CN219770177U - Unmanned aerial vehicle machine carries and fills ability safety device - Google Patents
Unmanned aerial vehicle machine carries and fills ability safety device Download PDFInfo
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- CN219770177U CN219770177U CN202321269771.1U CN202321269771U CN219770177U CN 219770177 U CN219770177 U CN 219770177U CN 202321269771 U CN202321269771 U CN 202321269771U CN 219770177 U CN219770177 U CN 219770177U
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- 238000007667 floating Methods 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 8
- 238000003825 pressing Methods 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000012423 maintenance Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
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Abstract
The utility model relates to the field of detonating devices and discloses an unmanned aerial vehicle onboard energy charging safety device, which comprises a machine body, wherein a connecting block is fixedly connected to the middle of the bottom side of the machine body, clamping grooves are formed in the left side and the right side of the inside of the connecting block, a connector is slidably connected to the middle of the connecting block, one side of a clamping block is connected to the inside of the left side and the right side of the connector through springs, a pressing rod is fixedly connected to the lower portion of the other side of the clamping block, the upper portion of the other side of the clamping block is slidably connected to the inside of the clamping groove, an energy charging plug is slidably connected to the inside of the connector, an energy charging line is fixedly connected to the bottom of the energy charging plug, supporting rods are rotatably connected to the two sides of the bottom of the machine body, and one end, far away from the machine body, of the supporting rods is fixedly connected with a bottom frame. According to the utility model, the accessory is connected with the energy charging plug through the cooperation of the connecting block, the connector, the clamping groove, the clamping block and the pressing rod.
Description
Technical Field
The utility model relates to the field of detonators, in particular to an unmanned aerial vehicle-mounted charging safety device.
Background
Unmanned aircraft, for short, "unmanned aircraft," is unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programming device, or is operated autonomously, either entirely or intermittently, by an on-board computer. Unmanned aircraft tend to be more suitable for tasks that are too "fooled, messy, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, 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 the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.
Unmanned aerial vehicle can be equipped with many accessories and use when using, these accessories need to use the machine to fill the ability device to fill the accessory when unmanned aerial vehicle flight is operated and use, and present accessory fills can with unmanned aerial vehicle fuselage socket connection commonly when can, this makes and inserts repeatedly, or unmanned aerial vehicle flight fills when can the unexpected in-process accessory drops, can make unmanned aerial vehicle fuselage fill can the interface receive the damage, leads to unmanned aerial vehicle unable normal use, increases unmanned aerial vehicle cost of maintenance. Therefore, an unmanned aerial vehicle onboard charging safety device is provided to solve the problems.
Disclosure of Invention
The utility model aims to solve the defects in the prior art, and provides an unmanned aerial vehicle-mounted charging safety device.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides an unmanned aerial vehicle carries and fills ability safeties, includes the fuselage, fuselage downside middle part fixedly connected with connecting block, the inside left and right sides of connecting block all is provided with the draw-in groove, connecting block middle part sliding connection has the connector, the inside one side that all has the fixture block through spring coupling of connector left and right sides, fixture block opposite side lower part fixedly connected with presses the pole, fixture block opposite side upper portion sliding connection is inside the draw-in groove, the inside sliding connection of connector has and fills can the plug, it can the line to fill ability plug bottom fixedly connected with.
As a further description of the above technical solution:
the two sides of the bottom of the machine body are respectively and rotatably connected with a supporting rod, one end, far away from the machine body, of the supporting rods is fixedly connected with a bottom frame, and the middle part of the upper side of each supporting rod is connected with the bottom of the machine body through a pneumatic spring rod.
As a further description of the above technical solution:
the inner side of the underframe is rotationally connected with a floating block, and the other side of the floating block is fixedly connected with a cross rod.
As a further description of the above technical solution:
connecting rods are arranged on the front side and the rear side of the floating block, and are connected with the cross rod and the underframe.
As a further description of the above technical solution:
the middle part of the chassis is provided with an auxiliary rod, and the middle part of the auxiliary rod is connected with the main rod in a sliding way.
As a further description of the above technical solution:
the main rod is connected with the auxiliary rod through a pressure spring.
As a further description of the above technical solution:
the inner top of the main rod is fixedly connected with an electromagnet, the top of the auxiliary rod is fixedly connected with a metal block, and the electromagnet and the metal block are attracted.
The utility model has the following beneficial effects:
according to the unmanned aerial vehicle energy charging device, the accessory is connected with the energy charging plug through the connection block, the connector, the clamping groove, the clamping block and the pressing rod, so that the energy charging interface of the unmanned aerial vehicle body is damaged when the accessory falls accidentally in the repeated plugging or unmanned aerial vehicle flight energy charging process, the unmanned aerial vehicle cannot be normally used, and the maintenance cost of the unmanned aerial vehicle is increased.
Drawings
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle-mounted charging safety device according to the present utility model;
fig. 2 is a schematic diagram of a connection block structure of an unmanned aerial vehicle-mounted charging safety device according to the present utility model;
fig. 3 is a schematic diagram of a connector structure of an unmanned aerial vehicle-mounted charging safety device according to the present utility model;
fig. 4 is a schematic diagram of a floating block structure of an unmanned aerial vehicle-mounted energy charging safety device according to the present utility model;
fig. 5 is a schematic diagram of a compression spring structure of an unmanned aerial vehicle-mounted energy charging safety device.
Legend description:
1. a body; 2. a floating block; 3. a connecting block; 4. an energy charging line; 5. a connector; 6. a chassis; 7. a clamping groove; 8. a clamping block; 9. pressing a pressing rod; 10. an energy charging plug; 11. a spring; 12. a pneumatic spring rod; 13. a main rod; 14. a support rod; 15. a cross bar; 16. a connecting rod; 17. an electromagnet; 18. a metal block; 19. a pressure spring; 20. and a secondary rod.
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. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, one embodiment provided by the present utility model is: the utility model provides an unmanned aerial vehicle machine carries and fills ability safeties, including fuselage 1, fuselage 1 downside middle part fixedly connected with connecting block 3, the inside left and right sides of connecting block 3 all is provided with draw-in groove 7, connecting block 3 middle part sliding connection has connector 5, the inside one side that all is connected with fixture block 8 through spring 11 in the connector 5 left and right sides, fixture block 8 opposite side lower part fixedly connected with presses pole 9, fixture block 8 opposite side upper portion sliding connection is inside draw-in groove 7, the inside sliding connection of connector 5 has and fills ability plug 10, fill ability plug 10 bottom fixedly connected with and fill ability line 4, insert the connecting block 3 and fill ability socket on the machine, use the screw to fix connecting block 3 at fuselage 1, press pressing pole 9 after fixing, insert inside connecting block 8 income connector 5, loosen pressing pole 9 again, it is fixed to push into the draw-in groove 7 with fixture block 8 protruding part through spring 11 production elasticity, it can use to fill ability plug 10 to insert connector 5 at last.
The utility model provides a fuselage 1 bottom both sides all rotate and are connected with bracing piece 14, the one end fixedly connected with chassis 6 of fuselage 1 is kept away from to bracing piece 14, bracing piece 14 upside middle part is connected with fuselage 1 bottom through pneumatic spring bar 12, chassis 6 inboard rotates and is connected with floating block 2, the opposite side fixedly connected with horizontal pole 15 of floating block 2, both sides all are provided with connecting rod 16 around the floating block 2, horizontal pole 15 and chassis 6 are connected to connecting rod 16, chassis 6 middle part is provided with auxiliary pole 20, auxiliary pole 20 middle part sliding connection mobile jib 13, mobile jib 13 and auxiliary pole 20 inside are connected through pressure spring 19, top fixedly connected with electro-magnet 17 in the mobile jib 13, auxiliary pole 20 top fixedly connected with metal piece 18, chassis 6 contacts the ground after, press pneumatic spring bar 12 shrink, thereby make bracing piece 14 rotate, unload the power to the power that receives, thereby make fuselage 1 drop more steadily, prevent unmanned aerial vehicle's normal use, when unmanned aerial vehicle's outage, thereby make electro-magnet 17 weaken the suction of metal piece 18, the pressure spring 19, thereby, lead to the pressure spring 19 to stretch out from the auxiliary pole 20, thereby pull down from the main pole 20, the speed of the landing from the external side of the fuselage 2, the external force of the thrust spring bar 17, the thrust piece 18 is increased, the speed of the landing from the external force of the main pole 20, the thrust spring bar is reduced, and the bottom of the fuselage 1 is more stable.
Working principle: when unmanned aerial vehicle on-vehicle can be used, firstly, insert the connecting block 3 and fill can the socket with the machine, use the screw to fix connecting block 3 at fuselage 1, press the depression bar 9 after fixing, with the inside back of fixture block 8 income connector 5, insert the connecting block 3 inside with the connector 5, loosen the depression bar 9 again, produce elasticity through spring 11 and push into the draw-in groove 7 with fixture block 8 protruding part and fix, can fill can the use with inserting the connector 5 with filling can plug 10 at last, when fuselage 1 descends, after chassis 6 contacted ground, press pneumatic spring bar 12 shrink, thereby make bracing piece 14 rotate, unload the power to the power that receives, thereby make fuselage 1 descend more steadily, prevent unmanned aerial vehicle and the damage of the equipment that carries thereof, guarantee unmanned aerial vehicle's normal use, when unmanned aerial vehicle cuts off the power supply, thereby, make electromagnet 17 weaken the suction of metal piece 18, the unable pull 19, lead to the pressure spring 19 to stretch out, thereby drive auxiliary rod 20 stretch out from mobile jib 13, with the external push out the sub-rod 2 and the horizontal pole 15, the falling speed of the pressure spring 1 of the bottom of fuselage is slowed down.
Finally, it should be noted that: the foregoing description is only illustrative of the preferred embodiments of the present utility model, and although the present utility model has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present utility model.
Claims (7)
1. Unmanned aerial vehicle machine carries and fills ability safeties, including fuselage (1), its characterized in that: fuselage (1) downside middle part fixedly connected with connecting block (3), connecting block (3) inside left and right sides all is provided with draw-in groove (7), connecting block (3) middle part sliding connection has connector (5), connecting block (5) inside all is connected with one side of fixture block (8) through spring (11) in the left and right sides, fixture block (8) opposite side lower part fixedly connected with presses pole (9), fixture block (8) opposite side upper portion sliding connection is inside draw-in groove (7), inside sliding connection of connector (5) has and fills can plug (10), fill can plug (10) bottom fixedly connected with and fill can line (4).
2. The unmanned aerial vehicle on-board charging safety device according to claim 1, wherein: the novel air conditioner is characterized in that support rods (14) are rotatably connected to two sides of the bottom of the machine body (1), one end, far away from the machine body (1), of each support rod (14) is fixedly connected with an underframe (6), and the middle part of the upper side of each support rod (14) is connected with the bottom of the machine body (1) through a pneumatic spring rod (12).
3. The unmanned aerial vehicle on-board charging safety device according to claim 2, wherein: the inner side of the underframe (6) is rotationally connected with a floating block (2), and the other side of the floating block (2) is fixedly connected with a cross rod (15).
4. A unmanned aerial vehicle on-board charging safety device according to claim 3, wherein: connecting rods (16) are arranged on the front side and the rear side of the floating block (2), and the connecting rods (16) are connected with the cross rod (15) and the underframe (6).
5. The unmanned aerial vehicle on-board charging safety device according to claim 2, wherein: an auxiliary rod (20) is arranged in the middle of the underframe (6), and the middle of the auxiliary rod (20) is connected with the main rod (13) in a sliding manner.
6. The unmanned aerial vehicle on-board charging safety device according to claim 5, wherein: the main rod (13) is connected with the auxiliary rod (20) through a pressure spring (19).
7. The unmanned aerial vehicle on-board charging safety device according to claim 5, wherein: the top fixedly connected with electro-magnet (17) in mobile jib (13), auxiliary rod (20) top fixedly connected with metal piece (18), electro-magnet (17) and metal piece (18) attract mutually.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321269771.1U CN219770177U (en) | 2023-05-24 | 2023-05-24 | Unmanned aerial vehicle machine carries and fills ability safety device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321269771.1U CN219770177U (en) | 2023-05-24 | 2023-05-24 | Unmanned aerial vehicle machine carries and fills ability safety device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219770177U true CN219770177U (en) | 2023-09-29 |
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ID=88107355
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321269771.1U Active CN219770177U (en) | 2023-05-24 | 2023-05-24 | Unmanned aerial vehicle machine carries and fills ability safety device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219770177U (en) |
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2023
- 2023-05-24 CN CN202321269771.1U patent/CN219770177U/en active Active
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