CN219192580U

CN219192580U - Mounting device for unmanned aerial vehicle

Info

Publication number: CN219192580U
Application number: CN202320438860.8U
Authority: CN
Inventors: 高风柱
Original assignee: Jiangsu Yida Weilan Intelligent Technology Co ltd
Current assignee: Jiangsu Yida Weilan Intelligent Technology Co ltd
Priority date: 2023-03-10
Filing date: 2023-03-10
Publication date: 2023-06-16
Anticipated expiration: 2033-03-10

Abstract

The utility model discloses a mounting device for an unmanned aerial vehicle, which comprises: unmanned aerial vehicle organism and year thing frame, the bottom of unmanned aerial vehicle organism is provided with two L type mounting panels that are symmetric distribution, and the intermediate position department of L type mounting panel terminal surface is provided with the slide rail, and the empty slot has been seted up at the top of year thing frame, and the top both ends of empty slot all are provided with the roof, and two roof slidable mounting respectively are located on the slide rail of both sides to the bottom of empty slot is provided with the bottom plate, and the top both ends of bottom plate all are provided with the flange, and the lower terminal surface at the roof is hugged closely to the flange. According to the mounting device disclosed by the utility model, the object carrying frame can be mounted at the bottom of the unmanned aerial vehicle under the condition that the unmanned aerial vehicle body is not damaged, so that the trouble that the object carrying frame can be mounted only by damaging the unmanned aerial vehicle body is avoided, the situation that the stability of the object carrying frame is influenced due to the fact that bolts slide in threaded holes when the object carrying frame is dismounted is avoided, the mounting device is simple in structure and convenient to operate, and the mounting device is favorable for later dismounting work.

Description

Mounting device for unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle mounting, in particular to a mounting device for an unmanned aerial vehicle.

Background

The unmanned plane is called as an unmanned plane for short, is a non-manned plane operated by using radio remote control equipment and a self-provided program control device, has no cockpit, is provided with equipment such as an autopilot, a program control device and the like, and is tracked, positioned, remotely controlled, remotely measured and digitally transmitted by personnel on the ground, a naval vessel or a master remote control station through equipment such as radar and the like, so that the unmanned plane has the advantages of low cost, low risk, strong survivability, good maneuverability and the like, and is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-photography, express transportation, disaster rescue, wild animal observation, mapping, news report, electric power inspection, disaster relief, video shooting and the like;

however, when being applied to unmanned aerial vehicle in fields such as take photo by plane, transportation, rescue, can carry the goods and materials such as camera, rescue article to unmanned aerial vehicle bottom through mounting device generally, but, current mounting device mostly all installs in unmanned aerial vehicle bottom through the bolt, still need offer in unmanned aerial vehicle's bottom and be used for bolt installation screw hole, can destroy unmanned aerial vehicle organism to, when carrying the dismouting to mounting device, the dismouting that relapse leads to the bolt easily to slide the silk in the screw hole, can't fix mounting device, has influenced mounting device's steadiness. Therefore, a person skilled in the art provides a mounting device for an unmanned aerial vehicle, so as to solve the problems set forth in the background art.

Disclosure of Invention

The utility model aims to provide a mounting device for an unmanned aerial vehicle, which aims to solve the problems in the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

a mounting device for an unmanned aerial vehicle, comprising: unmanned aerial vehicle organism and year thing frame, the bottom of unmanned aerial vehicle organism is provided with two L type mounting panels that are symmetric distribution, the intermediate position department of L type mounting panel terminal surface is provided with the slide rail, the empty slot has been seted up at the top of year thing frame, the top both ends of empty slot all are provided with the roof, two roof slidable mounting are on the slide rail in both sides respectively, and the bottom of empty slot is provided with the bottom plate, the top both ends of bottom plate all are provided with the flange, the flange is hugged closely at the lower terminal surface of roof, and the top of bottom plate is located and is provided with the recess between two flanges, the equal slidable mounting of two L type mounting panels is in the inside of recess and laminating at the lower terminal surface of roof, the top of flange is located the both sides of roof and all rotates the threaded rod, the outer wall slidable mounting of threaded rod has the clamp plate, and, the part of clamp plate extends to the up end of L type mounting panel and hugs closely in roof, one side of slide rail, the one end that is located the clamp plate top is provided with spacing section of thick bamboo, spacing section of thick bamboo suit is at the top of threaded rod and hug closely at the up end of clamp plate.

Preferably, a sliding groove is formed in the position, corresponding to the sliding rail, of the bottom of the top plate, and the top plate is slidably mounted outside the sliding rail through the sliding groove and is tightly attached to the upper end face of the L-shaped mounting plate.

Preferably, the top of the convex plate is provided with clamping grooves on two sides of the top plate, the pressing plate is clamped and installed in the clamping grooves, and the upper end face of the convex plate is flush with the upper end face of the L-shaped mounting plate.

Preferably, the through hole is formed in the pressing plate, and the pressing plate is slidably mounted on the outer wall of the threaded rod through the through hole.

Preferably, the limiting cylinder comprises a first fixed cylinder, a second fixed cylinder and an extending cylinder, the extending cylinder is arranged between the first fixed cylinder and the second fixed cylinder, a first slot and a second slot are respectively formed in one ends, close to the extending cylinder, of the first fixed cylinder and the second fixed cylinder, and two ends of the extending cylinder are respectively slidably mounted in the first slot and the second slot.

Preferably, the first thread groove and the second thread groove are respectively formed in the inner sides of the first slot and the second slot of the first fixed cylinder and the second fixed cylinder, the first fixed cylinder and the second fixed cylinder are respectively arranged on the outer wall of the threaded rod through the first thread groove and the second thread groove, and the internal thread directions of the first thread groove and the second thread groove are opposite.

Compared with the prior art, the utility model has the advantages that:

through setting up L type mounting panel and year thing frame, can be earlier through roof with year thing frame slidable mounting in the bottom of two L type mounting panels, screw limit cylinder in proper order, let the clamp plate compress tightly in the top of L type mounting panel and hug closely in roof, one side of slide rail, accomplish the installation of year thing frame, can be with L type mounting panel centre gripping between clamp plate and bottom plate and inject the position of roof, can install the thing frame in unmanned aerial vehicle's bottom under the circumstances that does not damage unmanned aerial vehicle organism, the trouble that need destroy unmanned aerial vehicle organism just can install the thing frame has been avoided appearing, also avoided the circumstances that influences year thing frame steadiness because of the bolt slides the silk in the screw hole when dismouting year thing frame takes place, simple structure, the simple operation is favorable to the going on of later stage dismouting work;

through setting up spacing section of thick bamboo, can install the position of prescribing a limit to the clamp plate at the outer wall of threaded rod with first fixed section of thick bamboo earlier through first screw thread groove, rethread second screw thread groove installs the position of prescribing a limit to first fixed section of thick bamboo with second screw thread section of thick bamboo on the threaded rod, can carry out dual spacing to the clamp plate, avoided leading to first fixed section of thick bamboo to become flexible because of unmanned aerial vehicle produces vibrations in the flight and cause the condition that carries the thing frame to rock to take place, guaranteed the steadiness that carries the thing frame to install.

Drawings

Fig. 1 is a schematic diagram of connection between a drone body and a mounting device according to an embodiment of the present utility model;

FIG. 2 is a perspective view of a carrying frame according to an embodiment of the utility model;

FIG. 3 is a schematic perspective view of an L-shaped mounting plate according to one embodiment of the utility model;

fig. 4 is a schematic diagram illustrating the detachment of the stopper rod according to an embodiment of the present utility model.

In the figure: 1. an unmanned aerial vehicle body; 11. an L-shaped mounting plate; 12. a slide rail; 2. a carrying frame; 201. a hollow groove; 21. a top plate; 211. a chute; 22. a bottom plate; 221. a groove; 23. a convex plate; 231. a clamping groove; 24. a threaded rod; 25. a pressing plate; 251. a through hole; 26. a limiting cylinder; 261. a first fixed cylinder; 2611. a first thread groove; 2612. a first slot; 262. a second fixed cylinder; 2621. a second thread groove; 2622. a second slot; 263. an extension cylinder.

Detailed Description

In the description of the present utility model, it should be understood that the terms "center," "lateral," "upper," "lower," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the utility model and simplify the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation or be constructed and operated in a particular orientation, and thus should not be construed as limiting the utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more. In addition, the term "include" and any variations thereof are intended to cover a non-exclusive inclusion.

As shown in fig. 1, 2 and 3, the unmanned aerial vehicle body 1 and the carrying frame 2 are combined, two L-shaped mounting plates 11 which are symmetrically distributed are arranged at the bottom of the unmanned aerial vehicle body 1, sliding rails 12 are arranged at the middle positions of the end faces of the L-shaped mounting plates 11, empty slots 201 are formed in the tops of the carrying frame 2, top plates 21 are arranged at two ends of the tops of the empty slots 201, sliding grooves 211 are formed in positions, corresponding to the sliding rails 12, of the bottom of the top plates 21, the top plates 21 are slidably arranged outside the sliding rails 12 through the sliding grooves 211 and are tightly attached to the upper end faces of the L-shaped mounting plates 11, a bottom plate 22 is arranged at the bottom of the empty slots 201, convex plates 23 are arranged at two ends of the top of the bottom plate 22, concave grooves 221 are formed between the two convex plates 23 at the tops of the bottom plate 22, the two L-shaped mounting plates 11 are slidably mounted in the grooves 221 and are attached to the lower end face of the top plate 21, threaded rods 24 are rotatably mounted on two sides of the top plate 21 at the top of the convex plate 23, pressing plates 25 are slidably mounted on the outer walls of the threaded rods 24, the upper end faces of the convex plate 23 are flush with the upper end faces of the L-shaped mounting plates 11, clamping grooves 231 are formed in the two sides of the top plate 21 at the tops of the convex plate 23, the pressing plates 25 are mounted in the clamping grooves 231 in a clamping mode, the pressing plates 25 extend to the upper end faces of the L-shaped mounting plates 11 and are attached to the top plate 21 and one side of the sliding rail 12 in a clinging mode, limiting cylinders 26 are arranged at one ends of the threaded rods 24 located above the pressing plates 25, and the limiting cylinders 26 are sleeved on the tops of the threaded rods 24 and are attached to the upper end faces of the pressing plates 25 in a clinging mode.

In one embodiment, when the carrying frame 2 is installed, the top plate 21 is firstly slidably installed on the slide rail 12 through the sliding groove 211, the L-shaped mounting plate 11 is slid between the top plate 21 and the bottom plate 22, then the pressing plate 25 is sequentially slid on the outer wall of the threaded rod 24 through the through hole 251, the pressing plate 25 is clamped in the clamping groove 231 and tightly pressed on the upper end face of the L-shaped mounting plate 11 and one side of the top plate 21 and the slide rail 12, finally, the limiting cylinder 26 is sequentially screwed, the limiting cylinder 26 is tightly pressed on the top of the pressing plate 25 to limit the position of the pressing plate 25, the carrying frame 2 is installed, the L-shaped mounting plate 11 can be clamped between the pressing plate 25 and the bottom plate 22 and limit the position of the top plate 21, the carrying frame 2 can be installed on the bottom of the unmanned aerial vehicle body under the condition that the unmanned aerial vehicle body 1 is not damaged, the trouble that the unmanned aerial vehicle body 1 is required to be damaged is avoided, the carrying frame 2 is also prevented from being influenced due to the fact that bolts slide in the threaded holes when the carrying frame 2 is dismounted, the structure is simple, the operation is convenient, and the carrying frame 2 is convenient to operate.

In one embodiment, after the position of the pressing plate 25 is defined, the pressing plate 25 can be clamped in the clamping groove 231 and tightly pressed on the upper end surface of the L-shaped mounting plate 11 and on one side of the top plate 21 and one side of the sliding rail 12, and the pressing plate 25 can play a limiting role on the top plate 21 while clamping the L-shaped mounting plate 11, so that the situation that the carrier frame 2 shakes at the bottom of the unmanned aerial vehicle body 1 due to the fact that the top plate 21 slides on the sliding rail 12 is avoided.

As shown in fig. 1, 2 and 4, one end of the threaded rod 24 above the pressing plate 25 is provided with a limiting cylinder 26, the limiting cylinder 26 is sleeved on the top of the threaded rod 24 and is tightly attached to the upper end surface of the pressing plate 25, the limiting cylinder 26 comprises a first fixed cylinder 261, a second fixed cylinder 262 and an extending cylinder 263, the extending cylinder 263 is arranged between the first fixed cylinder 261 and the second fixed cylinder 262, one ends of the first fixed cylinder 261 and the second fixed cylinder 262, which are close to the extending cylinder 263, are respectively provided with a first slot 2612 and a second slot 2622, two ends of the extending cylinder 263 are respectively slidably mounted in the first slot 2612 and the second slot 2622, the inner sides of the first fixed cylinder 261 and the second fixed cylinder 262 are respectively provided with a first thread groove 2611 and a second thread groove 2621, the first fixed cylinder 261 and the second fixed cylinder 262 are respectively arranged on the outer wall of the threaded rod 24 through the first thread groove 2611 and the second thread groove 2621, and the inner threads 2621 are opposite in directions.

In one embodiment, when the pressing plate 25 is installed, since the directions of the internal threads of the first thread groove 2611 and the second thread groove 2621 are opposite, the first fixing cylinder 261 is screwed by the first thread groove 2611, the first fixing cylinder 261 is tightly pressed on the upper end surface of the pressing plate 25 to limit the position of the pressing plate 25, the second fixing cylinder 262 is screwed by the second thread groove 2621, the second fixing cylinder 262 is tightly pressed on the upper side of the first fixing cylinder 261 to limit the position of the first fixing cylinder 261, double limiting can be performed on the pressing plate 25, the condition that the pressing plate 25 and the carrying frame 2 shake due to loosening of the first fixing cylinder 261 caused by vibration generated in the flight process of the unmanned aerial vehicle is avoided, and the installation stability of the carrying frame 2 is ensured.

In one embodiment, when the limiting cylinder 26 is installed, the first fixed cylinder 261 is screwed through the first thread groove 2611, the first fixed cylinder 261 is tightly pressed on the upper end surface of the pressing plate 25, the threaded rod 24 can extend into the extending cylinder 263 to be in contact with the second fixed cylinder 262, the first fixed cylinder 261 is continuously screwed, the threaded rod 24 pushes the second fixed cylinder 262 to move upwards, the extending cylinder 263 can be pulled out of the first slot 2612 and the second slot 2622, the length of the limiting cylinder 26 is prolonged, finally, the second fixed cylinder 262 is screwed through the second thread groove 2621, the second fixed cylinder 262 is tightly pressed above the first fixed cylinder 261 to limit the position of the first fixed cylinder 261, so that the installation of the limiting cylinder 26 is completed, the first fixed cylinder 261 can be limited, the situation that the first fixed cylinder 261 is loose due to the vibration produced by an unmanned aerial vehicle in the flight process is avoided, the installation firmness of the limiting cylinder 26 is guaranteed, and at the same time, the first fixed cylinder 262 can be prevented from being interfered by the second fixed cylinder 262 to rotate in the first slot 2612.

The working principle of the utility model is as follows: when the carrying frame 2 is installed, the top plate 21 is firstly slidably installed on the sliding rail 12, the L-shaped mounting plate 11 is slid between the top plate 21 and the bottom plate 22, then the pressing plates 25 are sequentially slid, the pressing plates 25 are tightly pressed on the upper end surfaces of the L-shaped mounting plate 11 and are tightly attached to the top plate 21 and one side of the sliding rail 12, finally the limiting cylinders 26 are sequentially screwed, the limiting cylinders 26 are tightly pressed on the tops of the pressing plates 25 to limit the positions of the pressing plates 25, the carrying frame 2 is installed, the L-shaped mounting plate 11 can be clamped between the pressing plates 25 and the bottom plate 22 and limit the positions of the top plate 21, the carrying frame 2 can be installed at the bottom of an unmanned aerial vehicle under the condition that the unmanned aerial vehicle body 1 is not damaged, the trouble that the unmanned aerial vehicle body 1 can be damaged to install the carrying frame 2 is avoided, the situation that the stability of the carrying frame 2 is influenced due to the fact that bolts slide in threaded holes when the carrying frame 2 is dismounted is avoided, the structure is simple, the operation is convenient, and the carrying frame 2 is favorable for later dismounting work;

when the position of the pressing plate 25 is limited, the first fixed cylinder 261 is screwed through the first thread groove 2611, the first fixed cylinder 261 is tightly pressed on the upper end face of the pressing plate 25 to limit the position of the pressing plate 25, the second fixed cylinder 262 is screwed through the second thread groove 2621, the second fixed cylinder 262 is tightly pressed on the upper side of the first fixed cylinder 261 to limit the position of the first fixed cylinder 261, double limiting can be carried out on the pressing plate 25, the condition that the pressing plate 25 and the carrying frame 2 shake due to loosening of the first fixed cylinder 261 caused by vibration generated in the flight process of the unmanned aerial vehicle is avoided, and the installation stability of the carrying frame 2 is ensured.

The foregoing description is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical solution of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.

Claims

1. A mounting device for an unmanned aerial vehicle, comprising: unmanned aerial vehicle organism (1) and year thing frame (2), a serial communication port, the bottom of unmanned aerial vehicle organism (1) is provided with two L type mounting panel (11) that are symmetrical distribution, the intermediate position department of L type mounting panel (11) terminal surface is provided with slide rail (12), empty slot (201) have been seted up at the top of year thing frame (2), the top both ends of empty slot (201) all are provided with roof (21), two roof (21) slidable mounting respectively are located on slide rail (12) of both sides, and, the bottom of empty slot (201) is provided with bottom plate (22), the top both ends of bottom plate (22) all are provided with flange (23), flange (23) are hugged closely the lower terminal surface of roof (21), just the top of bottom plate (22) is located two be provided with recess (221) between flange (23), two L type mounting panel (11) all slidable mounting are in the inside of recess (221) and laminating are in the lower terminal surface of roof (21), the bottom plate (21) is located bottom plate (22), threaded rod (23) is located the top (24) and is located the top plate (25) is located on the top plate (25) and is located the top plate (25) of extension type of top plate (24) One side of the sliding rail (12), one end of the threaded rod (24) above the pressing plate (25) is provided with a limiting cylinder (26), and the limiting cylinder (26) is sleeved at the top of the threaded rod (24) and clings to the upper end face of the pressing plate (25).

2. The mounting device for the unmanned aerial vehicle according to claim 1, wherein a sliding groove (211) is formed in a position, corresponding to the sliding rail (12), of the bottom of the top plate (21), and the top plate (21) is slidably mounted outside the sliding rail (12) through the sliding groove (211) and is tightly attached to the upper end face of the L-shaped mounting plate (11).

3. The mounting device for the unmanned aerial vehicle according to claim 1, wherein the top of the convex plate (23) is positioned at two sides of the top plate (21) and is provided with clamping grooves (231), the pressing plate (25) is clamped and mounted in the clamping grooves (231), and the upper end face of the convex plate (23) is flush with the upper end face of the L-shaped mounting plate (11).

4. The mounting device for the unmanned aerial vehicle according to claim 1, wherein a through hole (251) is formed in the pressing plate (25), and the pressing plate (25) is slidably mounted on the outer wall of the threaded rod (24) through the through hole (251).

5. The mounting device for an unmanned aerial vehicle according to claim 1, wherein the limiting cylinder (26) comprises a first fixed cylinder (261), a second fixed cylinder (262) and an extending cylinder (263), the extending cylinder (263) is arranged between the first fixed cylinder (261) and the second fixed cylinder (262), a first slot (2612) and a second slot (2622) are respectively formed in one ends, close to the extending cylinder (263), of the first fixed cylinder (261) and the second fixed cylinder (262), and two ends of the extending cylinder (263) are respectively slidably mounted in the first slot (2612) and the second slot (2622).

6. The mounting device for an unmanned aerial vehicle according to claim 5, wherein the first and second fixing barrels (261, 262) are located inside the first and second slots (2612, 2622) and have first and second screw grooves (2611, 2621) respectively formed therein, and the first and second fixing barrels (261, 262) are mounted on the outer wall of the threaded rod (24) through the first and second screw grooves (2611, 2621) respectively, and the internal screw directions of the first and second screw grooves (2611, 2621) are opposite.