CN217691673U - Unmanned aerial vehicle anticreep connects electrical terminal structure - Google Patents

Unmanned aerial vehicle anticreep connects electrical terminal structure Download PDF

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Publication number
CN217691673U
CN217691673U CN202221414273.7U CN202221414273U CN217691673U CN 217691673 U CN217691673 U CN 217691673U CN 202221414273 U CN202221414273 U CN 202221414273U CN 217691673 U CN217691673 U CN 217691673U
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China
Prior art keywords
unmanned aerial
aerial vehicle
terminal
fixedly connected
tie
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CN202221414273.7U
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Chinese (zh)
Inventor
王神玉
戴永东
王茂飞
毛锋
方成
张韧
周燚
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Taizhou Power Supply Co of State Grid Jiangsu Electric Power Co Ltd
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Taizhou Power Supply Co of State Grid Jiangsu Electric Power Co Ltd
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Priority to CN202221414273.7U priority Critical patent/CN217691673U/en
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an anti-disconnecting terminal structure of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein a power-on terminal is arranged in the middle of the lower end face of the unmanned aerial vehicle body, and a lower power-off terminal is inserted into the power-on terminal; clamping holes are formed in the left side and the right side of the lower electric connecting terminal, a cavity is formed in the fixed block, two ends of the reset spring respectively abut against the inner wall of the cavity and the moving block, and a clamping rod is fixedly connected to one side, close to the lower electric connecting terminal, of the moving block; the utility model discloses a movable block, kelly and movable rod, cooperation reset spring, arm-tie, spout and slider for when will connecting the electricity terminal down and insert, can stimulate the arm-tie, thereby make the kelly remove, prevent to stop connecting the electricity terminal down, after inserting, loosen the arm-tie, reset spring's effect of stretching down can promote the movable plate, thereby make the kelly insert the downthehole portion of card of connecting the electricity terminal down, thereby fix connecting the electricity terminal down.

Description

Unmanned aerial vehicle anticreep connects electrical terminal structure
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle anticreep connects electrical terminal structure.
Background
The bottom of unmanned aerial vehicle generally installs the electrical connection terminal and is used for the condition such as transmission data, and the in-process that uses after will receiving the electrical connection terminal and inserting the butt joint produces when rocking, because do not have the structure of anticreep, leads to very easily that the electrical connection terminal drops, and the butt joint electric terminal that can not be convenient is fixed, leads to the inconvenient use of follow-up user.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides an unmanned aerial vehicle anticreep connects electrical terminal structure possesses the butt electrical terminal of being convenient for and fixes advantages such as, has solved the unable anticreep problem of traditional electrical terminal.
The utility model discloses an unmanned aerial vehicle anticreep connects electrical terminal structure, including the unmanned aerial vehicle body, the middle part of unmanned aerial vehicle body lower extreme face is installed and is connected electrical terminal, and the inside of connecting electrical terminal inserts and connects electrical terminal down;
the left side and the right side of the lower electric connecting terminal are both provided with clamping holes, the lower end surface of the unmanned aerial vehicle body and the positions close to the left side and the right side are both fixedly connected with a fixed block, the inside of the fixed block is provided with a cavity, the inside of the cavity is movably connected with a movable block and a reset spring, the two ends of the reset spring respectively support against the inner wall of the cavity and the movable block, one side of the movable block close to the lower electric connecting terminal is fixedly connected with a clamping rod, one side of the clamping rod penetrates through the fixed block and is inserted into the clamping holes, the other side of the movable plate is fixedly connected with a movable rod, and the movable rod passes the fixed block, the surface of movable rod is located to the reset spring movable sleeve, terminal surface just is close to the position department on left right side through hinged joint have the arm-tie under the unmanned aerial vehicle body, the spout has been seted up to one side that the arm-tie is close to the movable rod, the inside sliding connection of spout has the slider, one side of movable rod is connected with the slider through the hinge, can conveniently stimulate the kelly, from not influencing down the electrical connector male while, can fix the electrical connector, thereby can prevent to descend the electrical connector to drop, inconvenient user uses.
Further, the top and the bottom of the inner wall of the cavity are both provided with stabilizing grooves along the extension direction of the return spring, and the stabilizing grooves are connected with stabilizing blocks in a sliding mode and fixedly connected with moving blocks.
Furthermore, one side of the clamping rod is arc-shaped and is matched with the clamping hole, and one side of the clamping rod is fixedly connected with soft rubber.
Furthermore, one side of the pulling plate is arc-shaped, and a rubber pad is fixedly connected to the outer surface of the pulling plate.
Further, unmanned aerial vehicle's all has the mounting panel through hinged joint on the left and right sides, and the mounting panel is close to one side fixedly connected with installation piece of arm-tie, the mounting hole has been seted up to one side of arm-tie, and the installation piece inserts in the inside of mounting hole.
Furthermore, one side of the mounting plate, which is far away from the pulling plate, is fixedly connected with a handle.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. through the movable block, kelly and movable rod, cooperation reset spring, the arm-tie, spout and slider for when will descend the electrical terminal to insert, can stimulate the arm-tie, thereby make the kelly remove, prevent to stop lower electrical terminal, after inserting, loosen the arm-tie, reset spring's the effect of stretching down can promote the movable plate, thereby make the kelly insert the downthehole portion of card of lower electrical terminal, thereby fix lower electrical terminal.
2. Through the mounting panel, the cooperation installation piece for when using for a long time, prevent that the arm-tie is automatic from removing, can select the mounting panel to drive the installation piece and remove, the inside of arm-tie is inserted to the easy to assemble piece, thereby fixes the arm-tie, prevents automatic removing.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:
FIG. 1 is a schematic view of the overall front cross-sectional structure of the present invention;
FIG. 2 is an enlarged schematic view of the structure at A in FIG. 1;
fig. 3 is a schematic view of the three-dimensional structure of the fixing block of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a connecting terminal is connected; 3. a lower power connection terminal; 301. a clamping hole; 4. a fixed block; 401. a cavity; 5. a moving block; 6. a clamping rod; 7. a stabilizing slot; 701. a stabilizing block; 8. a movable rod; 801. a return spring; 9. pulling a plate; 10. a chute; 1001. a slider; 11. mounting a plate; 1101. and (7) installing the block.
Detailed Description
Referring to fig. 1-3, the utility model discloses an unmanned aerial vehicle anti-releasing terminal structure, including unmanned aerial vehicle body 1, the middle part of the lower end face of unmanned aerial vehicle body 1 is installed with upper connecting terminal 2, lower connecting terminal 3 is inserted into the interior of upper connecting terminal 2;
lower left and right sides of electricity terminal 3 has all seted up calorie hole 301, equal fixedly connected with fixed block 4 in terminal surface and the position department that is close to left and right side under the unmanned aerial vehicle body 1, cavity 401 has been seted up to the inside of fixed block 4, the inside swing joint of cavity 401 is equipped with movable block 5 and reset spring 801, cavity 401 inner wall and movable block 5 are supported respectively at reset spring 801's both ends, one side fixedly connected with kelly 6 that movable block 5 is close to electricity terminal 3 down, one side of kelly 6 is passed fixed block 4 and is inserted inside calorie hole 301, the other one side fixedly connected with movable rod 8 of movable plate, and movable rod 8 passes fixed block 4, reset spring 801 movable sleeve locates the surface of movable rod 8, there is arm 9 terminal end under the unmanned aerial vehicle body 1 and the position department that is close to left and right side through hinged joint, chute 10 has been seted up to one side that arm 9 is close to movable rod 8, the inside sliding connection of chute 10 has slider 1001, one side of movable rod 8 is connected with slider 1001 through the hinge, can conveniently stimulate kelly 6, from not influencing when lower electricity terminal 3 inserts down, can fix the butt joint, thereby can prevent that the user from coming off the electricity terminal.
Further, stability groove 7 has all been seted up along the flexible direction of reset spring 801 to the top and the bottom of cavity 401 inner wall, and the inside sliding connection of stability groove 7 has stabilizing block 701, stabilizing block 701 and movable block 5 fixed connection, and this structure setting for movable block 5 is carrying out the in-process that removes, stability more can be more, makes its kelly 6 also can remain stable when inserting the inside of calorie hole 301.
Further, one side of kelly 6 is the arc, and with calorie hole 301 looks adaptation, one side fixedly connected with flexible glue of kelly 6, this structure setting for can conveniently insert the inside of calorie hole 301, the condition of preventing skidding appears, conveniently fixes.
Further, one side of arm-tie 9 is the arc, and the fixed surface of arm-tie 9 is connected with the rubber pad, and this structure setting for the user can conveniently promote arm-tie 9, thereby conveniently stimulates kelly 6.
Further, unmanned aerial vehicle's all there is mounting panel 11 on the left and right sides through hinged joint, and one side fixedly connected with installation piece 1101 that mounting panel 11 is close to arm-tie 9, and the mounting hole has been seted up to one side of arm-tie 9, and installation piece 1101 inserts in the inside of mounting hole, and this structure sets up for under long-time use, can fix arm-tie 9, thereby prevent that arm-tie 9 can be automatic to remove, lead to the kelly 6 can't fix.
Further, one side fixedly connected with handle that mounting panel 11 kept away from arm-tie 9, this structural setting for the user can conveniently remove and rotate mounting panel 11, conveniently fixes.
In use the utility model discloses in the time, at first, when connecting terminal 3 and inserting down, can grasp arm-tie 9 and stimulate, thereby drive movable rod 8 and remove, make slider 1001 slide in the inside of spout 10, thereby it removes to drive movable block 5, make reset spring 801 compressed, movable block 5 can drive stable piece 701 simultaneously and slide in the inside of stabilizing trough 7, thereby it removes to drive kelly 6, make the insertion that connects terminal 3 can be convenient down, insert the back, loosen arm-tie 9, reset spring 801 stretches, promote movable block 5, thereby make kelly 6 remove, inside inserting the card hole 301 that connects terminal 3 down, fix connecting terminal 3 down.
The above description is only for the embodiment of the present invention, and is not intended to limit the present invention. Various modifications and variations of the present invention will be apparent to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims (6)

1. The utility model provides an unmanned aerial vehicle anticreep connects electrical terminal structure, includes unmanned aerial vehicle body (1), its characterized in that: the middle part of the lower end face of the unmanned aerial vehicle body (1) is provided with an upper connecting terminal (2), and a lower connecting terminal (3) is inserted into the upper connecting terminal (2);
card hole (301) have all been seted up on the left and right sides of lower electricity connection terminal (3), equal fixedly connected with fixed block (4) of terminal surface and position department near left and right side under unmanned aerial vehicle body (1), cavity (401) have been seted up to the inside of fixed block (4), the inside swing joint of cavity (401) is equipped with movable block (5) and reset spring (801), cavity (401) inner wall and movable block (5) are supported respectively to the both ends of reset spring (801), one side fixedly connected with kelly (6) of lower electricity connection terminal (3) are close to in movable block (5), one side of kelly (6) is passed fixed block (4) and is inserted inside calorie hole (301), one side fixedly connected with movable rod (8) in addition of movable plate, and movable rod (8) pass fixed block (4), the surface of movable rod (8) is located to reset spring (801) movable sleeve, there is arm-tie (9) through hinged joint in the position department of terminal surface and near left right side under unmanned aerial vehicle body (1), arm-tie (9) are close to one side of movable rod (8) and have seted up (10), the inside connection with slider (1001) of spout (10), slider (1001) is connected with hinge through hinge (1001) one side.
2. The unmanned aerial vehicle anticreep connection terminal structure of claim 1, its characterized in that: the top and the bottom of the inner wall of the cavity (401) are both provided with a stabilizing groove (7) along the extension direction of the return spring (801), the interior of the stabilizing groove (7) is connected with a stabilizing block (701) in a sliding manner, and the stabilizing block (701) is fixedly connected with the moving block (5).
3. The unmanned aerial vehicle anticreep connection terminal structure of claim 1, its characterized in that: one side of the clamping rod (6) is arc-shaped and is matched with the clamping hole (301), and one side of the clamping rod (6) is fixedly connected with soft rubber.
4. The unmanned aerial vehicle anticreep connection terminal structure of claim 1, its characterized in that: one side of the pulling plate (9) is arc-shaped, and a rubber pad is fixedly connected to the outer surface of the pulling plate (9).
5. The unmanned aerial vehicle anticreep connection terminal structure of claim 1, its characterized in that: unmanned aerial vehicle's left and right sides all has mounting panel (11) through hinged joint, and one side fixedly connected with installation piece (1101) that mounting panel (11) are close to arm-tie (9), the mounting hole has been seted up to one side of arm-tie (9), and installation piece (1101) inserts in the inside of mounting hole.
6. The unmanned aerial vehicle anticreep connection terminal structure of claim 5, characterized in that: and a handle is fixedly connected to one side of the mounting plate (11) far away from the pulling plate (9).
CN202221414273.7U 2022-06-08 2022-06-08 Unmanned aerial vehicle anticreep connects electrical terminal structure Active CN217691673U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221414273.7U CN217691673U (en) 2022-06-08 2022-06-08 Unmanned aerial vehicle anticreep connects electrical terminal structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221414273.7U CN217691673U (en) 2022-06-08 2022-06-08 Unmanned aerial vehicle anticreep connects electrical terminal structure

Publications (1)

Publication Number Publication Date
CN217691673U true CN217691673U (en) 2022-10-28

Family

ID=83707746

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221414273.7U Active CN217691673U (en) 2022-06-08 2022-06-08 Unmanned aerial vehicle anticreep connects electrical terminal structure

Country Status (1)

Country Link
CN (1) CN217691673U (en)

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