一种无人机远程充能装置

Abstract

本实用新型涉及一种无人机远程充能装置，旨在解决当前环形磁铁与弧形磁铁易出现吸附不精准活距离较远无法实现的问题，导致导电机构与充电机构无法精准对接导通，进而无法对无人机本体进行有效充电的技术问题，包括：充能箱，所述充能箱的内腔中固定连接有支撑板，所述支撑板的中部开设有圆孔，所述支撑板的表面放置有无人机本体；充电机构，用于对停放状态的无人机本体进行无线充电，本实用新型通过居中限位机构可对停放在支撑板上的无人机本体进行多维度位置校准，无论无人机本体初始降落位置是否偏移，均能通过机械调整使其精准处于充电机构的对位中心，彻底避免传统磁铁吸附因距离偏差或角度偏移导致的充电失效，确保充电过程稳定导通。

Claims

1. A remote energy charging device for unmanned aerial vehicles, characterized in that, include: A charging box (1) has a support plate (4) fixedly connected in its inner cavity. A round hole (42) is opened in the middle of the support plate (4). The drone body (5) is placed on the surface of the support plate (4). A charging mechanism for wirelessly charging the drone body (5) in a parked state; A centering limiting mechanism is provided inside the charging box (1) to keep the drone body (5) which is parked on the surface of the support plate (4) in a charging state centered, so as to ensure that the drone body (5) is accurately aligned with the charging mechanism and to achieve limiting during the charging process.

2. The unmanned aerial vehicle remote energy charging device of claim 1, wherein, The charging mechanism includes: A push rod motor (44) is fixedly connected to the bottom of the inner cavity of the charging box (1); The primary coil (41) is fixedly connected to the telescopic end of the push rod motor (44) and placed in the round hole (42) in the middle of the support plate (4); The battery pack (51) is fixedly connected to the bottom middle of the drone body (5). A secondary coil (52) is installed at the bottom of the battery pack (51). The secondary coil (52) corresponds to the primary coil (41) in position and is adapted in size.

3. The unmanned aerial vehicle remote energy charging device of claim 1, wherein, The centering limiting mechanism includes: Two first slide grooves (26) are opened at both ends of the inner cavity of the charging box (1) above the support plate (4). The inner cavity of one of the first slide grooves (26) is rotatably connected to a first bidirectional lead screw (27) through a bearing. Two first sliders (28) are slidably connected in both of the first slide grooves (26), and the first sliders (28) are threaded on the outside of the first bidirectional lead screw (27). Two inverted U-shaped push plates (29) are fixedly connected between the two first sliders (28) on both sides; The first drive motor (21) is installed on one side of the charging box (1), and the drive end of the first drive motor (21) is connected to the first bidirectional lead screw (27) through a coupling. Two second slide grooves (22) are opened at the other two ends of the inner cavity of the charging box (1) above the support plate (4). The inner cavity of one of the second slide grooves (22) is rotatably connected to a second bidirectional lead screw (23) through a bearing. Two second sliders (24) are slidably connected in both of the second slide grooves (22), and the second sliders (24) are threaded on the outside of the second bidirectional lead screw (23). Two movable plates (25) are fixedly connected between the two second sliders (24) on both sides. Both movable plates (25) penetrate the bottom of the two inverted U-shaped push plates (29) and are perpendicular to each other. The second drive motor (2) is installed on the other side of the charging box (1). The drive end of the second drive motor (2) is connected to the second bidirectional lead screw (23) through a coupling.

4. The unmanned aerial vehicle remote energy charging device of claim 3, wherein, The inner cavity of the charging box (1) has rectangular slots (34) above the two ends of the first sliding grooves (26). An exhaust pipe (37) and a collection pipe (35) are respectively installed in the two rectangular slots (34). Multiple jet nozzles (38) are equidistantly connected to the end of the exhaust pipe (37) near the end of the collection pipe (35), and the multiple jet nozzles (38) are arranged in a fan shape. The end of the collection pipe (35) near the end of the exhaust pipe (37) has a... An air inlet (36) is provided. A filter cartridge (31) that drives the filter element and a blower box (32) that drives the blower are installed at one end of the outer side of the charging box (1). The filter element is installed in the inner cavity of the filter cartridge (31), and the blower is installed in the inner cavity of the blower box (32). A conduit is connected between the filter cartridge (31) and the blower box (32). A connecting pipe (3) is connected between the collecting pipe (35) and the filter cartridge (31) and between the blower box (32) and the air outlet pipe (37).

5. The unmanned aerial vehicle remote energy charging device of claim 1 or 3, wherein, The charging box (1) has a third sliding groove (13) on both sides of its surface. The inner cavity of one of the third sliding grooves (13) is rotatably connected to a third bidirectional lead screw (15) via a bearing. The top opening of the charging box (1) has a box cover (11) on both sides. The bottom sides of the two box covers (11) are fixedly connected to a third slider (14). The third slider (14) is threaded onto the outside of the third bidirectional lead screw (15). The charging box (1) has a third drive motor (12) installed on one side near the first drive motor (21). The drive end of the third drive motor (12) is connected to the third bidirectional lead screw (15) via a coupling.

6. The remote charging device for unmanned aerial vehicles as described in claim 1, characterized in that, The charging box (1) is equipped with a wireless receiver (43) and a controller (45) at the bottom of its inner cavity, which are used to receive terminal operation commands and realize remote charging of the UAV body (5).

7. The unmanned aerial vehicle remote recharging device of claim 4, wherein, Both of the connecting pipes (3) are detachably connected to the filter cartridge (31) and the blower box (32) respectively via flanges (33), and the filter cartridge (31) and the blower box (32) are detachably connected via flanges (33).

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