阅读说明：本技术 一种无人机机库 (Unmanned aerial vehicle hangar ) 是由 曹亚兵 韩兵 严凯 徐方甫 于 2021-08-09 设计创作，主要内容包括：本发明公开了一种无人机机库,该无人机机库包括框架、降落平台和驱动机构,框架沿其周向设置多个间隔设置的出入口,降落平台可活动地设在框架内,且降落平台为多个,多个降落平台与多个出入口一一对应设置,驱动机构设在框架上,驱动机构为多个,多个驱动机构与多个降落平台一一配合,驱动机构用于驱动降落平台沿上下方向及进出出入口的方向运动。该无人机机库能够容纳多个无人机且能够实现多个无人机的同时起降。(The invention discloses an unmanned aerial vehicle hangar which comprises a frame, a plurality of landing platforms and a driving mechanism, wherein the frame is provided with a plurality of entrances and exits arranged at intervals along the circumferential direction of the frame, the landing platforms are movably arranged in the frame and are arranged in a plurality of one-to-one correspondence with the entrances and exits, the driving mechanism is arranged on the frame, the driving mechanism is arranged in a plurality of driving mechanisms, the driving mechanisms are matched with the landing platforms one by one, and the driving mechanism is used for driving the landing platforms to move along the up-down direction and the direction of the entrances and exits. This unmanned aerial vehicle hangar can hold a plurality of unmanned aerial vehicles and can realize taking off and landing when a plurality of unmanned aerial vehicles.)

1. An unmanned aerial vehicle hangar, comprising:

the frame (1), the said frame (1) sets up the access & exit (11) that multiple intervals set up along its circumference;

the landing platforms (2) are movably arranged in the frame (1), the number of the landing platforms (2) is multiple, and the landing platforms (2) and the entrances and exits (11) are arranged in a one-to-one correspondence manner;

actuating mechanism (3), actuating mechanism (3) are established on frame (1), actuating mechanism (3) are a plurality of, and are a plurality of actuating mechanism (3) and a plurality of descending platform (2) cooperation one by one, actuating mechanism (3) are used for the drive descending platform (2) are along upper and lower direction and business turn over the direction motion of access & exit (11).

2. Unmanned hangar according to claim 1, wherein each of said drive mechanisms (3) comprises:

a first drive module (31), the first drive module (31) being provided on the frame (1);

the connecting frame (32) is connected with the power output end of the first driving module (31), and the connecting frame (32) can move in the vertical direction under the driving of the first driving module (31);

second drive module (33), second drive module (33) are established on link (32), the power take off end of second drive module (33) with it links to each other to descend platform (2), second drive module (33) are used for the drive descend platform (2) along the business turn over the direction motion of access & exit (11).

3. The unmanned aerial vehicle hangar of claim 2, wherein the first drive module (31) comprises:

a first drive source (311), the first drive source (311) being mounted on the frame (1);

a rotating shaft (312), the rotating shaft (312) being engaged with an output shaft of the first driving source (311);

a sliding component (313), wherein the sliding component (313) is matched on the frame (1) in a sliding way along the up-down direction and is connected with the connecting frame (32);

and one end of the connecting rope is wound on the rotating shaft (312), and the other end of the connecting rope is connected to the sliding component (313).

4. The unmanned aerial vehicle hangar of claim 3, wherein the frame (1) is provided with a sliding part (12), and the sliding part (12) is provided with a sliding groove (121) extending in the up-down direction;

the sliding assembly (313) comprises:

a sliding support (3131), the sliding support (3131) being connected to the connection string and the connection frame (32);

a sliding wheel (3132), wherein the sliding wheel (3132) is rotatably arranged on the sliding support (3131) and is matched in the sliding groove (121).

5. The unmanned aerial vehicle hangar of claim 3, wherein both ends of the rotating shaft (312) are provided with a matching portion (3121), each matching portion (3121) is provided with the connecting rope in a matching manner, the other end of each connecting rope is connected with one sliding assembly (313), and the two sliding assemblies (313) are located on both sides of the landing platform (2).

6. The unmanned hangar of claim 2, wherein the second drive module (33) comprises:

a second driving source (331), the second driving source (331) being mounted on the link frame (32);

a gear (332), the gear (332) being engaged with an output shaft of the second driving source (331);

a rack (333), the rack (333) is engaged with the gear (332) and is connected with the landing platform (2).

7. The unmanned aerial vehicle hangar of claim 2, characterized in that, the unmanned aerial vehicle hangar still includes slide rail (321) and slider (211) that mutually support, slide rail (321) are along getting into the direction extension setting of access & exit (11), slide rail (321) are established on link (32), slider (211) with it links to each other to descend platform (2).

8. Unmanned aerial vehicle hangar according to any of claims 1 to 7, wherein the landing platform (2) comprises:

a platform body (21), the platform body (21) cooperating with the drive mechanism (3);

centering component (22), centering component (22) is established on platform body (21), centering component (22) is used for fixing a position unmanned aerial vehicle, centering component (22) includes along the position sensor of the edge setting of platform body (21).

9. Unmanned aerial vehicle hangar according to any of claims 1 to 7, wherein the landing platform (2) is provided with a charging interface for cooperation with an unmanned aerial vehicle; or:

the unmanned aerial vehicle hangar further comprises a manipulator, the manipulator is arranged in the frame (1), and the manipulator can replace a battery of the unmanned aerial vehicle.

10. The unmanned aerial vehicle hangar of any of claims 1-7, further comprising a door body (4), wherein the door body (4) is openably and closably fitted on the frame (1), and the door body (4) can close the access opening (11).

Technical Field

The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle hangar.

Background

At present, most unmanned aerial vehicle hangars in the market are one-machine-one-base, the utilization rate of the hangars is low, accordingly, the patrol range and patrol frequency of the unmanned aerial vehicle are greatly reduced, and patrol tasks cannot be efficiently executed. Although a small part of the hangar can accommodate a plurality of unmanned aerial vehicles, the unmanned aerial vehicles cannot take off and land simultaneously due to only one entrance.

Disclosure of Invention

The invention aims to provide an unmanned aerial vehicle hangar which can accommodate a plurality of unmanned aerial vehicles and can realize simultaneous take-off and landing of the unmanned aerial vehicles.

In order to achieve the technical effects, the technical scheme of the invention is as follows:

the invention discloses an unmanned aerial vehicle hangar, which comprises: the frame is provided with a plurality of inlets and outlets arranged at intervals along the circumferential direction; the landing platforms are movably arranged in the frame, the number of the landing platforms is multiple, and the landing platforms and the access ports are arranged in a one-to-one correspondence manner; the driving mechanism is arranged on the frame and is multiple, the driving mechanism is matched with the landing platforms one by one, and the driving mechanism is used for driving the landing platforms to move along the up-down direction and in and out of the gateway.

In some embodiments, each of the drive mechanisms comprises: the first driving module is arranged on the frame; the connecting frame is connected with the power output end of the first driving module and can move up and down under the driving of the first driving module; the second drive module, the second drive module is established on the link, the power take off end of second drive module with it links to each other to descend the platform, the second drive module is used for the drive descend the platform along the business turn over the direction motion of access & exit.

In some specific embodiments, the first driving module comprises: a first driving source mounted on the frame; a rotating shaft which is matched with an output shaft of the first driving source; the sliding assembly is matched on the frame in a sliding mode along the vertical direction and is connected with the connecting frame; and one end of the connecting rope is wound on the rotating shaft, and the other end of the connecting rope is connected to the sliding assembly.

In some more specific embodiments, the frame is provided with a sliding part, and the sliding part is provided with a sliding groove extending in the up-down direction; the sliding assembly includes: the sliding support is connected with the connecting rope and the connecting frame; the sliding wheel is rotatably arranged on the sliding support and is matched in the sliding groove.

In some more specific embodiments, the two ends of the rotating shaft are provided with matching portions, each matching portion is matched with the connecting rope, the other end of each connecting rope is connected with one sliding assembly, and the two sliding assemblies are located on two sides of the descending platform.

In some specific embodiments, the second driving module comprises: a second driving source mounted on the link frame; a gear engaged with an output shaft of the second drive source; and the rack is meshed with the gear and is connected with the landing platform.

In some specific embodiments, unmanned aerial vehicle hangar still includes slide rail and the slider of mutually supporting, the slide rail is along getting into the direction extension setting of access & exit, the slide rail is established on the link, the slider with it links to each other to descend the platform.

In some embodiments, the landing platform comprises: a platform body, the platform body cooperating with the drive mechanism; the middle component is arranged on the platform body and used for positioning the unmanned aerial vehicle, and the middle component comprises a position sensor arranged along the edge of the platform body.

In some embodiments, the landing platform is provided with a charging interface for cooperating with the drone; or: the unmanned aerial vehicle hangar still includes the manipulator, the manipulator is established in the frame, the manipulator can be changed unmanned aerial vehicle's battery.

In some embodiments, the unmanned aerial vehicle hangar further comprises a door body, wherein the door body is fitted to the frame in an openable and closable manner, and the door body can close the entrance and the exit.

The unmanned aerial vehicle hangar has the beneficial effects that: because the number of the entrances and exits, the landing platforms and the driving mechanisms is multiple, in the actual working process, the multiple lifting platforms can move simultaneously, so that the landing of multiple unmanned aerial vehicles is realized, and the inspection range and the dead time of the unmanned aerial vehicles are greatly improved; because when not using, a plurality of lift platform are along the range upon range of setting of upper and lower direction for the unmanned aerial vehicle hangar is not showing the grow, and the cost of unmanned aerial vehicle hangar also can reduce by a wide margin.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle hangar according to an embodiment of the present invention;

fig. 2 is a schematic partial structure diagram of an unmanned aerial vehicle hangar according to an embodiment of the present invention;

fig. 3 is another partial structural schematic diagram of the unmanned aerial vehicle hangar according to the embodiment of the invention.

Reference numerals:

1. a frame; 11. an entrance and an exit; 12. a slider; 121. a chute;

2. landing the platform; 21. a platform body; 211. a slider; 22. a centering component;

3. a drive mechanism;

31. a first driving module; 311. a first drive source; 312. a rotating shaft; 3121. a fitting portion; 313. a sliding assembly; 3131. a sliding support; 3132. a sliding wheel;

32. a connecting frame; 321. a slide rail;

33. a second driving module; 331. a second drive source; 332. a gear; 333. a rack;

4. a door body; 5. a top cover; 6. an electric control cabinet.

Detailed Description

In order to make the technical problems solved, the technical solutions adopted and the technical effects achieved by the present invention clearer, the technical solutions of the present invention are further described below by way of specific embodiments with reference to the accompanying drawings.

In the description of the present invention, it is to be understood that the terms "central," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," "axial," "radial," "circumferential," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the invention and to simplify the description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the invention.

Furthermore, features defined as "first" and "second" may explicitly or implicitly include one or more of the features for distinguishing between descriptive features, non-sequential, non-trivial and non-trivial. In the description of the present invention, "a plurality" means two or more unless otherwise specified.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

The specific structure of the unmanned aerial vehicle hangar of the embodiment of the present invention is described below with reference to fig. 1 to 3.

The invention discloses an unmanned aerial vehicle hangar, as shown in figure 1, the unmanned aerial vehicle hangar comprises a frame 1, landing platforms 2 and driving mechanisms 3, wherein the frame 1 is provided with a plurality of entrances and exits 11 arranged at intervals along the circumferential direction of the frame 1, the landing platforms 2 are movably arranged in the frame 1, the landing platforms 2 are arranged in a plurality, the landing platforms 2 are arranged in a one-to-one correspondence with the entrances and exits 11, the driving mechanisms 3 are arranged on the frame 1, the driving mechanisms 3 are arranged in a plurality, the driving mechanisms 3 are matched with the landing platforms 2 one by one, and the driving mechanisms 3 are used for driving the landing platforms 2 to move along the up-down direction and the direction of entering and exiting the entrances and exits 11.

It will be appreciated that when not in use, a plurality of landings 2 are stowed within the frame 1 in layers from top to bottom. In the use, descending platform 2 is out of the warehouse under actuating mechanism 3's effect, and descending platform 2 passes access & exit 11 promptly and stretches out frame 1, and actuating mechanism 3 continues descending platform 2 up-and-down motion after that, makes its rise to the position that flushes with the top of frame 1, waits for unmanned aerial vehicle to descend. Because access & exit 11, descending platform 2 and actuating mechanism 3 are a plurality ofly, in the actual work process, a plurality of lift platforms can the simultaneous movement, realize a plurality of unmanned aerial vehicle's lift to promote unmanned aerial vehicle's tour scope and hang-up time greatly, unmanned aerial vehicle hangar does not show the grow simultaneously, and the cost that unmanned aerial vehicle arranged also can reduce by a wide margin.

In some embodiments, as shown in fig. 2, each driving mechanism 3 includes a first driving module 31, a connecting frame 32 and a second driving module 33, the first driving module 31 is disposed on the frame 1, the connecting frame 32 is connected to a power output end of the first driving module 31, the connecting frame 32 can move in an up-and-down direction under the driving of the first driving module 31, the second driving module 33 is disposed on the connecting frame 32, the power output end of the second driving module 33 is connected to the landing platform 2, and the second driving module 33 is configured to drive the landing platform 2 to move in a direction of entering and exiting the doorway 11. It can be understood that, in the actual work process, second drive module 33 drive lift platform stretches out, and first drive module 31 drive link 32 and second drive module 33 rise after lift platform moves the assigned position, make it rise to wait for unmanned aerial vehicle to descend with the position that the top of frame 1 was flushed. From this, can realize descending platform 2's lift and stretch out to ensure that unmanned aerial vehicle can descend steadily.

In some specific embodiments, as shown in fig. 2, the first driving module 31 includes a first driving source 311, a rotating shaft 312, a sliding component 313 and a connecting rope (not shown), the first driving source 311 is installed on the frame 1, the rotating shaft 312 is engaged with an output shaft of the first driving source 311, the sliding component 313 is slidably engaged on the frame 1 along the up-down direction and is connected with the connecting frame 32, one end of the connecting rope is wound on the rotating shaft 312, and the other end of the connecting rope is connected to the sliding component 313. It will be appreciated that, in actual operation, during the rotation of the rotating shaft 312 driven by the first driving source 311, the connecting rope can be wound up or released, thereby moving the sliding assembly 313 up and down. Because the sliding component 313 is connected with the connecting frame 32, the descending platform 2 can be driven to ascend and descend by the sliding component 313 in the process of moving up and down.

In some more specific embodiments, as shown in fig. 1, the frame 1 is provided with a sliding member 12, the sliding member 12 is provided with a sliding slot 121 extending in the up-down direction, as shown in fig. 3, the sliding assembly 313 includes a sliding support 3131 and a sliding wheel 3132, the sliding support 3131 is connected to the connecting rope and the connecting frame 32, and the sliding wheel 3132 is rotatably provided on the sliding support 3131 and is fitted in the sliding slot 121. It is understood that the connecting string can move the sliding support 3131 up and down during the rotation of the rotating shaft 312 driven by the first driving source 311, and the sliding wheel 3132 can slide in the sliding groove 121 during the up and down sliding of the sliding support 3131. The cooperation of the sliding wheel 3132 and the sliding groove 121 can limit the moving direction of the sliding support 3131, so as to prevent the lifting platform from tilting due to the tilting of the sliding support 3131, and can reduce the friction between the sliding wheel 3132 and the sliding member 12, thereby ensuring that the sliding support 3131 can move stably.

Alternatively, the sliding wheel 3132 may be bolted to the sliding support 3131 using a bearing. It will be appreciated that the bearings and bolts are standard components, simplifying the construction of the slide assembly 313 and reducing the cost of manufacturing the slide assembly 313.

In some more specific embodiments, as shown in fig. 2, the two ends of the rotating shaft 312 are provided with engaging portions 3121, each engaging portion 3121 is engaged with a connecting rope, the other end of each connecting rope is connected with one sliding assembly 313, and the two sliding assemblies 313 are located at both sides of the landing platform 2. It can be understood that, two slip subassemblies 313 promote simultaneously and descend platform 2, can guarantee that descending platform 2 can go up and down steadily to avoid descending platform 2 crooked and lead to the phenomenon emergence that unmanned aerial vehicle can not stably keep on descending platform 2.

In some specific embodiments, as shown in fig. 2, the second driving module 33 includes a second driving source 331, a gear 332, and a rack 333, the second driving source 331 is mounted on the connecting frame 32, the gear 332 is engaged with an output shaft of the second driving source 331, and the rack 333 is engaged with the gear 332 and connected with the landing platform 2. It can be understood that, in actual operation, the second driving source 331 drives the gear 332 to rotate, and the gear 332 rotates to drive the rack 333 to move. This kind of structure that adopts gear 332 cooperation rack 333, power transmission efficiency is higher and simple structure, not only can ensure that second drive module 33 can drive landing platform 2 stably and stretch out or retract frame 1, can also simplify the structure of second drive module 33, reduces the manufacturing cost of whole unmanned aerial vehicle hangar.

It should be additionally noted that the second driving module 33 may also adopt other structures, for example, a transmission belt structure, a cylinder structure, etc. are not limited to the structure of the gear 332 and the rack 333 in this embodiment.

In some specific embodiments, as shown in fig. 3, the unmanned aerial vehicle hangar further includes a sliding rail 321 and a sliding block 211, which are matched with each other, the sliding rail 321 extends along a direction entering the entrance 11, the sliding rail 321 is disposed on the connecting frame 32, and the sliding block 211 is connected with the landing platform 2. It can be understood that, when the second driving source 331 drives the landing platform 2 to extend or retract into the frame 1, if the landing platform 2 is inclined, the probability that the landing platform 2 is stuck is increased, and thus the reliability of the unmanned aerial vehicle hangar is reduced. In this embodiment, through set up slide rail 321 on link 32, be equipped with slider 211 on descending platform 2, when descending platform 2 moves, slider 211 can only slide along the extending direction of slide rail 321, has restricted descending platform 2's direction of motion betterly, has avoided descending platform 2 to appear the dead phenomenon of card, has promoted the use reliability of the unmanned aerial vehicle hangar of this embodiment.

Preferably, both sides of the landing platform 2 are provided with a plurality of sliding blocks 211, and both sides of the connecting frame 32 are provided with sliding rails 321. From this, can further promote the limited action to descending platform 2, guarantee the reliability that unmanned aerial vehicle descends.

Of course, it should be additionally described here that, in other embodiments of the present invention, the structure for limiting the movement direction of the landing platform 2 is not limited to the structure in which the sliding rail 321 is matched with the sliding block 211, and may also be selected according to actual needs, for example, a guide post is arranged on the landing platform 2, and a guide groove matched with the guide post is arranged on the connecting frame 32.

It should be added that, in other embodiments of the present invention, the driving mechanism 3 may be formed as a driving structure of a robot, and is not limited to the structure of two mutually perpendicular driving modules of this embodiment.

In some embodiments, as shown in fig. 3, the landing platform 2 comprises a platform body 21 and a centering assembly 22, the platform body 21 cooperates with the driving mechanism 3, the centering assembly 22 is provided on the platform body 21, the centering assembly 22 is used for positioning the drone, and the centering assembly 22 comprises a position sensor provided along an edge of the platform body 21. It can be understood that, at the unmanned aerial vehicle landing in-process, position sensor can detect unmanned aerial vehicle's position, and cooperation unmanned aerial vehicle hangar and unmanned aerial vehicle's control system can ensure that unmanned aerial vehicle lands on landing platform 2's assigned position, avoids unmanned aerial vehicle landing offset to lead to the phenomenon of unmanned aerial vehicle falling from landing platform 2 to take place. In addition, the centering component 22 ensures that the landing of the drone is beneficial to charging or other subsequent operations such as cleaning the drone at a specified location.

It should be additionally noted that, in the embodiment of the present invention, the type and distribution of the position sensors may be selected according to actual needs, and no limitation is made to the specific type of the position sensors.

In some embodiments, the landing platform 2 is provided with a charging interface for cooperation with the drone. It can be understood that, when unmanned aerial vehicle fell to the assigned position of landing platform 2, thereby the contact that charges on the unmanned aerial vehicle can with the interface cooperation that charges realize unmanned aerial vehicle's charging. That is to say, the unmanned aerial vehicle hangar of this embodiment not only can store unmanned aerial vehicle and can also realize the unmanned aerial vehicle function of charging, has promoted user's use satisfaction.

In some embodiments, the unmanned aerial vehicle hangar further comprises a manipulator, the manipulator is arranged in the frame 1, and the manipulator can replace a battery of the unmanned aerial vehicle. It can be understood that, when unmanned aerial vehicle fell to the assigned position of landing platform 2, the manipulator can be changed the lower battery of the inside electric quantity of unmanned aerial vehicle into full charge battery to guarantee that unmanned aerial vehicle has longer flight time when leaving the unmanned aerial vehicle hangar. That is to say, the unmanned aerial vehicle hangar of this embodiment not only can store unmanned aerial vehicle and can also realize the unmanned aerial vehicle function of charging, has promoted user's use satisfaction.

In some embodiments, as shown in fig. 1, the unmanned aerial vehicle hangar further includes a door 4, the door 4 is openably and closably fitted on the frame 1, and the door 4 can close the doorway 11. It can be understood that, because the access & exit 11 opens the setting, will cause outside debris or rainwater to get into inside frame 1 if the unmanned aerial vehicle hangar is used for open-air occasion to lead to the phenomenon that whole unmanned aerial vehicle hangar broke down. In this embodiment, be equipped with the door body 4 that can seal access & exit 11 on the frame 1, when the unmanned aerial vehicle hangar was used for open occasion not had unmanned aerial vehicle take off and land, close door body 4 inside in order to avoid outside debris or rainwater entering frame 1, prolonged the life of unmanned aerial vehicle hangar. And when unmanned aerial vehicle takes off and land, open door body 4 and make descending platform 2 stretch out frame 1 can.

It should be additionally noted herein that the opening and closing of the door 4 may be automatic or manual, and may be specifically selected according to actual needs. When the door body 4 is automatically opened and closed, only one push rod structure needs to be arranged on the frame 1.

Example (b):

an unmanned hangar in accordance with one embodiment of the present invention is described below with reference to fig. 1-3.

This unmanned aerial vehicle hangar includes frame 1, descending platform 2, actuating mechanism 3, the door body 4, top cap 5 and automatically controlled cabinet 6, and frame 1 sets up the access & exit 11 that a plurality of intervals set up for the quadrangle along its circumference, and the both sides of access & exit 11 all are equipped with slider 12, are equipped with the spout 121 that the direction extends from top to bottom on slider 12. Descending platform 2 movably establishes in frame 1, and descends platform 2 and four 11 one-to-one settings of access & exit, and actuating mechanism 3 establishes on frame 1, and actuating mechanism 3 is four, and four actuating mechanism 3 cooperate with four descending platform 2 one by one, and actuating mechanism 3 is used for driving descending platform 2 along the direction motion of upper and lower direction and business turn over access & exit 11.

Each driving mechanism 3 includes a first driving module 31, a connecting frame 32, and a second driving module 33, and the first driving module 31 includes a first driving source 311, a rotating shaft 312, a sliding member 313, and a connecting rope. First driving source 311 installs on frame 1, and pivot 312 and the output shaft cooperation of first driving source 311, the both ends of pivot 312 all are equipped with cooperation portion 3121, all cooperate on every cooperation portion 3121 to connect the rope, and the one end of every connection rope all is connected with a cooperation portion 3121, and two sliding assembly 313 are located the both sides of descending platform 2. Each sliding assembly 313 includes a sliding support 3131 and a sliding wheel 3132, the sliding support 3131 is provided with a suspension ring connected to the other end of the connection rope, and the sliding support 3131 is connected to the connection frame 32, the sliding wheels 3132 are five and are bearings, and the five bearings are respectively connected to the sliding support 3131 by using five bolts. The sliding support 3131 is provided with a sliding rail 321, the sliding rail 321 extends along the direction of entering the doorway 11, the second driving module 33 includes a second driving source 331, a gear 332 and a rack 333, the second driving source 331 is mounted on the connecting frame 32, the gear 332 is matched with the output shaft of the second driving source 331, and the rack 333 is engaged with the gear 332 and connected with the landing platform 2.

Descending platform 2 includes platform body 21 and the subassembly 22 of returning to the heart, and platform body 21 is connected on rack 333, and is equipped with on platform body 21 with slide rail 321 complex slider 211, and the subassembly 22 of returning to the heart is established on platform body 21, and the subassembly 22 of returning to the heart is used for fixing a position unmanned aerial vehicle, and the subassembly 22 of returning to the heart includes the position sensor who sets up along the edge of platform body 21. Unmanned aerial vehicle hangar still includes the door body 4, and descending platform 2 is equipped with the interface that charges with unmanned aerial vehicle complex (not shown). The door 4 is openably and closably fitted to the frame 1, and the door 4 can close the doorway 11. The top cover 5 is buckled at the top of the frame 1, and the electric control cabinet 6 is arranged in the frame 1. The electric control cabinet 6 can be provided with a partition plate or a sheet metal door for beautifying the hangar and can be opened.

The beneficial effect of the unmanned aerial vehicle hangar of this embodiment is as follows:

firstly, the method comprises the following steps: because the number of the entrances and exits 11, the landing platforms 2 and the driving mechanisms 3 is four, in the actual working process, the four lifting platforms can move simultaneously to realize the lifting of one to four unmanned aerial vehicles, so that the inspection range and the dead time of the unmanned aerial vehicles are greatly improved, meanwhile, the hangar of the unmanned aerial vehicles is not remarkably enlarged, and the cost for arranging the unmanned aerial vehicles can be greatly reduced;

secondly, the method comprises the following steps: when unmanned aerial vehicle fell to the assigned position of descending platform 2, thereby the contact of charging on the unmanned aerial vehicle can with the interface cooperation that charges realize charging of unmanned aerial vehicle.

In the description herein, references to the description of "some embodiments," "other embodiments," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The above description is only a preferred embodiment of the present invention, and for those skilled in the art, the present invention should not be limited by the description of the present invention, which should be interpreted as a limitation.