Unmanned aerial vehicle hangar with unmanned aerial vehicle centering function

Abstract

An unmanned aerial vehicle hangar with an unmanned aerial vehicle centering function comprises a supporting bracket, a placement panel is mounted above the supporting bracket, a control mainboard is mounted on one side of the back of the placement panel, an unmanned aerial vehicle take-off and landing bracket is arranged above the placement panel, and a first centering mechanism and a second centering mechanism are mounted on the supporting bracket; the first centering mechanism and the second centering mechanism are arranged on the adjacent support plates of the supporting support in an included angle of 90 degrees, and a wire harness protection chain is installed on the inner wall of the supporting support. The unmanned aerial vehicle take-off and landing device has the beneficial effects that by additionally arranging the first centering mechanism and the second centering mechanism, the unmanned aerial vehicle and the unmanned aerial vehicle take-off and landing bracket can be quickly centered, so that the unmanned aerial vehicle can take off and land conveniently, and the charging connector is arranged, so that the unmanned aerial vehicle can be charged after being centered, and the charging efficiency is improved. The first centering mechanism and the second centering mechanism are each provided with a single motor, and therefore it is guaranteed that energy consumption of the equipment is reduced while the centering stability of the equipment is guaranteed.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle hangars, and in particular to an unmanned aerial vehicle hangar with a unmanned aerial vehicle centering function. Background Art

[0002] As an important type of aircraft, drones have broad application prospects in both military and civilian fields. They are aircraft that can fly autonomously or remotely without human control. They are usually controlled by remote control or autonomous control systems and can perform tasks in a variety of environments. Drone hangars are special parking places designed specifically for drones. Drone hangars greatly improve the operating efficiency and endurance of drones. At the same time, hangars also have functions such as emergency communication network relays, which can quickly establish a reliable communication network in remote areas or when disasters occur, providing emergency communication support for trapped people.

[0003] Although the current drone hangars can park drones and charge drones, they are unable to center the drones and the landing and take-off brackets, which in turn affects the next takeoff and parking of the drones. Workers are still required to manually center the drones and the landing and take-off brackets, which increases the workload of the workers to a certain extent. Summary of the invention

[0004] The purpose of the present invention is to provide a drone hangar with a drone centering function in response to the shortcomings and defects in the prior art. The device can quickly center its drone and drone landing bracket by adding a first centering mechanism and a second centering mechanism, thereby facilitating the drone to take off and land. A charging connector is provided so that the drone can be charged after being centered. The first centering mechanism and the second centering mechanism are both provided with only a single motor, thereby ensuring that the energy consumption of the equipment is reduced while ensuring the stability of its centering.

[0005] To achieve the above-mentioned purpose, the present invention adopts the following technical scheme: a drone hangar with a drone centering function, which includes a supporting bracket 7, a placement panel 1 is installed above the supporting bracket 7, a control main board 8 is installed on one side of the back of the placement panel 1, and a drone take-off and landing bracket 3 is provided above the placement panel 1, a first centering mechanism 4 and a second centering mechanism 6 are installed on the supporting bracket 7, the first centering mechanism 4 and the second centering mechanism 6 are respectively arranged on the bracket plates adjacent to the supporting bracket 7 at an angle of 90°, and a wiring harness protection chain 9 is installed on the inner wall of the supporting bracket 7, and the control main board 8 is electrically connected to the first centering mechanism 4 through the wiring harness protection chain 9.

[0006] Furthermore, side protection frames 5 for protecting the support bracket 7 are installed on the tops of the four ends of the support bracket 7.

[0007] Furthermore, a handle 2 is installed on one side of the top of the support bracket 7 to facilitate the staff to carry the device.

[0008] Further, the first centering mechanism 4 includes a first power motor 412, a first motor seat 413 is installed on one side of the first power motor 412, and the first power motor 412 is installed on the inner wall of the support bracket 7 through the first motor seat 413, a first motor shaft column 411 is installed on the output end of the first power motor 412, and first driving guide wheels 410 are installed at both ends of the first motor shaft column 411, and the first driving guide wheel 410 is sleeved with a first transmission belt 49, and the other end of the first transmission belt 49 is sleeved on the first driven guide wheel 44, and the first guide rail 46 and the first guide rail 46 are installed on the support bracket 7. The first driven guide wheel 44 is mounted on the outer end of the support bracket 7 through the first driven guide wheel 44, the first transmission belt 49 is engaged with a first belt connecting plate 45 and a second belt connecting plate 47, the inner sides of the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 are slidably connected to the first guide rail 46, and the top ends of the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 are fixedly connected with a first push plate connecting frame 48, the first push plate connecting frame 48 is installed with a first centering push plate 41, the first centering push plate 41 is installed with a charging connector 42, and the charging connector 42 is electrically connected to the control main board 8.

[0009] Furthermore, there are two No. 1 belt connecting plates 45 and No. 2 belt connecting plates 47, and the No. 1 belt connecting plates 45 and the No. 2 belt connecting plates 47 are symmetrically arranged at both ends of the first motor shaft column 411. The tops of the two No. 1 belt connecting plates 45 and the two No. 2 belt connecting plates 47 are both installed with a first push plate connecting frame 48. The No. 1 belt connecting plate 45 is engaged with the top of one side of the first transmission belt 49, and the No. 2 belt connecting plate 47 is engaged with the bottom of the other side of the first transmission belt 49.

[0010] Furthermore, the second centering mechanism 6 includes a second motor seat 612, which is mounted on the supporting bracket 7, and the outer end of the supporting bracket 7 is equipped with a second guide rail 69 and a second guide wheel mounting seat 611, the second motor seat 612 is equipped with a second power motor 61, the output end of the second power motor 61 is mechanically connected to a second motor shaft column 62, both ends of the second motor shaft column 62 are equipped with second driving guide wheels 63, the two second driving guide wheels 63 are both sleeved with a second transmission belt 64, the other end of the second transmission belt 64 is sleeved on the second driven guide wheel 610, and the second driven guide wheel 610 is mounted on the second guide wheel mounting seat 611, and the second transmission belt 64 is provided with a third belt connecting plate 67 and a fourth belt connecting plate 68 on both sides, and a second push plate connecting frame 66 is installed on the top of the third belt connecting plate 67 and the fourth belt connecting plate 68, and a second centering push plate 65 is installed on the top of the second push plate connecting frame 66.

[0011] Furthermore, there are two No. 3 belt connecting plates 67 and two No. 4 belt connecting plates 68 , and the two No. 3 belt connecting plates 67 are arranged above one side of the second transmission belt 64 , and the two No. 4 belt connecting plates 68 are arranged below the other side of the second transmission belt 64 .

[0012] Furthermore, the second return push plates 65 and the first return push plates 41 are each provided with two groups, and the two groups of second return push plates 65 are parallel to each other, and the two groups of first return push plates 41 are parallel to each other. The two groups of second return push plates 65 and the two groups of first return push plates 41 are cross-arranged at 90° on the placement panel 1, and the second return push plates 65 are located below the first return push plates 41.

[0013] Furthermore, a plurality of ventilation holes 101 are provided on the placement panel 1 .

[0014] Furthermore, the UAV landing bracket 3 includes a rear support seat 34, which is provided with four groups, and a connecting cross bar 33 is provided between two adjacent groups of rear support seats 34, and a positioning buckle rod 31 is installed at the upper end of each group of rear support seats 34, and a movable ball 32 is provided at the lower end of each group of rear support seats 34.

[0015] After adopting the above technical scheme, the beneficial effect of the present invention is as follows: by adding a first centering mechanism and a second centering mechanism, the device can quickly center its UAV and the UAV landing and take-off bracket, thereby facilitating the take-off and landing operations of the UAV, and is provided with a charging connector, so that after the UAV is centered, the UAV can be charged. The first centering mechanism and the second centering mechanism are both provided with only a single motor, thereby ensuring that the energy consumption of the equipment is reduced while ensuring the stability of its centering. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative labor.

[0017] Figure 1 It is a structural schematic diagram of the present invention,

[0018] Figure 2 is a schematic diagram of the bottom structure of the present invention,

[0019] Figure 3 It is a structural schematic diagram of the UAV take-off and landing bracket in the present invention.

[0020] Figure 4 It is a schematic diagram of the bottom structure of the UAV take-off and landing bracket in the present invention.

[0021] Figure 5 It is a structural schematic diagram of the first centering mechanism in the present invention.

[0022] Figure 6 It is a schematic diagram of the bottom structure of the first centering mechanism in the present invention.

[0023] Figure 7 yes Figure 5 Enlarged structural diagram at A in the middle.

[0024] Figure 8 It is a structural schematic diagram of the second centering mechanism in the present invention.

[0025] Fig. 9 It is a schematic diagram of the bottom structure of the second centering mechanism in the present invention.

[0026] Fig.10 yes Figure 8 Enlarged structural diagram at B in the middle.

[0027] Description of the accompanying drawings: placement panel 1, handle 2, drone landing bracket 3, first centering mechanism 4, side protection frame 5, second centering mechanism 6, support bracket 7, control main board 8, wire harness protection chain 9, first centering push plate 41, charging connector 42, first guide wheel mounting seat 43, first driven guide wheel 44, No. 1 belt connecting plate 45, first guide rail 46, No. 2 belt connecting plate 47, first push plate connecting frame 48, first transmission belt 49, first active guide wheel 410, first motor shaft column 411 , the first power motor 412, the first motor seat 413, the second power motor 61, the second motor shaft 62, the second driving guide wheel 63, the second transmission belt 64, the second centering push plate 65, the second push plate connecting frame 66, the third belt connecting plate 67, the fourth belt connecting plate 68, the second guide rail 69, the second driven guide wheel 610, the second guide wheel mounting seat 611, the second motor seat 612, the positioning buckle rod 31, the front support seat 32, the connecting cross bar 33, the rear support seat 34, and the ventilation vent 101. DETAILED DESCRIPTION

[0028] See also Figure 1-Figure 10 As shown, the technical solution adopted in this specific embodiment is: it includes a supporting bracket 7, a placement panel 1 is installed above the supporting bracket 7, a control main board 8 is installed on one side of the back of the placement panel 1, and a UAV landing and take-off bracket 3 is provided above the placement panel 1, and a first centering mechanism 4 and a second centering mechanism 6 are installed on the supporting bracket 7, and the first centering mechanism 4 and the second centering mechanism 6 are respectively arranged on the bracket plates adjacent to the supporting bracket 7 at an angle of 90°, and a wiring harness protection chain 9 is installed on the inner wall of the supporting bracket 7, and the control main board 8 is electrically connected to the first centering mechanism 4 through the wiring harness protection chain 9.

[0029] More specifically, the tops of the four ends of the support bracket 7 are equipped with side protection frames 5 for protecting the support bracket 7. The side protection frames 5 are installed on the four ends of the support bracket 7, and the side protection frames 5 can protect the support bracket 7 to the greatest extent, reducing the damage and deformation of the support bracket 7 caused by collision.

[0030] More specifically, a handle 2 is installed on one side of the top of the support bracket 7 to facilitate the staff to carry the device.

[0031] More specifically, the first centering mechanism 4 includes a first power motor 412, a first motor seat 413 is installed on one side of the first power motor 412, and the first power motor 412 is installed on the inner wall of the support bracket 7 through the first motor seat 413, a first motor shaft column 411 is installed on the output end of the first power motor 412, and both ends of the first motor shaft column 411 are installed with a first driving guide wheel 410, the first driving guide wheel 410 is sleeved with a first transmission belt 49, and the other end of the first transmission belt 49 is sleeved on the first driven guide wheel 44, and the first guide rail 46 and the first guide rail 46 are installed on the support bracket 7. The first driven guide wheel 44 is mounted on the outer end of the support bracket 7 through the first driven guide wheel 44, and the first transmission belt 49 is engaged with a first belt connecting plate 45 and a second belt connecting plate 47, the inner sides of the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 are slidably connected to the first guide rail 46, and the top ends of the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 are fixedly connected with a first push plate connecting frame 48, the first push plate connecting frame 48 is installed with a first centering push plate 41, the first centering push plate 41 is installed with a charging connector 42, and the charging connector 42 is electrically connected to the control main board 8. When it is necessary to perform the centering operation of the UAV and the UAV landing bracket 3, the first power motor 412 will drive the first motor shaft column 411 to rotate, thereby driving the first active guide wheels 410 on both sides through the first motor shaft column 411, and utilizing the first active guide wheel 410 to drive its first transmission belt 49, so that the first transmission belt 49 can drive its No. 1 belt connecting plate 45 and No. 2 belt connecting plate 47 to move under the limit of the first guide rail 46, so that the No. 1 belt connecting plate 45 and No. 2 belt connecting plate 47 drive the first centering push plate 41 to move, thereby completing the centering operation of the UAV and the UAV landing bracket 3, wherein the first driven guide wheel 44 can ensure the operating stability of its first transmission belt 49.

[0032] To be more specific, there are two No. 1 belt connecting plates 45 and two No. 2 belt connecting plates 47, and the No. 1 belt connecting plates 45 and the No. 2 belt connecting plates 47 are symmetrically arranged at both ends of the first motor shaft column 411. The tops of the two No. 1 belt connecting plates 45 and the two No. 2 belt connecting plates 47 are installed with a first push plate connecting frame 48. The No. 1 belt connecting plate 45 is engaged with the upper side of one side of the first transmission belt 49, and the No. 2 belt connecting plate 47 is engaged with the lower side of the other side of the first transmission belt 49. By setting two No. 1 belt connecting plates 45 and two No. 2 belt connecting plates 47, it can be ensured that the two first centering push plates 41 can be subjected to force on both sides synchronously during the centering operation, thereby ensuring the stability of the first centering push plates 41. The No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 are respectively set at different positions of the first transmission belt 49, and the first transmission belt 49 can be used to drive the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 to run in opposite directions, thereby allowing the No. 1 belt connecting plate 45 and the No. 2 belt connecting plate 47 to complete the centering operation.

[0033] To be more specific, the second centering mechanism 6 includes a second motor seat 612, which is mounted on the supporting bracket 7, and the outer end of the supporting bracket 7 is mounted with a second guide rail 69 and a second guide wheel mounting seat 611, a second power motor 61 is mounted on the second motor seat 612, and the output end of the second power motor 61 is mechanically connected to a second motor shaft column 62, both ends of the second motor shaft column 62 are mounted with second driving guide wheels 63, the two second driving guide wheels 63 are both sleeved with a second transmission belt 64, the other end of the second transmission belt 64 is sleeved on the second driven guide wheel 610, and the second driven guide wheel 610 is mounted on the second guide wheel mounting seat 611, and a third belt connecting plate 67 and a fourth belt connecting plate 68 are respectively provided on both sides of the second transmission belt 64, a second push plate connecting frame 66 is installed on the top of the third belt connecting plate 67 and the fourth belt connecting plate 68, and a second centering push plate 65 is installed on the top of the second push plate connecting frame 66. When performing the centering operation of the UAV and the UAV landing bracket 3, its second power motor 61 will drive the second motor shaft column 62 to rotate, and drive the second active guide wheels 63 on both sides through the second motor shaft column 62, and then the second active guide wheel 63 drives the second transmission belt 64 to operate, and under the operation of the second transmission belt 64, the third belt connecting plate 67 and the fourth belt connecting plate 68 on both sides move. Under the action of the third belt connecting plate 67 and the fourth belt connecting plate 68, the second centering push plate 65 can push its UAV and the UAV landing bracket 3, and cooperate with the first centering push plate 41 to quickly complete the centering operation of the UAV and the UAV landing bracket 3.

[0034] More specifically, two No. 3 belt connection plates 67 and No. 4 belt connection plates 68 are provided, and the two No. 3 belt connection plates 67 are arranged above one side of the second transmission belt 64, and the two No. 4 belt connection plates 68 are arranged below the other side of the second transmission belt 64. The two No. 3 belt connection plates 67 and No. 4 belt connection plates 68 drive the two sets of second centering push plates 65, which can ensure the operation stability of the second centering push plates 65, and the No. 3 belt connection plates 67 and No. 4 belt connection plates 68 are respectively arranged at the upper and lower ends of both sides of the second transmission belt 64, so that when the second transmission belt 64 is running, it can ensure that the No. 3 belt connection plates 67 and the No. 4 belt connection plates 68 run in opposite directions, so as to better perform the centering operation.

[0035] More specifically, the second return-to-center push plates 65 and the first return-to-center push plates 41 are each provided with two groups, and the two groups of the second return-to-center push plates 65 are parallel to each other, and the two groups of the first return-to-center push plates 41 are parallel to each other, and the two groups of the second return-to-center push plates 65 and the two groups of the first return-to-center push plates 41 are arranged crosswise at 90° on the placement panel 1, and the second return-to-center push plates 65 are located below the first return-to-center push plates 41. The two groups of the second return-to-center push plates 65 and the two groups of the first return-to-center push plates 41 can perform multi-angle return-to-center operations on the drone and the drone landing bracket 3, and the second return-to-center push plates 65 are arranged below the first return-to-center push plates 41, so that the second return-to-center push plates 65 and the first return-to-center push plates 41 will not interfere with each other.

[0036] To be more specific, a plurality of ventilation holes 101 are provided on the placement panel 1 .

[0037] More specifically, the drone landing bracket 3 includes a rear support seat 34, which is provided with four groups, and a connecting cross bar 33 is provided between two adjacent groups of rear support seats 34, a positioning buckle rod 31 is installed at the upper end of each group of rear support seats 34, and a moving ball 32 is provided at the lower end of each group of rear support seats 34. The moving ball 32 can facilitate the movement of the drone landing bracket 3 on the placement panel 1.

[0038] The working principle of the present invention is as follows: when it is necessary to park the drone, the staff can use the device. When the drone is placed on the placement panel 1 with a certain offset, the staff can start the first centering mechanism 4 and the second centering mechanism 6, and push the first centering push plate 41 and the second centering push plate 65 to enable the drone to quickly perform the centering operation, ensuring that the drone is in the middle of the placement panel 1. The staff can use the drone landing bracket 3 to assist the drone in taking off and landing, and quickly complete the drone's take-off operation through the drone landing bracket 3. Since the drone will cause a certain offset movement to its drone landing bracket 3 when taking off, its first centering mechanism 4 and the second centering mechanism 6 can also quickly center its drone landing bracket 3, so that the drone landing bracket 3 can facilitate the drone to take off and land. After the drone is parked and placed, the staff can charge the drone through the charging connector 42. Among them, the staff can also fix the drone through the positioning buckle rod 31 to prevent the drone from unnecessary displacement when placed, thereby increasing the safety of the drone.

[0039] The above is only used to illustrate the technical solution of the present invention rather than to limit it. Other modifications or equivalent substitutions made to the technical solution of the present invention by ordinary technicians in this field should be included in the scope of the claims of the present invention as long as they do not depart from the spirit and scope of the technical solution of the present invention.

Claims

1. A drone hangar with a drone centering function, characterized in that: It comprises a support bracket (7), a placement panel (1) is installed above the support bracket (7), a control mainboard (8) is installed on one side of the back of the placement panel (1), and a UAV take-off and landing bracket (3) is arranged above the placement panel (1), a first centering mechanism (4) and a second centering mechanism (6) are installed on the support bracket (7), the first centering mechanism (4) and the second centering mechanism (6) are respectively arranged on bracket plates adjacent to the support bracket (7) at an angle of 90°, and a wire harness protection chain (9) is installed on the inner wall of the support bracket (7), and the control mainboard (8) is electrically connected to the first centering mechanism (4) through the wire harness protection chain (9).

2. The drone hangar with drone centering function according to claim 1, characterized in that: Side protection frames (5) for protecting the support bracket (7) are installed on the tops of the four ends of the support bracket (7).

3. The drone hangar with drone centering function according to claim 1, characterized in that: A handle (2) is installed on one side of the top of the support bracket (7) to facilitate workers to carry the device.

4. The drone hangar with drone centering function according to claim 1, characterized in that: The first centering mechanism (4) comprises a first power motor (412), a first motor seat (413) is installed on one side of the first power motor (412), and the first power motor (412) is installed on the inner wall of the support bracket (7) through the first motor seat (413), a first motor shaft column (411) is installed on the output end of the first power motor (412), both ends of the first motor shaft column (411) are installed with a first driving guide wheel (410), a first transmission belt (49) is sleeved on the first driving guide wheel (410), and the other end of the first transmission belt (49) is sleeved on the first driven guide wheel (44), and a first guide rail (46) and a first guide wheel mounting seat are installed on the support bracket (7). (43), and the first driven guide wheel (44) is installed on the outer end of the support bracket (7) through the first driven guide wheel (44), the first transmission belt (49) is engaged with a first belt connecting plate (45) and a second belt connecting plate (47), the inner sides of the first belt connecting plate (45) and the second belt connecting plate (47) are slidably connected to the first guide rail (46), and the top ends of the first belt connecting plate (45) and the second belt connecting plate (47) are fixedly connected with a first push plate connecting frame (48), the first push plate connecting frame (48) is installed with a first return push plate (41), the first return push plate (41) is installed with a charging connector (42), and the charging connector (42) is electrically connected to the control main board (8).

5. The drone hangar with drone centering function according to claim 1, characterized in that: The first belt connecting plate (45) and the second belt connecting plate (47) are each provided with two, and the first belt connecting plate (45) and the second belt connecting plate (47) are symmetrically arranged at the two ends of the first motor shaft column (411), and the tops of the two first belt connecting plates (45) and the two second belt connecting plates (47) are each installed with a first push plate connecting frame (48), the first belt connecting plate (45) is engaged with the upper side of one side of the first transmission belt (49), and the second belt connecting plate (47) is engaged with the lower side of the other side of the first transmission belt (49).

6. The drone hangar with drone centering function according to claim 1, characterized in that: The second centering mechanism (6) comprises a second motor seat (612), the second motor seat (612) is mounted on a support bracket (7), and a second guide rail (69) and a second guide wheel mounting seat (611) are mounted on the outer end of the support bracket (7), a second power motor (61) is mounted on the second motor seat (612), a second motor shaft column (62) is mechanically connected to the output end of the second power motor (61), second driving guide wheels (63) are mounted on both ends of the second motor shaft column (62), and the two second driving guide wheels (63) are mounted on the second power motor (61). A second transmission belt (64) is sleeved on each of the two belts, the other end of which is sleeved on a second driven guide wheel (610), which is mounted on a second guide wheel mounting seat (611). A third belt connecting plate (67) and a fourth belt connecting plate (68) are respectively provided on both sides of the second transmission belt (64), a second push plate connecting frame (66) is installed on the top of the third belt connecting plate (67) and the fourth belt connecting plate (68), and a second centering push plate (65) is installed on the top of the second push plate connecting frame (66).

7. The drone hangar with drone centering function according to claim 1, characterized in that: The number three belt connecting plate (67) and the number four belt connecting plate (68) are both provided with two, and the two number three belt connecting plates (67) are arranged above one side of the second transmission belt (64), and the two number four belt connecting plates (68) are arranged below the other side of the second transmission belt (64).

8. The drone hangar with drone centering function according to claim 1, characterized in that: The second return center push plates (65) and the first return center push plates (41) are each provided with two groups, and the two groups of second return center push plates (65) are parallel to each other, and the two groups of first return center push plates (41) are parallel to each other, and the two groups of second return center push plates (65) and the two groups of first return center push plates (41) are cross-arranged at 90 degrees on the placement panel (1), and the second return center push plates (65) are located below the first return center push plates (41).

9. The drone hangar with drone centering function according to claim 1, characterized in that: The placement panel (1) is provided with a plurality of ventilation holes (101).

10. The drone hangar with drone centering function according to claim 1, characterized in that: The unmanned aerial vehicle landing bracket (3) comprises a rear support seat (34), wherein the rear support seat (34) is provided in four groups, and a connecting cross bar (33) is provided between two adjacent groups of rear support seats (34), a positioning buckle rod (31) is installed at the upper end of each group of rear support seats (34), and a movable ball (32) is provided at the lower end of each group of rear support seats (34).

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