CN212921997U - Unmanned aerial vehicle carries quick detach mechanism - Google Patents

Unmanned aerial vehicle carries quick detach mechanism Download PDF

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Publication number
CN212921997U
CN212921997U CN202020943123.XU CN202020943123U CN212921997U CN 212921997 U CN212921997 U CN 212921997U CN 202020943123 U CN202020943123 U CN 202020943123U CN 212921997 U CN212921997 U CN 212921997U
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
main
vaulting pole
auxiliary
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202020943123.XU
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Chinese (zh)
Inventor
邢赢
汪晓丽
刘铭
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Shenyang Zc Uav Technology Co ltd
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Shenyang Zc Uav Technology Co ltd
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Priority to CN202020943123.XU priority Critical patent/CN212921997U/en
Application granted granted Critical
Publication of CN212921997U publication Critical patent/CN212921997U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an unmanned aerial vehicle carries quick detach mechanism, including unmanned aerial vehicle, panoramic camera and main tributary vaulting pole, the lower surface intermediate position fixed mounting of unmanned aerial vehicle has the worker's type piece, the cross-section of worker's type piece is square shape, panoramic camera flange joint is in the bottom of main tributary vaulting pole, the top fixed mounting of main tributary vaulting pole has the auxiliary stay bar, sliding connection has the main slide cartridge on the main tributary vaulting pole, the bilateral symmetry sliding connection that is located the main tributary vaulting pole on the auxiliary stay bar has the auxiliary slide cartridge, the both sides wall of main slide cartridge all is connected with the one end of connecting rod through hinge ear symmetry rotation, the utility model discloses, when installing and dismantling, only need control two holding rods to fold and then loosen, make two machinery hold at I-shaped piece or loosen I-shaped piece, just can accomplish installation or dismantlement, improved the efficiency of installation and dismantlement, reduced the time that the staff stopped, prevent that there is danger in the unmanned aerial vehicle bottom for a long time.

Description

Unmanned aerial vehicle carries quick detach mechanism
Technical Field
The utility model relates to an unmanned air vehicle technique field, concrete field is an unmanned aerial vehicle carry quick detach mechanism.
Background
The unmanned plane is called unmanned plane for short, and is called UAV in English, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. From a technical point of view, the definition can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane aircraft, and the like; unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to 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, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Present unmanned aerial vehicle is when carrying out panoramic video's shooting, need carry the panoramic camera on large-scale unmanned aerial vehicle, the mode of its carry starts unmanned aerial vehicle earlier, make unmanned aerial vehicle fly to the height about 2 meters, then artificial bracing piece one end carry that the downside from unmanned aerial vehicle is connected the panoramic camera on the unmanned aerial vehicle bottom surface, also directly take off it from the unmanned aerial vehicle bottom surface during its dismantlement, current carry dismantlement mode step is more, the waste time, it is also dangerous for a long time at the unmanned aerial vehicle downside.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle carry quick detach mechanism to it is more to provide current carry dismantlement mode step in solving above-mentioned background art, the waste time, long-time also more dangerous problem at the unmanned aerial vehicle downside.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle hanging quick-release mechanism comprises an unmanned aerial vehicle, a panoramic camera and a main support rod, wherein an I-shaped block is fixedly installed at the middle position of the lower surface of the unmanned aerial vehicle, the cross section of the I-shaped block is square, the panoramic camera is connected to the bottom end of the main support rod in a flange mode, an auxiliary support rod is fixedly installed at the top end of the main support rod, a main sliding barrel is connected onto the main support rod in a sliding mode, auxiliary sliding barrels are symmetrically and slidably connected onto the auxiliary support rod and located on two sides of the main support rod, two side walls of the main sliding barrel are symmetrically and rotatably connected with one end of a connecting rod through hinge lugs, the other end of each connecting rod is respectively and rotatably connected onto the side walls of the two auxiliary sliding barrels through hinge lugs, baffles are fixedly installed at two ends of the auxiliary support rod, a locking spring is arranged between the auxiliary sliding barrel on each side and the baffle close to the position, two ends of the, the side wall of the auxiliary sliding cylinder is fixedly provided with one end of a handle arm, the other end of the handle arm is fixedly provided with a manipulator, the two manipulators are clamped in the I-shaped groove of the I-shaped block in an attaching mode, the side wall of the main sliding cylinder is fixedly provided with a holding rod, and the side wall of the main supporting rod and the upper portion of the main sliding cylinder are also fixedly provided with the holding rod.
Preferably, the side wall of the main sliding cylinder is provided with a slot, and the side wall of the main supporting rod is provided with an inserting block matched with the slot for use.
Preferably, one end of the insertion block close to the slot is in a semicircular shape.
Preferably, the inner side wall of the I-shaped groove of the I-shaped block is sleeved with a magnetic ring.
Preferably, the magnetic ring is rectangular, the manipulator is made of iron materials, and the manipulator is magnetically connected to the magnetic ring.
Preferably, the holding rod is perpendicular to the main support rod.
Preferably, the side wall of the holding rod is provided with a holding groove.
Compared with the prior art, the beneficial effects of the utility model are that: a main sliding cylinder and an auxiliary sliding cylinder can be connected through a connecting rod, when the main sliding cylinder moves, the auxiliary sliding cylinder can also move synchronously along with the main sliding cylinder, the auxiliary sliding cylinder can be pushed to move through a locking spring, so that two manipulators are mutually close and attached to each other, when the two manipulators are clamped in an I-shaped groove of an I-shaped block, a panoramic camera can be arranged on the unmanned aerial vehicle, when the unmanned aerial vehicle needs to be disassembled, the GPS unmanned aerial vehicle is firstly automatically stopped in the air of about two meters, then two holding rods are respectively held by two hands and move towards the mutually close direction, so that the two manipulators can be separated, when the two manipulators are completely far away from the I-shaped groove of the I-shaped block, the two holding rods can be taken away, so that the rapid disassembly of the unmanned aerial vehicle mounting can be completed, the utility model discloses, when in the mounting and the disassembly, only the two holding rods need to be controlled to be folded and then loosened, so that the two mechanical hands hold the I-shaped block or the I-, the efficiency of installation dismantlement is improved, has reduced the staff simultaneously and has stopped the time in unmanned aerial vehicle bottom, prevents to have danger in unmanned aerial vehicle bottom for a long time.
Drawings
Fig. 1 is a schematic view of the structure of the assembled i-shaped block and manipulator of the present invention;
FIG. 2 is a schematic view of the structure of the I-shaped block and the manipulator of the present invention when they are not assembled;
fig. 3 is a schematic rear view of the present invention;
FIG. 4 is an enlarged view of the structure at A in FIG. 3;
FIG. 5 is an enlarged view of the structure at B in FIG. 3;
FIG. 6 is a schematic side view of the grip of the present invention;
fig. 7 is a schematic top view and sectional view of the inventive fixture block.
In the figure: 1-unmanned aerial vehicle, 2-panoramic camera, 3-main support rod, 4-shaping block, 5-auxiliary support rod, 6-main sliding barrel, 7-auxiliary sliding barrel, 8-connecting rod, 9-baffle, 10-locking spring, 11-handle arm, 12-mechanical arm, 13-holding rod, 14-slot, 15-insertion block and 16-magnetic ring.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-7, the present invention provides a technical solution: an unmanned aerial vehicle carries quick detach mechanism, includes unmanned aerial vehicle 1, panoramic camera 2 and main tributary vaulting pole 3, unmanned aerial vehicle 1's lower surface intermediate position fixed mounting has an industry piece 4, the cross-section of industry piece 4 is square shape, prevents to take place to rotate at two manipulators 12, panoramic camera 2 flange joint is in the bottom of main tributary vaulting pole 3, the top fixed mounting of main tributary vaulting pole 3 has a vice bracing piece 5, sliding connection has a main slide cartridge 6 on the main tributary vaulting pole 3, the bilateral symmetry sliding connection that just is located main tributary vaulting pole 3 on the vice bracing piece 5 has a vice slide cartridge 7, the both sides wall of main slide cartridge 6 all is connected with the one end of connecting rod 8 through hinge lug symmetry rotation, two the other end of connecting rod 8 all rotates respectively through hinge lug and connects on two the lateral wall of vice slide cartridge 7, the both ends of vice bracing piece 5 all fixed mounting has baffle 9, a locking spring 10 is arranged between the auxiliary sliding barrel 7 and the baffle 9 close to each other at each side, two ends of the locking spring 10 are respectively and fixedly installed on the baffle 9 and the auxiliary sliding barrel 7, one end of a handle 11 is fixedly installed on the side wall of the auxiliary sliding barrel 7, the other end of the handle 11 is fixedly installed with a manipulator 12, the two manipulators 12 are clamped in the I-shaped groove of the I-shaped block 4 in a fitting manner, a holding rod 13 is fixedly installed on the side wall of the main sliding barrel 6, a holding rod 13 is also fixedly installed on the side wall of the main supporting rod 3 and on the upper portion of the main sliding barrel 6, when the unmanned aerial vehicle 1GPS is automatically stopped in the air about two meters when the unmanned aerial vehicle needs to be disassembled, then two hands respectively hold the two holding rods 13 and move towards the direction of closing each other, at the moment, the two auxiliary sliding barrels 7 are respectively located on the auxiliary supporting rod 5 and slide towards the direction far away from the main supporting rod 3, and are, make two manipulators 12 part, when keeping away from the worker's type inslot of worker's type piece 4 completely, just can take it away to accomplish the quick dismantlement of unmanned aerial vehicle 1 carry.
Particularly, the lateral wall of main smooth section of thick bamboo 6 is equipped with slot 14, the lateral wall of main tributary vaulting pole 3 is equipped with the inserted block 15 that cooperatees and use with slot 14, sets up through the cooperation of slot 14 and inserted block 15, can restrict the rotation of main smooth section of thick bamboo 6, prevents that unmanned aerial vehicle 1 from causing the torsional force to connecting rod 8 at the flight in-process to it is not hard up with articulated ear to make connecting rod 8, causes and rocks the phenomenon.
Specifically, the insertion block 15 has a semicircular shape at one end thereof close to the insertion groove 14.
Specifically, the inner side wall of the I-shaped groove of the I-shaped block 4 is sleeved with a magnetic ring 16.
Specifically, the magnetic ring 16 is rectangular, the manipulator 12 is made of iron material, the manipulator 12 is magnetically connected to the magnetic ring 16, and the two manipulators can be stabilized on the i-shaped block 4 by the matching arrangement of the magnetic ring 16 and the iron manipulator 12.
Specifically, the holding rods 13 are perpendicular to the main support rod 3, and the two holding rods 13 are parallel to each other, so that the holding rods 13 can be conveniently controlled by two hands.
Specifically, the side wall of the holding rod 13 is provided with a holding groove, so that the holding rod 13 can be conveniently held to control the movement of the holding rod 13.
The working principle is as follows: in the utility model, the main support rod 3 can support the panoramic camera 2, the main slide cylinder 6 and the auxiliary slide cylinder 7 can be connected through the connecting rod 8, when the main slide cylinder 6 moves, the auxiliary slide cylinder 7 can also move synchronously with the main slide cylinder 6, the auxiliary slide cylinder 7 can be pushed to move through the locking spring 10, so that the two manipulators 12 are mutually close and jointed, when the two manipulators 12 are clamped in the industrial groove of the I-shaped block 4, the panoramic camera 2 can be arranged on the unmanned aerial vehicle 1, when the unmanned aerial vehicle 1 needs to be disassembled, the GPS is automatically stopped in the air about two meters, then two hands respectively hold the two holding rods 13 and move towards the mutually close direction, at the moment, the two auxiliary slide cylinders 7 are respectively positioned on the auxiliary support rod 5 and slide towards the direction far away from the main support rod 3, the two manipulators 12 are separated through the connection of the arms, when the industrial groove of the industrial block 4 is completely far away, just can take it away to accomplish the quick dismantlement of unmanned aerial vehicle 1 carry, the utility model discloses, when installation and dismantlement, only need control two holding rods 13 and fold and then loosen, make two manipulators 12 hold at I-shaped piece 4 or loosen I-shaped piece 4, just can accomplish the installation or dismantle, improved the efficiency of installation dismantlement, reduced the staff simultaneously and stopped the time in unmanned aerial vehicle 1 bottom, prevent that it is dangerous in unmanned aerial vehicle 1 bottom for a long time.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connection mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt prior art, and conventional model, including circuit connection adopts conventional connection mode among the prior art, does not detailed here again.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides an unmanned aerial vehicle carries quick detach mechanism, includes unmanned aerial vehicle (1), panorama camera (2) and main tributary vaulting pole (3), its characterized in that: the lower surface intermediate position fixed mounting of unmanned aerial vehicle (1) has industry piece (4), the cross-section of industry piece (4) is square shape, panoramic camera (2) flange joint is in the bottom of main tributary vaulting pole (3), the top fixed mounting of main tributary vaulting pole (3) has auxiliary support pole (5), sliding connection has main slide cartridge (6) on main tributary vaulting pole (3), the bilateral symmetry sliding connection who just is located main tributary vaulting pole (3) on auxiliary support pole (5) has auxiliary slide cartridge (7), the both sides wall of main slide cartridge (6) all rotates the one end that is connected with connecting rod (8) through articulated ear symmetry, two the other end of connecting rod (8) all rotates respectively through articulated ear and connects two on the lateral wall of auxiliary slide cartridge (7), the equal fixed mounting in both ends of auxiliary support pole (5) has baffle (9), on each side all be equipped with between baffle (9) that auxiliary slide cartridge (7) and position are close to each other and lock spring (10) The two ends of the locking spring (10) are fixedly mounted on the baffle (9) and the auxiliary sliding barrel (7) respectively, one end of an arm (11) is fixedly mounted on the side wall of the auxiliary sliding barrel (7), a manipulator (12) is fixedly mounted at the other end of the arm (11), and two manipulators (12) are attached to the inner side of the work-shaped groove of the I-shaped block (4), a holding rod (13) is fixedly mounted on the side wall of the main sliding barrel (6), and a holding rod (13) is also fixedly mounted on the side wall of the main supporting rod (3) and located on the upper portion of the main sliding barrel (6).
2. The unmanned aerial vehicle carries quick detach mechanism of claim 1, characterized in that: the side wall of the main sliding barrel (6) is provided with a slot (14), and the side wall of the main supporting rod (3) is provided with an inserting block (15) matched with the slot (14) for use.
3. The unmanned aerial vehicle carries quick detach mechanism of claim 2, its characterized in that: one end of the insertion block (15) close to the slot (14) is in a semicircular shape.
4. The unmanned aerial vehicle carries quick detach mechanism of claim 1, characterized in that: and a magnetic ring (16) is sleeved on the inner side wall of the I-shaped groove of the I-shaped block (4).
5. The unmanned aerial vehicle carries quick detach mechanism of claim 4, its characterized in that: the magnetic ring (16) is rectangular, the manipulator (12) is made of iron materials, and the manipulator (12) is magnetically connected to the magnetic ring (16).
6. The unmanned aerial vehicle carries quick detach mechanism of claim 1, characterized in that: the holding rod (13) is perpendicular to the main support rod (3).
7. The unmanned aerial vehicle carries quick detach mechanism of claim 1, characterized in that: the side wall of the holding rod (13) is provided with a holding groove.
CN202020943123.XU 2020-05-29 2020-05-29 Unmanned aerial vehicle carries quick detach mechanism Expired - Fee Related CN212921997U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020943123.XU CN212921997U (en) 2020-05-29 2020-05-29 Unmanned aerial vehicle carries quick detach mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020943123.XU CN212921997U (en) 2020-05-29 2020-05-29 Unmanned aerial vehicle carries quick detach mechanism

Publications (1)

Publication Number Publication Date
CN212921997U true CN212921997U (en) 2021-04-09

Family

ID=75318678

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020943123.XU Expired - Fee Related CN212921997U (en) 2020-05-29 2020-05-29 Unmanned aerial vehicle carries quick detach mechanism

Country Status (1)

Country Link
CN (1) CN212921997U (en)

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Granted publication date: 20210409