CN218506137U - Unmanned aerial vehicle landing gear - Google Patents
Unmanned aerial vehicle landing gear Download PDFInfo
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- CN218506137U CN218506137U CN202223129449.7U CN202223129449U CN218506137U CN 218506137 U CN218506137 U CN 218506137U CN 202223129449 U CN202223129449 U CN 202223129449U CN 218506137 U CN218506137 U CN 218506137U
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- aerial vehicle
- unmanned aerial
- buffer
- sliding
- sliding sleeve
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Abstract
The utility model provides an unmanned aerial vehicle landing gear, it belongs to the unmanned aerial vehicle field, and it includes: a support base; the electromagnetic unmanned aerial vehicle comprises a buffer plate, wherein an electromagnet is arranged on the buffer plate, an unmanned aerial vehicle is arranged on the electromagnet, a bracket is arranged at the bottom of the unmanned aerial vehicle, and a magnetic absorption layer is wrapped at the bottom of the bracket; the buffer assembly comprises a positioning block fixed on the supporting base, a sliding sleeve is connected to the guide rod in a sliding mode, a sliding block fixedly connected with the sliding sleeve is sleeved on the sliding sleeve, an elastic buffer piece is installed between the sliding sleeve and the positioning block, and a connecting rod is connected between the sliding block and the buffer plate in a hinged mode. The utility model discloses well unmanned aerial vehicle falls on the buffer board back as an organic whole with the buffer board, can guarantee the stability that unmanned aerial vehicle fell on the buffer board, can not have the unstable condition of turning on one's side, utilizes elastic buffer to realize the buffering to slider and sliding sleeve, and then realizes the protection to unmanned aerial vehicle to buffer board and unmanned aerial vehicle's buffering.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle landing gear.
Background
The pilotless plane is called unmanned plane for short, and is a pilotless plane controlled by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is a general name of an unmanned aerial vehicle, and the unmanned aerial vehicle is not provided with a cockpit on the vehicle, but is provided with an autopilot, a program control device and other equipment.
When the existing unmanned aerial vehicle rises and falls, the buffering performance is poor, and the existing unmanned aerial vehicle is easily damaged due to overlarge collision force in the rising and falling process, so that the service life of the unmanned aerial vehicle is influenced; secondly, the existing unmanned aerial vehicle landing gear is not provided with a positioning device matched with an unmanned aerial vehicle, so that the unmanned aerial vehicle can not stably turn on one side, and the stability of the unmanned aerial vehicle can be ensured if the unmanned aerial vehicle is limited and cannot move after falling on the landing gear; an unmanned aircraft landing gear as in CN202121391096.0 lacking a locating device for the unmanned aircraft when it falls.
SUMMERY OF THE UTILITY MODEL
To the not enough that exists among the prior art, the utility model provides an unmanned aerial vehicle landing gear.
An embodiment of the utility model provides an unmanned aerial vehicle landing gear, include:
a support base;
the electromagnetic unmanned aerial vehicle comprises a buffer plate, wherein an electromagnet is arranged on the buffer plate, an unmanned aerial vehicle is arranged on the electromagnet, a bracket is arranged at the bottom of the unmanned aerial vehicle, and a magnetic absorption layer is wrapped at the bottom of the bracket;
the buffer assembly comprises a positioning block fixed on the supporting base, a guide rod is fixedly connected to the positioning block, a sliding sleeve is connected to the guide rod in a sliding mode, a sliding block fixedly connected to the sliding sleeve is sleeved on the sliding sleeve, an elastic buffer piece is installed between the sliding sleeve and the positioning block, and a connecting rod is connected between the sliding block and the buffer plate in a hinged mode.
Furthermore, the bottom of the supporting base is provided with an anti-slip mat, and the bottom of the anti-slip mat is provided with anti-slip lines.
Further, a power supply is installed on the supporting base and connected with the electromagnet through an electric wire, and a switch is installed on the power supply.
Furthermore, elastic buffer is the spring, the both ends of spring respectively with locating piece and sliding sleeve fixed connection, the spring housing is not supported the setting in the outside of guide bar.
Furthermore, the slider is the rectangle piece, the slider slides with the upper end of supporting the base and offsets.
Furthermore, the bottom of the connecting rod is hinged to the upper end of the sliding block, and the upper end of the connecting rod is hinged to the upper end of the buffer plate.
Compared with the prior art, the utility model discloses following beneficial effect has:
the utility model discloses well unmanned aerial vehicle falls on the buffer board back as an organic whole with the buffer board, can guarantee the stability that unmanned aerial vehicle fell on the buffer board, can not have the unstable condition of turning on one's side, utilizes elastic buffer to realize the buffering to slider and sliding sleeve, and then realizes the protection to unmanned aerial vehicle to buffer board and unmanned aerial vehicle's buffering.
Drawings
Fig. 1 is a top view of an unmanned aircraft landing gear according to an embodiment of the present invention.
Fig. 2 is a side view of a support base in an unmanned landing gear of an embodiment of the present invention.
In the above drawings: 1 supports base, 2 unmanned aerial vehicle, 3 supports, 4 buffer boards, 5 magnetism suction layer, 6 power, 7 electric wires, 8 switches, 9 locating pieces, 10 guide bars, 11 connecting rods, 12 sliding sleeves, 13 elastic buffer spare, 14 slipmats, 15 sliders, 16 electro-magnets.
Detailed Description
The technical solution of the present invention will be further explained with reference to the accompanying drawings and embodiments.
As shown in fig. 1-2, an embodiment of the present invention provides an unmanned aerial vehicle landing gear, including:
a support base 1; the bottom of the supporting base 1 is provided with the non-slip mat 14, the bottom of the non-slip mat 14 is provided with non-slip lines, and the non-slip mat 14 is made of rubber materials, so that the supporting base 1 can be stably supported;
the buffer plate 4 is provided with an electromagnet 16, the support base 1 is provided with a power supply 6, the power supply 6 is connected with the electromagnet 16 through an electric wire 7, and the power supply 6 is provided with a switch 8 which can control the electromagnet 16 to be powered on or off; the electromagnet 16 is provided with the unmanned aerial vehicle 2, the support 3 is installed at the bottom of the unmanned aerial vehicle 2, the magnetic attraction layer 5 is wrapped at the bottom of the support 3, and the magnetic attraction layer 5 is non-magnetic, so that the influence on the unmanned aerial vehicle 2 can be avoided, and the magnetic attraction layer 5 can be an iron sheet sprayed with protective paint;
the buffer assembly comprises a positioning block 9 fixed on the support base 1, a guide rod 10 is fixedly connected on the positioning block 9, a sliding sleeve 12 is slidably connected on the guide rod 10, a sliding block 15 which is fixedly connected is sleeved on the sliding sleeve 12, the sliding block 15 is a rectangular block, and the sliding block 15 is slidably abutted against the upper end of the support base 1; install elastic buffer 13 between sliding sleeve 12 and the locating piece 9, elastic buffer 13 is the spring, the both ends of spring respectively with locating piece 9 and sliding sleeve 12 fixed connection, the spring housing does not set up in the outside of guide bar 10 counterbalance, the articulated connecting rod 11 that is connected with between slider 15 and the buffer board 4, the articulated connection in upper end with slider 15 of bottom of connecting rod 11, the articulated connection in upper end with the buffer board 4 of connecting rod 11.
The utility model discloses a detailed working process as follows:
1. when the unmanned aerial vehicle is used, the unmanned aerial vehicle 2 is placed on the buffer board 4, and the unmanned aerial vehicle 2 can take off by remote control (the electromagnet 16 is in a power-off state at the moment);
2. when the unmanned aerial vehicle 2 falls down, the switch 8 is pressed, the power supply 6 and the electric wire 7 are used for electrifying the electromagnet 16, the upper end surface of the electromagnet 16 is magnetic, and when the unmanned aerial vehicle 2 falls down, the magnetic absorption layer 5 on the support 3 at the bottom of the unmanned aerial vehicle 2 is abutted against and attracted with the electromagnet 16, so that the stability of the unmanned aerial vehicle 2 falling on the buffer board 4 can be ensured, and the unstable rollover condition can not occur;
3. unmanned aerial vehicle 2 falls on buffer board 4 back as an organic whole with buffer board 4, and its pressure that falls drives buffer board 4 and moves down, and buffer board 4 moves down drive connecting rod 11 and moves, and connecting rod 11 drive slider 15 and sliding sleeve 12 move, and springiness cushioning spare 13 this moment is compressed, realizes the buffering to slider 15 and sliding sleeve 12, and then realizes the buffering to buffer board 4 and unmanned aerial vehicle 2.
Finally, it is noted that the above embodiments are only used for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solutions of the present invention can be modified or replaced by equivalents without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the scope of the claims of the present invention.
Claims (6)
1. An unmanned aerial vehicle landing gear, its characterized in that includes:
a support base (1);
the device comprises a buffer plate (4), wherein an electromagnet (16) is arranged on the buffer plate (4), an unmanned aerial vehicle (2) is arranged on the electromagnet (16), a support (3) is installed at the bottom of the unmanned aerial vehicle (2), and a magnetic absorption layer (5) is wrapped at the bottom of the support (3);
the buffer assembly comprises a positioning block (9) fixed on a supporting base (1), a guide rod (10) fixedly connected with the positioning block (9), a sliding sleeve (12) connected with the guide rod (10) in a sliding manner, a sliding block (15) fixedly connected with the sliding sleeve (12) in a sliding manner, an elastic buffer part (13) installed between the sliding sleeve (12) and the positioning block (9), and a connecting rod (11) hinged between the sliding block (15) and the buffer plate (4).
2. An unmanned landing gear, according to claim 1, wherein:
the bottom of the supporting base (1) is provided with an anti-slip pad (14), and the bottom of the anti-slip pad (14) is provided with anti-slip lines.
3. An unmanned landing gear, according to claim 1, wherein:
support and install on base (1) power (6), power (6) are connected with electro-magnet (16) through electric wire (7), install switch (8) on power (6).
4. An unmanned aircraft landing gear according to claim 1, wherein:
the elastic buffer piece (13) is a spring, two ends of the spring are fixedly connected with the positioning block (9) and the sliding sleeve (12) respectively, and the spring sleeve is arranged outside the guide rod (10) in a non-abutting mode.
5. An unmanned aircraft landing gear according to claim 1, wherein:
the sliding block (15) is a rectangular block, and the sliding block (15) is in sliding and abutting contact with the upper end of the supporting base (1).
6. An unmanned landing gear, according to claim 1, wherein:
the bottom of the connecting rod (11) is hinged to the upper end of the sliding block (15), and the upper end of the connecting rod (11) is hinged to the upper end of the buffer plate (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223129449.7U CN218506137U (en) | 2022-11-24 | 2022-11-24 | Unmanned aerial vehicle landing gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223129449.7U CN218506137U (en) | 2022-11-24 | 2022-11-24 | Unmanned aerial vehicle landing gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218506137U true CN218506137U (en) | 2023-02-21 |
Family
ID=85220232
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223129449.7U Active CN218506137U (en) | 2022-11-24 | 2022-11-24 | Unmanned aerial vehicle landing gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218506137U (en) |
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2022
- 2022-11-24 CN CN202223129449.7U patent/CN218506137U/en active Active
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