CN217227926U

CN217227926U - Equipment mounting structure for unmanned aerial vehicle

Info

Publication number: CN217227926U
Application number: CN202220439387.0U
Authority: CN
Inventors: 邹静; 杨巍; 时迪; 赵宏锁; 高智慧; 张朋浩; 奚晶瑾
Original assignee: Pla 66389
Current assignee: Pla 66389
Priority date: 2022-03-02
Filing date: 2022-03-02
Publication date: 2022-08-19
Anticipated expiration: 2032-03-02

Abstract

The utility model discloses an equipment carry structure for unmanned aerial vehicle belongs to unmanned aerial vehicle carry device technical field, include the connecting box and set up in the storing box of connecting box below, rotate through the bearing in the connecting box and be connected with the regulating spindle, two sets of thread grooves that move towards opposite are seted up to the outer wall of regulating spindle, and the equal threaded connection outside two sets of thread grooves of regulating spindle outer wall has the regulating block, the bottom fixedly connected with connecting rod of regulating block, spacing spout has all been seted up to the both sides outer wall of storing box, and sliding connection has spacing slider, two in the spacing spout of storing box spacing slider is located the outside terminal surface of storing box and all rotates through the pivot and be connected with the bracing piece, the first one of bracing piece also rotates through pivot and connecting rod to be connected, and the interior symmetry of storing box is equipped with two limiting plates. This equipment carry structure for unmanned aerial vehicle not only can adjust according to the size of article, conveniently fixes article moreover.

Description

Equipment mounting structure for unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle carry device, concretely relates to equipment carry structure for unmanned aerial vehicle.

Background

An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles tend to be more suitable for tasks that are more "dirty or dangerous" than manned aircraft. At present, the application in the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like greatly expands the application of the unmanned aerial vehicle

The mount is all installed to most unmanned aerial vehicle's bottom, and the structure of current unmanned aerial vehicle mount is comparatively fixed, when transporting the article of different volumes, will receive the restriction of different mount article volumes to inconvenience when having leaded to the use, and then influenced the result of use.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an equipment carry structure for unmanned aerial vehicle to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an equipment carry structure for unmanned aerial vehicle, includes the connecting box and sets up in the storing box of connecting box below, rotate through the bearing in the connecting box and be connected with the regulating spindle, two sets of opposite thread grooves of trend are seted up to the outer wall of regulating spindle, and the equal threaded connection outside two sets of thread grooves of regulating spindle outer wall has the regulating block, the bottom fixedly connected with connecting rod of regulating block, spacing spout has all been seted up to the both sides outer wall of storing box, and sliding connection has spacing slider, two in the spacing spout of storing box the terminal surface that spacing slider is located the storing box outside all rotates through the pivot and is connected with the bracing piece, the first one of bracing piece also rotates through pivot and connecting rod to be connected, and the symmetry is equipped with two limiting plates in the storing box.

In a further embodiment, the storage box is rotatably connected with a connecting shaft through a bearing, two groups of thread grooves with opposite directions are symmetrically formed in the outer wall of the connecting shaft, and the limiting plate is in threaded connection with the connecting shaft.

In a further embodiment, two supporting blocks are symmetrically installed at the bottom of the storage box, and supporting sleeves are connected to the outer portions of the two supporting blocks in a sliding mode.

In a further embodiment, a connecting column is fixedly connected in the supporting sleeve, two sliding blocks are slidably connected to the outer portion of the connecting column, and a buffer spring is fixedly connected between the two sliding blocks.

In a further embodiment, a first connecting seat is fixedly connected to the surface of the sliding block, a fixing rod is rotatably connected to the first connecting seat, and a second connecting seat is rotatably connected to the upper half portion of the fixing rod.

In a further embodiment, the inner walls of the two sides of the supporting sleeve are provided with limiting grooves, and the outer walls of the two sides of the supporting block are fixedly connected with limiting blocks which slide in the limiting grooves of the supporting sleeve.

The utility model discloses a technological effect and advantage:

according to the equipment mounting structure for the unmanned aerial vehicle, the adjusting shaft is rotated to drive the adjusting block and the connecting rods to move, so that the two ends of the two connecting rods are driven to move oppositely or oppositely, the distance between the connecting box and the storage box can be adjusted according to the volume of a loaded article, and the equipment mounting structure is more flexible to use; the distance between the two limiting plates can be adjusted by rotating the connecting shaft, the two limiting plates are attached to the two sides of the article, the article can be fixed, and accidents caused by article shaking when the unmanned aerial vehicle flies are avoided; through supporting the setting of parts such as cover cooperation buffer spring and supporting shoe, can be when unmanned aerial vehicle descends, through supporting shoe extrusion dead lever, promote the sliding block and remove to stretch buffer spring, absorb the produced impact force of unmanned aerial vehicle descending, guarantee the stability of unmanned aerial vehicle descending, this unmanned aerial vehicle equipment carry structure not only can be adjusted according to the size of article, and the convenience is fixed article moreover.

Drawings

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

FIG. 2 is a cross-sectional view of the connecting box and the storage box of the present invention;

fig. 3 is an enlarged view of a portion a of fig. 1 according to the present invention;

fig. 4 is a sectional view of the support sleeve and the support block of the present invention.

In the figure: 1. a connecting box; 11. an adjustment shaft; 12. an adjusting block; 13. a connecting rod; 2. a storage box; 21. a connecting shaft; 22. a limiting plate; 23. a limiting slide block; 24. a support bar; 3. a support sleeve; 31. connecting columns; 32. a slider; 33. a buffer spring; 34. fixing the rod; 35. and (7) a supporting block.

Detailed Description

In the following description, numerous specific details are set forth in order to provide a more thorough understanding of the present invention. It will be apparent, however, to one skilled in the art, that the present invention may be practiced without one or more of these specific details. In other instances, well-known features have not been described in order to avoid obscuring the present invention.

In order to adjust according to the size of an article and conveniently fix the article, as shown in fig. 1, fig. 2 and fig. 3, a plurality of through holes are symmetrically formed in an adjusting box, the adjusting box is conveniently connected with an unmanned aerial vehicle through bolt matching through holes, an adjusting shaft 11 is rotatably connected in a connecting box 1 through a bearing, one end of the adjusting shaft 11 extends out of the connecting box 1, an adjusting ring is fixedly connected to the end surface of the adjusting shaft 11, which is positioned outside the connecting box 1, two groups of thread grooves with opposite directions are formed in the outer wall of the adjusting shaft 11, adjusting blocks 12 are respectively in threaded connection with the two groups of thread grooves in the outer wall of the adjusting shaft 11, a moving groove for the adjusting blocks 12 to move is formed in the bottom of the adjusting box, and a connecting rod 13 is fixedly connected to the bottom of the adjusting blocks 12;

the lower part of the adjusting box is provided with a storage box 2, the outer walls of two sides of the storage box 2 are respectively provided with a limiting sliding groove, the limiting sliding grooves of the storage box 2 are connected with a limiting sliding block 23 in a sliding way, the end surfaces of the two limiting sliding blocks 23 positioned outside the storage box 2 are respectively connected with a supporting rod 24 in a rotating way through a rotating shaft, the upper half part of the supporting rod 24 is also connected with a connecting rod 13 in a rotating way through a rotating shaft, the two supporting rods 24 are also connected in a rotating way through a rotating shaft, the inside of the storage box 2 is rotatably connected with a connecting shaft 21 through a bearing, the connecting shaft 21 is positioned at the rear half part of the storage box 2 to facilitate the storage of the storage box 2, one end of the adjusting shaft 11 extends out of the storage box 2, the end surface of the adjusting shaft 11 positioned outside the storage box 2 is fixedly connected with a turntable, the outer wall of the connecting shaft 21 is symmetrically provided with two groups of thread grooves with opposite directions, and the two groups of outer walls of the adjusting shaft 11 are both connected with a limiting plate 22 in a threaded manner, rotate connecting axle 21 through the carousel, adjust the distance between two limiting plates 22, make two limiting plates 22 laminating in the both sides of article, can fix article.

In order to absorb the impact force generated by the landing of the unmanned aerial vehicle when the unmanned aerial vehicle lands, ensure the landing stability of the unmanned aerial vehicle, as shown in fig. 1 and 4, two supporting blocks 35 are symmetrically installed at the bottom of the storage box 2, a supporting sleeve 3 is slidably connected to the outer portions of the two supporting blocks 35, a connecting column 31 is fixedly connected to the inside of the supporting sleeve 3, two sliding blocks 32 are slidably connected to the outside of the connecting column 31, a buffer spring 33 is fixedly connected between the two sliding blocks 32, a first connecting seat is fixedly connected to the surface of the sliding block 32, a fixing rod 34 is rotatably connected to the first connecting seat, a second connecting seat fixedly connected to the supporting blocks 35 is rotatably connected to the upper half portion of the fixing rod 34, limiting grooves are formed in the inner walls of the two sides of the supporting sleeve 3, and the outer walls of the two sides of the supporting block 35 are fixedly connected with limiting blocks which slide in the limiting grooves of the supporting sleeve 3, so that the supporting block 35 is prevented from slipping out of the supporting sleeve 3.

The working principle is as follows:

when the unmanned aerial vehicle equipment mounting structure is used, the adjusting box is connected with the unmanned aerial vehicle through the through holes in the bolt matching connecting box 1, the adjusting shaft 11 is rotated through the adjusting ring, the adjusting block 12 and the connecting rod 13 are driven to move, so that two ends of the two connecting rods 13 are driven to move in the opposite direction or opposite directions, the distance between the connecting box 1 and the storage box 2 is adjusted according to the volume of a carried article, after the distance of the storage box 2 is adjusted, the article is placed between the two limiting plates 22, the connecting shaft 21 is rotated through the turntable, the distance between the two limiting plates 22 is adjusted, the two limiting plates 22 are attached to two sides of the article, the article is fixed, and the problem that the article shakes when the unmanned aerial vehicle flies is avoided;

when unmanned aerial vehicle descends, support cover 3 upwards slides in the outside of supporting shoe 35, and supporting shoe 35 extrudees dead lever 34, promotes sliding block 32 and removes to stretch buffer spring 33, buffer spring 33 deformation absorbs the produced impact force of unmanned aerial vehicle descending, guarantees the descending stability of unmanned aerial vehicle.

Finally, it should be noted that: the foregoing is merely a preferred embodiment of the present invention and is not intended to limit the scope of the invention.

Claims

1. The utility model provides an equipment carry structure for unmanned aerial vehicle, includes connecting box (1) and sets up in storing box (2) of connecting box (1) below, its characterized in that: rotate through the bearing in connecting box (1) and be connected with regulating spindle (11), two sets of screw thread grooves that move towards opposite are seted up to the outer wall of regulating spindle (11), and the equal threaded connection outside two sets of screw thread grooves of regulating spindle (11) outer wall has regulating block (12), the bottom fixedly connected with connecting rod (13) of regulating block (12), spacing spout has all been seted up to the both sides outer wall of storing box (2), and sliding connection has spacing slider (23), two in the spacing spout of storing box (2) spacing slider (23) are located the outside terminal surface of storing box (2) and all rotate through the pivot and are connected with bracing piece (24), the first half of bracing piece (24) also rotates through pivot and connecting rod (13) to be connected, and storing box (2) interior symmetry is equipped with two limiting plates (22).

2. The device mounting structure for the unmanned aerial vehicle according to claim 1, characterized in that: the storage box is characterized in that a connecting shaft (21) is rotatably connected into the storage box (2) through a bearing, two sets of thread grooves with opposite trends are symmetrically formed in the outer wall of the connecting shaft (21), and a limiting plate (22) is in threaded connection with the connecting shaft (21).

3. The apparatus mounting structure for an unmanned aerial vehicle according to claim 2, characterized in that: two supporting blocks (35) are symmetrically installed at the bottom of the storage box (2), and the outer parts of the two supporting blocks (35) are connected with supporting sleeves (3) in a sliding mode.

4. The apparatus mounting structure for an unmanned aerial vehicle according to claim 3, characterized in that: support cover (3) internal fixedly connected with spliced pole (31), the outside sliding connection of spliced pole (31) has two sliding blocks (32), two fixedly connected with buffer spring (33) between sliding block (32).

5. The apparatus mounting structure for an unmanned aerial vehicle according to claim 4, wherein: the surface of the sliding block (32) is fixedly connected with a first connecting seat, a fixing rod (34) is rotatably connected in the first connecting seat, and the upper half part of the fixing rod (34) is rotatably connected with a second connecting seat.

6. The device mounting structure for the unmanned aerial vehicle according to claim 3, wherein: the inner walls of the two sides of the supporting sleeve (3) are provided with limiting grooves, and the outer walls of the two sides of the supporting block (35) are fixedly connected with limiting blocks which slide in the limiting grooves of the supporting sleeve (3).