CN219313393U

CN219313393U - Protection component for unmanned aerial vehicle transport case

Info

Publication number: CN219313393U
Application number: CN202320299440.6U
Authority: CN
Inventors: 任亚龙; 王红兵; 刘云洁
Original assignee: Individual
Current assignee: Individual
Priority date: 2023-02-23
Filing date: 2023-02-23
Publication date: 2023-07-07
Anticipated expiration: 2033-02-23

Abstract

The utility model discloses a protection component for an unmanned aerial vehicle transport case, which comprises a shell, wherein a clamping mechanism is arranged in the shell, the clamping mechanism comprises a storage seat arranged in the shell, the lower end of the storage seat is fixedly connected with a fixed foot, the inside of the front side and the rear side of the storage seat are respectively provided with a mounting groove, the inside of each of the two groups of the mounting grooves is movably connected with a screw rod, the middle positions of the two groups of screw rods are fixedly connected with a turbine, the inside of the storage seat is close to the lower side of the turbine and is provided with a worm, and the front end of the worm is fixedly connected with a button block. According to the protection component for the unmanned aerial vehicle transport case, the two groups of clamping plates are driven to be close to each other through the rotary button block, so that two sides of an object to be transported are clamped, the shaking of the outer shell due to wind force and inertia force in the flying process is avoided, and the object transported inside is made to shake.

Description

Protection component for unmanned aerial vehicle transport case

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle transport cases, in particular to a protection component for an unmanned aerial vehicle transport case.

Background

With the development of the times, the living standard of people is continuously improved, ^{general purpose medicine} The unmanned low-altitude aircraft which is operated by using the radio remote control equipment and the self-contained program control device carries the package and automatically arrives at the destination, and the remote control system has the advantages of mainly solving the distribution problem in remote areas, improving the distribution efficiency and reducing the labor cost. The defects are mainly that no one has the opportunity to deliver goods powerless in severe weather, and artificial damage cannot be avoided in the flying process. Meanwhile, when tasks or works are carried out outdoors, the unmanned aerial vehicle can also complete work which cannot be completed due to limited manpower, and object transportation in a crossing environment, objects and the like is realized; when carrying out transportation, current unmanned aerial vehicle transport case, direct placement in the transport case when article is mostly, for example patent number is: CN201820822616.0 is a multifunctional unmanned aerial vehicle transport case for field industry, but is affected by wind force and the inertial force of the transport case itself in the flight process, the transport case swings easily, so that the objects inside shake, the flight of the unmanned aerial vehicle is affected, and the unmanned aerial vehicle is damaged easily.

Disclosure of Invention

The utility model mainly aims to provide a protection component for an unmanned aerial vehicle transport case, which can effectively solve the problems in the background technology.

In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:

the utility model provides a protection component that unmanned aerial vehicle transport case was used, includes the shell, shell internally mounted has clamping mechanism, clamping mechanism is including setting up the inside thing seat of putting of shell, the lower extreme fixedly connected with fixed foot of putting the thing seat, the mounting groove has been seted up respectively to the inside front and back both sides of putting the thing seat, two sets of the inside equal swing joint of mounting groove has the lead screw, two sets of the equal fixedly connected with turbine of intermediate position of lead screw, the inboard of putting the thing seat is close to turbine downside position and is provided with the worm, the front end fixedly connected with button piece of worm, two sets of the both sides of lead screw respectively swing joint have movable block, movable block upper end fixedly connected with fixed block, the upper end fixedly connected with splint of fixed block, the position that the upper end of putting the thing seat is close to the fixed block has seted up two sets of movable grooves.

Preferably, the quantity of fixed foot is four groups, fixed foot and shell are fixed connection, fixed foot is located the lower extreme of putting the thing seat and is close to the corner, the outside of lead screw sets up to control two sets of spiral line respectively.

Preferably, the worm penetrates through the inside of the two groups of mounting grooves, spiral threads are arranged on the outer side of the worm close to the two groups of turbines, the worm is movably connected with the storage seat, and the worm is meshed with the two groups of turbines respectively.

Preferably, the movable blocks are respectively in threaded connection with the screw rod, the fixed blocks are matched with the movable grooves, and the clamping plate is fixedly connected with two groups of fixed blocks on one side.

Preferably, the front side swing joint of shell has the chamber door, the upper end fixedly connected with mounting of shell, the upper end fixedly connected with ring of mounting, the spread groove has been seted up to the downside of shell, the inboard swing joint of spread groove has the connecting block, fixedly connected with spring between the upside inner wall of connecting block and spread groove, the lower extreme fixedly connected with bottom plate of connecting block, the inboard position fixedly connected with cover piece that the upper end of connecting block is close to the spring, the sleeve has been cup jointed to the upside of cover piece.

Preferably, the mounting is located the upper end of shell and is close to central point, connecting block and spread groove are swing joint, the quantity of spring is a plurality of groups, the spring is the array and arranges, the bottom plate presents as an organic wholely with the connecting block, sleeve and the upside inner wall fixed connection of spread groove, the cover piece cup joints the setting for the damping with the sleeve.

Compared with the prior art, the utility model has the following beneficial effects:

1. before flying, the two groups of clamping plates are driven to be close to each other through the rotary button block, two sides of an object to be transported are clamped, the shaking of the shell, which is influenced by wind force and inertia force in the flying process, is avoided, and the object transported inside is shaking.

2. The whole body can be carried out through the circular ring, and when the whole body falls, the bottom plate can fall to the ground firstly, the connecting block fixedly connected with the upper end slides in the connecting groove, the spring is compressed, and the damping sleeve joint block and the sleeve are matched for use, so that the damping effect is achieved when the whole body falls.

Drawings

Fig. 1 is a schematic diagram of the overall structure of a protection assembly for an unmanned aerial vehicle transport case according to the present utility model;

FIG. 2 is a schematic view of a partially cut-away configuration of a protective assembly for an unmanned aerial vehicle transport pod of the present utility model;

FIG. 3 is a schematic view of a partially cut-away structure of a securing mechanism of a protective assembly for an unmanned aerial vehicle transport case of the present utility model;

fig. 4 is a schematic view of a partial structure of a fixing mechanism of a protection assembly for an unmanned aerial vehicle transport case.

In the figure: 1. a housing; 2. a door; 3. a fixing member; 4. a circular ring; 5. a connecting groove; 6. a connecting block; 7. a spring; 8. a bottom plate; 9. a clamping mechanism; 91. a storage seat; 92. a fixed foot; 93. a mounting groove; 94. a screw rod; 95. a turbine; 96. a worm; 97. a button block; 98. a movable block; 99. a fixed block; 910. a clamping plate; 911. a movable groove; 10. sleeving blocks; 11. a sleeve.

Detailed Description

The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.

As shown in fig. 1-4, a protection component for an unmanned aerial vehicle transport case comprises a housing 1, clamping mechanism 9 is installed in housing 1, clamping mechanism 9 is including setting up at the inside thing seat 91 of putting of housing 1, fixed foot 92 of lower extreme fixedly connected with of thing seat 91, the mounting groove 93 has been seted up respectively to the inside front and back both sides of putting of thing seat 91, the inside all swing joint of two sets of mounting grooves 93 has lead screw 94, the intermediate position of two sets of lead screw 94 is all fixedly connected with turbine 95, the inboard of putting of thing seat 91 is close to turbine 95 downside position and is provided with worm 96, the front end fixedly connected with button piece 97 of worm 96, the both sides of two sets of lead screw 94 are swing joint movable block 98 respectively, movable block 98 upper end fixedly connected with fixed block 99, the upper end fixedly connected with splint 910 of fixed block 99, two sets of movable grooves 911 have been seted up to the position that the upper end of putting of thing seat 91 is close to fixed block 99.

In this embodiment, the number of the fixing pins 92 is four, the fixing pins 92 are fixedly connected with the housing 1, the fixing pins 92 are located at the lower end of the storage seat 91 and near the corners, the outer sides of the screw rods 94 are respectively provided with left and right screw threads, the worm 96 penetrates through the inside of the two sets of mounting grooves 93, the outer sides of the worm 96 are respectively provided with screw threads near the positions of the two sets of turbines 95, the worm 96 is movably connected with the storage seat 91, the worm 96 is respectively meshed with the two sets of turbines 95, the movable blocks 98 are respectively in threaded connection with the screw rods 94, the fixed blocks 99 are matched with the movable grooves 911, and the clamping plates 910 are fixedly connected with the two sets of fixed blocks 99 on one side.

Specifically, through opening chamber door 2, put into the upper end of putting thing seat 91 with the article that needs to transport, rethread rotation knob piece 97, drive fixed connection's worm 96 and rotate, and the rotation of worm 96 makes two sets of turbines 95 rotate, and two sets of turbines 95 are fixed connection with two sets of lead screws 94 respectively, so make two sets of lead screws 94 rotate, and the outside of two sets of lead screws 94 is left and right sides screw thread setting, make threaded connection's two sets of movable blocks 98 draw close each other, thereby drive fixed connection's two sets of fixed blocks 99 and splint 910, move along two sets of movable groove 911 respectively, two sets of splint 910 draw close each other and press from both sides the article clamp of placing at putting thing seat 91 upper end, realize fixed connection, avoid wind-force and inertial force influence shell 1 inside article to rock in the flight, influence unmanned aerial vehicle's work.

In this embodiment, the front side swing joint of shell 1 has chamber door 2, the upper end fixedly connected with mounting 3 of shell 1, the upper end fixedly connected with ring 4 of mounting 3, spread groove 5 has been seted up to the downside of shell 1, the inboard swing joint of spread groove 5 has connecting block 6, fixedly connected with spring 7 between the upside inner wall of connecting block 6 and spread groove 5, the lower extreme fixedly connected with bottom plate 8 of connecting block 6, the inboard position that the upper end of connecting block 6 is close to spring 7 fixedly connected with cover piece 10, sleeve 11 has been cup jointed to the upside of cover piece 10, mounting 3 is located the upper end of shell 1 and is close to central point, connecting block 6 and spread groove 5 are swing joint, the quantity of spring 7 is a plurality of groups, spring 7 is the array range, bottom plate 8 presents as an organic wholely with connecting block 6, sleeve 11 and the upside inner wall fixedly connected with of spread groove 5, cover piece 10 is the damping cup joints setting with sleeve 11.

Specifically, the whole body can be carried through the circular ring 4, and when the whole body falls, the bottom plate 8 can fall to the ground first, the connecting block 6 fixedly connected with the upper end slides in the connecting groove 5, the spring 7 is compressed, and the damping sleeve block 10 and the sleeve 11 are matched for use, so that the purpose of damping is achieved when the whole body falls.

Working principle:

when the damping device is used, firstly, objects to be transported are placed at the upper end of the storage seat 91, then the rotating knob block 97 drives the worm 96 which is fixedly connected to rotate, the worm 96 rotates to enable the two groups of turbines 95 to rotate, the two groups of turbines 95 are fixedly connected with the two groups of screw rods 94 respectively, so that the two groups of screw rods 94 rotate, the outer sides of the two groups of screw rods 94 are provided with left and right threads, the two groups of movable blocks 98 which are in threaded connection are mutually closed, so that the two groups of fixed blocks 99 and the clamping plates 910 which are fixedly connected are driven to move along the two groups of movable grooves 911 respectively, the two groups of clamping plates 910 are mutually closed to clamp the objects placed at the upper end of the storage seat 91, the fixed connection is realized, the influence of wind force and inertia force on the objects in the shell 1 in a flight process is avoided, the work of an unmanned aerial vehicle is affected, the whole is supported through the circular ring 4, the whole is enabled to fall on the ground firstly, the upper end of the bottom plate 8 is fixedly connected to slide in the connecting groove 5, the spring 7 is compressed, the whole damping device is matched with the sleeve joint block 10, and the whole damping device 11 is used for damping the whole connecting block 11.

The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a protection subassembly that unmanned aerial vehicle transport case was used, includes shell (1), its characterized in that: the utility model discloses a clamping mechanism, including shell (1) internally mounted has clamping mechanism (9), clamping mechanism (9) is including setting up in the inside thing seat (91) of putting of shell (1), the lower extreme fixedly connected with fixed foot (92) of putting thing seat (91), mounting groove (93) have been seted up respectively to the inside both sides around putting thing seat (91), two sets of the inside equal swing joint of mounting groove (93) has lead screw (94), two sets of the intermediate position of lead screw (94) is all fixedly connected with turbine (95), the inboard of putting thing seat (91) is close to turbine (95) downside position and is provided with worm (96), the front end fixedly connected with button piece (97) of worm (96), two sets of both sides of lead screw (94) are swing joint movable block (98) respectively, movable block (98) upper end fixedly connected with fixed block (99), the upper end fixedly connected with splint (910) of fixed block (99), the upper end of putting thing seat (91) is close to the position of fixed block (99) and is seted up two sets of movable grooves (911).

2. The protective assembly for an unmanned aerial vehicle transport pod of claim 1, wherein: the number of the fixing feet (92) is four, the fixing feet (92) are fixedly connected with the shell (1), the fixing feet (92) are located at the lower end of the storage seat (91) and close to the corners, and the outer sides of the screw rods (94) are respectively provided with left and right spiral lines.

3. The protective assembly for an unmanned aerial vehicle transport pod of claim 1, wherein: the worm (96) penetrates through the two groups of mounting grooves (93), spiral threads are arranged on the outer side of the worm (96) close to the positions of the two groups of turbines (95), the worm (96) is movably connected with the storage seat (91), and the worm (96) is meshed with the two groups of turbines (95) respectively.

4. The protective assembly for an unmanned aerial vehicle transport pod of claim 1, wherein: the movable blocks (98) are respectively in threaded connection with the screw rods (94), the fixed blocks (99) are matched with the movable grooves (911), and the clamping plates (910) are fixedly connected with two groups of fixed blocks (99) on one side.

5. The protective assembly for an unmanned aerial vehicle transport pod of claim 1, wherein: front side swing joint of shell (1) has chamber door (2), the upper end fixedly connected with mounting (3) of shell (1), the upper end fixedly connected with ring (4) of mounting (3), spread groove (5) have been seted up to the downside of shell (1), the inboard swing joint of spread groove (5) has connecting block (6), fixedly connected with spring (7) between the upside inner wall of connecting block (6) and spread groove (5), the lower extreme fixedly connected with bottom plate (8) of connecting block (6), the inboard position fixedly connected with cover piece (10) that the upper end of connecting block (6) is close to spring (7), sleeve (11) have been cup jointed to the upside of cover piece (10).

6. The protective assembly for an unmanned aerial vehicle transport pod of claim 5, wherein: the fixing piece (3) is located at the upper end of the shell (1) and is close to the center, the connecting blocks (6) are movably connected with the connecting grooves (5), the springs (7) are arranged in a plurality of groups, the springs (7) are arranged in a matrix mode, the bottom plate (8) and the connecting blocks (6) are integrally formed, the sleeve (11) is fixedly connected with the upper inner wall of the connecting grooves (5), and the sleeve block (10) is sleeved with the sleeve (11) in a damping mode.