CN214899042U

CN214899042U - A can dismantle fixed knot structure for unmanned aerial vehicle power supply aviation plug

Info

Publication number: CN214899042U
Application number: CN202121569951.2U
Authority: CN
Inventors: 郭阳
Original assignee: Xianning Lusheng Agricultural Technology Co ltd
Current assignee: HARBIN NEW-CREATE PROCESSING EQUIPMENT MANUFACTURING CO LTD
Priority date: 2021-07-12
Filing date: 2021-07-12
Publication date: 2021-11-26
Anticipated expiration: 2031-07-12

Abstract

The utility model provides a can dismantle fixed knot construct for unmanned aerial vehicle power supply aviation plug relates to unmanned air vehicle technical field, including the connecting plate, the fixed orifices has been seted up at the top of connecting plate, the inner wall sliding connection of fixed orifices has fixed pipe. The utility model discloses in, in the use, fix fixed pipe through the fixed orifices, prevent that fixed pipe from taking place the slope, spacing groove through above the connecting plate is fixed the fixed plate, prevent that the fixed plate from sliding, the sliding tray above the fixture block can be fixed the limiting plate, prevent the limiting plate rotation, thereby can't fix the fixed plate, it is fixed through the multilayer, solve the easy skew problem in situ of aviation plug, the fixed orifices can prevent that fixed pipe from taking place the slope, the stable in structure of increase equipment, the fixed plate can be fixed the aviation plug main part, prevent that the aviation plug main part from removing at will, the stable in structure of increase equipment, the spacing groove can be fixed the fixed plate, prevent that the fixed plate from sliding from top to bottom, the stable in structure of increase equipment.

Description

A can dismantle fixed knot structure for unmanned aerial vehicle power supply aviation plug

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a can dismantle fixed knot construct that is used for unmanned aerial vehicle power supply to insert by plane.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

But current unmanned aerial vehicle in use, unmanned aerial vehicle's battery gives the motor power supply, but because unmanned aerial vehicle needs regular maintenance, generally all use between battery and the motor to insert and carry out electric connection, nevertheless current boat insert under long-time work, the original position of deviating easily to can lead to contact failure, make the unable normal work of unmanned aerial vehicle, give people and bring very big puzzlement.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving and having unmanned aerial vehicle in use among the prior art, unmanned aerial vehicle's battery supplies power for the motor, but because unmanned aerial vehicle needs periodic maintenance, generally all use between battery and the motor to insert and carry out electric connection, nevertheless current boat is inserted under long-time work, the former position of easy skew to can lead to contact failure, make the unable normal problem of working of unmanned aerial vehicle, and the detachable fixed knot who is used for unmanned aerial vehicle power supply boat to insert that provides constructs.

In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides a can dismantle fixed knot construct for unmanned aerial vehicle power supply boat is inserted, includes the connecting plate, the fixed orifices has been seted up at the top of connecting plate, the inner wall sliding connection of fixed orifices has fixed pipe, the one end welding that fixed pipe kept away from the fixed orifices has the fixed plate, one side that fixed pipe was kept away from to the fixed plate is provided with the boat and inserts the main part, the top of connecting plate is rotated through the pivot and is connected with two limiting plates, two one side that the limiting plate is close to the connecting plate all seted up with fixed plate assorted spacing groove, two be connected with the surface block of fixed plate between the inner wall of spacing groove.

Preferably, the outer surface sliding connection of inserting the main part by plane has solid fixed ring, gu fixed ring's outer surface welding has four extension boards.

Preferably, the supporting plate is close to one side of the fixed plate and is provided with a clamping groove, four the inner walls of the clamping grooves are in sliding connection with the outer surface of the fixed plate, two the limiting plates are close to one side of the limiting groove and are provided with clamping grooves, and the inner walls of the clamping grooves are clamped with the outer surface of the fixing ring.

Preferably, one side of the connecting plate, which is close to the limiting plate, is welded with two fixing blocks, and one side of each fixing block is provided with a sliding groove.

Preferably, two equal sliding connection of inner wall of spout has the slide bar, two the spring has all been welded to the one end that the slide bar is close to the spout, the one end that the slide bar was kept away from to the spring welds with the inner wall of spout.

Preferably, two the slide bar is kept away from the one end of spring and all is welded the fixture block, two the slide bar was kept away from to the fixture block one end all seted up with limiting plate assorted sliding tray, the inner wall of sliding tray and the surface sliding connection of limiting plate, two the arm-tie is all welded to one side that the connecting plate was kept away from to the fixture block.

Compared with the prior art, the utility model has the advantages and positive effects that,

1. the utility model discloses in, in the use, fix fixed pipe through the fixed orifices, prevent that fixed pipe from taking place the slope, spacing groove through above the connecting plate is fixed the fixed plate, prevent that the fixed plate from sliding, the sliding tray above the fixture block can be fixed the limiting plate, prevent the limiting plate rotation, thereby can't fix the fixed plate, it is fixed through the multilayer, solve the easy skew problem in situ of aviation plug, the fixed orifices can prevent that fixed pipe from taking place the slope, the stable in structure of increase equipment, the fixed plate can be fixed the aviation plug main part, prevent that the aviation plug main part from removing at will, the stable in structure of increase equipment, the spacing groove can be fixed the fixed plate, prevent that the fixed plate from sliding from top to bottom, the stable in structure of increase equipment.

2. The utility model discloses in, in the use, if the aviation plug main part need take out, the pulling arm-tie makes connecting plate and sliding tray separation, just can take out the aviation plug main part at this moment and overhaul, and the spring makes the fixture block fix the limiting plate, increases the stable in structure of equipment, and the arm-tie can provide a stress point, and the work efficiency of equipment is increased to the convenient control to the fixture block.

Drawings

Fig. 1 is a perspective view of a detachable fixing structure for an unmanned aerial vehicle power supply aerial plug provided by the present invention;

fig. 2 is an exploded perspective view of a detachable fixing structure for an unmanned aerial vehicle power supply aerial plug according to the present invention;

fig. 3 is a bottom perspective exploded view of a detachable fixing structure for an unmanned aerial vehicle power supply pod according to the present invention;

fig. 4 is the utility model provides a fixed block sectional structure stereogram that is used for unmanned aerial vehicle power supply to insert by plane's fixed block of dismantling.

Illustration of the drawings: 1. a connecting plate; 2. a fixing hole; 3. a fixed tube; 4. a fixing plate; 5. an aerial main body; 6. a fixing ring; 7. a support plate; 8. a clamping groove; 9. a limiting plate; 10. a limiting groove; 11. a card slot; 12. a fixed block; 13. a chute; 14. a slide bar; 15. a spring; 16. a clamping block; 17. a sliding groove; 18. and (5) pulling the plate.

Detailed Description

In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.

In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the present invention is not limited to the limitations of the specific embodiments of the present disclosure.

Embodiment 1, as shown in fig. 1-4, the utility model provides a can dismantle fixed knot structure for unmanned aerial vehicle power supply boat inserts, including connecting plate 1, fixed orifices 2 has been seted up at connecting plate 1's top, the inner wall sliding connection of fixed orifices 2 has fixed pipe 3, the one end welding that fixed pipe 3 kept away from fixed orifices 2 has fixed plate 4, one side that fixed pipe 3 was kept away from to fixed plate 4 is provided with boat and inserts main part 5, the top of connecting plate 1 is rotated through the pivot and is connected with two limiting plates 9, one side that two limiting plates 9 are close to connecting plate 1 all seted up with fixed plate 4 assorted spacing groove 10, be connected with fixed plate 4's surface block between the inner wall of two spacing grooves 10, boat and insert main part 5's surface sliding connection has solid fixed ring 6, gu fixed ring 6's surface welding has four extension boards 7.

The whole embodiment 1 achieves the effects that, in use, the fixing tube 3 is fixed through the fixing hole 2, the fixing tube 3 can be prevented from inclining, so that the aviation plug main body 5 is fixed, the fixing plate 4 is fixed through the limiting groove 10 on the limiting plate 9, the fixing plate 4 is prevented from sliding, so that the aviation plug main body 5 is fixed, the sliding groove 17 on the fixture block 16 can fix the limiting plate 9, the limiting plate 9 is prevented from rotating, so that the limiting plate 9 cannot be fixed, the problem that the aviation plug is easy to deviate from the original position is solved through multi-layer fixing, the fixing hole 2 can be designed to prevent the fixing tube 3 from inclining, the structural stability of the device is increased, the fixing plate 4 can be fixed through the design of the fixing hole 4, the aviation plug main body 5 is prevented from moving randomly, the structural stability of the device is increased, and the fixing plate 4 can be fixed through the design of the limiting groove 10, the fixing plate 4 is prevented from sliding up and down, and the structural stability of the equipment is increased.

Example 2, as shown in fig. 3-4, one side of the support plate 7 close to the fixed plate 4 is provided with clamping grooves 8, inner walls of four clamping grooves 8 are slidably connected with an outer surface of the fixed plate 4, one side of each of the two limiting plates 9 close to the limiting groove 10 is provided with a clamping groove 11, inner walls of the clamping grooves 11 are clamped with an outer surface of the fixing ring 6, one side of the connecting plate 1 close to the limiting plates 9 is welded with two fixing blocks 12, one side of each of the two fixing blocks 12 is provided with a sliding groove 13, inner walls of the two sliding grooves 13 are slidably connected with sliding rods 14, one ends of the two sliding rods 14 close to the sliding grooves 13 are welded with springs 15, one ends of the springs 15 far away from the sliding rods 14 are welded with inner walls of the sliding grooves 13, one ends of the two sliding rods 14 far away from the springs 15 are welded with clamping blocks 16, one ends of the two clamping blocks 16 far away from the sliding rods 14 are provided with sliding grooves 17 matched with the limiting plate 9, inner walls of the sliding grooves 17 are slidably connected with the outer surfaces of the limiting plates 9, and pull plates 18 are welded on one sides of the two clamping blocks 16 far away from the connecting plate 1.

The effect that its whole embodiment 2 reaches does, in use, if the aviation plug main part 5 need take out, pulling arm-tie 18, can make fixture block 16 remove, limiting plate 9 and sliding tray 17 separation this moment, just can stimulate solid fixed ring 6 this moment, then take out solid fixed ring 6, just can take out fixed plate 4 afterwards, fixed plate 4 takes out this moment and will take out aviation plug main part 5, this moment just can overhaul aviation plug main part 5, and spring 15's design makes fixture block 16 fix limiting plate 9, increase the stable in structure of equipment, and arm-tie 18's design can provide a stress point, the convenience is to fixture block 16's control, increase the work efficiency of equipment.

The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms, and any person skilled in the art may use the above-mentioned technical contents to change or modify the equivalent embodiment into equivalent changes and apply to other fields, but any simple modification, equivalent change and modification made to the above embodiments according to the technical matters of the present invention will still fall within the protection scope of the technical solution of the present invention.

Claims

1. The utility model provides a can dismantle fixed knot structure for unmanned aerial vehicle power supply aviation plug, includes connecting plate (1), its characterized in that: fixed orifices (2) have been seted up at the top of connecting plate (1), the inner wall sliding connection of fixed orifices (2) has fixed pipe (3), the one end welding of fixed orifices (2) is kept away from in fixed pipe (3) has fixed plate (4), one side that fixed pipe (3) were kept away from in fixed plate (4) is provided with aviation plug main part (5), the top of connecting plate (1) is rotated through the pivot and is connected with two limiting plates (9), two limiting plate (9) are close to one side of connecting plate (1) and all seted up with fixed plate (4) assorted spacing groove (10), two be connected with the surface block of fixed plate (4) between the inner wall of spacing groove (10).

2. The detachable fixing structure for the unmanned aerial vehicle power supply aerial plug of claim 1, wherein: the outer surface sliding connection of boat inserting main part (5) has solid fixed ring (6), the outer surface welding of solid fixed ring (6) has four extension boards (7).

3. The detachable fixing structure for the unmanned aerial vehicle power supply aerial plug of claim 2, wherein: clamping groove (8), four have all been seted up to one side that extension board (7) are close to fixed plate (4) surface sliding connection with fixed plate (4) between the inner wall in clamping groove (8), two draw-in groove (11) have all been seted up to one side that limiting plate (9) are close to spacing groove (10), the surface block with solid fixed ring (6) between the inner wall of draw-in groove (11).

4. The detachable fixing structure for the unmanned aerial vehicle power supply aerial plug of claim 1, wherein: one side welding that connecting plate (1) is close to limiting plate (9) has two fixed blocks (12), two spout (13) have all been seted up to one side of fixed block (12).

5. A detachable fixed knot structure for unmanned aerial vehicle power supply aviation plug of claim 4, characterized in that: two equal sliding connection in inner wall of spout (13) has slide bar (14), two spring (15) have all been welded to the one end that slide bar (14) are close to spout (13), the one end that slide bar (14) were kept away from in spring (15) welds with the inner wall of spout (13).

6. A detachable fixed knot structure for unmanned aerial vehicle power supply aviation plug of claim 5, characterized in that: two slide bar (14) keep away from the one end of spring (15) and all have welded fixture block (16), two slide bar (14) was kept away from in fixture block (16) one end all seted up with limiting plate (9) assorted sliding tray (17), the inner wall of sliding tray (17) and the surface sliding connection of limiting plate (9), two draw plate (18) all have welded in one side that connecting plate (1) was kept away from in fixture block (16).