CN218929842U - Protection frame for unmanned aerial vehicle for collecting remote sensing big data - Google Patents

Protection frame for unmanned aerial vehicle for collecting remote sensing big data Download PDF

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CN218929842U
CN218929842U CN202320207279.5U CN202320207279U CN218929842U CN 218929842 U CN218929842 U CN 218929842U CN 202320207279 U CN202320207279 U CN 202320207279U CN 218929842 U CN218929842 U CN 218929842U
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connecting rod
unmanned aerial
aerial vehicle
ring
semi
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赵民鑫
满旺
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Xiamen University of Technology
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Xiamen University of Technology
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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Abstract

The utility model discloses a protection frame for an unmanned aerial vehicle for collecting remote sensing big data, relates to the technical field of protection frames for unmanned aerial vehicles, and aims to solve the problems that the existing protection frame for the unmanned aerial vehicle only can protect a wing structure and can not protect an aerial camera structure in the installation and use process, and when a camera is impacted, the unprotected structure is easy to damage, so that the service life of the aerial camera is influenced. The wing sleeving ring seat is internally provided with four mounting connecting holes, and the mounting connecting holes and the wing sleeving ring seat are integrally formed; further comprises: the connecting rods are arranged on the outer wall of the wing sleeve ring seat, two connecting rods are arranged, four wing sleeve ring seats are arranged, bearing inner cavities are formed in the connecting rods, the bearing inner cavities and the connecting rods are integrally formed, and horizontal connecting rods are arranged in two adjacent bearing inner cavities; the vertical connecting rod is arranged on one side of the connecting rod, the vertical connecting rod and the connecting rod are integrally formed, and the lower end of the vertical connecting rod is provided with a sleeved column.

Description

Protection frame for unmanned aerial vehicle for collecting remote sensing big data
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle protection frames, in particular to a protection frame for an unmanned aerial vehicle for remote sensing big data collection.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using radio remote control equipment and a self-provided program control device, or is operated completely or intermittently and autonomously by a vehicle-mounted computer, the unmanned aerial vehicle for collecting the remote sensing big data is an unmanned aerial vehicle for performing aerial photography by using a remote sensing big data collecting technology, and a protection frame is required to be installed for protecting the body structure of the unmanned aerial vehicle in the flying process.
For example, bulletin numbers: CN208119419U (named as a fender bracket for environmental monitoring unmanned aerial vehicle), which comprises a bod, the organism outside is equipped with the wing, the organism outer wall is equipped with the go-between, the go-between outside is equipped with the safety cover body, be equipped with the connecting rod between safety cover body and the organism, connecting rod and safety cover body junction are equipped with spacing, be equipped with spacing cavity between spacing and the safety cover body, spacing cavity inside is equipped with the mount, be equipped with reset spring between mount and the spacing, be equipped with the gyro wheel on the mount, the inside protective washer that is equipped with of gyro wheel, the inside fixed slot that is equipped with of safety cover body, the safety cover body bottom is equipped with the deformation callus on the sole, deformation callus on the sole is equipped with the fixed tooth with the fixed slot junction.
Above-mentioned unmanned aerial vehicle protection frame can only protect wing structure at the in-process of installation use, can't protect the camera structure of taking photo by plane, when the camera receives the striking, because no protection structure appears damaging easily, leads to influencing the life of taking photo by plane the camera, and for this reason, we provide a protection frame for unmanned aerial vehicle of remote sensing big data collection.
Disclosure of Invention
The utility model aims to provide a protection frame for an unmanned aerial vehicle for collecting remote sensing big data, which aims to solve the problems that the existing protection frame for the unmanned aerial vehicle provided in the background art only can protect a wing structure and can not protect an aerial camera structure in the installation and use process, and when a camera is impacted, the unprotected structure is easy to damage, so that the service life of the aerial camera is influenced.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the protection frame for the unmanned aerial vehicle for collecting the remote sensing big data comprises a wing sleeve ring seat and a bottom support plate, wherein four mounting connection holes are formed in the wing sleeve ring seat, and the mounting connection holes and the wing sleeve ring seat are integrally formed;
further comprises:
the connecting rods are arranged on the outer wall of the wing sleeve ring seat, two connecting rods are arranged, four wing sleeve ring seats are arranged, bearing inner cavities are formed in the connecting rods, the bearing inner cavities and the connecting rods are integrally formed, and horizontal connecting rods are arranged in two adjacent bearing inner cavities;
the vertical connecting rod is arranged on one side of the connecting rod, the vertical connecting rod and the connecting rod are integrally formed, a sleeved column is arranged at the lower end of the vertical connecting rod, and the sleeved column and the vertical connecting rod are integrally formed;
the camera protection cover is arranged at the upper end position of the bottom support plate, the bottom support plate and the camera protection cover are integrally formed, and the camera port is arranged on the outer wall of the camera protection cover and integrally formed with the camera protection cover;
the first semi-ring and the second semi-ring are both installed on the outer wall of the sleeving column, and the outer wall of the first semi-ring and the outer wall of the bottom supporting plate are both provided with wire connecting rings, and the wire connecting rings, the first semi-ring and the bottom supporting plate are integrally formed.
Preferably, the two ends of the first semi-ring and the second semi-ring are provided with an assembly lug plate, the assembly lug plate and the first semi-ring and the second semi-ring are integrally formed, a through hole is formed in the assembly lug plate, and the through hole and the assembly lug plate are integrally formed.
Preferably, two adjacent internally mounted of cross-under hole has cross-under screw rod, stop nut is all installed at the both ends of cross-under screw rod, and stop nut's size is greater than the bore of cross-under hole.
Preferably, the both ends of horizontal connecting rod all are provided with the anticreep piece, and the anticreep piece sets up with horizontal connecting rod integrated into one piece, the activity port on the one end position of connecting rod, the inside intercommunication setting of activity port and bearing inner chamber.
Preferably, the size of the anti-drop block is larger than the caliber of the movable port, and the horizontal connecting rod is movably connected with the connecting rod in a penetrating way through the movable port.
Preferably, a wire rope is arranged between two adjacent wiring rings, and the wire rope is respectively connected with the two wiring rings in a binding way.
Preferably, the lower end of the sleeving column is provided with a limiting end block, and the limiting end block and the sleeving column are integrally formed.
Preferably, a plurality of micro sensors are embedded in the bottom support plate, and the micro sensors are electrically connected.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the utility model, the camera protection cover is sleeved and mounted on the external position of the remote sensing camera, the lens part of the remote sensing camera on the unmanned aerial vehicle corresponds to the camera port for aerial photographing, finally, the eight first semi-rings and the eight second semi-rings are connected in a combined manner and are sleeved and mounted on the outer walls of the eight sleeved posts, and then, two adjacent wiring rings are connected in series by selecting a wire rope with proper length according to actual intervals, so that the purpose of quickly and integrally mounting and protecting the remote sensing camera is achieved, the problem that the existing unmanned aerial vehicle protection frame only can protect a wing structure and cannot protect an aerial photographing camera structure in the mounting and using process is solved, and when the camera is impacted, the service life of the aerial photographing camera is influenced due to the fact that the unprotected structure is easy to damage.
2. Through with the wing cup joint ring seat install unmanned aerial vehicle's four wing supports on to through the internally mounted bolt at the installation connect hole with the wing cup joint ring seat with unmanned aerial vehicle's wing support fixed connection, the in-process of installation can be according to the actual position pulling connecting rod of unmanned aerial vehicle wing support to four wings cup joint the interval between the ring seat and match the regulation, thereby can satisfy the four wing unmanned aerial vehicle installation of different specifications and use.
Drawings
Fig. 1 is a schematic diagram of the whole structure of a protection frame for a remote sensing big data collection unmanned aerial vehicle;
FIG. 2 is a schematic view of a bottom bracket structure according to the present utility model;
FIG. 3 is a schematic diagram of a connection structure of a first half ring and a second half ring according to the present utility model;
FIG. 4 is a schematic view of the internal structure of the connecting rod according to the present utility model;
in the figure: 1. the wing is sleeved with the ring seat; 2. mounting the connecting hole; 3. a connecting rod; 4. a vertical link; 5. sleeving a column; 6. limiting end blocks; 7. a bottom support plate; 8. a camera protection cover; 9. an imaging port; 10. a first half ring; 11. a second half ring; 12. assembling the ear plate; 13. penetrating the hole; 14. threading a screw; 15. a limit nut; 16. a wire connecting ring; 17. a wire rope; 18. a load bearing inner cavity; 19. a horizontal link; 20. an anti-falling block; 21. an active port.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Referring to fig. 1-4, an embodiment of the present utility model is provided: the protection frame for the unmanned aerial vehicle for collecting the remote sensing big data comprises a wing sleeve ring seat 1 and a bottom support plate 7, wherein four mounting connection holes 2 are formed in the wing sleeve ring seat 1, and the mounting connection holes 2 and the wing sleeve ring seat 1 are integrally formed;
further comprises:
the connecting rods 3 are arranged on the outer wall of the wing sleeve ring seat 1, two connecting rods 3 are arranged, four wing sleeve ring seats 1 are arranged, bearing inner cavities 18 are arranged in the connecting rods 3, the bearing inner cavities 18 and the connecting rods 3 are integrally formed, and horizontal connecting rods 19 are arranged in two adjacent bearing inner cavities 18; wherein, two connecting rods 3 weld and fix the two sides of the same wing sleeve ring seat 1.
The vertical connecting rod 4 is arranged on one side of the connecting rod 3, the vertical connecting rod 4 and the connecting rod 3 are integrally formed, a sleeved column 5 is arranged at the lower end of the vertical connecting rod 4, and the sleeved column 5 and the vertical connecting rod 4 are integrally formed;
the camera protection cover 8 is arranged at the upper end position of the bottom support plate 7, the bottom support plate 7 and the camera protection cover 8 are integrally formed, the camera port 9 is arranged on the outer wall of the camera protection cover 8, and the camera port 9 and the camera protection cover 8 are integrally formed;
the first half ring 10 and the second half ring 11 are both installed on the outer wall of the sleeving column 5, and the outer wall of the first half ring 10 and the outer wall of the bottom supporting plate 7 are both provided with wire connecting rings 16, and the wire connecting rings 16, the first half ring 10 and the bottom supporting plate 7 are integrally formed.
During the use, cup joint and install the remote sensing camera external position through the camera guard shield on, remote sensing camera lens part on the unmanned aerial vehicle corresponds the port of making a video recording, and last with eight first semi-rings and eight second semi-rings composite connection and cup joint and install on eight outer walls of cup jointing the post, then according to actual interval, select wire rope two adjacent wiring rings of suitable length to establish ties.
Referring to fig. 3, the assembly lugs 12 are disposed at two ends of the first half ring 10 and the second half ring 11, the assembly lugs 12 are disposed at two sides of the first half ring 10 and the second half ring 11, the assembly lugs 12 are disposed inside the assembly lugs 12, the assembly lugs 13 and the assembly lugs 12 are integrally formed, and the assembly lugs 12 disposed at two ends of the first half ring 10 and the second half ring 11 serve as assembly connection members for facilitating assembly connection of the first half ring 10 and the second half ring 11.
Referring to fig. 3, the two adjacent through holes 13 are internally provided with through screws 14, two ends of each through screw 14 are respectively provided with a limit nut 15, the size of each limit nut 15 is larger than the caliber of each through hole 13, and the through screws 14 arranged in the two adjacent through holes 13 play a role in connecting adjacent assembly lugs 12 in a through manner.
Referring to fig. 4, the two ends of the horizontal connecting rod 19 are respectively provided with an anti-falling block 20, the anti-falling blocks 20 and the horizontal connecting rod 19 are integrally formed, a movable port 21 is arranged at one end position of the connecting rod 3, the movable port 21 is communicated with the interior of the bearing cavity 18, and the anti-falling blocks 20 arranged at the two ends of the horizontal connecting rod 19 play a role in facilitating the anti-falling connection of the horizontal connecting rod 19 and the two connecting rods 3. In this embodiment, the connecting rod 3 is a telescopic rod, and is mainly used for adjusting the intervals between the four wing sleeved ring seats 1.
Referring to fig. 4, the size of the anti-falling block 20 is larger than the caliber of the movable port 21, and the horizontal connecting rod 19 is movably connected with the connecting rod 3 through the movable port 21 in a penetrating way.
Referring to fig. 3, a wire rope 17 is installed between two adjacent wire rings 16, the wire rope 17 is respectively connected with the two wire rings 16 in a binding manner, and the wire rope 17 installed between the two adjacent wire rings 16 plays a role in connecting the two wire rings 16.
Referring to fig. 1, a limiting end block 6 is disposed at the lower end of the socket post 5, the limiting end block 6 and the socket post 5 are integrally formed, and the limiting end block 6 disposed at the lower end of the socket post 5 plays a role in mounting and limiting the first semi-ring 10 and the second semi-ring 11.
Referring to fig. 2, the bottom support plate 7 is embedded with a plurality of micro sensors 71, a plurality of micro sensors 71 are electrically connected with each other, the micro sensors 71 are electrically connected with an unmanned aerial vehicle (not shown in the drawing) for supplying power to the micro sensors 71, and meanwhile, the information detected and collected by the micro sensors 71 can be transmitted to the unmanned aerial vehicle, and further, the information detected and collected is transmitted to a user terminal by means of a wireless transceiver unit on the unmanned aerial vehicle, or the information detected and collected is stored in a storage unit on the unmanned aerial vehicle, in this embodiment, the micro sensors 71 comprise pressure sensors for collecting impact forces of the unmanned aerial vehicle falling in different environments, altitude sensors for collecting altitude and speed sensors for collecting speed in the flight, and in other embodiments, the micro sensors with different functions can be configured according to actual use requirements.
Working principle: during the use, first will the wing cup joint ring seat 1 and install on unmanned aerial vehicle's four wing supports to through the internally mounted bolt at installation connecting hole 2 cup joint ring seat 1 with unmanned aerial vehicle's wing support below through bolt fixed connection, the in-process of installation can be according to the actual position of unmanned aerial vehicle wing support, the pulling connecting rod 3 carries out the matching adjustment to the interval between four wings cup joint ring seat 1, thereby can satisfy the four wing unmanned aerial vehicle installation of different specifications and use, then cup joint the bottom stay plate 7 through camera protection cover 8 and install on the remote sensing camera external position, remote sensing camera lens part on the unmanned aerial vehicle corresponds camera port 9 and take photo by plane, finally with eight first semi-rings 10 and eight second semi-rings 11 make up and cup joint and install on eight outer walls of cup joint post 5, then according to actual interval, select two adjacent wire ropes 17 to connect in series, thereby reach the purpose of quick combination installation protection remote sensing machine, protect the unmanned aerial vehicle below the camera, accomplish the use remote sensing support for the unmanned aerial vehicle that big data was collected.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims (8)

1. The protection frame for the unmanned aerial vehicle for collecting the remote sensing big data comprises a wing sleeve ring seat (1) and a bottom support plate (7), wherein four mounting connecting holes (2) are formed in the wing sleeve ring seat (1), and the mounting connecting holes (2) and the wing sleeve ring seat (1) are integrally formed;
the method is characterized in that: further comprises:
the connecting rods (3) are arranged on the outer wall of the wing sleeve ring seat (1), two connecting rods (3) are arranged, four wing sleeve ring seats (1) are arranged, bearing inner cavities (18) are formed in the connecting rods (3), the bearing inner cavities (18) and the connecting rods (3) are integrally formed, and horizontal connecting rods (19) are arranged in the two adjacent bearing inner cavities (18);
the vertical connecting rod (4) is arranged on one side of the connecting rod (3), the vertical connecting rod (4) and the connecting rod (3) are integrally formed, a sleeved column (5) is arranged at the lower end of the vertical connecting rod (4), and the sleeved column (5) and the vertical connecting rod (4) are integrally formed;
the camera protection cover (8) is arranged at the upper end position of the bottom supporting plate (7), the bottom supporting plate (7) and the camera protection cover (8) are integrally formed, an image pickup port (9) is arranged on the outer wall of the camera protection cover (8), and the image pickup port (9) and the camera protection cover (8) are integrally formed;
the first semi-ring (10) and the second semi-ring (11) are both installed on the outer wall of the sleeving column (5), and the wire connecting rings (16) are arranged on the outer wall of the first semi-ring (10) and the outer wall of the bottom supporting plate (7), and the wire connecting rings (16) are integrally formed with the first semi-ring (10) and the bottom supporting plate (7).
2. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 1, wherein: the utility model discloses a semi-ring assembly device, including first semi-ring (10) and second semi-ring (11), both ends of first semi-ring (10) and second semi-ring (11) all are provided with equipment otic placode (12), and equipment otic placode (12) and first semi-ring (10) and second semi-ring (11) integrated into one piece set up, the inside of equipment otic placode (12) is provided with cross-under hole (13), and cross-under hole (13) and equipment otic placode (12) integrated into one piece set up.
3. The unmanned aerial vehicle fender bracket for remote sensing big data collection according to claim 2, wherein: and two adjacent cross-connection holes (13) are internally provided with cross-connection screws (14), both ends of each cross-connection screw (14) are provided with limiting nuts (15), and the size of each limiting nut (15) is larger than the caliber of each cross-connection hole (13).
4. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 1, wherein: the two ends of the horizontal connecting rod (19) are respectively provided with an anti-falling block (20), the anti-falling blocks (20) and the horizontal connecting rod (19) are integrally formed, one end of the connecting rod (3) is provided with a movable port (21), and the movable port (21) is communicated with the inside of the bearing inner cavity (18).
5. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 4, wherein: the size of the anti-falling block (20) is larger than the caliber of the movable port (21), and the horizontal connecting rod (19) is movably connected with the connecting rod (3) in a penetrating way through the movable port (21).
6. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 1, wherein: a wire rope (17) is arranged between two adjacent wiring rings (16), and the wire ropes (17) are respectively connected with the two wiring rings (16) in a binding way.
7. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 1, wherein: the lower extreme of cup jointing post (5) is provided with spacing end block (6), and spacing end block (6) and cup jointing post (5) integrated into one piece set up.
8. The unmanned aerial vehicle fender bracket for remote sensing big data collection of claim 1, wherein: a plurality of micro sensors (71) are embedded in the bottom support plate (7), and the micro sensors (71) are electrically connected.
CN202320207279.5U 2023-02-13 2023-02-13 Protection frame for unmanned aerial vehicle for collecting remote sensing big data Active CN218929842U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320207279.5U CN218929842U (en) 2023-02-13 2023-02-13 Protection frame for unmanned aerial vehicle for collecting remote sensing big data

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320207279.5U CN218929842U (en) 2023-02-13 2023-02-13 Protection frame for unmanned aerial vehicle for collecting remote sensing big data

Publications (1)

Publication Number Publication Date
CN218929842U true CN218929842U (en) 2023-04-28

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Application Number Title Priority Date Filing Date
CN202320207279.5U Active CN218929842U (en) 2023-02-13 2023-02-13 Protection frame for unmanned aerial vehicle for collecting remote sensing big data

Country Status (1)

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CN (1) CN218929842U (en)

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