CN213168588U

CN213168588U - Unmanned aerial vehicle flies to control navigation head

Info

Publication number: CN213168588U
Application number: CN202022274814.8U
Authority: CN
Inventors: 张前; 郭竟翔
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-10-13
Filing date: 2020-10-13
Publication date: 2021-05-11
Anticipated expiration: 2030-10-13

Abstract

The utility model discloses an unmanned aerial vehicle flies accuse navigation head, including the installation shell, the equal fixedly connected with fixed box in both sides of installation shell inner chamber bottom, the top of fixed box is provided with the installation piece, the top fixedly connected with navigation head body of two installation pieces, the both sides at installation shell top are all seted up flutedly, recess inner chamber's bottom is provided with the briquetting, the top fixedly connected with pull rod of briquetting, the surface cover of pull rod is equipped with first spring, the top of pull rod extends to the top of installation shell, the inner chamber of fixed box is provided with the movable block. The utility model discloses a set up installation shell, fixed box, installation piece, navigation equipment body, recess, briquetting, pull rod, first spring, movable block, second spring, carriage release lever, ejector pad, fixture block and draw-in groove, solved current unmanned aerial vehicle and flown the problem of controlling navigation equipment and be not convenient for maintain, this unmanned aerial vehicle flies to control navigation equipment, possesses the advantage of being convenient for maintain.

Description

Unmanned aerial vehicle flies to control navigation head

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle flies to control navigation equipment.

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, unmanned aerial vehicle navigation equipment is usually fixed through bolts, and when the navigation equipment is required to be disassembled for maintenance, special tools are required to be used for operating a plurality of bolts, so that a large amount of time of workers is wasted, the practicability of the unmanned aerial vehicle navigation equipment is reduced, and the unmanned aerial vehicle navigation equipment is not beneficial to use.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle flies to control navigation equipment possesses the advantage of being convenient for to maintain, has solved the problem that current unmanned aerial vehicle flies to control navigation equipment and is not convenient for maintain.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle flight control navigation device comprises a mounting shell, wherein both sides of the bottom of an inner cavity of the mounting shell are fixedly connected with a fixed box, the top of the fixed box is provided with a mounting block, the tops of the two mounting blocks are fixedly connected with a navigation device body, both sides of the top of the mounting shell are provided with grooves, the bottom of the inner cavity of the groove is provided with a pressing block, the top of the pressing block is fixedly connected with a pull rod, the surface of the pull rod is sleeved with a first spring, the top of the pull rod extends to the top of the mounting shell, the inner cavity of the fixed box is provided with moving blocks, one sides of the two moving blocks opposite are fixedly connected with a second spring, one sides of the two moving blocks opposite are fixedly connected with a moving rod, one end of the moving rod, far away from the moving blocks, sequentially penetrates through the fixed box and the mounting shell to extend to the, the bottom of the mounting block is provided with a clamping groove matched with the clamping block for use, and the top of the clamping block penetrates through the fixing box and extends to the inner cavity of the clamping groove.

Preferably, the surface of the push block is in contact with the press block, and one side, far away from the moving block, of the second spring is fixedly connected with the inner wall of the fixed box.

Preferably, the bottom of the mounting block is in contact with the fixed box, the top of the pull rod is fixedly connected with a pull ring, and the clamping block and the clamping groove are L-shaped.

Preferably, the bottom of the two sides of the mounting shell is fixedly connected with a fixing block, and mounting holes are formed in the front side and the rear side of the top of the fixing block.

Preferably, the surface of the navigation device body is in contact with the inner wall of the mounting shell, and the surface of the moving block is in sliding connection with the inner wall of the fixing box.

Preferably, the top of fixed box is seted up with the opening that the fixture block cooperation was used, the through-hole that uses with the carriage release lever cooperation is all seted up to one side that two fixed boxes are opposite.

Preferably, the bottom of installation shell inner chamber just is located the spacing box of fixedly connected with between two fixed boxes, the bottom fixedly connected with third spring of spacing box inner chamber, the top fixedly connected with push pedal of third spring, the top fixedly connected with push rod of push pedal, the top of push rod runs through spacing box and contacts with the navigation equipment body.

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

1. the utility model discloses a set up installation shell, fixed box, installation piece, navigation equipment body, recess, briquetting, pull rod, first spring, movable block, second spring, carriage release lever, ejector pad, fixture block and draw-in groove, solved current unmanned aerial vehicle and flown the problem of controlling navigation equipment and be not convenient for maintain, this unmanned aerial vehicle flies to control navigation equipment, possesses the advantage of being convenient for maintain, is worth promoting.

2. The utility model discloses a set up the briquetting, the removal of ejector pad of can being convenient for, through setting up the draw-in groove, the use of the fixture block of can being convenient for, through setting up fixed block and mounting hole, the fixing of installation shell of can being convenient for, through setting up spacing box, third spring, push pedal and push rod, the dismantlement of navigation equipment body of can being convenient for, through setting up the pull ring, can the person of facilitating the use stimulate the pull rod, through setting up the opening, the use of the fixture block of can being convenient for, through setting up the through-hole, the use of carriage release lever.

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 cross-sectional view of the limiting box of the present invention.

In the figure: 1. mounting a shell; 2. a fixing box; 3. mounting blocks; 4. a navigation device body; 5. a groove; 6. briquetting; 7. a pull rod; 8. a first spring; 9. a moving block; 10. a second spring; 11. a travel bar; 12. a push block; 13. a clamping block; 14. a card slot; 15. a fixed block; 16. mounting holes; 17. a limiting box; 18. a third spring; 19. pushing the plate; 20. a push rod; 21. and (4) a pull ring.

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 navigation device comprises a mounting shell 1, wherein both sides of the bottom of an inner cavity of the mounting shell 1 are fixedly connected with a fixed box 2, the top of the fixed box 2 is provided with a mounting block 3, the tops of the two mounting blocks 3 are fixedly connected with a navigation device body 4, both sides of the top of the mounting shell 1 are provided with grooves 5, the bottom of the inner cavity of each groove 5 is provided with a pressing block 6, the top of each pressing block 6 is fixedly connected with a pull rod 7, the surface of each pull rod 7 is sleeved with a first spring 8, the top of each pull rod 7 extends to the top of the mounting shell 1, the inner cavity of the fixed box 2 is provided with a moving block 9, one opposite side of each moving block 9 is fixedly connected with a second spring 10, one opposite side of each moving block 9 is fixedly connected with a moving rod 11, one end of each moving rod 11, far away from the corresponding moving block 9, the top of the moving block 9 is fixedly connected with a clamping block 13, the bottom of the mounting block 3 is provided with a clamping groove 14 matched with the clamping block 13 for use, the top of the clamping block 13 penetrates through the fixed box 2 and extends to an inner cavity of the clamping groove 14, the surface of the push block 12 is contacted with the pressing block 6, one side of the second spring 10 far away from the moving block 9 is fixedly connected with the inner wall of the fixed box 2, the bottom of the mounting block 3 is contacted with the fixed box 2, the top of the pull rod 7 is fixedly connected with a pull ring 21, the clamping block 13 and the clamping groove 14 are both L-shaped, the bottoms of two sides of the mounting shell 1 are both fixedly connected with fixed blocks 15, the front side and the rear side of the top of each fixed block 15 are both provided with mounting holes 16, the surface of the navigation device body 4 is contacted with the inner wall of the mounting shell 1, the surface of the moving block 9 is slidably connected with the inner wall of the fixed box 2, the bottom of the inner cavity of the mounting shell 1 is fixedly connected with a limiting box 17 between the two fixing boxes 2, the bottom of the inner cavity of the limiting box 17 is fixedly connected with a third spring 18, the top of the third spring 18 is fixedly connected with a push plate 19, the top of the push plate 19 is fixedly connected with a push rod 20, the top of the push rod 20 penetrates through the limiting box 17 and contacts with the navigation equipment body 4, the movement of the push block 12 can be facilitated by arranging the press block 6, the use of the fixture block 13 can be facilitated by arranging the clamping groove 14, the fixing of the mounting shell 1 can be facilitated by arranging the fixing block 15 and the mounting hole 16, the dismounting of the navigation equipment body 4 can be facilitated by arranging the limiting box 17, the third spring 18, the push plate 19 and the push rod 20, the pulling rod 7 can be conveniently pulled by a user by arranging the pull ring 21, the use of the fixture block 13 can be facilitated by arranging an opening, the use, through setting up installation shell 1, fixed box 2, installation piece 3, navigation head body 4, recess 5, briquetting 6, pull rod 7, first spring 8, movable block 9, second spring 10, carriage release lever 11, ejector pad 12, fixture block 13 and draw-in groove 14, solved current unmanned aerial vehicle and flown the problem of controlling navigation head and be not convenient for maintain, this unmanned aerial vehicle flies to control navigation head, possesses the advantage of being convenient for to maintain, is worth promoting.

When the device is used, a user pulls the pull ring 21 upwards, the pull ring 21 drives the press block 6 to move upwards through the matching of the pull rod 7 to extrude the first spring 8, the limit on the push block 12 is removed, the second spring 10 resets to drive the two moving blocks 9 to be away from each other, the moving blocks 9 drive the clamp block 13 to move, the limit on the installation block 3 is removed, then the navigation device body 4 can be moved upwards to be disassembled, when the navigation device needs to be assembled, the navigation device body 4 is moved into the installation shell 1 after the pull ring 21 is pulled, the mounting block 3 is sleeved on the clamping block 13, the pull ring 21 is loosened, the first spring 8 resets to drive the pressing block 6 to move downwards to extrude the pushing block 12, the two pushing blocks 12 are driven to move towards the middle, the pushing block 12 drives the two moving blocks 9 to move towards the middle through the matching of the moving rod 11, the moving blocks 9 drive the two clamping blocks 13 to move towards the middle, the mounting block 3 is limited, and the mounting is completed.

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 flies accuse navigation equipment, includes installation shell (1), its characterized in that: the navigation device is characterized in that fixed boxes (2) are fixedly connected to two sides of the bottom of an inner cavity of the mounting shell (1), mounting blocks (3) are arranged at the top of each fixed box (2), a navigation device body (4) is fixedly connected to the tops of the two mounting blocks (3), grooves (5) are formed in two sides of the top of the mounting shell (1), pressing blocks (6) are arranged at the bottom of the inner cavity of each groove (5), pull rods (7) are fixedly connected to the tops of the pressing blocks (6), first springs (8) are sleeved on the surfaces of the pull rods (7), the tops of the pull rods (7) extend to the tops of the mounting shell (1), moving blocks (9) are arranged in the inner cavity of the fixed boxes (2), second springs (10) are fixedly connected to opposite sides of the two moving blocks (9), moving rods (11) are fixedly connected to opposite sides of the two moving blocks (9), one end, far away from the moving block (9), of the moving rod (11) penetrates through the fixing box (2) and the mounting shell (1) in sequence and extends to an inner cavity of the groove (5) and is fixedly connected with the push block (12), the top of the moving block (9) is fixedly connected with the clamping block (13), the bottom of the mounting block (3) is provided with a clamping groove (14) matched with the clamping block (13) in use, and the top of the clamping block (13) penetrates through the fixing box (2) and extends to the inner cavity of the clamping groove (14).

2. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the surface of the push block (12) is in contact with the press block (6), and one side, far away from the moving block (9), of the second spring (10) is fixedly connected with the inner wall of the fixed box (2).

3. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the bottom of the mounting block (3) is in contact with the fixed box (2), the top of the pull rod (7) is fixedly connected with a pull ring (21), and the clamping block (13) and the clamping groove (14) are L-shaped.

4. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the bottom of installation shell (1) both sides all fixedly connected with fixed block (15), mounting hole (16) have all been seted up to the front side and the rear side at fixed block (15) top.

5. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the surface of the navigation equipment body (4) is in contact with the inner wall of the mounting shell (1), and the surface of the moving block (9) is in sliding connection with the inner wall of the fixing box (2).

6. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the top of the fixed box (2) is provided with an opening matched with the clamping block (13) for use, and one side of the two fixed boxes (2) opposite to each other is provided with a through hole matched with the moving rod (11) for use.

7. The unmanned aerial vehicle flight control navigation device of claim 1, wherein: the bottom of installing shell (1) inner chamber just is located spacing box of fixedly connected with (17) between two fixed box (2), the bottom fixedly connected with third spring (18) of spacing box (17) inner chamber, the top fixedly connected with push pedal (19) of third spring (18), the top fixedly connected with push rod (20) of push pedal (19), the top of push rod (20) is run through spacing box (17) and is contacted with navigation equipment body (4).