CN111688944A - Full-automatic unmanned aerial vehicle cabin - Google Patents

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a full-automatic unmanned aerial vehicle cabin which comprises a box body, a lifting bearing mechanism and a box door mechanism, wherein the lifting bearing mechanism is arranged in the box body, and the box door mechanism is arranged at an opening of the box body and is used for opening or closing the opening; the lifting bearing mechanism is linked with the box door mechanism and is used for driving the unmanned aerial vehicle to pass through the opening and driving the box door mechanism to turn upwards or downwards. Its lift bears mechanism and promotes unmanned aerial vehicle and rises until the in-process outside the release box opening, and lift bears mechanism and also drives the upwards upset of chamber door mechanism and open the opening of box until the opening of box is opened completely, and at this in-process, chamber door mechanism upwards overturns all the time, and chamber door mechanism can not overturn the side of box and occupy the space of box side completely like this, the area after this full-automatic unmanned aerial vehicle cabin opens a door that has significantly reduced.

Description

Full-automatic unmanned aerial vehicle cabin

Technical Field

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a full-automatic unmanned aerial vehicle cabin.

Background

At present, unmanned aerial vehicles are increasingly used in a wide range of applications, for example: the fields of aerial photography, agricultural pesticide spraying, road patrol, exploration and the like; unmanned aerial vehicle is at the in-process that uses, need store the device with unmanned aerial vehicle and use together, the top opening part that stores the device has seted up two chamber doors usually, two chamber doors when opening, need to the translation of both sides to open the top opening that stores the device, so that unmanned aerial vehicle takes off and descends, but the chamber door that two open can occupy the space of box both sides at the in-process of opening, so can cause unmanned aerial vehicle elevating gear's use to have the big problem of area.

Disclosure of Invention

The invention aims to provide a full-automatic unmanned aerial vehicle cabin, and aims to solve the technical problem that the occupied area is large when the full-automatic unmanned aerial vehicle cabin in the prior art is opened.

In order to achieve the purpose, the invention adopts the technical scheme that: a full-automatic unmanned aerial vehicle cabin comprises a box body, a lifting bearing mechanism and a box door mechanism, wherein the lifting bearing mechanism is arranged in the box body, and the box door mechanism is arranged at an opening of the box body and used for opening or closing the opening; the lifting bearing mechanism is linked with the box door mechanism and is used for driving the unmanned aerial vehicle to pass through the opening and driving the box door mechanism to turn upwards or downwards.

Optionally, the box door mechanism includes a box door and a connecting piece, one side of the box door is hinged to the opening and used for opening or closing the opening, one end of the connecting piece is rotatably connected to the lifting bearing mechanism, and the other end of the connecting piece is slidably connected to the box door and slides in a direction perpendicular to the hinge axis of the box door.

Optionally, the door mechanism further comprises a sliding rod and a sliding sleeve, wherein the sliding sleeve is provided with a sliding hole, the sliding rod is arranged in the sliding hole in a penetrating manner, the sliding rod is arranged on the door and is arranged along a direction perpendicular to the hinge axis of the door, and the sliding sleeve is arranged on the connecting piece.

Optionally, the box door mechanism further includes a slide rail and a slide block, the slide block is slidably mounted on the slide rail, the slide rail is mounted on the box door and is arranged along a direction perpendicular to the hinge axis of the box door, and the sliding sleeve is mounted on the connecting piece.

Optionally, the box door mechanism further comprises a rotating shaft, one end of the rotating shaft is fixedly connected with the connecting piece, a rotating hole is formed in the lifting bearing mechanism, and the other end of the rotating shaft is inserted into the rotating hole; or one end of the rotating shaft is fixedly connected with the lifting bearing mechanism, a rotating hole is formed in the connecting piece, and the other end of the rotating shaft is inserted into the rotating hole.

Optionally, the lift load-bearing mechanism includes first lift driving piece, first crane and is used for bearing unmanned aerial vehicle's platform, first lift driving piece install in the box, the platform with first crane is connected, the drive end of first lift driving piece is connected with first crane and is used for driving first crane goes up and down so that the platform stretches out or retracts the opening, chamber door mechanism with first crane links mutually.

Optionally, the lifting and carrying mechanism further comprises a second lifting frame and a second lifting driving member, the second lifting frame is installed on the first lifting frame and located in the first lifting frame, the platform is installed on the second lifting frame, and a driving end of the second lifting driving member is connected with the second lifting frame.

Optionally, the platform includes a loading board, a third lifting driving element and a fixing board, the loading board is installed on the second lifting frame and used for loading the unmanned aerial vehicle, the fixing board is located above the loading board, the third lifting driving element is installed on the second lifting frame, and a driving end of the third lifting driving element is connected with the fixing board.

Optionally, the quantity of fixed plate is two, two the fixed plate interval sets up, the platform still includes mounting panel and two horizontal driving spare, the mounting panel install in the drive end of third lift driving spare, two the horizontal driving spare install in on the mounting panel, two the drive end of horizontal driving spare respectively with two the fixed plate is connected and is used for driving two the fixed plate is close to relatively so that two the fixed plate will unmanned aerial vehicle presss from both sides tightly or unclamps.

Optionally, two the relative both sides portion of fixed plate all is equipped with and is used for the joint breach of unmanned aerial vehicle's stabilizer blade.

One or more technical schemes in the full-automatic unmanned aerial vehicle cabin provided by the invention at least have one of the following technical effects: when the full-automatic unmanned aerial vehicle cabin is used, the full-automatic unmanned aerial vehicle cabin is placed on the ground, and the opening of the box body is arranged upwards; when unmanned aerial vehicle need shift out from the box in, the lift bears the weight of the mechanism and promotes that unmanned aerial vehicle rises until outside releasing the box opening, simultaneously, the lift bears the weight of the mechanism and also drives the upwards upset of box door mechanism and open the opening of box until the box is opened completely, and at foretell in-process, box door mechanism upwards overturns all the time, and box door mechanism can not overturn the side of box and occupy the space of box side completely like this, the area after this full-automatic unmanned aerial vehicle cabin opens the door that has significantly reduced.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise.

Fig. 1 is a schematic structural diagram of a view angle when a door of a cabin of a full-automatic unmanned aerial vehicle is closed according to an embodiment of the present invention.

Fig. 2 is a schematic structural view of the cabin of the full-automatic unmanned aerial vehicle shown in fig. 1 when a part of the door of the cabin is opened.

Fig. 3 is a schematic structural view of the cabin of the full-automatic unmanned aerial vehicle shown in fig. 1 when the door of the cabin is fully opened.

Fig. 4 is a schematic structural view of another view of the cabin of the fully automatic unmanned aerial vehicle shown in fig. 1.

Fig. 5 is a partial enlarged view of a portion a in fig. 4.

Fig. 6 is an exploded view of the cabin of the fully automatic drone shown in fig. 3.

Fig. 7 is a partial enlarged view of fig. 6 at B.

Fig. 8 is a schematic structural view of the connection piece of the full-automatic unmanned aerial vehicle cabin shown in fig. 6.

Fig. 9 is a schematic structural view of the second crane, the platform and the unmanned aerial vehicle of the full-automatic unmanned aerial vehicle cabin shown in fig. 6.

Fig. 10 is an exploded view of the second crane, platform and drone of the fully automated drone nacelle shown in fig. 9.

Wherein, in the figures, the respective reference numerals:

10-box body 11-opening 20-lifting bearing mechanism

21-first lifting frame 22-platform 23-second lifting frame

30-door mechanism 31-door 32-link

33-sliding rod 34-sliding sleeve 35-rotating shaft

36-hinge 40-unmanned aerial vehicle 41-support leg

42-projection 221-bearing plate 222-third lifting driving piece

223-fixing plate 224-horizontal driving piece 225-connecting block

226-mounting plate 321-rotating hole 2231-clamping notch.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to fig. 1-10 are exemplary and intended to be illustrative of the invention and should not be construed as limiting the invention.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

As shown in fig. 1 to 10, in an embodiment of the present invention, a full-automatic unmanned aerial vehicle cabin is provided, which includes a box body 10, a lifting bearing mechanism 20 and a door mechanism 30, wherein the lifting bearing mechanism 20 is disposed in the box body 10, and the lifting bearing mechanism 20 bears an unmanned aerial vehicle 40 and is used for pushing the unmanned aerial vehicle 40 out of the box body 10, so as to facilitate takeoff and landing of the unmanned aerial vehicle 40; the door mechanism 30 is disposed at the opening 11 of the cabinet 10 and opens or closes the opening 11; the lifting bearing mechanism 20 is linked with the door mechanism 30, and is used for driving the unmanned aerial vehicle 40 to turn over upwards or downwards when passing through the opening 11, wherein the lifting bearing mechanism 20 and the door mechanism 30 can adopt a movable connection mode, so that in the process of driving the unmanned aerial vehicle 40 to lift by the lifting bearing mechanism 20, the door mechanism 30 can be driven to turn over upwards to open the opening 11 of the box body 10, or the door mechanism 30 is driven to turn over downwards to close the opening 11 of the box body 10.

Referring to fig. 1 and 2, in the full-automatic unmanned aerial vehicle cabin according to the embodiment of the present invention, in use, the full-automatic unmanned aerial vehicle cabin is placed on the ground and the opening 11 of the box body 10 is disposed upward; when unmanned aerial vehicle 40 need shift out from the box in, lift bearing mechanism 20 promotes unmanned aerial vehicle 40 and rises until pushing out outside box 10 opening 11, and simultaneously, lift bearing mechanism 20 also drives chamber door mechanism 30 and upwards overturns and open the opening 11 of box 10 until the opening 11 of box 10 is opened completely, and at foretell in-process, chamber door mechanism 30 overturns upwards all the time, and chamber door mechanism 30 can not overturn the side of box 10 and occupy the space of box 10 side completely like this, the area after this full-automatic unmanned aerial vehicle cabin opens the door that has significantly reduced.

Further, when unmanned aerial vehicle 40 need store in box 10, go up and down to bear mechanism 20 and move down and accomodate unmanned aerial vehicle 40 in the box 10, and go up and down to bear mechanism 20 and be moving down the in-process, drive unmanned aerial vehicle 40 upset down simultaneously until closing the opening 11 of box 10, so just accomplished accomodating of unmanned aerial vehicle 40 and stored.

In the embodiment, in the process that the full-automatic unmanned aerial vehicle cabin drives the unmanned aerial vehicle 40 to ascend and descend through the lifting bearing mechanism 20, the box door 31 can be driven to open or close the opening 11 of the box body 10, so that a separate device for driving the box door 31 to open or close is not needed, the whole device is simple in structure, convenient and fast to use, and time and labor are saved; in addition, the ascending and descending of the unmanned aerial vehicle 40 and the overturning of the door mechanism 30 are carried out simultaneously, so that the movement time of the whole device is reduced, and the efficiency is improved.

Furthermore, it should be noted that the box 10 includes a frame and a steel plate covering the frame, the box door 31 includes a doorframe and a steel plate installed on the doorframe, and only the frame and the doorframe are shown in fig. 1 to 7.

In another embodiment of the present invention, the door mechanism 30 of the fully automatic unmanned aerial vehicle cabin comprises a door 31 and a link 32, wherein one side of the door 31 is hinged at the opening 11 and is used for opening or closing the opening 11, one end of the link 32 is rotatably connected with the lifting carriage 20, and the other end of the link 32 is slidably connected with the door 31 and slides along a direction perpendicular to the hinge axis of the door 31.

Specifically, in the process that the lifting bearing mechanism 20 drives the unmanned aerial vehicle 40 to ascend, the connecting piece 32 ascends along with the unmanned aerial vehicle 40, and the end part of the connecting piece 32 connected with the box door 31 is gradually far away from the hinged part of the box door 31, so that the box door 31 is pulled upwards, and the box door 31 is turned upwards; when the lifting bearing mechanism 20 drives the unmanned aerial vehicle 40 to move downwards, the end part of the connecting piece 32 connected with the box door 31 gradually moves towards the hinge joint of the box door 31, so that the box door 31 is pulled to turn downwards, and the closing of the box door 31 is realized; in addition, in the process of pushing the door 31 to open and close, the link 32 can rotate relative to the lifting support mechanism 20, so that the link 32 is prevented from being locked with the door 31, and the door 31 can be opened and closed more smoothly and stably.

Further, the number of the doors 31 is two, and the two doors 31 are hinged at two sides of the opening 11 of the box 10, so that the two doors 31 are turned outwards and unfolded towards the box 10 to close the opening 11, and the two doors 31 are turned inwards and unfolded towards the box 10 to close the opening 11 of the box 10.

Furthermore, the door 31 is mounted on the cabinet 10 by the hinge 36, and the hinge 36 is used for connection, so that the mounting mode is simple, and the door 31 is stable and reliable in rotation.

In another embodiment of the invention, referring to fig. 4 and 5, the door mechanism 30 of the full-automatic unmanned aerial vehicle cabin further includes a sliding rod 33 and a sliding sleeve 34, the sliding sleeve 34 is disposed on the sliding rod 33, the sliding rod 33 is mounted on the door 31 and is disposed along a direction perpendicular to a hinge axis of the door 31, and the sliding sleeve 34 is mounted on the connecting member 32. Specifically, the sliding of the sliding sleeve 34 on the sliding rod 33 is realized, so that the sliding of the connecting piece 32 on the door 31 is realized, and in addition, the sliding of the sliding sleeve 34 on the sliding rod 33 is labor-saving and smooth, so that the connecting piece 32 drives the opening and closing operations of the door 31, and the operation is time-saving, labor-saving, stable and smooth.

In another embodiment of the present invention, the door mechanism 30 of the fully automatic unmanned aerial vehicle cabin further includes a slide rail (not shown) and a slide block (not shown), the slide block is slidably mounted on the slide rail, the slide rail is mounted on the door 31 and is arranged along a direction perpendicular to the hinge axis of the door 31, and the sliding sleeve 34 is mounted on the connecting member 32. Specifically, the sliding of the sliding block on the sliding rail is realized, so that the sliding of the connecting piece 32 on the box door 31 is realized, in addition, the sliding of the sliding block on the sliding rail is labor-saving and smooth, and the connecting piece 32 drives the opening and closing operations of the box door 31, so that the time and the labor are saved, and the operation is stable and smooth.

In another embodiment of the present invention, the door mechanism 30 of the cabin of the fully automatic unmanned aerial vehicle further includes a rotating shaft 35, one end of the rotating shaft 35 is fixedly connected to the connecting member 32, the lifting bearing mechanism 20 is provided with a rotating hole 321, and the other end of the rotating shaft 35 is inserted into the rotating hole 321; specifically, the rotating shaft 35 rotates in the rotating hole 321, so that the connecting member 32 and the lifting bearing mechanism 20 are relatively rotatably connected, the sliding movement of the connecting member 32 on the door 31 is adapted, the connecting member 32 is prevented from being stuck between the lifting bearing mechanism 20 and the door 31, the door 31 is ensured to be smoothly opened and closed, and the structure is simple and the connection stability and reliability are good.

In another embodiment of the present invention, referring to fig. 6, 7 and 8, one end of a rotating shaft 35 of the cabin of the fully automatic unmanned aerial vehicle is fixedly connected to the lifting and carrying mechanism 20, a rotating hole 321 is formed on the connecting member 32, and the other end of the rotating shaft 35 is inserted into the rotating hole 321. Specifically, the rotating shaft 35 rotates in the rotating hole 321, so that the connecting member 32 and the lifting support mechanism 20 rotate relatively, the connecting member 32 is prevented from being stuck between the lifting support mechanism 20 and the door 31, the door 31 is ensured to be opened and closed smoothly, and the connecting structure is simple and convenient to assemble.

In another embodiment of the present invention, referring to fig. 1, 2 and 6, the provided lifting and carrying mechanism 20 of the cabin of the fully automatic unmanned aerial vehicle includes a first lifting and carrying driving member (not shown), a first lifting frame 21 and a platform 22 for carrying the unmanned aerial vehicle 40, the first lifting and carrying driving member is installed in the box body 10, the platform 22 is connected with the first lifting frame 21, a driving end of the first lifting and carrying driving member is connected with the first lifting frame 21 and is used for driving the first lifting frame 21 to lift and lower so that the platform 22 extends out of or retracts into the opening 11, and the door mechanism 30 is linked with the first lifting frame 21.

Specifically, the first lifting driving member drives the first lifting frame 21 to move upwards, and the first lifting frame 21 lifts the platform 22 installed on the first lifting frame 21, so that the unmanned aerial vehicle 40 borne on the platform 22 is lifted through the opening 11 of the box body 10, and the unmanned aerial vehicle 40 can take off and land conveniently; after the unmanned aerial vehicle 40 lands on the platform 22, the first lifting driving piece drives the first lifting frame 21 to move downwards, the first lifting frame 21 drives the box door 31 to turn downwards and close, and meanwhile, the unmanned aerial vehicle 40 borne on the platform 22 descends and is stored in the box body 10, so that the storage and storage of the unmanned aerial vehicle 40 are completed; more specifically, the rotating shaft 35 or the rotating hole 321 is disposed at the top of the first lifting frame 21, so that the first lifting frame 21 drives the connecting member 32 to lift and the connecting member 32 drives the door 31 to turn upwards or downwards during the lifting process, thereby opening and closing the opening 11 of the container 10.

In another embodiment of the present invention, referring to fig. 1, 2 and 6, the provided lifting and carrying mechanism 20 of the full-automatic unmanned aerial vehicle cabin further includes a second lifting frame 23 and a second lifting driving member (not shown), the second lifting frame 23 is installed on the first lifting frame 21 and is located in the first lifting frame 21, the lifting platform 22 is installed on the second lifting frame 23, and a driving end of the second lifting driving member is connected to the second lifting frame 23.

Specifically, first lift driving piece drive first crane 21 upwards moves, open the back with chamber door 31 completely, first crane 21 is located the top of box 10, in addition, second lift driving piece drive second crane 23 upwards moves, second crane 23 shifts out platform 22 outside first crane 21, thereby be convenient for the takeoff and the landing of unmanned aerial vehicle 40, and at this moment, platform 22's position is higher than the top position of box 10, this full-automatic unmanned aerial vehicle cabin can lift unmanned aerial vehicle 40 to higher height, can only say that unmanned aerial vehicle 40 lifts the top surface parallel position that box 10 was lifted to unmanned aerial vehicle 40 with current full-automatic unmanned aerial vehicle cabin, the full-automatic unmanned aerial vehicle cabin of the embodiment of the invention adopts the mechanism that the secondary rises, can lift unmanned aerial vehicle 40 to higher height, for example: the unmanned aerial vehicle 40 can be lifted 1.8 times higher than the top surface of the box body 10; in addition, compared with the existing full-automatic unmanned aerial vehicle cabin, on the basis of meeting the same takeoff height, the overall height of the full-automatic unmanned aerial vehicle cabin can be effectively reduced, so that the whole device is smaller in size and more convenient for the unmanned aerial vehicle 40 to use and carry; and, can rise first crane 21 and second crane 23 simultaneously, unmanned aerial vehicle 40 risees like this and goes on simultaneously with opening of chamber door 31, has reduced the movement time, has improved efficiency.

In another embodiment of the present invention, referring to fig. 9 and 10, the platform 22 of the fully automatic unmanned aerial vehicle cabin includes a bearing plate 221, a third lifting driving element 222 and a fixing plate 223, the bearing plate 221 is installed on the second lifting frame 23 and is used for bearing the unmanned aerial vehicle 40, the fixing plate 223 is located above the bearing plate 221, the third lifting driving element 222 is installed on the second lifting frame 23, and a driving end of the third lifting driving element 222 is connected with the fixing plate 223. Specifically, after the unmanned aerial vehicle 40 lands on the bearing plate 221, the third lifting driving member 222 is started, and the third lifting driving member 222 drives the fixing plate 223 to move downwards, so that the fixing plate 223 is pressed on the protrusions 42 on the supporting legs of the unmanned aerial vehicle 40, thereby realizing the fixed locking of the unmanned aerial vehicle 40 and preventing the unmanned aerial vehicle 40 from moving in the second fixing frame and being damaged; when the third lifting driving member 222 is started again, the third lifting driving member 222 drives the fixing plate 223 to move upwards, so that the fixing plate 223 is lifted up from the protrusion 42, the unmanned aerial vehicle 40 is unlocked, and the unmanned aerial vehicle 40 can take off conveniently.

In another embodiment of the present invention, referring to fig. 9 and 10, the number of the fixing plates 223 of the cabin of the fully automatic unmanned aerial vehicle is two, the two fixing plates 223 are arranged at intervals, the platform 22 further includes a mounting plate 226 and two horizontal driving members 224, the mounting plate 226 is mounted at the driving end of the third lifting driving member 222, the two horizontal driving members 224 are mounted on the mounting plate 226, and the driving ends of the two horizontal driving members 224 are respectively connected with the two fixing plates 223 and are used for driving the two fixing plates 223 to relatively approach each other so that the two fixing plates 223 clamp or release the unmanned aerial vehicle 40.

Specifically, the unmanned aerial vehicle 40 is arranged between two fixing plates 223, the two horizontal driving pieces 224 drive the two fixing plates 223 to be relatively close to each other, so that the unmanned aerial vehicle 40 is clamped and fixed, damage caused by movement of the unmanned aerial vehicle 40 on the bearing plate 221 is avoided, the two horizontal driving pieces 224 drive the two fixing plates 223 to be relatively far away from each other, the fixing plates 223 are separated from the unmanned aerial vehicle 40, and clamping and fixing of the unmanned aerial vehicle 40 are removed; in addition, the mounting plate 226 provides a mounting base for the two horizontal driving members 224, the driving end of the third lifting driving member 222 is connected to the mounting plate 226, and the horizontal driving member 224 mounted on the mounting plate 226 is driven to move up and down by the third lifting driving member 222 in the process of driving the mounting plate 226 to lift up and down, so as to realize the up-and-down movement of the fixing plate 223.

In another embodiment of the present invention, referring to fig. 9 and 10, two opposite side portions of two fixing plates 223 of the cabin of the fully automatic drone are provided with clamping notches 2231 for clamping the legs 41 of the drone 40. Specifically, after unmanned aerial vehicle 40 descends on loading board 221, two horizontal drive spare 224 drive two fixed plates 223 respectively and remove towards unmanned aerial vehicle 40 from both sides respectively, block unmanned aerial vehicle 40's landing leg until joint breach 2231, the tight spacing effect that receives joint breach 2231 of the tight clamp of unmanned aerial vehicle 40's landing leg fixed plate 223 makes unmanned aerial vehicle 40 unable to move on loading board 221, unmanned aerial vehicle 40 is better in the fixed reliability of stability in this full-automatic unmanned aerial vehicle cabin.

Further, joint breach 2231 is V type groove, and the 11 width in opening in V type groove is bigger and bigger, and unmanned aerial vehicle 40's landing leg gets into V type inslot easy operation to, along with the removal of fixed plate 223, thereby with unmanned aerial vehicle 40's landing leg card in the bottom in V type groove, thereby realize unmanned aerial vehicle 40's spacing fixed.

Furthermore, the number of the third lifting driving members 222 is two, the two third lifting driving members 222 are respectively connected to two opposite sides of the mounting plate 226, the lifting movement of the mounting plate 226 is stable, so that the fixing plate 223 is stably pressed on the protrusion 42 of the drone 40, and the pressing and fixing of the drone 40 are stable and reliable.

Further, be equipped with four stabilizer blades 41 on the unmanned aerial vehicle 40, four stabilizer blades 41 are located four bights of unmanned aerial vehicle 40 respectively, are equipped with two joint breach 2231 on every fixed plate 223, and four stabilizer blades 41 of unmanned aerial vehicle 40 can block into four joint breachs 2231 respectively like this for unmanned aerial vehicle 40 can't remove in the horizontal plane, and its is fixed reliable and stable.

Furthermore, the platform 22 further includes two connection blocks 225, the third lifting driving member 222 and the horizontal driving member 224 are both located in the second lifting frame 23, the two connection blocks 225 are respectively located at the left and right sides of the loading plate 221, the upper end of the connection block 225 is connected with the fixing plate 223, and the lower end of the connection block 225 is connected with the driving ends of the two horizontal driving members 224, so that the horizontal driving member 224 located below the loading plate 221 is connected with the fixing plate 223, and the overall layout is compact in structure and small in size.

Furthermore, the first lifting driving member, the second lifting driving member, the third lifting driving member 222 and the horizontal driving member 224 are all linear modules, the first lifting driving member, the second lifting driving member and the third lifting driving member 222 are all vertically arranged, so that the vertical movement of the connecting component with the first lifting driving member, the second lifting driving member and the third lifting driving member 222 is realized, and the horizontal arrangement of the horizontal driving member 224 is used for driving the fixing plate 223 connected with the horizontal driving member to translate.

The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (10)

1. The utility model provides a full-automatic unmanned aerial vehicle cabin which characterized in that: the lifting bearing mechanism is arranged in the box body, and the box door mechanism is arranged at an opening of the box body and is used for opening or closing the opening;

the lifting bearing mechanism is linked with the box door mechanism and is used for driving the unmanned aerial vehicle to pass through the opening and driving the box door mechanism to turn upwards or downwards.

2. The fully automatic unmanned aerial vehicle cabin of claim 1, wherein: the box door mechanism comprises a box door and a connecting piece, one side of the box door is hinged to the opening and used for opening or closing the opening, one end of the connecting piece is rotatably connected with the lifting bearing mechanism, and the other end of the connecting piece is connected with the box door in a sliding mode and slides along the direction perpendicular to the hinge axis of the box door.

3. The fully automatic unmanned aerial vehicle cabin of claim 2, wherein: the box door mechanism further comprises a sliding rod and a sliding sleeve, a sliding hole is formed in the sliding sleeve, the sliding rod penetrates through the sliding hole, the sliding rod is installed on the box door and is arranged in the direction perpendicular to the hinge axis of the box door, and the sliding sleeve is installed on the connecting piece.

4. The fully automatic unmanned aerial vehicle cabin of claim 3, wherein: the box door mechanism further comprises a sliding rail and a sliding block, the sliding block is slidably mounted on the sliding rail, the sliding rail is mounted on the box door and arranged along the direction perpendicular to the hinge axis of the box door, and the sliding sleeve is mounted on the connecting piece.

5. The fully automatic unmanned aerial vehicle cabin of claim 2, wherein: the box door mechanism further comprises a rotating shaft, one end of the rotating shaft is fixedly connected with the connecting piece, a rotating hole is formed in the lifting bearing mechanism, and the other end of the rotating shaft is inserted into the rotating hole;

or one end of the rotating shaft is fixedly connected with the lifting bearing mechanism, a rotating hole is formed in the connecting piece, and the other end of the rotating shaft is inserted into the rotating hole.

6. The full-automatic unmanned aerial vehicle cabin of any one of claims 1 ~ 5, characterized in that: the lifting bearing mechanism comprises a first lifting driving piece, a first lifting frame and a platform used for bearing the unmanned aerial vehicle, the first lifting driving piece is installed in the box body, the platform is connected with the first lifting frame, the driving end of the first lifting driving piece is connected with the first lifting frame and used for driving the first lifting frame to lift so that the platform extends out of or retracts into the opening, and the box door mechanism is linked with the first lifting frame.

7. The fully automatic unmanned aerial vehicle cabin of claim 6, wherein: the lifting bearing mechanism further comprises a second lifting frame and a second lifting driving piece, the second lifting frame is installed on the first lifting frame and located in the first lifting frame, the platform is installed on the second lifting frame, and the driving end of the second lifting driving piece is connected with the second lifting frame.

8. The fully automated drone nacelle of claim 7, wherein: the platform includes loading board, third lift driving piece and fixed plate, the loading board install in on the second crane and be used for bearing unmanned aerial vehicle, the fixed plate is located the top of loading board, third lift driving piece install in on the second crane, the drive end of third lift driving piece with the fixed plate is connected.

9. The fully automated drone nacelle of claim 8, wherein: the quantity of fixed plate is two, two the fixed plate interval sets up, the platform still includes mounting panel and two horizontal driving spare, the mounting panel install in the drive end of third lift driving spare, two horizontal driving spare install in on the mounting panel, two horizontal driving spare's drive end respectively with two the fixed plate is connected and is used for driving two the fixed plate is close to relatively so that two the fixed plate will unmanned aerial vehicle presss from both sides tightly or loosens.

10. The fully automated drone nacelle of claim 9, wherein: two the relative both sides portion of fixed plate all is equipped with and is used for the joint breach of unmanned aerial vehicle's stabilizer blade.

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