CN220662879U

CN220662879U - Camera holder for aircraft

Info

Publication number: CN220662879U
Application number: CN202322438735.XU
Authority: CN
Inventors: 洪永霖; 冯逸华; 许丽清; 宋玮
Original assignee: Guangdong University of Technology
Current assignee: Guangdong University of Technology
Priority date: 2023-09-07
Filing date: 2023-09-07
Publication date: 2024-03-26
Anticipated expiration: 2033-09-07

Abstract

The utility model discloses a camera holder for an aircraft, which relates to the technical field of aerial photography aircraft and comprises an aircraft, two clamping assemblies, two auxiliary assemblies, an energy supply assembly, a support assembly, a camera assembly and a plug pin assembly, wherein a connecting block is fixedly arranged at the bottom of the aircraft, the plug pin assembly is arranged between the connecting block and the camera assembly, and the clamping assemblies are arranged at two sides of the interior of the connecting block and are positioned at two sides of the plug pin assembly. This a camera cloud platform for aircraft, through setting up the bolt subassembly, make things convenient for the aircraft to dismantle and assemble the subassembly of making a video recording of connecting block bottom, further convenient the maintenance of changing of the camera in the subassembly of making a video recording, through setting up joint subassembly to cooperate auxiliary assembly, the enhancement aircraft is dismantled and is assembled the subassembly of making a video recording of connecting block bottom, improves the efficiency of changing the maintenance to the camera, further improves work efficiency.

Description

Camera holder for aircraft

Technical Field

The utility model belongs to the technical field of aerial photography aircrafts, and particularly relates to a camera holder for an aircraft.

Background

The four-axis aircraft is also called four-rotor aircraft, four-rotor helicopter for short, the four-axis aircraft is a multi-rotor aircraft, four propellers of the four-axis aircraft are all simple mechanisms with motors directly connected, the cross-shaped layout allows the aircraft to obtain the force of rotating a fuselage by changing the rotation speed of the motors so as to adjust the posture of the aircraft, and the camera cradle head is an installation platform formed by two alternating current or direct current motors, can move horizontally and vertically, and needs to install the camera cradle head on the aircraft due to certain special work requirements, so that pictures can be captured more conveniently.

The utility model with the authority of publication number CN 203461140U provides an unmanned aerial vehicle, and the protection rights: the device comprises a cabin and a cradle head arranged at the front end of the cabin, wherein a first rotating shaft extending forwards and backwards is arranged at the rear end of the cradle head, and the cradle head is rotationally connected with the cabin through the first rotating shaft. The cradle head is positioned in front of the engine room and is positioned on the same horizontal plane with the unmanned aerial vehicle, so that the requirements of all-angle and all-dimensional shooting are met. The cradle head can rotate around the first rotating shaft for 360 degrees relative to the aircraft body, the fixed plate for supporting the camera shooting equipment rotates around the second rotating shaft for 360 degrees relative to the cradle head, and by utilizing the structure, the cradle head can be kept horizontally stable no matter how the aircraft rotates, tilts and overturns, and the quality of a film is high.

However, in the above patent, in this device, although the camera on the pan-tilt can be kept horizontally stable, the camera on the pan-tilt cannot be quickly assembled and disassembled, so that a new camera cannot be quickly replaced in time, and only the camera on the aircraft can be continuously maintained, so that the working efficiency is reduced, and the practicability of the device is further reduced.

Disclosure of Invention

The present utility model is directed to a camera pan-tilt for an aircraft, which solves the above-mentioned problems of the prior art.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a camera cloud platform for aircraft, includes aircraft, two joint subassemblies, two auxiliary assembly, energy supply subassembly, supporting component, subassembly and bolt subassembly make a video recording, the bottom fixed mounting of aircraft has the connecting block, the bolt subassembly sets up between connecting block and the subassembly of making a video recording, the joint subassembly sets up in the inside both sides of connecting block and is located the both sides of bolt subassembly, auxiliary assembly all sets up in the both sides of joint subassembly, energy supply subassembly sets up in the both sides of subassembly of making a video recording, the supporting component sets up in the four corners of aircraft bottom and is located the outside of connecting block;

the clamping assembly comprises two first sliding grooves, two first sliding blocks and four springs, wherein the first sliding grooves are formed in two sides of the inside of the connecting block, the first sliding blocks are connected in the first sliding grooves in a sliding mode, and the springs are fixedly connected between the first sliding blocks and the inner walls of the first sliding grooves.

Preferably, the camera shooting assembly comprises a cradle head and a camera, wherein the cradle head is arranged at the bottom of the connecting block, and the camera is fixedly arranged at the bottom of the cradle head.

Preferably, the latch component comprises a slot and a plug rod, the slots are formed in the bottom of the connecting block, the plug rod is fixedly mounted at the top of the cradle head, and the plug rod is inserted into the corresponding slots.

Preferably, the clamping assembly further comprises two clamping blocks, two clamping grooves, two first sliding rods and two pull handles, wherein the clamping blocks are fixedly installed on one side, away from the first sliding rods, of the first sliding rods, the clamping grooves are formed in the outer sides of the inserting rods, the clamping blocks penetrate through the inner walls of the connecting blocks and extend to the inner parts of the clamping grooves, the first sliding rods are fixedly installed on one sides, away from the clamping blocks, of the first sliding rods and located between the two springs, one ends, away from the first sliding rods, of the first sliding rods are fixedly installed on the outer sides of the connecting blocks, and the pull handles are fixedly installed on one ends of the first sliding rods and located on the outer sides of the connecting blocks.

Preferably, the auxiliary assembly comprises two second sliding grooves, two second sliding rods and two second sliding blocks, wherein the second sliding grooves are formed in two sides of the first sliding groove, the second sliding grooves are communicated with the first sliding groove, the second sliding rods are fixedly arranged in the second sliding grooves, the second sliding blocks are slidably connected to the outer sides of the second sliding rods, and one sides of the second sliding blocks are fixedly connected with two sides of the first sliding blocks.

Preferably, the energy supply assembly comprises two storage batteries and photovoltaic panels, wherein the storage batteries are fixedly arranged on two sides of the bottom end of the cradle head, the photovoltaic panels are fixedly arranged on the top of the aircraft, and the photovoltaic panels are electrically connected with the storage batteries.

Preferably, the support assembly comprises four connecting rods and four supporting rods, wherein the connecting rods are fixedly installed at four corners of the bottom of the aircraft, and the supporting rods are fixedly installed at the bottom ends of the connecting rods.

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

(1) This equipment, through setting up the bolt subassembly, make things convenient for the aircraft to dismantle and assemble the subassembly of making a video recording of connecting block bottom, further convenient the maintenance of changing of the camera in the subassembly of making a video recording, through setting up joint subassembly to cooperate auxiliary assembly, the improvement aircraft is dismantled and is assembled the subassembly of making a video recording of connecting block bottom, improves the efficiency of changing the maintenance to the camera, further improves work efficiency.

(2) This equipment, through setting up energy supply subassembly, turn into the electric energy with light energy, conveniently energy supply to the camera, through setting up supporting component, can place the aircraft steadily, also support the protection to the camera simultaneously, increase equipment's practicality.

Drawings

FIG. 1 is a schematic perspective view of the present utility model;

FIG. 2 is a schematic view of a front view, partially in section, of the present utility model;

FIG. 3 is an enlarged view of the structure of FIG. 2A in accordance with the present utility model;

fig. 4 is an enlarged view of the structure at B in fig. 2 according to the present utility model.

In the figure: 1. an aircraft; 2. a connecting block; 3. a cradle head; 4. a camera; 5. a slot; 6. a rod; 7. a first chute; 8. a first slider; 9. a clamping block; 10. a clamping groove; 11. a first slide bar; 12. a spring; 13. a pull handle; 14. a second chute; 15. a second slide bar; 16. a second slider; 17. a connecting rod; 18. a support rod; 19. a storage battery; 20. a photovoltaic panel.

Detailed Description

Referring to fig. 1-4, the utility model provides a camera holder for an aircraft, which comprises an aircraft 1, two clamping components, two auxiliary components, an energy supply component, a supporting component, a camera shooting component and a plug pin component, wherein a connecting block 2 is fixedly arranged at the bottom of the aircraft 1, the plug pin component is arranged between the connecting block 2 and the camera shooting component, the clamping components are arranged at two sides of the inside of the connecting block 2 and are positioned at two sides of the plug pin component, the auxiliary components are arranged at two sides of the clamping components, the energy supply component is arranged at two sides of the camera shooting component, and the supporting component is arranged at four corners of the bottom of the aircraft 1 and is positioned at the outer side of the connecting block 2.

In this embodiment, through setting up the bolt subassembly, make things convenient for aircraft 1 to dismantle and assemble the subassembly of making a video recording of connecting block 2 bottom, further make things convenient for changing the maintenance to camera 4 in the subassembly of making a video recording, through setting up joint subassembly, and cooperate auxiliary assembly, the subassembly of making a video recording of reinforcing aircraft 1 to connecting block 2 bottom is dismantled and is assembled, improve the efficiency of changing the maintenance to camera 4, further improve work efficiency, through setting up energy supply subassembly, convert light energy into the electric energy, conveniently energy supply to camera 4, through setting up supporting component, can place aircraft 1 steadily, also support the protection to camera 4 simultaneously, the practicality of increase equipment is favorable to actual application and operation.

In this embodiment, preferably, the bolt subassembly includes slot 5 and inserted bar 6, and slot 5 all sets up in the bottom of connecting block 2, and the equal fixed mounting of inserted bar 6 is at the top of cloud platform 3, and inside the inserted bar 6 all inserts the slot 5 that corresponds with it, the inside of inserting slot 5 that the inserted bar 6 at the top of cloud platform 3 all corresponds, conveniently changes the maintenance to the camera 4 in the subassembly of making a video recording.

In this embodiment, preferably, the joint subassembly includes two first spouts 7, two first sliders 8, four springs 12, two fixture blocks 9, two draw-in grooves 10, two first slide bars 11 and two pull handles 13, the both sides inside connecting block 2 are all offered to first spout 7, the equal sliding connection of first slider 8 is in the inside of first spout 7, two equal fixed connection of springs 12 is between the inner wall of first slider 8 and first spout 7, the one side of first slide bar 11 is kept away from at first slider 8 to fixture block 9 equal fixed mounting, the outside at inserted bar 6 is all offered to the draw-in groove 10, fixture block 9 all passes the inner wall of connecting block 2 and extends to the inside of draw-in groove 10, the equal fixed mounting of first slide bar 11 is kept away from one side of fixture block 9 and is located between two springs 12, the one end that first slide bar 8 was kept away from to connecting block 2 all, the one end that pull handle 13 equal fixed mounting was located first slide bar 11 is in the outside of connecting block 2, through pulling pull handles 13, thereby drive first slide bar 11 and slide bar 11 carries out sliding, and then drive the inside of first slider 8 and carry out the inside of jack block 7 when the inside of jack block 9 is kept away from to the inside 5, the inside of jack 9 is realized, the inside the jack-up device is moved to the inside of jack-up 5 is moved to the jack-up to the inside 5, the jack-up device is moved to the jack-up inside 5, the jack 9 is moved to the inside is moved to the jack-up, the jack-up device is moved to the inside 5, the jack-up from the inside jack 9 is moved, and the jack-up device is moved to be moved to the inside 5, and the jack-up is moved to be moved to the jack-jack 9 is moved to be moved to the inside, and is moved.

In this embodiment, preferably, the auxiliary assembly includes two second sliding grooves 14, two second sliding bars 15 and two second sliding blocks 16, the second sliding grooves 14 are all opened at two sides of the first sliding groove 7, the second sliding grooves 14 are communicated with the first sliding groove 7, the second sliding bars 15 are all fixedly installed in the second sliding grooves 14, the second sliding blocks 16 are all slidingly connected at the outer sides of the second sliding bars 15, one sides of the second sliding blocks 16 are all fixedly connected with two sides of the first sliding blocks 8, and the second sliding blocks 16 are driven to slide on the second sliding bars 15 in the second sliding grooves 14 through the sliding of the first sliding blocks 8, so as to realize an auxiliary sliding effect.

In this embodiment, preferably, the subassembly of making a video recording includes cloud platform 3 and camera 4, and cloud platform 3 sets up in the bottom of connecting block 2, and camera 4 fixed mounting is in the bottom of cloud platform 3, through the camera 4 of drive cloud platform 3 bottom, conveniently carries out the picture to the external world and catches.

In this embodiment, preferably, the energy supply assembly includes two batteries 19 and a photovoltaic panel 20, the batteries 19 are all fixedly installed on two sides of the bottom end of the cradle head 3, the photovoltaic panel 20 is fixedly installed on the top of the aircraft 1, the photovoltaic panel 20 is electrically connected with the batteries 19, and sunlight is converted into electric energy by utilizing the photovoltaic panel 20, so that the power supply effect for the camera 4 is achieved.

In this embodiment, preferably, the supporting component includes four connecting rods 17 and four bracing pieces 18, and the equal fixed mounting of connecting rod 17 is in the four corners of aircraft 1 bottom, and the equal fixed mounting of bracing piece 18 is in the bottom of connecting rod 17, through setting up the bracing piece 18 of connecting rod 17 bottom, can place aircraft 1 steadily, also support the protection to camera 4 simultaneously, extension camera 4's life.

The working principle and the using flow of the utility model are as follows: when equipment is required to be used, pull handle 13 is pulled, thereby drive first slide bar 11 and slide, and then drive first slider 8 and slide in the inside of first spout 7, drive the inside of the first spout 7 of fixture block 9 follow slot 5 of internal withdrawal simultaneously, insert the inside of slot 5 with the equal correspondence of inserted link 6 at cloud platform 3 top, loosen pull handle 13 again, and cooperate spring 12, drive the inside that fixture block 9 on first slider 8 extends to draw-in groove 10 from the inside of first spout 7, simultaneously slide through first slider 8, drive second slider 16 and slide on the inside second slide bar 15 of second spout 14, realize that reinforcing aircraft 1 is dismantled and is assembled to the subassembly of taking a photograph of connecting block 2 bottom, improve the efficiency of changing the maintenance to camera 4, further improve work efficiency, fly through starting external control panel drive aircraft 1, also drive camera 4 simultaneously, take a photograph the capture to the picture, the internet terminal, the confession staff looks over, when the electric quantity is not enough, with the photovoltaic board 20 at aircraft 1 top, power supply efficiency is improved, the efficiency of carrying out power supply with the camera 4, practical operation is good for practical, practical operation, the practicality is improved.

Claims

1. A camera cloud platform for aircraft, including aircraft (1), two joint subassemblies, two auxiliary assembly, energy supply subassembly, supporting component, subassembly and bolt subassembly make a video recording, its characterized in that: the bottom of the aircraft (1) is fixedly provided with a connecting block (2), the bolt assembly is arranged between the connecting block (2) and the camera shooting assembly, the clamping assembly is arranged on two sides of the inside of the connecting block (2) and is positioned on two sides of the bolt assembly, the auxiliary assemblies are arranged on two sides of the clamping assembly, the energy supply assembly is arranged on two sides of the camera shooting assembly, and the supporting assemblies are arranged at four corners of the bottom of the aircraft (1) and are positioned on the outer sides of the connecting block (2);

the clamping assembly comprises two first sliding grooves (7), two first sliding blocks (8) and four springs (12), wherein the first sliding grooves (7) are formed in two sides of the inside of the connecting block (2), the first sliding blocks (8) are connected in a sliding mode inside the first sliding grooves (7), and the springs (12) are fixedly connected between the first sliding blocks (8) and the inner walls of the first sliding grooves (7).

2. A camera head for an aircraft according to claim 1, wherein: the camera shooting assembly comprises a cradle head (3) and a camera (4), wherein the cradle head (3) is arranged at the bottom of the connecting block (2), and the camera (4) is fixedly arranged at the bottom of the cradle head (3).

3. A camera head for an aircraft according to claim 2, wherein: the plug pin assembly comprises a slot (5) and a plug rod (6), wherein the slot (5) is formed in the bottom of the connecting block (2), the plug rod (6) is fixedly mounted at the top of the cradle head (3), and the plug rod (6) is inserted into the corresponding slot (5).

4. A camera head for an aircraft according to claim 3, wherein: the clamping assembly further comprises two clamping blocks (9), two clamping grooves (10), two first sliding rods (11) and two pull handles (13), wherein the clamping blocks (9) are fixedly installed on one side, far away from the first sliding rods (11), of the first sliding blocks (8), the clamping grooves (10) are formed in the outer side of the inserting rod (6), the clamping blocks (9) penetrate through the inner wall of the connecting block (2) and extend to the inner side of the clamping grooves (10), the first sliding rods (11) are fixedly installed on one side, far away from the clamping blocks (9), of the first sliding blocks (8) and located between the two springs (12), one ends, far away from the first sliding blocks (8), of the first sliding rods (11) are fixedly installed on one ends of the first sliding rods (11) and located on the outer side of the connecting block (2).

5. A camera head for an aircraft according to claim 4, wherein: the auxiliary assembly comprises two second sliding grooves (14), two second sliding rods (15) and two second sliding blocks (16), wherein the second sliding grooves (14) are formed in two sides of the first sliding groove (7), the second sliding grooves (14) are communicated with the first sliding groove (7), the second sliding rods (15) are fixedly arranged in the second sliding grooves (14), the second sliding blocks (16) are connected to the outer sides of the second sliding rods (15) in a sliding mode, and one sides of the second sliding blocks (16) are fixedly connected with two sides of the first sliding blocks (8).

6. A camera head for an aircraft according to claim 2, wherein: the energy supply assembly comprises two storage batteries (19) and a photovoltaic panel (20), wherein the storage batteries (19) are fixedly arranged on two sides of the bottom end of the cradle head (3), the photovoltaic panel (20) is fixedly arranged on the top of the aircraft (1), and the photovoltaic panel (20) is electrically connected with the storage batteries (19).

7. A camera head for an aircraft according to claim 1, wherein: the support assembly comprises four connecting rods (17) and four supporting rods (18), the connecting rods (17) are fixedly arranged at four corners of the bottom of the aircraft (1), and the supporting rods (18) are fixedly arranged at the bottom ends of the connecting rods (17).