding sleeve (13) and a second spring (14) from top to bottom, connecting strips (15) are movably connected to the two sides of the sliding sleeve (13), one end, far away from the sliding sleeve (13), of each connecting strip (15) is movably connected with the moving rod (10), and an operating plate (16) is fixedly connected to the front side of the sliding sleeve (13, the front side of the operation plate (16) penetrates to the front side of the mounting seat (3).

2. The unmanned aerial vehicle flight control monitoring sensor of claim 1, wherein: the sensor is characterized in that the bottom parts of the two sides of the mounting seat (3) are fixedly connected with mounting blocks, mounting holes are formed in the front side and the rear side of the top of each mounting block, and the surface of the sensor body (1) is in contact with the fixed shell (2).

3. The unmanned aerial vehicle flight control monitoring sensor of claim 1, wherein: the top and the bottom of the movable plate (7) are both fixedly connected with sliding blocks (17), and sliding grooves (18) matched with the sliding blocks (17) for use are formed in the top and the bottom of the inner cavity of the mounting seat (3).

4. The unmanned aerial vehicle flight control monitoring sensor of claim 3, wherein: one side of the sliding block (17) far away from the moving plate (7) extends to an inner cavity of the sliding groove (18), and the surface of the sliding block (17) is in sliding connection with the inner wall of the sliding groove (18).

5. The unmanned aerial vehicle flight control monitoring sensor of claim 1, wherein: a groove (19) is formed in the top of the mounting seat (3), and a push plate (20) is arranged at the top of an inner cavity of the groove (19).

6. The unmanned aerial vehicle flight control monitoring sensor of claim 5, wherein: a third spring (21) is fixedly connected between the bottom of the push plate (20) and the inner wall of the groove (19), and an opening matched with the operating plate (16) for use is formed in the front side of the mounting seat (3).

7. The unmanned aerial vehicle flight control monitoring sensor of claim 1, wherein: the two ends of the connecting bar (15) are movably connected with the joints of the sliding sleeve (13) and the moving rod (10) through rotating shafts.