WO2019019093A1

WO2019019093A1 - Unmanned aerial vehicle assembly

Info

Publication number: WO2019019093A1
Application number: PCT/CN2017/094671
Authority: WO
Inventors: 廖然; 周岱俊
Original assignee: 深圳市大疆创新科技有限公司
Priority date: 2017-07-27
Filing date: 2017-07-27
Publication date: 2019-01-31
Also published as: CN108513554A; CN108513554B

Abstract

Disclosed is an unmanned aerial vehicle assembly, comprising: a first body (10), a second body (20), a position-limiting structure arranged on the first body (10) and/or the second body (20), and a state-sensing device arranged on the first body (10) and/or the second body (20), wherein the position-limiting structure is used for limiting the first body (10) to a pre-set position on the second body (20) so that the first body (10) and the second body (20) are in an assembled state; and the state-sensing device is used to sense the relative state of the first body (10) and the second body (20). The first body (10) comprises a body of an unmanned aerial vehicle or a component of the body of the unmanned aerial vehicle, and the second body (20) involves a remote controller; or, the first body (10) comprises a remote controller or a component of the remote controller, and the second body (20) involves a body of an unmanned aerial vehicle. The body of the unmanned aerial vehicle and/or the remote controller control(s) their/its own corresponding function(s) according to the relative state.

Description

UAV component

Technical field

Embodiments of the present invention relate to the field of drones, and more particularly to a drone assembly.

Background technique

With the development of technology and economy, drones are more and more popular among ordinary consumers or enterprise users because they can complete aerial photography or investigation. They are usually controlled by a remote controller installed at the ground end. Users usually control the remote control. To control the take-off, landing or return of the drone.

In the prior art, the body of the UAV and the remote controller are structurally independent of each other. When in use, the 2.4G or 5.8G wireless signal transmission is generally used between the remote control and the body of the UAV, and when not in use, no The body and remote control of the man-machine are still independent of each other. The separate structure design makes the body and the remote control of the drone need to be placed separately when stored and carried, not portable, and easy to forget the problem, which is very inconvenient.

Summary of the invention

The embodiment of the invention provides a UAV assembly to solve the problem of inconvenient storage and carrying of the remote controller of the UAV existing in the prior art.

An embodiment of the present invention provides a UAV assembly, including: a first body, a second body, a limiting structure disposed on the first body and/or the second body, and being disposed on the first a state sensing device on the body and/or the second body, the limiting structure configured to define the first body at a preset position on the second body such that the first body and the first body The second body is in an assembled state; the state sensing device is configured to sense a relative state of the first body and the second body;

The first body comprises a body of the drone or a component of the body of the drone, and the second body is a remote controller; or the first body comprises a component of a remote controller or a remote controller, and the second body is a drone Body

The body of the drone and/or the remote controller controls itself according to the relative state The corresponding function.

The UAV assembly provided in this embodiment assembles the body of the UAV with the remote controller through the limiting structure, and senses the relative state between the body of the UAV and the remote controller through the state sensing device, so that The body and/or the remote control of the drone adjust its corresponding function according to the relative state, so that the remote controller and the body of the drone can be assembled, are easy to carry, are not easily lost, and can flexibly according to the relative state of the two. Control the corresponding functions of the drone's body and / or remote control.

DRAWINGS

In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly described below. It is obvious that the drawings in the following description are some embodiments of the present invention. Other drawings may also be obtained from those of ordinary skill in the art in view of the drawings.

1 is a schematic view showing a state of a first type of UAV assembly before assembly according to an embodiment of the present invention;

FIG. 2 is a schematic diagram showing the assembled state of the first type of UAV assembly according to an embodiment of the present invention; FIG.

3 is a schematic diagram of a state of a second type of UAV assembly before assembly according to an embodiment of the present invention;

4 is a schematic diagram of a state in the assembly of a second type of UAV assembly according to an embodiment of the present invention;

FIG. 5 is a schematic diagram of a state in assembly of a third type of UAV assembly according to an embodiment of the present invention; FIG.

6 is a schematic diagram of a state in assembly of a fourth type of unmanned aerial vehicle assembly according to an embodiment of the present invention;

FIG. 7 is a schematic diagram of a state of a fifth unmanned aerial vehicle assembly before assembly according to an embodiment of the present invention; FIG.

FIG. 8 is a schematic diagram showing a state in assembly of a fifth type of UAV assembly according to an embodiment of the present invention; FIG.

FIG. 9 is a schematic diagram showing the state of assembly of a sixth type of UAV assembly according to an embodiment of the present invention; Figure

FIG. 10 is a schematic diagram of a state of an assembled UAV assembly according to an embodiment of the present invention; FIG.

FIG. 11 is a schematic diagram of a state of a seventh unmanned aerial vehicle assembly before assembly according to an embodiment of the present invention; FIG.

12 is a schematic diagram showing a state in assembly of a seventh unmanned aerial vehicle assembly according to an embodiment of the present invention;

FIG. 13 is a schematic diagram of a state of an assembled UAV assembly according to an embodiment of the present invention.

Reference mark:

10-first body; 20-second body;

30-drawer; 11-mating;

12-slot; 21-engagement;

22-accommodating chamber; 23-cover;

24-slide; 25-groove;

221-opening; 251- bottom wall;

252-front wall; 253-left side wall;

254-right side wall; 201-separate;

2011- accommodation space.

Detailed ways

The technical solutions in the embodiments of the present invention will be clearly described with reference to the accompanying drawings in the embodiments of the present invention. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without creative efforts are within the scope of the present invention.

It should be noted that when a component is referred to as being "fixed" to another component, it can be directly on the other component or the component can be in the middle. When a component is considered to "connect" another component, it can be directly connected to another component or possibly a central component.

All technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, unless otherwise defined. The terminology used in the description of the present invention is for the purpose of describing particular embodiments and is not intended to limit the invention. The term "and/or" used herein includes any and all combinations of one or more of the associated listed items.

Some embodiments of the present invention are described in detail below with reference to the accompanying drawings. The features of the embodiments and examples described below can be combined with each other without conflict.

Embodiment 1

Referring to FIG. 1 to FIG. 13 , the embodiment provides a UAV assembly, including: a first body 10 and a second body 20 , and a limiting structure disposed on the first body 10 and/or the second body 20 , And a state sensing device disposed on the first body 10 and/or the second body 20, the limiting structure is configured to define the first body 10 at a preset position on the second body 20, so that the first body 10 and the first body 10 The second body 20 is in an assembled state; the state sensing device is configured to sense a relative state of the first body 10 and the second body 20.

The first body 10 includes a component of the body of the drone or the body of the drone, and the second body 20 is a remote controller; or the first body 10 includes a component of a remote controller or a remote controller, and the second body 20 It is the body of the drone. That is, the first body 10 may be assembled in the second body 20 in a complete shape, or the first body 10 may be disassembled into a dispersed component to be assembled in the second body 20. For example, the body of the drone can be disassembled, and some or all of the components such as the battery and the pan/tilt after the disassembly are installed in the remote controller.

It should be noted that, in the embodiment, the body of the UAV can be the UAV itself other than the remote controller in the UAV system.

The limiting structure may be disposed on the first body 10 or the second body 20, or a limiting structure is disposed on the first body 10 and the second body 20. When the finite structure is disposed on the first body 10 and the second body 20, the limiting structures on the first body 10 and the second body 20 may be different, and may be structurally matched to each other, for example, in the first body 10 A latch is disposed on the second body 20 to fix the first body 10 and the second body 20 relative to each other.

It should be noted that, in the assembled state described above, the first body 10 and the second body 20 may be in a relatively fixed state. It is also possible to include the first body 10 and the second body 20 allowing relative movement within a predetermined relative range. For example, the second body 20 is provided with a capacity for accommodating the first body 10 In the nanocavity, the shape of the first body 10 can be matched with the accommodating cavity to prevent the first body 10 from shaking in the second body 20, and the first body 10 and the second body 20 are in a relatively fixed state. Alternatively, the first body 10 is smaller in size than the receiving cavity, and the first body 10 can be shaken in the receiving cavity. The first body 10 and the second body 20 allow relative movement within a predetermined relative range, but can be closed by other structures. The cavity prevents the first body 10 from coming out of the second body 20.

In this embodiment, in the assembled state, the relative positional relationship between the first body 10 and the second body 20 may be the following: in the assembled state, the first body 10 may be located on the outer surface of the second body 20, for example, A body 10 can be adhered to the outer surface of the second body 20. Alternatively, in the assembled state, the first body 10 may be located wholly or partially inside the second body 20. Regardless of the relative position of the first body 10 and the second body 20 in the assembled state, as long as the first body 10 and the second body 20 can be assembled.

The body and/or the remote control of the drone can control its corresponding function according to the relative state described above. The relative state may include at least one of the following: a separated state, an assembled state, an electrically connected state, and a communicated state.

When the state sensing device detects that the remote controller is separated from the body of the drone, the body of the drone is automatically turned on, and each system is preheated, wherein each system may include: a flight control system, a data link system, a launch recovery system, and the like. . When the state sensing device detects that the remote controller and the body of the drone are in an assembled state, a prompt signal may be issued to prompt the user to be assembled. When the state sensing device detects that the remote controller is electrically connected to the body of the drone, the battery of the remote controller can charge the battery of the body of the drone, or the battery of the body of the drone charges the battery of the remote controller. When the state sensing device detects that the remote controller is in communication with the body of the drone, the body data of the drone can be transmitted to the mobile device on the remote controller or the remote controller, or the data of the mobile device or the data of the remote controller can be transmitted. Go to the body of the drone.

The corresponding data interface can be respectively arranged on the body of the drone and the remote controller. When the body of the drone and the remote controller are assembled, the body of the drone and the remote controller can be electrically connected through the data interface. Transmit power in one or two directions. It is also possible that the body of the drone and the remote controller are in an assembled state, and the body of the drone and the remote controller can be communicably connected to transmit data in one direction or two directions.

Of course, when the body of the drone is separated from the remote control, but the distance between the two is relatively close, the electrical connection can be made through the connecting wires, and the communication can be realized through short-distance communication. connection.

In the embodiment, the data transmitted between the body of the drone and the remote controller may include at least one of the following: flight data, photographing, and upgrade package.

In the prior art, there is no physical connection between the body of the drone and the remote controller, and the transmission rate is limited by using the wireless connection, and the power transmission cannot be realized. In fact, the operator will start to transmit a large amount of data after the drone has landed, such as the original picture or high-definition video. In this embodiment, the physical connection method or the near field communication method can be used to transmit data at a faster rate. Two-way transmission of electrical energy can be achieved through an electrical interface.

The embodiment of the invention realizes assembling the body of the drone with the remote controller through the limit structure, and sensing the relative state between the body of the drone and the remote controller through the state sensing device, so that the body of the drone is And/or the remote controller adjusts its corresponding function according to the relative state, so that the remote controller and the body of the drone can be assembled, is convenient to carry, is not easy to be lost, and can flexibly realize the drone according to the relative state of the two. The corresponding functions of the body and / or remote control.

Embodiment 2

As shown in FIG. 1 and FIG. 2, the embodiment provides a UAV component with a specific limit structure. Based on the first embodiment, the above-mentioned limiting structure is a detachable component for detachably connecting the first body 10 and the second body 20. Specifically, the limiting structure may include an engaging portion 21 formed on one of the first body 10 and the second body 20. In FIG. 1 and FIG. 2, the engaging portion is formed on the second body 20, when the card The joint portion 21 is disposed on the other of the first body 10 and the second body 20. In FIGS. 1 and 2, the engaging portion 21 is caught on the first body 10 to connect the first body 10 and the second body. 20 connected together. Of course, the engaging portion 21 can also be formed on the first body 10 and be affixed to the second body 20. The detachable connection between the first body 10 and the second body 20 can also be achieved. The detachable connection between the first body 10 and the second body 20 is realized by the engaging portion 21, and the first body 10 and the second body 20 can be stably fixed and can be easily disassembled.

The engaging portion 21 may be at least one of the following: a hook, an engaging post, and an elastic card.

In this embodiment, preferably, the engaging portion 21 is a hook. As shown in FIG. 1 and FIG. 2, the hook may be disposed on the second body 20. The number of the hooks may be two, and the two hooks may be preset. The spacing is oppositely disposed between the two hooks for the first body 10 to extend into, and the two bodies can provide a balanced clamping force for the first body 10, which is beneficial to ensure the stability of the structure.

The engaging portion 21 can be a snapping post, and the engaging post can be formed on one of the first body 10 and the second body 20. The other one of the first body 10 and the second body 20 can be provided for The engaging groove is matched with the engaging post, and the engaging post is inserted into the engaging groove to fix the first body 10 and the second body 20 relative to each other.

The engaging portion 21 can also be an elastic card. The elastic card can be formed on one of the first body 10 and the second body 20. The elastic card can be a metal elastic card and can be deformed under external force when needed. When the first body 10 is fixed on the second body 20, the elastic card can be bent to catch the other one of the first body 10 and the second body 20, thereby aligning the first body 10 and the second body 20 fixed.

The above-mentioned limiting structure may further include a mating portion 11 formed on the other of the first body 10 and the second body 20. The engaging portion 21 and the engaging portion 11 cooperate to make the first body 10 and the second body 20 Connected disassembled. The stability of the engagement with the engaging portion 21 can be enhanced by the engaging portion 11, so that the first body 10 and the second body 20 do not easily fall off in the assembled state.

The engaging portion 11 may specifically include at least one of the following: a matching groove, a matching hole, and a matching buckle. For example, as shown in FIG. 1 and FIG. 2, a fitting groove is provided on the first body 10, and the fitting groove can be used for hooking the hook so that the hook is not easily detached from the first body 10, so as to further strengthen the first The stability of a body 10 after being connected to the second body 20.

In addition, as another manner of implementing the detachable connection between the first body 10 and the second body 20, the above-mentioned limiting structure may further include at least one of the following: a strap, a magnet, and a velcro. Alternatively, the first body 10 and the second body 20 can be detachably connected together by bolts, screws, and the like, and the detachable connection between the first body 10 and the second body 20 can be implemented in various manners. The situation is chosen.

In this embodiment, the first body 10 and the second body 20 are detachably connected by a detachable component to realize assembly of the first body 10 and the second body 20, and the utility model has the advantages of simple structure, convenient disassembly and assembly, and The structure change of one body 10 and the second body 20 itself is small, and has a small modification cost.

Embodiment 3

The embodiment is based on the first embodiment or the second embodiment. Further, the second body 20 is provided with a receiving cavity 22, and the receiving cavity 22 is configured to fit the first body 10 into the second body 20. The opening 221, in the assembled state, the first body 10 is wholly or partially housed in the accommodating cavity 22, and the cavity wall of the accommodating cavity 22 is provided with the above-mentioned limiting structure.

When the accommodating cavity 22 disposed on the second body 20 houses the first body 10 therein, the size of the first body 10 can be completely matched with the accommodating cavity 22, so that the first body 10 can be just snapped into the accommodating cavity 22, Not easy to shake. Of course, the size of the first body 10 can also be smaller than the size of the accommodating cavity 22, which is not limited in this embodiment.

In the present embodiment, the preset position is the range of motion allowed by the accommodating chamber 22. In the unmanned aerial vehicle assembly of the present embodiment, in the assembled state, since the first body 10 is partially or entirely accommodated in the second body 20, the entire drone assembly can be made small in size and easy to carry.

Embodiment 4

As shown in FIG. 3 to FIG. 5, the present embodiment is an improvement based on the third embodiment. The difference from the third embodiment is that a cover 23 for covering the opening 221 is further provided at the opening 221, and the cover body is provided. 23 is movably coupled to the second body 20 to open or close the opening 221. Of course, as a further optimization, the cover body 23 and/or the second body 20 may further be provided with locking means for locking the cover body 23 and the second body 20 together, for example, a buckle, a limit pin, and the like. In order to ensure that the lid body 23 can maintain the closed state after the lid is closed.

Specifically, the cover body 23 and the second body 20 are movably connected in various manners. For example, the cover body 23 can be slidably connected to the second body 20 or the cover body 23 can be rotatably connected to the second body 20.

As shown in FIG. 3 and FIG. 4 , the cover body 23 is slidably disposed on the second body 20 , and a rail may be disposed between the cover body 23 and the second body 20 , and the cover body 23 can slide along the track on the second body 20 . To open or close the second body 20. The opening and closing operation of the opening of the second body 20 is realized by means of a sliding connection, which has the advantage of simple and convenient operation.

The cover body 23 and the second body 20 are rotatably connected. For example, as shown in FIG. 5, specifically, one end of the cover body 23 can be connected to the second body 20 through a tilting shaft. During the rotation, the cover body 23 can be flipped with respect to the second body 20 as a center, that is, The cover 23 is said to be connected to the second body 20 in an articulated manner.

In another possible manner, the cover body 23 and the second body 20 can also be connected by a rotating shaft, and the cover body 23 rotates relative to the second body 20 about the rotating shaft, that is, the cover body 23 can be in the plane of the opening 221 . The inner rotation is to open or close the opening 221.

The assembling and separating operation process of the unmanned aerial vehicle assembly provided by this embodiment: opening the cover body 23, the first body 10 is placed in the accommodating cavity 22, and the cover body 23 is closed. The lid body 23 is opened, the first body 10 is taken out, and the lid body 23 is closed.

In this embodiment, the first body 10 can be enclosed in the accommodating cavity 22 of the second body 20 through the cover body 23. In the assembled state, only the second body 20 can be seen in appearance, and due to the setting of the cover body 23, A body 10 is not easily detached from the second body 20, and the assembled structure is stable, and the entire drone assembly is minimized in size and is easy to carry.

Embodiment 5

As shown in FIG. 6 , the embodiment is an improvement based on the third embodiment. The difference between the embodiment and the fourth embodiment is that the first body 10 is directly slid into the second body 20 during the assembly process. In the accommodating chamber 22, at least one pair of side walls of the first body 10 are matched with the size of the pair of chamber walls of the accommodating chamber 22 to enable the first body 10 to slide in the direction defined by the chamber wall of the accommodating chamber 22 Within the body 20.

In the present embodiment, the accommodating cavity 22 may be located on the side wall of the second body 20, and the first body 10 is inserted into the second body 20 in a front-rear manner.

The first body 10 is directly pushed into the accommodating chamber 22, and the first body 10 is also not easily detached from the accommodating chamber 22 under the definition of the chamber wall of the accommodating chamber 22. It is only necessary to provide a corresponding accommodating cavity 22 on the second body 20 according to the size of the first body 10 without any other improvement, which is low in cost and simple in operation.

Embodiment 6

As shown in FIG. 7 and FIG. 8 , the embodiment is an improvement based on the third embodiment. The difference between the embodiment and the fifth embodiment is that the drone assembly of the embodiment further includes a drawer 30 and a drawer 30 . In cooperation with the above-described accommodating chamber 22, in the assembled state, the first body 10 is housed in the drawer 30, and the drawer 30 is housed in the accommodating chamber 22. Preferably, the shape of the first body 10 can also cooperate with the inner shape of the drawer 30, so that the first body 10 is not easily shaken in the drawer 30, and is not in the process of pulling the drawer 30, due to the first body 10 Shake and hurt the first body 10.

Similar to the fifth embodiment, the receiving cavity 22 can be located on the side wall of the second body 20, the drawer 30 The second body 20 is loaded into the front and rear propulsion manner.

In addition, it can be understood that, in order to facilitate the pulling of the drawer 30, the outer surface of the side wall of the drawer 30 for closing the opening 221 may be provided with a handle for the operator to pull the drawer 30 through the handle, thereby improving Operability.

A rail (not shown) may be provided between the drawer 30 and the accommodating chamber 22, and a roller for sliding on the rail may be provided on the drawer 30 so that the drawer 30 can smoothly slide in the accommodating chamber 22.

The assembly and separation operation process of the UAV assembly provided by this embodiment: the drawer 30 is pulled out, the first body 10 is placed in the drawer 30, and the drawer 30 is pushed into the accommodating cavity 22. The drawer 30 is pulled out, the first body 10 is taken out, and the drawer 30 is pushed into the accommodating chamber 22.

In this embodiment, the drawer 30 is designed, and the first body 10 is directly placed in the drawer 30 and then pushed into the second body 20. Compared with the fifth embodiment, the first body 10 can be completely closed, and the first body 10 can be ensured. While the second body 20 can be smoothly loaded, the first body 10 can be better protected from damage of the first body 10.

Example 7

The present embodiment is based on any of the above embodiments. Further, as shown in FIG. 9 and FIG. 10, one of the first body 10 and the second body 20 is provided with a sliding portion, the first body 10 and the first The other of the two bodies 20 is provided with a guiding portion, and the sliding portion is slidable along the guiding portion to slide the first body 10 at a predetermined position on the second body 20 at the guiding of the guiding portion. The first body 10 and the second body 20 can be smoothly slid relative to each other by the cooperation of the sliding portion and the guiding portion, so that the first body 10 can be assembled during the assembly of the first body 10 and the second body 20 Each time it slides to a predetermined position of the second body 20 in a predetermined direction, the assembly is more convenient and the operation is more convenient.

As shown in FIG. 9 and FIG. 10, the sliding portion in this embodiment may be a sliding slot 12, and the guiding portion may be a sliding rail 24, and the sliding slot 12 may be disposed on one of the first body 10 and the second body 20. Correspondingly, the slide rail 24 may be disposed on the other of the first body 10 and the second body 20. As shown in FIG. 9 and FIG. 10, the slide rail 12 is disposed on the first body 10, and the chute 24 is disposed on the second body 20. It can be understood that the slide rail 12 can also be disposed on the second body 20, and correspondingly, the sliding slot 24 is disposed on the first body 10.

As an alternative, the sliding portion may also be a sliding sleeve, and the corresponding guiding portion is a guiding rod. Specifically, the sliding sleeve can be hollow tubular, and the guiding rod is inserted into the sliding sleeve to move linearly along the axial direction of the sliding sleeve to realize the sliding guiding effect.

As shown in FIG. 9 and FIG. 10, further, a groove 25 may be formed on the second body 20. The groove 25 includes a bottom wall 251, a front side wall 252, and oppositely disposed left side walls 253 and right side. Wall 254. As a preferred embodiment, the sliding portion or the guiding portion on the second body 20 is formed on the left side wall 253 and/or the right side wall 254, that is, the sliding portion or the guiding portion may be disposed on the left side wall 253. Alternatively, the sliding portion or the guiding portion is provided on the right side wall 254, or a sliding portion or a guiding portion is provided on both the left side wall 253 and the right side wall 254. Correspondingly, the guiding portion or the sliding portion on the first body 10 is formed on two opposite side walls of the first body 10.

In this embodiment, preferably, the number of the sliding portions may be two, and the number of the guiding portions is also two. For example, as shown in FIG. 9 and FIG. 10, the two sliding rails 24 are symmetrically disposed on the left side wall 253 and the right side wall 254. The sliding groove 12 matching the two sliding rails 24 is disposed on the first body 10, so that the first body 10 can slide into the second body in a predetermined direction under the guidance of the sliding rails 24 on the second body 20. In the groove 25 of 20, and the shape of the groove 25 can be matched with the first body 10, the first body 10 can be restricted inside by the groove 25 after being slid into the groove 25, and is not easy to shake easily, and at the same time, concave The design of the slot 25 also facilitates reducing the volume of the first body 10 and the second body 20 after assembly, facilitating portability.

In addition, as an alternative, the sliding portion and the guiding portion may not be disposed on the side wall of the recess 25 or on the side wall of the first body 10. Specifically, the sliding portion or the guiding portion on the second body 20 may be formed on the outer surface of the second body 20, and the guiding portion or the sliding portion on the first body 10 is formed on the bottom wall of the first body 10. In this way, a guiding track is formed between the upper and lower contact surfaces of the first body 10 and the second body 20, and the sliding guiding of the first body 10 and the second body 20 can also be achieved.

Of course, it can be understood that, in this embodiment, the second body 20 can also have the above-mentioned groove 25, and correspondingly, the sliding portion or the guiding portion on the second body 20 can be formed on the second body. On the bottom wall 251 of the recess 20, a guide or sliding portion on the first body 10 is formed on the bottom wall of the first body 10, that is, on the surface opposite to the bottom wall 251 of the second body 20.

Example eight

As shown in FIG. 11 to FIG. 13 , the embodiment may be based on any of the above embodiments. Further, the second body 20 may include a plurality of split bodies 201 that are movably connected to each other, and the plurality of split bodies 201 can adjust the relative positions to The second body 20 is switched in an unfolded state (state shown in FIG. 12) and a closed state (state shown in FIG. 11), wherein in the unfolded state, the second body 20 is formed for accommodation by the first body 10. Accommodate space 2011.

Wherein, the plurality of split bodies 201 can be hinged to each other to achieve an active connection. Alternatively, the plurality of split bodies 201 can be slidably engaged with each other to achieve an active connection. There are many ways to realize the active connection of multiple splits 201, which will not be repeated here.

In this embodiment, the second body 20 is designed to have a plurality of movable connected split bodies 201, and the second body 20 is switched in the unfolded state and the closed state by the deformation of the split body 201, and the first body 10 is accommodated in the unfolded state. The first body 10 and the second body 20 are assembled, and the operability is strong, and compared with the above embodiment, the second body 20 can be closed in the present embodiment, and therefore, the first body 10 and the second body In a state where the body 20 is separated, the second body 20 may have a particularly smaller volume.

In the several embodiments provided by the present invention, the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interfaces, devices or units, which may be electrical, mechanical. Or other forms.

Finally, it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, and are not intended to be limiting; although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art will understand that The technical solutions described in the foregoing embodiments may be modified, or some or all of the technical features may be equivalently replaced; and the modifications or substitutions do not deviate from the technical solutions of the embodiments of the present invention. range.

Claims

A UAV assembly, comprising: a first body, a second body, a limiting structure disposed on the first body and/or the second body, and a first body disposed on the first body And/or a state sensing device on the second body, the limiting structure for defining the first body at a preset position on the second body such that the first body and the first body The second body is in an assembled state; the state sensing device is configured to sense a relative state of the first body and the second body;

The first body comprises a body of the drone or a component of the body of the drone, and the second body is a remote controller; or the first body comprises a component of a remote controller or a remote controller, and the second body is a drone Body

The body of the drone and/or the remote controller controls its respective function according to the relative state.
The UAV assembly according to claim 1, wherein the relative state comprises at least one of a separation state, an assembly state, an electrical connection state, and a communication state.
The drone assembly of claim 1 wherein, in said assembled condition, said first body is located on an outer surface of said second body.
The drone assembly of claim 1 wherein, in said assembled state, said first body is wholly or partially located inside said second body.
The drone assembly of claim 1 wherein said stop structure is a detachable member for detachably attaching said first body to said second body.
The UAV assembly according to claim 5, wherein the limiting structure comprises an engaging portion formed on one of the first body and the second body, the engaging portion being disposed at the The other of the first body and the second body is coupled to the first body and the two bodies.
The UAV assembly according to claim 6, wherein the engaging portion comprises at least one of the following: a hook, an engaging post, and an elastic card.
The UAV assembly according to claim 7, wherein the limiting structure further comprises a fitting portion formed on the other one of the first body and the second body, the engaging portion Cooperating with the mating portion to detachably connect the first body and the second body.
The UAV assembly according to claim 8, wherein the engaging portion comprises at least one of the following: a fitting groove, a fitting hole, and a fitting buckle.
The UAV assembly according to claim 5, wherein the limiting structure comprises at least one of the following: a strap, a magnet, and a Velcro.
The UAV assembly of claim 1 wherein said second body is provided with a receiving cavity, said receiving cavity including an opening for said first body to fit within said second body In the assembled state, the first body is wholly or partially housed in the receiving cavity, and the cavity wall of the receiving cavity is provided with the limiting structure.
The UAV assembly according to claim 11, wherein a cover for covering the opening is further provided at the opening, and the cover is movably connected to the second body to open or close The opening.
The drone assembly of claim 12 wherein said cover is slidably coupled to said second body.
The drone assembly of claim 12 wherein said cover is rotatably coupled to said second body.
The UAV assembly according to claim 14, wherein the cover body and the second body are connected by a flip shaft, and the cover body is turned over with respect to the second body with the flip shaft as a center Or the cover body and the second body are connected by a rotating shaft, and the cover body rotates relative to the second body about the rotating shaft.
The drone assembly of claim 11 wherein said drone assembly further comprises a drawer, said drawer mating with said receiving cavity, said first body receiving in said assembled state Within the drawer, the drawer is received within the receiving cavity.
The drone assembly of claim 11 wherein at least one pair of side walls of said first body match a size of a pair of chamber walls of said receiving chamber to enable said first body to Sliding into the second body in a direction defined by the wall of the chamber.
The UAV assembly according to claim 1, wherein the second body comprises a plurality of separate bodies that are movably connected to each other, and the plurality of separate bodies are capable of adjusting a relative position such that the second body is in an unfolded state. Switching in the closed state, wherein the accommodation space for the first body is formed in the second body in the unfolded state.
The UAV assembly of claim 1 wherein said first body And a sliding portion is disposed on one of the second body, and the other one of the first body and the second body is provided with a guiding portion, the sliding portion is slidable along the guiding portion, The guiding of the first body at the guiding portion is slid into a preset position on the second body.
The UAV assembly according to claim 19, wherein the sliding portion is a sliding rail, and the guiding portion is a sliding groove; or the sliding portion is a sliding sleeve, and the guiding portion is a guiding rod.
The UAV assembly according to claim 19, wherein said second body is formed with a groove, said groove comprising a bottom wall, a front side wall, and opposite left and right side walls .
The UAV assembly according to claim 21, wherein a sliding portion or a guiding portion on the second body is formed on the left side wall and/or the right side wall, on the first body A guide or a sliding portion is formed on two opposite side walls of the first body.
The UAV assembly according to claim 21, wherein a sliding portion or a guiding portion on the second body is formed on an outer surface of the second body, and a guide portion on the first body or A sliding portion is formed on a bottom wall of the first body.
The UAV assembly according to claim 1, wherein in the assembled state, the first body and the second body are electrically connected to transmit electrical energy.
The UAV assembly of claim 1 wherein, in said assembled state, said first body is communicatively coupled to said second body for transmitting data.
The UAV assembly of claim 25, wherein the transmitted data comprises at least one of: flight data, photographs taken, upgrade packages.