Failed aircraft storage canopy, failed aircraft storage hangar, and failed aircraft storage method

Abstract

The application discloses a malfunction aircraft storage top cover, a malfunction aircraft storage hangar and a malfunction aircraft storage method. The malfunction aircraft storage top cover comprises a top plate, an enclosure and a plurality of bearing members. The top plate is connected with the enclosure, and the top plate and the enclosure define a storage cavity with an opening. The end of the enclosure close to the opening is rotationally connected with a hangar body. The plurality of bearing members are located in the storage cavity and connected with the enclosure, and are used for bearing arms of the malfunction aircraft. That is, a plurality of unmanned aerial vehicles can be stored in the hangar body. The enclosure can rotate on the hangar body to open or close the entrance of the hangar body, so that the unmanned aerial vehicles can enter or exit the hangar body. When a malfunction occurs in one of the unmanned aerial vehicles in the hangar body, the malfunction aircraft can be placed in the storage cavity, and the plurality of arms of the malfunction aircraft can abut against the plurality of bearing members, so that the malfunction aircraft can be stored in the malfunction aircraft storage top cover, and the malfunction aircraft cannot occupy the space of the hangar body and cannot hinder the normal take-off of the other unmanned aerial vehicles in the hangar body.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of unmanned aerial vehicles, in particular to a malfunctioning UAV storage top cover, a malfunctioning UAV storage hangar and a malfunctioning UAV storage method. BACKGROUND

[0002] With the progress of society, unmanned aerial vehicles have gradually spread from military fields to civilian fields, including logistics, surveying and mapping, plant protection, photography, power, communication or rescue, etc. sub-branches, achieving good technical spillover and social and economic benefits. The prior art stores multiple unmanned aerial vehicles in a hangar, and the unmanned aerial vehicles can also take off from the hangar. However, when a malfunctioning unmanned aerial vehicle in the hangar cannot take off normally, the malfunctioning unmanned aerial vehicle not only occupies the space of the hangar, but also hinders the normal take-off of other unmanned aerial vehicles. SUMMARY

[0003] The present application provides a malfunctioning UAV storage top cover, a malfunctioning UAV storage hangar and a malfunctioning UAV storage method to solve the problem that the malfunctioning unmanned aerial vehicle in the prior art hangar occupies the space of the hangar and hinders the normal take-off of other unmanned aerial vehicles.

[0004] In a first aspect, the present application provides a malfunctioning UAV storage top cover applied in a hangar, comprising: a top plate, a surrounding plate and a plurality of bearing members;

[0005] The top plate is connected with the surrounding plate, and the top plate and the surrounding plate define a storage cavity with an opening. The end of the surrounding plate close to the opening is rotationally connected with a hangar body.

[0006] The plurality of bearing members are located in the storage cavity and connected with the surrounding plate, and are used to bear the arms of malfunctioning unmanned aerial vehicles.

[0007] In some possible implementation manners, the bearing member comprises a bottom plate and two side plates connected with the bottom plate, and the bottom plate and the two side plates define a clamping groove for accommodating the arm.

[0008] In some possible implementation manners, the plurality of bearing members constitute at least two bearing modules, and the at least two bearing modules are arranged in a direction perpendicular to the top plate.

[0009] In some possible implementation manners, the plurality of bearing members in each bearing module are located on the same horizontal plane.

[0010] In a second aspect, the present application provides a malfunctioning UAV storage hangar, comprising: a hangar body, the above-mentioned malfunctioning UAV storage top cover, and a carrying device.

[0011] The hangar body stores a plurality of unmanned aerial vehicles, wherein the malfunctioning unmanned aerial vehicle is one of the plurality of unmanned aerial vehicles that has malfunctioned.

[0012] The carrying device is located in the library body and is used to carry the faulty machine into the storage cavity so that the plurality of arms of the faulty machine abut against the plurality of carriers respectively.

[0013] In some possible implementation manners, the carrying device comprises a support connected with the library body, a sliding member in sliding connection with the support, and a tray in rotational connection with the sliding member.

[0014] In some possible implementation manners, the tray is provided with a limiting slot for accommodating the fuselage of the faulty machine.

[0015] In some possible implementation manners, the surrounding plate is provided with a giving slot, and a part of the support is located in the giving slot.

[0016] In some possible implementation manners, the carrying device further comprises a telescopic member in movable connection with the sliding member, and the telescopic member is in rotational connection with the tray.

[0017] In some possible implementation manners, the telescopic member comprises a cylinder connected with the sliding member, a telescopic rod connected with the cylinder, and a carrier plate connected with the telescopic rod, and the carrier plate is in rotational connection with the tray.

[0018] In a third aspect, the present application further provides a faulty machine storage method applied to the faulty machine storage hangar, and the method comprises the following steps:

[0019] The carrying device moves to the storage position corresponding to the faulty machine and abuts against the bottom of the faulty machine;

[0020] The carrying device moves into the storage cavity, and the faulty machine is placed on the plurality of carriers so that the plurality of arms of the faulty machine abut against the plurality of carriers respectively.

[0021] The faulty machine storage top cover provided by the present application comprises a top plate, a surrounding plate and a plurality of carriers. The top plate is connected with the surrounding plate, and the top plate and the surrounding plate define a storage cavity with an opening. The surrounding plate is rotatably connected with the library body of the hangar at one end close to the opening. The plurality of carriers are located in the storage cavity and connected with the surrounding plate, and are used to carry the arms of the faulty machine. That is, a plurality of unmanned aerial vehicles can be stored in the library body. The surrounding plate can rotate on the library body to open or close the entrance of the library body, so that the unmanned aerial vehicles can enter or exit the library body. When one unmanned aerial vehicle in the library body fails, the faulty machine can be placed in the storage cavity, and the plurality of arms of the faulty machine abut against the plurality of carriers respectively, so as to store the faulty machine in the faulty machine storage top cover, so that the faulty machine does not occupy the space of the library body and does not hinder the normal take-off of the other unmanned aerial vehicles in the library body. BRIEF DESCRIPTION OF DRAWINGS

[0022] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following will briefly introduce the drawings needed in the embodiment description. Obviously, the drawings in the following description only show some embodiments of the present application, and for those skilled in the art, other drawings can also be obtained from these drawings without creative labor.

[0023] Figure 1 Fig. 1 is a first perspective view of a malfunctioning aircraft storage top cover and malfunctioning aircraft storage system according to an embodiment of the present application;

[0024] Figure 2 Fig. 2 is a second perspective view of a malfunctioning aircraft storage top cover and malfunctioning aircraft storage system according to an embodiment of the present application;

[0025] Figure 3 Fig. 3 is a schematic view of a surrounding plate and a bearing part of a malfunctioning aircraft storage top cover according to an embodiment of the present application;

[0026] Figure 4 Fig. 4 is a first perspective view of a carrying device of a malfunctioning aircraft storage system according to an embodiment of the present application;

[0027] Figure 5 Fig. 5 is a second perspective view of a carrying device of a malfunctioning aircraft storage system according to an embodiment of the present application;

[0028] Figure 6 Fig. 6 is a working logic diagram of a malfunctioning aircraft storage system according to an embodiment of the present application;

[0029] Figure 7 Fig. 7 is a flow chart of an automatic carrying method according to an embodiment of the present application. DETAILED DESCRIPTION

[0030] The technical solutions in the embodiments of the present application will be described clearly and completely with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only some embodiments of the present application, but not all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor are within the scope of protection of the present application.

[0031] In the description of the present application, it needs to be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like are based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present application and simplifying the description, and does not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the present application. In addition, the terms "first", "second" are only for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first", "second" can explicitly or implicitly include one or more of the features. In the description of the present application, the meaning of "a plurality of" is two or more, unless otherwise explicitly specified and limited.

[0032] In the description of the present application, it needs to be understood that unless otherwise explicitly specified and limited, the terms "mounting", "connecting", "connecting" should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected or can communicate with each other; it can be directly connected, or indirectly connected through an intermediate medium; it can be the internal communication of two elements or the interaction relationship between two elements. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0033] The malfunctioning machine storage top cover of the present application can be applied to a hangar and rotationally connected with a hangar body, so as to open or close the entrance of the hangar body, so that the unmanned aerial vehicle can enter and exit the hangar body. When one unmanned aerial vehicle in the hangar body malfunctions, the malfunctioning machine can be placed in the storage cavity, and the plurality of arms of the malfunctioning machine can be abutted with the plurality of bearing pieces respectively, so as to store the malfunctioning machine in the malfunctioning machine storage top cover, so that the malfunctioning machine does not occupy the space of the hangar body and does not hinder the normal take-off of other unmanned aerial vehicles in the hangar body.

[0034] Please refer to Figures 1 to 3 In the embodiments of the present application, a malfunctioning machine storage top cover 200 is applied to a hangar, and the malfunctioning machine storage top cover 200 comprises a top plate 1, a surrounding plate 2 and a plurality of bearing pieces 3.

[0035] The top plate 1 is connected with the surrounding plate 2, and the top plate 1 and the surrounding plate 2 define a storage cavity 12 with an opening 11, and the end of the surrounding plate 2 close to the opening 11 is rotationally connected with the hangar body 100.

[0036] The plurality of bearing pieces 3 are located in the storage cavity 12 and connected with the surrounding plate 2, and are used for bearing the arms of the malfunctioning machine 4.

[0037] It should be noted that the plurality of unmanned aerial vehicles can be stored in the warehouse body 100, and the warehouse body 100 has an entrance 101 at the top end for the unmanned aerial vehicles to enter and exit the warehouse body 100. The surrounding plate 2 can rotate on the warehouse body 100, that is, the malfunction aircraft storage top cover 200 can rotate on the warehouse body 100 to open or close the entrance 101 of the warehouse body 100, so that the unmanned aerial vehicles can enter and exit the warehouse body 100. When one of the unmanned aerial vehicles in the warehouse body 100 malfunctions, that is, the malfunctioning unmanned aerial vehicle is the malfunction aircraft 4, the malfunction aircraft 4 can be placed in the storage cavity 12, and the plurality of arms of the malfunction aircraft 4 can abut against the plurality of bearing pieces 3, respectively. The arm is a mechanism for bearing the propeller of the malfunction aircraft 4, which realizes the storage of the malfunction aircraft 4 in the malfunction aircraft storage top cover 200, so that the malfunction aircraft 4 does not occupy the space of the warehouse body 100, and the malfunction aircraft 4 can rotate with the surrounding plate 2 and does not hinder the normal take-off of other unmanned aerial vehicles in the warehouse body 100.

[0038] In this embodiment, the distance between the bearing piece 3 and the top plate 1 is slightly greater than the height of the mechanism above the arm of the malfunction aircraft 4, so that there is enough space between the bearing piece 3 and the top plate 1 to accommodate the malfunction aircraft 4, and the malfunction aircraft 4 will not fall from the storage cavity 12 when it rotates with the surrounding plate 2.

[0039] In addition, the plurality of bearing pieces 3 are arranged at intervals, and the distance between the plurality of bearing pieces 3 is greater than the width of the fuselage of the malfunction aircraft 4, so that there is enough space between the plurality of bearing pieces 3 to accommodate the fuselage of the malfunction aircraft 4.

[0040] In some embodiments, the surrounding plate 2 is rotatably connected to the warehouse body 100 through a rotating shaft, that is, the hangar has a rotating shaft rotatably connected to the warehouse body 100, and the surrounding plate 2 is fixedly connected to the rotating shaft. In addition, the hangar can also be provided with a driving motor, a cylinder or a hydraulic cylinder connected to the rotating shaft, so as to drive the surrounding plate 2 to rotate.

[0041] In some embodiments, please refer to Figure 2 and Figure 3 The bearing piece 3 includes a bottom plate 31 and two side plates 32 connected to the bottom plate 31, and the bottom plate 31 and the two side plates 32 define a clamping groove for accommodating the arm. After the arm is placed in the clamping groove, the clamping groove can limit the arm to improve the stability of the malfunction aircraft 4 during storage.

[0042] In this embodiment, the bottom plate 31 and / or the side plate 32 are connected to the surrounding plate 2. The side plate 32 can be connected perpendicularly to the bottom plate 31, and the side plate 32 extends in the direction close to the top plate 1, that is, the overall shape of the bottom plate 31 and the two side plates 32 is like a "U" shape.

[0043] In some embodiments, the plurality of carriers 3 constitutes at least two carrier modules, and the at least two carrier modules are arranged in a direction perpendicular to the top plate 1. Each carrier module has a plurality of carriers 3, and each carrier module can carry one faulty machine 4, thereby increasing the number of faulty machines 4 stored in the faulty machine storage top cover 200.

[0044] In addition, when storing the faulty machine 4, the faulty machine 4 is sequentially stored on the plurality of carrier modules from the direction close to the top plate 1 to the direction away from the top plate 1, so as to store the plurality of faulty machines 4 on the plurality of carrier modules respectively.

[0045] In this embodiment, the plurality of carriers 3 in each carrier module are located on the same horizontal plane, so that when the plurality of arms of the faulty machine 4 are located in the plurality of carriers 3, the plurality of arms are also located on the same horizontal plane, thereby improving the balance of the faulty machine 4 when stored.

[0046] In this embodiment, the plurality of carriers 3 in the plurality of carrier modules overlap in the orthographic projection on the top plate 1, that is, the orthographic projection of the plurality of carriers 3 in each carrier module on the top plate 1 overlaps with the orthographic projection of the plurality of carriers 3 in other carrier modules on the top plate 1, thereby facilitating the storage of the plurality of faulty machines 4 on the plurality of carrier modules respectively.

[0047] In this embodiment, the number and position of the carriers 3 in each carrier module can be correspondingly arranged according to the number and position of the arms of the faulty machine 4, so that each carrier 3 can carry one arm, or when the number of arms is greater than four, the number of carriers 3 is only four, and the four carriers 3 carry the four arms of the faulty machine 4 respectively, thereby ensuring the balance of the faulty machine 4 when stored and saving costs.

[0048] Please refer to Figures 1 to 6 , based on the above-mentioned faulty machine storage top cover 200, the application further provides a faulty machine storage hangar, comprising: a hangar body 100, the above-mentioned faulty machine storage top cover 200, and a carrying device 300.

[0049] The hangar body 100 stores a plurality of unmanned aerial vehicles, wherein the faulty machine 4 is one unmanned aerial vehicle that has failed in the plurality of unmanned aerial vehicles.

[0050] The carrying device 300 is located in the hangar body 100 and is used to carry the faulty machine 4 into the storage cavity 12, so that the plurality of arms of the faulty machine 4 respectively abut against the plurality of carriers 3.

[0051] It should be noted that when one of the drones in the library body 100 malfunctions, the carrying device 300 can carry the malfunctioning drone 4 to the storage cavity 12, at this time the malfunctioning drone storage top cover 200 is in a position closing the entrance 101 of the library body 100, so that the multiple arms of the malfunctioning drone 4 are respectively abutted with the multiple carriers 3, realizing the storage of the malfunctioning drone 4 in the malfunctioning drone storage top cover 200, so that the malfunctioning drone 4 does not occupy the space of the library body 100, and the malfunctioning drone 4 can rotate with the surrounding plate 2 and does not hinder the normal take-off of other drones in the library body 100.

[0052] In this embodiment, the malfunctioning drone storage top cover 200 can first rotate to a position opening the entrance 101 of the library body 100, so that the drones can enter and exit the library body 100, and when one of the drones in the library body 100 malfunctions, the malfunctioning drone storage top cover 200 can rotate to a position closing the entrance 101 of the library body 100, and the carrying device 300 carries the malfunctioning drone 4 to the storage cavity 12.

[0053] In some embodiments, the top end of the library body 100 has an entrance 101, and the library body 100 can have multiple layers of storage layers distributed in the vertical direction, and each layer of storage layer stores at least one drone. In addition, when the drone needs to take off, the carrying device 300 can carry the drone in the library body 100 to the storage layer on the uppermost layer, i.e., the storage layer closest to the entrance 101, so as to facilitate the take-off of the drone. The malfunction detection mechanism 400 can also be provided in the storage layer on the uppermost layer to detect the malfunction of the drone, and if the drone malfunctions, the carrying device 300 carries the malfunctioning drone 4 to the storage cavity 12.

[0054] In this embodiment, the malfunction detection mechanism 400 can be multiple cameras or multiple laser scanners to take pictures or laser scans of the drone in all directions, check whether the drone is damaged, structure is lost or other abnormal conditions, and determine whether the drone malfunctions.

[0055] In some embodiments, please refer to Figure 1 , Figure 2 , Figure 4 and Figure 5The carrying device 300 comprises a support 301 connected with the library body 100, a sliding piece 302 in sliding connection with the support 301, and a tray 303 in rotary connection with the sliding piece 302. The movement direction of the sliding piece 302 can be the vertical direction, and the rotary direction of the tray 303 can be the horizontal direction. The tray 303 is used for carrying the faulty drone 4. The process of carrying the faulty drone 4 by the carrying device 300 is as follows: the sliding piece 302 is first slid to the storage layer where the faulty drone 4 is located, for example, the uppermost storage layer, to drive the tray 303 to abut against the bottom of the faulty drone 4, so as to carry the faulty drone 4. The tray 303 is rotated in the horizontal direction, so that the faulty drone 4 is in a position not to contact the carrying piece 3. The sliding piece 302 is then slid upward into the storage cavity 12, to drive the faulty drone 4 to move into the storage cavity 12, and the arm of the faulty drone 4 is located above the carrying piece 3. The tray 303 is rotated in the horizontal direction, so that the arm of the faulty drone 4 is located directly above the carrying piece 3, that is, the normal projection of the arm and the carrying piece 3 on the top plate 1 overlaps. The sliding piece 302 is then slid downward, so that the arm abuts against the carrying piece 3, and the carrying piece 3 carries the arm. In this way, the faulty drone 4 is stored in the faulty drone storage top cover 200, so that the faulty drone 4 does not occupy the space of the library body 100, and does not hinder the normal take-off of other drones in the library body 100.

[0056] In addition, when the faulty drone storage top cover 200 has at least two carrying modules, the carrying device 300 can sequentially store the faulty drones 4 on the carrying modules from the direction close to the top plate 1 to the direction away from the top plate 1, so as to store the plurality of faulty drones 4 on the plurality of carrying modules respectively.

[0057] In this embodiment, the sliding piece 302 can comprise at least one guide rail connected with the support 301, and a sliding block in sliding connection with the guide rail. The guide rail extends in the vertical direction, and the sliding block can move on the guide rail in the vertical direction. The guide rail can be an electric guide rail, to drive the sliding block to slide.

[0058] In this embodiment, please refer to Figure 1 , Figure 2 , Figure 4 and Figure 5 The carrying device 300 can comprise a rotating shaft 305 in rotary connection with the sliding piece 302, and a driving motor connected with the rotating shaft 305 and the sliding piece 302. The rotating shaft 305 is fixedly connected with the tray 303, and the driving motor drives the rotating shaft 305 to rotate to drive the tray 303 to rotate.

[0059] In this embodiment, please refer to Figure 4The tray 303 is provided with a limiting groove 3031 for accommodating the fuselage of the faulty machine 4 to limit the faulty machine 4 and improve the carrying stability of the faulty machine 4. For example, the number and position of the limiting grooves 3031 are correspondingly arranged according to the position and the supporting legs on the fuselage, so that when the tray 303 carries the faulty machine 4, the supporting legs of the faulty machine 4 can be respectively located in the limiting grooves 3031.

[0060] In this embodiment, please refer to Figure 1 , Figure 2 , Figure 4 and Figure 5 The surrounding plate 2 is provided with a giving groove 21, and a part of the support 301 is located in the giving groove 21, so that the giving groove 21 can provide a moving space for the sliding piece 302, so that the sliding piece 302 can drive the tray 303 to move into the storage cavity 12, preventing the movement of the sliding piece 302 from being interfered by the surrounding plate 2.

[0061] In addition, the giving groove 21 can also be provided on the top plate 1, that is, the surrounding plate 2 and the top plate 1 can be provided with the giving groove 21 at the same time, so as to increase the moving space of the sliding piece 302, preventing the movement of the sliding piece 302 from being interfered by the top plate 1 and the surrounding plate 2.

[0062] In this embodiment, please refer to Figure 1 , Figure 2 , Figure 4 and Figure 5 The carrying device 300 further comprises a telescopic piece 304 movably connected with the sliding piece 302, and the telescopic piece 304 is rotatably connected with the tray 303. The telescopic piece 304 can be telescoped in the horizontal direction to drive the tray 303 to move in the horizontal direction, so as to adjust the position of the tray 303, thereby ensuring that the tray 303 can abut against the bottom of the faulty machine 4, and ensuring that the carrying piece 3 can carry the arm, so as to store the faulty machine 4 in the faulty machine storage top cover 200.

[0063] In this embodiment, the telescopic piece 304 can include a cylinder connected with the sliding piece 302, a telescopic rod 3041 connected with the cylinder, and a carrying plate 3042 connected with the telescopic rod 3041, and the carrying plate 3042 is rotatably connected with the tray 303. The carrying plate 3042 is used for carrying the tray 303, and the cylinder can drive the telescopic rod 3041 to be telescoped in the horizontal direction to drive the tray 303 to move in the horizontal direction, so as to adjust the position of the tray 303, thereby ensuring that the tray 303 can abut against the bottom of the faulty machine 4, and ensuring that the carrying piece 3 can carry the arm, so as to store the faulty machine 4 in the faulty machine storage top cover 200.

[0064] In addition, the above-mentioned rotating shaft 305 can be rotatably connected with the carrying plate 3042, and the above-mentioned driving motor can be connected with the carrying plate 3042.

[0065] In this embodiment, the cylinder can be a pneumatic cylinder or a hydraulic cylinder. The cylinder can be located inside the sliding member 302, and the telescopic rod 3041 can pass through the sliding member 302 to extend to the outside of the sliding member 302.

[0066] Referring to Figure 6 The following describes the working process of the malfunction aircraft storage warehouse for storing the malfunction aircraft 4.

[0067] The malfunction aircraft storage top cover 200 can be first rotated to a position for opening the entrance and exit 101 of the warehouse body 100, and the malfunction detection mechanism 400 performs malfunction detection on the unmanned aerial vehicle.

[0068] If the unmanned aerial vehicle has a malfunction, the sliding member 302 is first slid to the storage layer where the malfunction aircraft 4 is located, and the telescopic member 304 is telescoped in the horizontal direction to drive the tray 303 to move to the lower side of the malfunction aircraft 4. The sliding member 302 is then slid upwardly to abut the bottom of the malfunction aircraft 4 with the tray 303, so as to carry the malfunction aircraft 4.

[0069] The tray 303 is rotated in the horizontal direction, so that the malfunction aircraft 4 is in a position not to contact the carrying member 3.

[0070] The malfunction aircraft storage top cover 200 is then rotated to a position for closing the entrance and exit 101 of the warehouse body 100, and the sliding member 302 is slid upwardly into the storage cavity 12 to drive the malfunction aircraft 4 to move into the storage cavity 12, and the arms of the malfunction aircraft 4 are located above the carrying member 3.

[0071] The tray 303 is rotated in the horizontal direction, so that the arms of the malfunction aircraft 4 are located directly above the carrying member 3.

[0072] The sliding member 302 is then slid downwardly to abut the arms with the carrying member 3, and the carrying member 3 carries the arms.

[0073] Referring to Figure 7 Based on the above malfunction aircraft storage warehouse, the application further provides a malfunction aircraft storage method applied to the above malfunction aircraft storage warehouse. The malfunction aircraft storage method comprises the following steps.

[0074] In step S1, the carrying device 300 moves to the storage position corresponding to the malfunction aircraft 4 and abuts the bottom of the malfunction aircraft 4.

[0075] In step S2, the carrying device 300 moves into the storage cavity 12 and places the malfunction aircraft 4 on the plurality of carrying members 3, so that the plurality of arms of the malfunction aircraft 4 abut the plurality of carrying members 3, respectively.

[0076] It should be noted that when one of the drones in the warehouse body 100 fails, the carrying device 300 can carry the failed drone 4 to the storage cavity 12, at this time the failed drone storage top cover 200 is in a position closing the entrance 101 of the warehouse body 100, so that the plurality of arms of the failed drone 4 abut against the plurality of carriers 3, and the failed drone 4 is stored in the failed drone storage top cover 200, so that the failed drone 4 does not occupy the space of the warehouse body 100, and the failed drone 4 can rotate with the surrounding plate 2 and does not hinder the normal take-off of other drones in the warehouse body 100.

[0077] In the above embodiments, the description of each embodiment has its own focus, and the parts not described in detail in a certain embodiment can be referred to the detailed description of other embodiments above, which will not be repeated here.

[0078] In the implementation, each of the above components or structures can be implemented as an independent entity, or can be combined as the same or several entities, and the specific implementation of each of the above components or structures can refer to the previous embodiments, which will not be repeated here.

[0079] The above describes in detail a failed drone storage top cover, a failed drone storage hangar and a failed drone storage method provided by the embodiments of the present application. The specific examples are applied to describe the principles and implementation modes of the present application. The above embodiment is only used to help understand the method of the present application and its core idea. Meanwhile, for those skilled in the art, according to the idea of the present application, the specific implementation mode and application range will be changed. In summary, the content of the specification should not be understood as a limitation of the present application.

Claims

1. A faulty machine storage hangar, characterized in that, Includes the warehouse body, the storage cover for faulty machines, and the handling equipment; The faulty machine storage top cover includes: a top plate, a surrounding plate, and multiple load-bearing components; The top plate is connected to the enclosure plate, and the top plate and the enclosure plate define a storage cavity with an opening. The end of the enclosure plate near the opening is rotatably connected to the hangar body. Multiple of the aforementioned support members are located in the storage cavity and connected to the enclosure plate, for supporting the arm of the faulty machine; The support member includes a base plate and two side plates connected to the base plate, the base plate and the two side plates defining a slot for accommodating the arm; the base plate is located on the side of the slot away from the top plate; The storage facility contains multiple drones, wherein the faulty drone is one of the multiple drones that has malfunctioned. The transport device is located in the storage body and is used to transport the faulty machine to the storage cavity so that the multiple arms of the faulty machine respectively abut against the multiple carriers.

2. The faulty machine storage hangar as described in claim 1, characterized in that, Multiple load-bearing components constitute at least two load-bearing modules, and at least two of the load-bearing modules are arranged in a direction perpendicular to the top plate.

3. The faulty machine storage hangar as described in claim 2, characterized in that, The multiple carrier components in each of the carrier modules are located on the same horizontal plane.

4. The faulty machine storage hangar as described in claim 1, characterized in that, The handling device includes a bracket connected to the warehouse body, a sliding member slidably connected to the bracket, and a tray rotatably connected to the sliding member.

5. The faulty machine storage hangar as described in claim 4, characterized in that, The tray has a limiting groove for accommodating the body of the faulty machine.

6. The faulty machine storage hangar as described in claim 4, characterized in that, The enclosure has a clearance groove, and a portion of the bracket is located in the clearance groove.

7. The faulty machine storage hangar as described in claim 4, characterized in that, The handling device also includes a telescopic member that is movably connected to the sliding member, and the telescopic member is rotatably connected to the pallet.

8. The faulty machine storage hangar as described in claim 7, characterized in that, The telescopic component includes a cylinder connected to the sliding component, a telescopic rod connected to the cylinder, and a support plate connected to the telescopic rod. The support plate is rotatably connected to the tray.

9. A method for storing faulty machines, characterized in that, Applied to a faulty machine storage rack as described in any one of claims 1 to 8, the method comprises: The transport device moves to the storage location corresponding to the faulty machine and abuts against the bottom of the faulty machine; The transport device moves into the storage cavity and places the faulty machine on a plurality of the carriers, so that the plurality of arms of the faulty machine respectively abut against the plurality of the carriers.

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