CN209938991U

CN209938991U - Unmanned aerial vehicle space station cabin body and unmanned aerial vehicle space station

Info

Publication number: CN209938991U
Application number: CN201920251113.7U
Authority: CN
Inventors: 陈细平; 李湘驰; 李勇高; 陈国情
Original assignee: Shenzhen Lkk Industry Design Co Ltd
Current assignee: Shenzhen Lkk Industry Design Co Ltd
Priority date: 2019-02-27
Filing date: 2019-02-27
Publication date: 2020-01-14
Anticipated expiration: 2029-02-27

Abstract

The utility model discloses an unmanned aerial vehicle space station cabin body and have unmanned aerial vehicle space station of this cabin body, including cabin main part and hatch door, the cabin main part is including the cabin body frame that is used for injecing the cabin board of unmanned aerial vehicle cabin body space and in the inside cabin board that supports, cabin body frame includes the underframe, the side frame, the hatch door includes hatch door frame and hatch door board, the side frame is a plurality of, a plurality of side frames set up in the week portion of underframe frame and respectively with underframe frame fixed connection, and interconnect between the adjacent side frame, the side frame is even number, every two side frame frames set up for the axis axial symmetry of underframe frame, be provided with the slide rail on the at least a pair of relative side frame, the hatch door frame passes through the slide rail. It provides stable in structure's unmanned aerial vehicle space station cabin body structure, and the adoption has this unmanned aerial vehicle space station cabin body structure's unmanned aerial vehicle space station stability good, can effectually protect unmanned aerial vehicle, avoids receiving external adverse circumstances's influence to lead to unmanned aerial vehicle impaired.

Description

Unmanned aerial vehicle space station cabin body and unmanned aerial vehicle space station

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle space station cabin body and unmanned aerial vehicle space station.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

From a technical perspective, unmanned aerial vehicles can be defined as: unmanned helicopters, unmanned fixed wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned umbrella wing aircraft. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient carrying, simple operation, rapid response, rich load, wide task application, low requirement on environment for taking off and landing, and autonomous flight.

These superior capabilities make drones a more efficient tool for power grid line patrols. However, even if the unmanned aerial vehicle patrols the line and compares traditional mode efficiency and has promoted several times, nevertheless along with the increase of task volume, need more flyers to participate in, cause unmanned aerial vehicle running cost's increase, current unmanned aerial vehicle's duration is difficult to satisfy the user demand simultaneously, and the energy storage of constantly returning a journey has very big adverse effect to work efficiency.

To above-mentioned condition, the technical personnel in the field develop unmanned aerial vehicle space station and are used for depositing unmanned aerial vehicle and for the unmanned aerial vehicle energy storage, but do not have comparatively perfect unmanned aerial vehicle space station product at present.

SUMMERY OF THE UTILITY MODEL

The embodiment of the utility model provides an aim at: the utility model provides an unmanned aerial vehicle space station cabin body, its structural stability is strong, can realize the effective protection to unmanned aerial vehicle.

The embodiment of the utility model provides a another aim at: the utility model provides an unmanned aerial vehicle space station, its continuation of the journey problem that can solve unmanned aerial vehicle.

In order to achieve the purpose, the utility model adopts the following technical proposal:

in one aspect, an unmanned aerial vehicle space station cabin is provided, which includes a cabin main body and a cabin door, wherein the cabin main body includes cabin plates for defining an unmanned aerial vehicle cabin space and a cabin frame for supporting the cabin plates inside, the cabin frame includes a bottom frame and side frames, the cabin door includes a door frame and a door plate, the side frames are plural, the side frames are arranged on the periphery of the bottom frame and are respectively and fixedly connected with the bottom frame, and the adjacent side frames are connected with each other, the side frames are even, every two side frames are arranged in axial symmetry with respect to the axis of the bottom frame, at least one pair of opposite side frames are provided with slide rails, and the door frame is connected with the side frames in a relative sliding manner through the slide rails.

As an optimal technical scheme of the unmanned aerial vehicle space station cabin, the bottom frame is of a hexagonal structure, the number of the side frames is six, and the bottom frame is arranged corresponding to six sides of the bottom frame.

As a preferred technical solution of the space station cabin of the unmanned aerial vehicle, the cabin door frame includes a first movable frame and a second movable frame, the first movable frame and the second movable frame have the same shape, and the first movable frame and the second movable frame can jointly form a hexagonal structure having the same shape as the bottom frame.

As a preferable technical scheme of the cabin body of the unmanned aerial vehicle space station, the sliding rails arranged on the side frames arranged oppositely are a first sliding rail and a second sliding rail respectively;

the first movable frame is provided with two first pulley assemblies, and the two first pulley assemblies are respectively arranged relative to the first sliding rail and the second sliding rail so that the first movable frame can move relative to the side frame;

and two second pulley assemblies are arranged on the second movable frame and are respectively arranged relative to the first sliding rail and the second sliding rail, so that the second movable frame can move relative to the side frame.

As an optimal technical scheme of the cabin body of the unmanned aerial vehicle space station, the bottom frame, the side frames and the cabin door frame are respectively constructed by a plurality of stainless steel square pipes.

As an optimal technical scheme of the unmanned aerial vehicle space station cabin body, the stainless steel square pipes are connected with one another in one or more connection modes of riveting, welding and threaded connection.

As a preferable technical scheme of the unmanned aerial vehicle space station cabin body, the number of the cabin plates is the same as that of the cabin body frames, and the corresponding cabin plates are adapted to the shapes of the cabin body frames.

As a preferable technical solution of the cabin body of the unmanned aerial vehicle space station, the cabin plate is detachably connected with the cabin body frame.

As an optimal technical scheme of the unmanned aerial vehicle space station cabin body, a connecting piece is buckled on the cabin body frame, a through hole is formed in the connecting piece, a threaded hole is formed in the cabin body corresponding to the through hole, and the cabin plate is detachably connected with the cabin body frame through a screw.

In another aspect, a drone space station is provided having a drone space station capsule as described above.

The utility model has the advantages that:

it provides stable in structure's unmanned aerial vehicle space station cabin body structure, and the adoption has this unmanned aerial vehicle space station cabin body structure's unmanned aerial vehicle space station stability good, can effectually protect unmanned aerial vehicle, avoids receiving external adverse circumstances's influence to lead to unmanned aerial vehicle impaired.

Drawings

The present invention will be described in further detail with reference to the accompanying drawings and examples.

Fig. 1 is the embodiment of the utility model provides an unmanned aerial vehicle space station decomposes the state schematic diagram.

Fig. 2 is a schematic view of a three-dimensional structure of a cabin frame according to an embodiment of the present invention.

Fig. 3 is the embodiment of the utility model provides an unmanned aerial vehicle space station cabin door is opened and self-align lift platform rises state schematic diagram.

Fig. 4 is the embodiment of the utility model provides an unmanned aerial vehicle space station cabin door is opened and from positioning lift platform descending state schematic diagram.

Fig. 5 is the embodiment of the utility model provides an another visual angle structure schematic diagram of unmanned aerial vehicle space station cabin door open mode.

Fig. 5A is a partial enlarged view of fig. 5 at I.

Fig. 6 is the embodiment of the utility model provides an unmanned aerial vehicle space station is from location lift platform rising state inner structure schematic diagram.

Fig. 7 is the embodiment of the utility model provides an unmanned aerial vehicle space station is from location lift platform decline state inner structure schematic diagram.

Fig. 8 is a schematic view of a three-dimensional structure of a solar cell panel in an open state according to an embodiment of the present invention.

Fig. 9 is a schematic view of the internal structure of the solar cell panel in the open state according to the embodiment of the present invention.

Fig. 9A is a partial enlarged view of fig. 9 at II.

Fig. 10 is a schematic structural view of the open state of the clamping member on the top support plate according to the embodiment of the present invention.

Fig. 11 is a schematic view of another view of the top support plate according to the embodiment of the present invention in an open state of the clamping member.

Fig. 12 is a schematic structural view of a top support plate according to an embodiment of the present invention, showing a clamping member in a closed state.

Fig. 13 is a schematic view of another view angle of the top support plate with the clamping members in the closed state according to the embodiment of the present invention.

In the figure:

1. a cabin frame; 11. a bottom frame; 12. a side frame; 2. a deck board; 3. a cabin door; 31. a hatch frame; 32. a hatch panel; 33. a slide rail; 4. a wireless charging system; 51. a solar panel; 52. a telescoping device; 53. a solar device trough; 54. a top edge limiting groove; 6. a self-positioning lifting platform; 61. a bottom support plate; 62. a clamping member; 621. clamping the guide rail; 622. a clamping block; 63. a top support plate; 64. a support rod assembly; 65. a first support bar; 66. a second support bar; 67. a first support rail; 68. a second support rail; 69. a lift drive; 7. a track mechanism; 8. a drive mechanism; 81. a drive motor; 82. a transmission gear; 83. a drive rack; 84. and a limit switch.

Detailed Description

In order to make the technical problems, technical solutions and technical effects achieved by the present invention more clear, the embodiments of the present invention will be described in further detail with reference to the accompanying drawings, and obviously, the described embodiments are only some embodiments, not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention.

In the description of the present invention, unless otherwise expressly specified or limited, the term "connected" is to be construed broadly and "fixed", e.g., as a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

As shown in fig. 1-13, the present embodiment provides an unmanned aerial vehicle space station, including:

the cabin comprises a cabin frame 1, cabin plates 2 arranged at the bottom and the periphery of the cabin frame 1 and a cabin door 3 arranged at the top of the cabin frame 1; an unmanned aerial vehicle accommodating space is formed inside the cabin body;

the cabin body is used for accommodating the unmanned aerial vehicle, so that the unmanned aerial vehicle can stop in the cabin body and is protected by the cabin body;

specifically, the space station of the unmanned aerial vehicle in this embodiment further includes a heating system, the heating system is disposed in the cabin body and at the bottom of the cabin body, and is capable of generating heat and diffusing the heat into the cabin body;

in this embodiment heating system adopts traditional electrical heating form, and it is right including the device that generates heat the inside space in cabin body heats, evaporates the steam in the cabin body space, avoids causing the unmanned aerial vehicle short circuit.

The unmanned aerial vehicle heating system is characterized by further comprising a wireless charging system 4, wherein the wireless charging system 4 is arranged in parallel with the heating system and used for charging the unmanned aerial vehicle parked in the cabin body;

adopt wireless form of charging to charge for unmanned aerial vehicle in this embodiment, concrete charging structure adopts current wireless charging device's structure, no longer gives unnecessary details here.

Solar energy power supply system, including solar cell panel 51 and solar battery, for unmanned aerial vehicle space station provides the electric energy.

For the power supply of unmanned aerial vehicle space station through setting up solar power supply system in this scheme, can make full use of solar energy resource, because this equipment is applied to field environment usually, illumination is sufficient usually, sets up solar power supply system and can practice thrift the cost by a wide margin.

Simultaneously, still including the power supply system who adopts the power supply cable power supply in this scheme, can guarantee the reliable and stable operation of unmanned aerial vehicle space station through setting up solar energy power supply system and cable power supply system simultaneously, avoid the outage to cause the influence to equipment uses.

The unmanned aerial vehicle space station that provides in this scheme can provide multiple power supply system for unmanned aerial vehicle can obtain stable electric energy through multiple mode, has solved unmanned aerial vehicle's continuation of the journey problem at one stroke.

Specifically, the cabin body in this embodiment includes a cabin body and a cabin door 3, the cabin body includes a cabin plate 2 for defining a cabin space of the unmanned aerial vehicle and a cabin frame 1 for supporting the cabin plate 2 inside, the cabin frame 1 includes a bottom frame 11 and side frames 12, the cabin door 3 includes a door frame 31 and a door plate 32, the side frames 12 are plural, the side frames 12 are disposed on a periphery of the bottom frame 11 and fixedly connected to the bottom frame 11, respectively, and adjacent side frames 12 are connected to each other, the side frames 12 are even, each two side frames 12 are disposed axisymmetrically with respect to an axis of the bottom frame 11, at least one pair of the opposite side frames 12 is provided with a slide rail 33, and the door frame 31 is connected to the side frames 12 in a relatively sliding manner through the slide rail 33.

The cabin body is formed by arranging the cabin body frame 1 and the cabin plates 2, and a stable cabin body structure is formed to resist severe weather such as strong wind, rainstorm and the like.

Still be provided with data transmission device in this scheme simultaneously, the transmission that adopts electric power system's fiber circuit to carry out a large amount of data for unmanned aerial vehicle's the feedback that line data can be quick to control center that patrols, and need not artificial data collection, improve and patrol line efficiency, reduce the cost of labor.

The bottom frame 11 is of a hexagonal structure, the number of the side frames 12 is six, and the side frames are arranged corresponding to six sides of the bottom frame 11; the door frame 31 comprises a first movable frame and a second movable frame, which are identical in shape and together may constitute a hexagonal structure identical in shape to the base frame 11.

The slide rails 33 arranged on the side frames 12 arranged oppositely are a first slide rail 33 and a second slide rail 33 respectively; the first slide rail 33 and the second slide rail 33 are parallel to each other and are respectively disposed on the cabin body.

Two first pulley assemblies are arranged on the first movable frame, and the two first pulley assemblies are respectively arranged relative to the first sliding rail 33 and the second sliding rail 33, so that the first movable frame can move relative to the side frame 12;

the second movable frame is provided with two second pulley assemblies, and the two second pulley assemblies are respectively arranged relative to the first slide rail 33 and the second slide rail 33, so that the second movable frame can move relative to the side frame 12.

When the first movable frame and the second movable frame move relative to the side frames 12, the moving directions of the first movable frame and the second movable frame are opposite, that is, the first movable frame and the second movable frame move in a direction approaching each other or in a direction departing from each other at the same time;

when the unmanned aerial vehicle space station cabin body and the base frame move to the maximum stroke in the approaching direction, the opposite sides of the unmanned aerial vehicle space station cabin body and the base frame are contacted with each other, so that a hexagonal structure with the same shape as the bottom frame 11 is formed, and the unmanned aerial vehicle space station cabin body is closed;

when the unmanned aerial vehicle space station cabin body and the unmanned aerial vehicle space station cabin body move to the maximum stroke in the opposite direction, the unmanned aerial vehicle space station cabin body is opened.

The bottom frame 11, the side frames 12 and the hatch frame 31 are respectively constructed by a plurality of stainless steel square pipes.

The stainless steel square tubes are connected with each other in one or more of riveting, welding and threaded connection.

Specifically, in this embodiment, the stainless steel square tubes are connected by a threaded connection piece.

The number of the cabin plates 2 is the same as that of the cabin body frames 1, and the corresponding cabin plates 2 are matched with the shapes of the cabin body frames 1.

The cabin plate 2 is detachably connected with the cabin body frame 1.

The cabin body frame 1 is provided with a connecting piece in a buckled mode, the connecting piece is provided with a through hole, the cabin body is provided with a threaded hole corresponding to the through hole, and the cabin plate 2 is detachably connected with the cabin body frame 1 through screws.

Preferably, the unmanned aerial vehicle space station of this embodiment, still include from location lift platform 6, from location lift platform 6 includes bottom support plate 61 and top support plate 63 that mutual parallel arrangement set up, bottom support plate 61 with be provided with between the top support plate 63 and be used for the drive the top support version for the bracing piece subassembly 64 of bottom support plate 61 motion, be provided with clamping device on the top support plate 63, clamping device include a plurality of can in gliding clamping piece 62 on the top support plate 63, mutually support between the clamping piece 62 will be placed article clamp on the top support plate 63 is tight, or, releases the clamp to placing article on the top support plate 63.

Set up induction system on lift platform in this scheme, when unmanned aerial vehicle and platform contact, unmanned aerial vehicle triggered induction system, and induction system starts the clamping device action in the self-align lift platform 6 and presss from both sides tightly unmanned aerial vehicle, locks unmanned aerial vehicle to the intermediate position, and rethread control procedure starts the platform and descends, sends into unmanned aerial vehicle in the cabin body.

Specifically, the support rod assembly 64 at least comprises a first support rod 65 and a second support rod 66 which are hinged with each other at the middle part; the first support rod 65 is slidably connected with the bottom support plate 61 and is hinged with the top support plate 63; the second support bar 66 is slidably connected to the top support plate 63 and is hinged to the bottom support plate 61.

A first support guide rail 67 is arranged on the bottom support plate 61, a first guide rail wheel is arranged on the first support rod 65 corresponding to the first support guide rail 67, the first support rod 65 is hinged with the first guide rail wheel, and the first guide rail wheel can move along the first support guide rail 67;

the top support plate 63 is provided with a second support rail 68, the second support rod 66 is provided with a second rail wheel corresponding to the second support rail 68, the second support rod 66 is hinged to the second rail wheel, and the second rail wheel can move along the second support rail 68.

A lifting driving device 69 capable of driving the first supporting rod 65 and the second supporting rod 66 to rotate around a hinge shaft between the first supporting rod 65 and the second supporting rod 66 is arranged between the first supporting rod 65 and the second supporting rod 66.

The lifting driving device 69 is a telescopic rod, the telescopic rod includes a first sleeve and a second sleeve which are sleeved and can move relatively, the first sleeve is hinged to the first supporting rod 65, and the second sleeve is hinged to the second supporting rod 66.

During use, the self-positioning lifting platform 6 is lifted through the relative rotation of the first supporting rod 65 and the second supporting rod 66.

Further, the clamping member 62 includes a clamping rail 621 and a clamping block 622 capable of sliding on the clamping rail 621, and the clamping blocks 622 of a plurality of clamping members 62 can jointly form an annular clamping sleeve.

In the present embodiment, the number of the clamping members 62 is four, and the four clamping members 62 are uniformly arranged in the circumferential direction of a circle centered on the center point of the upper surface of the top support plate 63. The clamping rails 621 are arranged in a length direction along a radial direction of a circle centered on the upper surface of the top support plate 63 as a center point.

The clamping member 62 further comprises a clamping driving means for driving the clamping block 622 to slide on the clamping rail 621.

Preferably, the clamping driving device is a cylinder, a hydraulic cylinder or a stepping motor.

The specific way of driving the clamping block 622 to slide on the clamping rail 621 by using the air cylinder, the hydraulic cylinder and the stepping motor is realized by using a transmission structure commonly used in the prior art, and is not described herein again.

Preferably, the cabin body of the space station for unmanned aerial vehicles described in this embodiment has a top opening, and the cabin door 3 selectively closes or opens the top opening through a movement mechanism, where the movement mechanism includes a track mechanism 7 and a driving mechanism 8 for driving the cabin door 3 to move.

In this embodiment, hatch door 3 is in the closed condition under the condition that unmanned aerial vehicle enters into unmanned aerial vehicle space station completely or unmanned aerial vehicle flies from unmanned aerial vehicle space station, only opens at unmanned aerial vehicle entering or the in-process hatch door 3 that flies from unmanned aerial vehicle space station.

Can effectually avoid the foreign matter to enter into the unmanned aerial vehicle space station by hatch door 3 through setting up hatch door 3, avoid causing the damage and influence the operation to the unmanned aerial vehicle space station.

Specifically, the driving mechanism 8 includes a driving device and a transmission device;

the driving device is a driving motor 81, the transmission device comprises a transmission gear 82 arranged on an output shaft of the driving motor 81 and a transmission rack 83 arranged on the hatch door 3, and the transmission gear 82 is meshed with the transmission rack 83.

Through setting up rack and pinion transmission system, make unmanned aerial vehicle can open or close hatch door 3 through automatic control structure is automatic when contact unmanned aerial vehicle space station platform, let unmanned aerial vehicle space station more intelligent, automatic.

At least one end of the driving rack 83 is provided with a limit switch 84 for limiting a moving distance of the hatch frame 31.

The limit switch 84 can prevent the cabin door 3 from excessive collision, and reduce the damage of the cabin door 3.

The solar power supply system of the present embodiment includes a solar device, which is driven by a telescopic device 52 and can be turned over relative to the deck 2.

Specifically, the cabin frame 1 includes a bottom frame 11, side frames 12, and a door frame 31, wherein a bottom deck 2 is disposed corresponding to the bottom frame 11, a side deck 2 is disposed corresponding to the side frames 12, and a door panel 32 is disposed corresponding to the door frame 31.

The solar device is arranged on the side deck panel 2 and is located on the side of the side deck panel 2 away from the side frames 12. The solar device has a top edge close to one side of the door panel 32 and a bottom edge close to one side of the floor panel, and the side floor panel 2 is provided with a top edge limiting groove 54 corresponding to the top edge, and the solar device can rotate in the top edge limiting groove 54 by taking the top edge as a rotation center.

Specifically, the side deck boards 2 are provided with through holes through which the telescopic devices 52 can pass, and one ends of the telescopic devices 52 are hinged to the side frames 12, and the other ends of the telescopic devices 52 pass through the through holes to be hinged to the solar device.

Preferably, the through hole is a waist-shaped hole, and the length direction of the waist-shaped hole is arranged along the direction perpendicular to the top edge.

The telescopic means 52 comprises a fixed bar and a telescopic bar movable relative to the fixed bar, the movement of the telescopic bar relative to the fixed bar being driven by a hydraulic cylinder, a pneumatic cylinder or a motor.

In order to hide the solar device in the contracted state, the side deck plate 2 is provided with a solar device groove 53 in the scheme, the shape of the solar device groove 53 is adapted to the solar device, and the depth of the solar device groove 53 is greater than or equal to the thickness of the solar device.

Furthermore, in order to make full use of the electric energy obtained through solar energy, the solar energy device further comprises a charging system and an uninterruptible power supply for supplying power to the charging system, wherein the solar energy device is electrically connected with the uninterruptible power supply and stores the electric energy in the uninterruptible power supply.

Simultaneously, still provide a space station formula electric power in this embodiment and patrol line unmanned aerial vehicle system, it has as above unmanned aerial vehicle space station, and can hold in unmanned aerial vehicle in the space station.

This space station formula electric power patrols line unmanned aerial vehicle system has following advantage:

1. unmanned aerial vehicle patrols the line and has improved the speed and the efficiency that electric power was maintained and was overhauld, makes many work ability accomplish rapidly under the environment of complete electrification, has ensured power consumption safety.

2. Adopt unmanned aerial vehicle to carry out conventional transmission line patrolling, can reduce intensity of labour, compare with the line patrolling of someone helicopter, can improve the security of patrolling line operation personnel to reduce cost.

3. The unmanned aerial vehicle has the characteristics of high line patrol speed and instant emergency speed, timely finds defects, provides information, avoids line accident power failure and recovers high power failure cost loss.

4. The remote control shooting can be carried out on the conditions of power transmission ground wires, hardware fittings, insulators, iron tower corrosion and pollution, line corridors and the like, the image data of the power transmission lines are obtained in an all-round mode, and manual climbing and routing inspection are replaced.

5. The space station provides and patrols wireless the charging of line unmanned aerial vehicle, can solve unmanned aerial vehicle continuation of the journey problem.

6. The space station unmanned aerial vehicle 'wind shelter' can resist strong wind, rainstorm and the like, and can solve the problem of weather encountering severe force

7. Space station-air data service platform: the staff only need indoor landing backstage, can long-range commander carry out unmanned aerial vehicle electric power and patrol the line, but video picture and the system running state that remote real-time supervision unmanned aerial vehicle shot simultaneously.

In the description herein, it is to be understood that the terms "upper", "lower", "right", and the like are used in an orientation or positional relationship based on that shown in the drawings for convenience of description and simplicity of operation, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed in a particular orientation, and be operated, and therefore should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used merely for descriptive purposes and are not intended to have any special meaning.

In the description herein, references to the description of "an embodiment," "an example" or the like are intended to 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, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be appropriately combined to form other embodiments as will be appreciated by those skilled in the art.

The technical principle of the present invention is described above with reference to specific embodiments. The description is made for the purpose of illustrating the principles of the invention and should not be construed in any way as limiting the scope of the invention. Based on the explanations herein, those skilled in the art will be able to conceive of other embodiments of the present invention without any inventive effort, which would fall within the scope of the present invention.

Claims

1. The cabin body of the unmanned aerial vehicle space station comprises a cabin body and a cabin door, wherein the cabin body comprises cabin plates for limiting the cabin space of the unmanned aerial vehicle and a cabin body frame for supporting the cabin plates inside, the cabin body frame comprises a bottom frame and side frames, the cabin door comprises a cabin door frame and a cabin door plate, the side frames are multiple, the side frames are arranged on the periphery of the bottom frame and are fixedly connected with the bottom frame respectively, the adjacent side frames are connected with each other, the side frames are even, every two side frames are arranged in axial symmetry relative to the axis of the bottom frame, slide rails are arranged on at least one pair of opposite side frames, and the cabin door frame is connected with the side frames in a relative sliding mode through the slide rails.

2. The unmanned aerial vehicle space station capsule of claim 1, wherein the bottom frame is a hexagonal structure and the number of side frames is six, corresponding to six sides of the bottom frame.

3. The unmanned aerial vehicle space station capsule of claim 2, wherein the door frame comprises a first movable frame and a second movable frame, the first movable frame and the second movable frame being identical in shape and together comprising a hexagonal structure identical in shape to the base frame.

4. The unmanned aerial vehicle space station capsule of claim 3, wherein the slide rails provided on the oppositely disposed side frames are first and second slide rails, respectively;

5. The unmanned aerial vehicle space station capsule of claim 4, wherein the bottom, side, and door frames are each constructed from stainless steel square tubes.

6. The unmanned aerial vehicle space station capsule of claim 5, wherein the stainless steel square tubes are connected to each other by one or more of riveting, welding, and threaded connection.

7. The unmanned aerial vehicle space station capsule of claim 6, wherein the capsule plates are the same number as the capsule frame, and the corresponding capsule plates are adapted to the shape of the capsule frame.

8. The unmanned aerial vehicle space station pod of claim 7, wherein the pod plate is removably connected to the pod frame.

9. The unmanned aerial vehicle space station capsule of claim 8, wherein the capsule body frame is fastened with a connecting member, the connecting member is provided with a through hole, the capsule body is provided with a threaded hole corresponding to the through hole, and the capsule plate is detachably connected with the capsule body frame through a screw.

10. A drone space station having the drone space station capsule of any one of claims 1-9.