CN108513554B - Unmanned aerial vehicle subassembly - Google Patents
Unmanned aerial vehicle subassembly Download PDFInfo
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- CN108513554B CN108513554B CN201780005152.2A CN201780005152A CN108513554B CN 108513554 B CN108513554 B CN 108513554B CN 201780005152 A CN201780005152 A CN 201780005152A CN 108513554 B CN108513554 B CN 108513554B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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Abstract
An unmanned aerial vehicle assembly, comprising: the device comprises a first body (10), a second body (20), a 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 limiting structure is used for limiting the first body (10) at a preset position on the second body (20) so as to enable the first body (10) and the second body (20) to be in an assembled state; the state sensing device is used for sensing the relative state of the first body (10) and the second body (20); the first body (10) comprises an unmanned aerial vehicle body or a component of the unmanned aerial vehicle body, and the second body (20) is a remote controller; or the first body (10) comprises a remote controller or a component of the remote controller, and the second body (20) is an unmanned aerial vehicle body; the body and/or the remote controller of the unmanned aerial vehicle control the corresponding functions of the unmanned aerial vehicle according to the relative state.
Description
Technical Field
The embodiment of the invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle assembly.
Background
Along with the development of science and technology and economy, unmanned aerial vehicle receives ordinary consumer or enterprise user's liking more and more owing to it can accomplish work such as aerial photograph or investigation, and it is controlled by the remote controller that sets up on ground end usually, and the user controls operations such as unmanned aerial vehicle's takeoff, landing or return journey through manipulating the remote controller usually.
Unmanned aerial vehicle's organism and remote controller structurally mutual independence among the prior art, when using, generally adopt 2.4G or 5.8G wireless signal transmission between remote controller and unmanned aerial vehicle's the organism, and when not using, unmanned aerial vehicle's organism and remote controller still mutual independence, the structural design of separation makes unmanned aerial vehicle's organism and remote controller need separately place when depositing and carrying, inconvenient carrying, and the scheduling problem is forgotten to appear easily, it is very inconvenient.
Disclosure of Invention
The embodiment of the invention provides an unmanned aerial vehicle assembly, which is used for solving the problem that a remote controller of an unmanned aerial vehicle in the prior art is inconvenient to store and carry.
An embodiment of the present invention provides an unmanned aerial vehicle assembly, including: the device comprises a first body, a second body, a limiting structure and a state sensing device, wherein the limiting structure is arranged on the first body and/or the second body, and the state sensing device is arranged on the first body and/or the second body; the state sensing device is used for sensing the relative state of the first body and the second body;
the first body comprises an unmanned aerial vehicle body or a component of the unmanned aerial vehicle body, and the second body is a remote controller; or the first body comprises a remote controller or a component of the remote controller, and the second body is an unmanned aerial vehicle body;
the unmanned aerial vehicle's organism and/or the remote controller is according to relative state, the corresponding function of control self.
The unmanned aerial vehicle subassembly that this embodiment provided, organism and the remote controller through limit structure with unmanned aerial vehicle assemble together, and relative state between organism and the remote controller through state sensing device sensing unmanned aerial vehicle, make unmanned aerial vehicle's organism and/or remote controller adjust self corresponding function according to relative state, thereby make remote controller and unmanned aerial vehicle's organism can assemble together, portable, be difficult for losing, and can be according to the corresponding function of relative state control unmanned aerial vehicle's organism and/or remote controller between them in a flexible way.
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 description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are 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 labor.
Fig. 1 is a schematic diagram of a first drone component provided in an embodiment of the present invention in a state before assembly;
fig. 2 is a schematic assembled state diagram of a first drone component according to an embodiment of the present invention;
fig. 3 is a schematic diagram of a second drone component according to an embodiment of the present invention in a state before assembly;
fig. 4 is a schematic diagram of a second drone component in an assembled state according to an embodiment of the present invention;
fig. 5 is a schematic diagram of a third drone component according to an embodiment of the present invention in an assembled state;
fig. 6 is a schematic diagram of a fourth drone component in an assembled state according to an embodiment of the present invention;
fig. 7 is a schematic diagram of a fifth drone component according to an embodiment of the present invention in a state before assembly;
fig. 8 is a schematic diagram illustrating an assembled state of a fifth drone component according to an embodiment of the present invention;
fig. 9 is a schematic diagram illustrating a sixth drone component according to an embodiment of the present invention in an assembled state;
fig. 10 is an assembled state diagram of a sixth drone component according to an embodiment of the present invention;
fig. 11 is a schematic diagram illustrating a seventh drone component according to an embodiment of the present invention in a state before assembly;
fig. 12 is a schematic diagram illustrating an assembled state of a seventh drone component according to an embodiment of the present invention;
fig. 13 is an assembled state schematic diagram of a seventh drone component according to an embodiment of the present invention.
Reference numerals:
10-a first body; 20-a second body;
30-a drawer; 11-a mating portion;
12-a chute; 21-an engaging portion;
22-a containment chamber; 23-a cover body;
24-a slide rail; 25-a groove;
221-opening; 251-a bottom wall;
252-a front side wall; 253-left side wall;
254-right side wall; 201-split;
2011-accommodation space.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present.
Unless defined otherwise, 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. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Some embodiments of the invention are described in detail below with reference to the accompanying drawings. The embodiments described below and the features of the embodiments can be combined with each other without conflict.
Example one
Referring to fig. 1 to 13, the present embodiment provides an unmanned aerial vehicle assembly, including: the electronic device comprises a first body 10, a second body 20, a 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 limiting structure is used for limiting the first body 10 at a preset position on the second body 20 so that the first body 10 and the second body 20 are in an assembled state; the state sensing device is used for sensing the relative state of the first body 10 and the second body 20.
The first body 10 comprises an unmanned aerial vehicle body or a component of the unmanned aerial vehicle body, and the second body 20 is a remote controller; or, first body 10 includes the component part of remote controller or remote controller, and second body 20 is unmanned aerial vehicle's organism. 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 discrete parts and assembled in the second body 20. For example, the organism of unmanned aerial vehicle can be decomposed, and some or all spare parts such as battery, cloud platform after the decomposition are installed in the remote controller.
It should be noted that, in this embodiment, the body of the drone may be the drone itself in the drone system except for the remote controller.
The limiting structures may be disposed on the first body 10, or on the second body 20, or on both the first body 10 and the second body 20. When the first body 10 and the second body 20 are both provided with the limiting structures, the limiting structures on the first body 10 and the second body 20 may be different and may be structurally matched with each other, for example, a buckle is provided on the first body 10, and a slot is provided on the second body 20, so that the first body 10 and the second body 20 are relatively fixed.
In the assembled state, the first body 10 and the second body 20 may be fixed to each other. It may further comprise that the first body 10 and the second body 20 allow a relative movement within a preset relative range. For example, the second body 20 is provided with an accommodating cavity for accommodating the first body 10, 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. Or, the size of the first body 10 is smaller than that of the accommodating cavity, the first body 10 can rock in the accommodating cavity, the first body 10 and the second body 20 are allowed to move relatively within a preset relative range, but the accommodating cavity can be closed by other structures to prevent the first body 10 from being separated from the second body 20.
In this embodiment, in the assembled state, the relative position relationship between the first body 10 and the second body 20 may be as follows: in the assembled state, the first body 10 may be located on an outer surface of the second body 20, for example, the first body 10 may be adhered to the outer surface of the second body 20. Alternatively, in the assembled state, the first body 10 may be wholly or partially located inside the second body 20. Regardless of the relative positions of the first body 10 and the second body 20 in the assembled state, it is sufficient if the first body 10 and the second body 20 can be assembled together.
The organism and/or the remote controller of unmanned aerial vehicle can be according to above-mentioned relative state, control the corresponding function of self. The relative state may include at least one of: a detached state, an assembled state, an electrically connected state, a communication state.
When state sensing device detects remote controller and unmanned aerial vehicle's organism separation, unmanned aerial vehicle's organism is automatic to be started up, and each system preheats, and wherein, each system can include: flight control system, data link system, launch recovery system, etc. When state sensing device detects that remote controller and unmanned aerial vehicle's organism are in the assembled state, can send cue signal suggestion user and assemble the position. When state sensing device detected that remote controller and unmanned aerial vehicle's organism is in the electricity connection state, the battery of remote controller can charge for unmanned aerial vehicle's organism battery, or unmanned aerial vehicle's organism battery charges for the battery of remote controller. When state sensing device detects that remote controller and unmanned aerial vehicle's organism is in the communication state, unmanned aerial vehicle's organism data can transmit the mobile device on remote controller or the remote controller, perhaps, mobile device data or remote controller data can transmit unmanned aerial vehicle's organism.
Can be equipped with corresponding data interface on unmanned aerial vehicle's organism and the remote controller respectively, be in under the equipment state at unmanned aerial vehicle's organism and remote controller, unmanned aerial vehicle's organism can be connected through data interface electricity with the remote controller to one-way or two-way transmission electric energy. Can also be in under the equipment state at unmanned aerial vehicle's organism and remote controller, unmanned aerial vehicle's organism and remote controller can communication connection to one-way or two-way transmission data.
Of course, when unmanned aerial vehicle's organism and remote controller were in the separation state, but when the distance between the two was nearer, can realize the electricity through connecting wire and connect, can also realize communication connection through near field communication.
The data transmitted between the body of the unmanned aerial vehicle and the remote controller in this embodiment may include at least one of: flight data, taking pictures and upgrading the package.
Among the prior art, there is not the interface of physical connection between unmanned aerial vehicle's the organism and the remote controller, and the mode transmission rate that uses wireless connection is limited, and can't realize the transport of electric energy. In fact, the operator can start to transmit a large amount of data after the unmanned aerial vehicle lands, such as an original picture or a high-definition video, the data can be transmitted at a faster rate by adopting a physical connection mode or a near field communication mode, and bidirectional transmission of electric energy can be realized through an electric interface.
According to the embodiment of the invention, the body of the unmanned aerial vehicle and the remote controller are assembled together through the limiting structure, and the relative state between the body of the unmanned aerial vehicle and the remote controller is sensed through the state sensing device, so that the body of the unmanned aerial vehicle and/or the remote controller can adjust the corresponding functions according to the relative state, and the remote controller and the body of the unmanned aerial vehicle can be assembled together, are convenient to carry and difficult to lose, and can flexibly realize the corresponding functions of the body of the unmanned aerial vehicle and/or the remote controller according to the relative state of the body of the unmanned aerial vehicle and/or the remote controller.
Example two
As shown in fig. 1 and 2, the present embodiment provides an unmanned aerial vehicle assembly with a specific limiting structure. According to the first embodiment, the above-mentioned limiting structure is a detachable component for detachably connecting the first body 10 and the second body 20 together. Specifically, the limiting structure may include a clamping portion 21 formed on one of the first body 10 and the second body 20, in fig. 1 and 2, the clamping portion is formed on the second body 20, and when the clamping portion 21 is disposed on the other one of the first body 10 and the second body 20, in fig. 1 and 2, the clamping portion 21 is clamped on the first body 10 to connect the first body 10 and the second body 20 together. Of course, the engaging portion 21 may be formed on the first body 10 and engaged with the second body 20, and the first body 10 and the second body 20 may be detachably connected. The detachable connection between the first body 10 and the second body 20 is realized through the engaging portion 21, so that the first body 10 and the second body 20 can be stably fixed and can be conveniently detached.
The engaging portion 21 may be at least one of: the couple, block post, elasticity 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 disposed oppositely at a predetermined interval, and between the two hooks, the first body 10 may extend into the first body, and the two hooks may provide balanced engaging force for the first body 10, which is beneficial to ensuring the stability of the structure.
The engaging portion 21 may be an engaging post, the engaging post may be formed on one of the first body 10 and the second body 20, and an engaging groove for engaging with the engaging post may be formed on the other of the first body 10 and the second body 20, and the engaging post is inserted into the engaging groove to relatively fix the first body 10 and the second body 20.
The engaging portion 21 may also be an elastic clip, the elastic clip may be formed on one of the first body 10 and the second body 20, and the elastic clip may be a metal elastic clip and may deform under the action of an external force, when the first body 10 needs to be fixed on the second body 20, the elastic clip may be bent to another one of the first body 10 and the second body 20, so as to relatively fix the first body 10 and the second body 20.
The above-mentioned limit structure may further include an engaging portion 11 formed on the other one of the first body 10 and the second body 20, and the engaging portion 21 and the engaging portion 11 cooperate to detachably connect the first body 10 and the second body 20. 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 cannot easily fall off in the assembled state.
The fitting portion 11 may specifically include at least one of: the cooperation groove, the cooperation hole, cooperation buckle. For example, as shown in fig. 1 and 2, a fitting groove is provided on the first body 10, and the fitting groove can be used for the hook to be snapped into, so that the hook is not easy to fall off from the first body 10, and the stability after the first body 10 is connected to the second body 20 is further enhanced.
In addition, as another way of implementing the detachable connection between the first body 10 and the second body 20, the limiting structure may further include at least one of the following: bandage, magnet, magic subsides. Or, the first body 10 and the second body 20 can be detachably connected together through a bolt, a screw and other parts, so that the detachable connection of the first body 10 and the second body 20 can be realized in various ways, and the detachable connection can be specifically selected according to actual conditions.
The first body 10 and the second body 20 are detachably connected through the detachable part in the embodiment, so that the first body 10 and the second body 20 are assembled, the detachable part has the advantages of being simple in structure and convenient to disassemble and assemble, structural changes of the first body 10 and the second body 20 are small, and the detachable part has small transformation cost.
EXAMPLE III
In this embodiment, on the basis of the first embodiment or the second embodiment, further, the accommodating cavity 22 is provided on the second body 20, the accommodating cavity 22 includes an opening 221 for the first body 10 to be installed in the second body 20, in an assembled state, the first body 10 is wholly or partially accommodated 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 formed in the second body 20 accommodates the first body 10, 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 clamped into the accommodating cavity 22 and is not easy to shake. Of course, the size of the first body 10 may also be smaller than the size of the accommodating cavity 22, and the embodiment is not limited herein.
In the present embodiment, the preset position is a movable range allowed by the accommodating chamber 22. At the unmanned aerial vehicle subassembly of this embodiment, under the assembled condition, because first body 10 part or whole accommodate in second body 20, consequently, can be so that whole unmanned aerial vehicle subassembly's volume is less, portable.
Example four
As shown in fig. 3 to 5, the present embodiment is an improvement on the third embodiment, and is different from the third embodiment in that a cover 23 for covering the opening 221 is further disposed at the opening 221, and the cover 23 is movably connected to the second body 20 to open or close the opening 221. Of course, as a further optimization, the cover 23 and/or the second body 20 may further be provided with a locking device for locking the cover 23 and the second body 20 together, such as: a buckle, a limit pin and the like to ensure that the cover body 23 can keep a cover closing state after the cover is closed.
Specifically, the cover 23 is movably connected to the second body 20 in various ways, for example, the cover 23 may be slidably connected to the second body 20 or the cover 23 may be rotatably connected to the second body 20.
As shown in fig. 3 and 4, the cover 23 is slidably disposed on the second body 20, a rail may be disposed between the cover 23 and the second body 20, and the cover 23 may be slidable on the second body 20 along the rail to open or close the second body 20. The opening and closing operation of the opening of the second body 20 is realized by the sliding connection mode, and the operation is simple and convenient.
The cover 23 is rotatably connected to the second body 20. For example, as shown in fig. 5, in particular, one end of the cover 23 may be connected to the second body 20 through a flip shaft, and during the rotation, the cover 23 may be flipped with respect to the second body 20 centering on the flip shaft, that is, the cover 23 is connected to the second body 20 in a hinged manner.
Alternatively, the cover 23 and the second body 20 may be connected by a rotating shaft, and the cover 23 rotates relative to the second body 20 around the rotating shaft, that is, the cover 23 may rotate in the plane of the opening 221 to open or close the opening 221.
The unmanned aerial vehicle subassembly's that this embodiment provided equipment and separation operation process: the cover 23 is opened, the first body 10 is placed in the accommodating chamber 22, and the cover 23 is closed. The lid 23 is opened, the first body 10 is taken out, and the lid 23 is closed.
This embodiment can seal first body 10 in the chamber 22 that holds of second body 20 through lid 23, under the assembled state, can only see second body 20 in the outward appearance, and because the setting of lid 23 for first body 10 is difficult for droing from second body 20, stable in structure after the equipment, and has realized whole unmanned aerial vehicle subassembly volume minimizing, portable to the at utmost.
EXAMPLE five
As shown in fig. 6, this embodiment is an improvement on the third embodiment, and is different from the fourth embodiment in that, in the assembling process, the first body 10 is directly slid into the accommodating cavity 22 of the second body 20, and at least one pair of side walls of the first body 10 matches with a pair of cavity walls of the accommodating cavity 22 in size, so that the first body 10 can be slid into the second body 20 along the direction defined by the cavity walls of the accommodating cavity 22.
In this embodiment, the receiving cavity 22 may be located on a sidewall of the second body 20, and the first body 10 is inserted into the second body 20 in a back-and-forth pushing manner.
The first body 10 is pushed directly into the accommodating cavity 22, and the first body 10 is not easily pulled out of the accommodating cavity 22 under the limitation of the cavity wall of the accommodating cavity 22. The corresponding accommodation chamber 22 is only needed to be arranged on the second body 20 according to the size of the first body 10 in structure, other modifications are not needed, the cost is low, and the operation is simple.
EXAMPLE six
As shown in fig. 7 and 8, the present embodiment is an improvement on the basis of the third embodiment, and the difference between the present embodiment and the fifth embodiment is that the unmanned aerial vehicle assembly of the present embodiment further includes a drawer 30, the drawer 30 is matched with the accommodating cavity 22, in an assembled state, the first body 10 is accommodated in the drawer 30, and the drawer 30 is accommodated in the accommodating cavity 22. Preferably, the shape of the first body 10 may also match with the internal shape of the drawer 30, so that the first body 10 is not easily shaken in the drawer 30, and the first body 10 is not damaged due to shaking of the first body 10 in the process of drawing the drawer 30.
Similar to the fifth embodiment, the receiving cavity 22 may be located on a side wall of the second body 20, and the drawer 30 is loaded into the second body 20 in a front-rear pushing manner.
In addition, it can be understood that, in order to facilitate the drawing of the drawer 30, the outer surface of the sidewall of the drawer 30 for closing the opening 221 may be provided with a handle, so that an operator can draw the drawer 30 through the handle, thereby improving operability.
A rail (not shown) may be provided between the drawer 30 and the receiving chamber 22, and rollers may be provided on the drawer 30 to slide on the rail, so that the drawer 30 can smoothly slide in the receiving chamber 22.
The unmanned aerial vehicle subassembly's that this embodiment provided equipment and separation operation process: the drawer 30 is pulled out, the first body 10 is put into the drawer 30, and the drawer 30 is pushed into the accommodating chamber 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.
EXAMPLE seven
In this embodiment, on the basis of any of the above embodiments, as shown in fig. 9 and 10, one of the first body 10 and the second body 20 is provided with a sliding portion, and the other of the first body 10 and the second body 20 is provided with a guiding portion, and the sliding portion is slidable along the guiding portion, so that the first body 10 slides into a preset position on the second body 20 under the guidance of the guiding portion. Through the cooperation of sliding part and guide part, can further guarantee that first body 10 and second body 20 can smoothly relative slip for in-process of assembling first body 10 with second body 20, first body 10 can all slide to the preset position of second body 20 along predetermined direction at every turn, makes the equipment more convenient, and the operation is more convenient.
As shown in fig. 9 and 10, the sliding portion in the present embodiment may be a sliding groove 12, the guiding portion may be a sliding rail 24, the sliding groove 12 may be disposed on one of the first body 10 and the second body 20, and correspondingly, the sliding rail 24 may be disposed on the other of the first body 10 and the second body 20. As shown in fig. 9 and 10, the slide rail 12 is provided on the first body 10, and the slide groove 24 is provided on the second body 20. It is of course understood that the slide rail 12 may also be provided on the second body 20, and correspondingly, the slide groove 24 is provided on the first body 10.
As other alternatives, the sliding part may also be a sliding sleeve, and the corresponding guiding part is a guiding rod. Specifically, the sliding sleeve can be in a hollow tubular shape, and the guide rod is inserted into the sliding sleeve to linearly move along the axial direction of the sliding sleeve, so that the sliding guide effect is realized.
As shown in fig. 9 and 10, further, a groove 25 may be formed on the second body 20, and the groove 25 includes a bottom wall 251, a front side wall 252, and a left side wall 253 and a right side wall 254 which are oppositely arranged. As a preferred embodiment, the sliding or 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 or guiding portion may be provided on the left side wall 253, or the sliding or guiding portion may be provided on the right side wall 254, or both the sliding or guiding portion may be provided on the left side wall 253 and the right side wall 254. And correspondingly, the guide portions or the sliding portions on the first body 10 are formed on two opposite sidewalls of the first body 10.
Preferably, in the present embodiment, 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 10, two sliding rails 24 are symmetrically disposed on the left side wall 253 and the right side wall 254, and a sliding groove 12 matched with the two sliding rails 24 is disposed on the first body 10, so that the first body 10 can slide into the groove 25 of the second body 20 along a predetermined direction under the guidance of the sliding rails 24 on the second body 20, and the shape of the groove 25 can be matched with the first body 10, and the first body 10 can be limited inside by the groove 25 after sliding into the groove 25, and is not easy to shake, and meanwhile, the design of the groove 25 is also beneficial to reducing the volume of the first body 10 after being assembled with the second body 20, and is convenient to carry.
In addition, as an alternative, the sliding portion and the guide portion may not be provided on the sidewall of the groove 25 or the sidewall of the first body 10. Specifically, the sliding portion or the guide portion on the second body 20 may be formed on the outer surface of the second body 20, and the guide 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 guide rail is formed between upper and lower contact surfaces of the first body 10 and the second body 20, and the sliding guide function of the first body 10 and the second body 20 can be also achieved.
Of course, it is understood that in this embodiment, the second body 20 may also have the groove 25 described above, and correspondingly, the sliding portion or guide portion on the second body 20 may be formed on the bottom wall 251 of the groove of the second body 20, and the guide portion or sliding portion on the first body 10 may be 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 13, the present embodiment may be based on any one of the above embodiments, and further, the second body 20 may include a plurality of split bodies 201 movably connected to each other, and the plurality of split bodies 201 can adjust relative positions so as to switch the second body 20 between an expanded state (a state shown in fig. 12) in which an accommodating space 2011 for accommodating the first body 10 is formed in the second body 20 and a closed state (a state shown in fig. 11).
Wherein, a plurality of the split bodies 201 can be hinged with each other to realize the movable connection. Alternatively, the plurality of the sub-bodies 201 can be movably connected with each other in a sliding fit manner. There are various ways to realize the movable connection of the plurality of the split bodies 201, which are not described herein.
In the present embodiment, by designing the second body 20 to have a plurality of movably connected split bodies 201, the second body 20 is switched between the unfolded state and the folded state by the deformation of the split bodies 201, and the first body 10 is accommodated in the unfolded state, so that the first body 10 and the second body 20 are in the assembled state, and the operability is strong, and compared with the above-mentioned embodiment, since the second body 20 can be folded, in the state where the first body 10 and the second body 20 are separated, the second body 20 can be smaller in volume.
In the embodiments of the present invention, the shown or discussed mutual coupling or direct coupling or communication connection may be an indirect coupling or communication connection through some interfaces, devices or units, and may be in an electrical, mechanical or other form.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (25)
1. An unmanned aerial vehicle assembly, comprising: the device comprises a first body, a second body, a limiting structure and a state sensing device, wherein the limiting structure is arranged on the first body and/or the second body, and the state sensing device is arranged on the first body and/or the second body; the state sensing device is used for sensing a relative state of the first body and the second body, and the relative state comprises at least one of the following states: a separation state, an assembly state, an electrical connection state, and a communication state;
the first body comprises an unmanned aerial vehicle body or a component of the unmanned aerial vehicle body, and the second body is a remote controller; or the first body comprises a remote controller or a component of the remote controller, and the second body is an unmanned aerial vehicle body;
the body of the unmanned aerial vehicle and/or the remote controller control the corresponding functions of the unmanned aerial vehicle according to the relative state;
when the state sensing device detects that the remote controller is separated from the unmanned aerial vehicle body, the unmanned aerial vehicle body is automatically started.
2. A drone assembly according to claim 1, wherein in the assembled state the first body is located on an outer surface of the second body.
3. A drone assembly according to claim 1, characterised in that in the assembled state the first body is wholly or partially inside the second body.
4. The drone assembly of claim 1, wherein the stop structure is a detachable component for detachably connecting the first body with the second body.
5. The drone assembly of claim 4, wherein the restraining structure includes a snap-fit portion formed on one of the first and second bodies, the snap-fit portion being provided on the other of the first and second bodies to connect the first and second bodies together.
6. The drone assembly of claim 5, wherein the snap-fit portion includes at least one of: the couple, block post, elasticity card.
7. The drone assembly of claim 6, wherein the restraining structure further includes an engagement portion formed on the other of the first body and the second body, the engagement portion engaging the engagement portion to removably connect the first body to the second body.
8. The drone assembly of claim 7, wherein the engagement portion includes at least one of: the cooperation groove, the cooperation hole, cooperation buckle.
9. The drone assembly of claim 4, wherein the limit structure includes at least one of: bandage, magnet, magic subsides.
10. The UAV assembly according to claim 1, wherein the second body has a receiving cavity therein, the receiving cavity includes an opening for the first body to fit into the second body, in the assembled state, the first body is wholly or partially received in the receiving cavity, and the cavity wall of the receiving cavity is provided with the limiting structure.
11. The drone assembly of claim 10, further including a cover disposed at the opening for covering the opening, the cover being movably connected to the second body to open or close the opening.
12. The drone assembly of claim 11, wherein the cover is slidably connected with the second body.
13. The drone assembly of claim 11, wherein the cover is rotationally connected with the second body.
14. The drone assembly of claim 13, wherein the cover is connected to the second body by a flip shaft, the cover flipping over relative to the second body centered on the flip shaft; or, the cover body is connected with the second body through a rotating shaft, and the cover body rotates relative to the second body by taking the rotating shaft as a center.
15. The drone assembly of claim 10, further comprising a drawer that mates with the receiving cavity, the first body received within the drawer in the assembled state, the drawer received within the receiving cavity.
16. The drone assembly of claim 10, wherein the at least one pair of side walls of the first body match a size of a pair of cavity walls of the housing cavity to enable the first body to slide into the second body in a direction defined by the cavity walls of the housing cavity.
17. The drone assembly of claim 1, wherein the second body includes a plurality of separate bodies that are movably connected to each other, the plurality of separate bodies being adjustable in relative position to switch the second body between an expanded state in which an accommodation space for the first body to accommodate is formed therein and a closed state.
18. The UAV assembly according to claim 1, wherein one of the first body and the second body is provided with a sliding portion, and the other of the first body and the second body is provided with a guiding portion, and the sliding portion is slidable along the guiding portion so that the first body slides into a preset position on the second body under the guidance of the guiding portion.
19. The drone assembly of claim 18, wherein the sliding portion is a sliding track and the guide portion is a sliding slot; or, the sliding part is a sliding sleeve, and the guide part is a guide rod.
20. The drone assembly of claim 18, wherein the second body has a recess formed therein, the recess including a bottom wall, a front side wall, and oppositely disposed left and right side walls.
21. A drone assembly according to claim 20, characterised in that the slides or guides on the second body are formed on the left and/or right side wall and the guides or slides on the first body are formed on two opposite side walls of the first body.
22. A drone assembly according to claim 20, characterised in that the sliding or guiding portion on the second body is formed on an outer surface of the second body and the guiding or sliding portion on the first body is formed on a bottom wall of the first body.
23. A drone assembly according to claim 1, wherein in the assembled state, the first and second bodies are electrically connected to transmit electrical energy.
24. A drone assembly according to claim 1, wherein in the assembled state the first body is communicatively connected with the second body to transmit data.
25. A drone assembly according to claim 24, wherein the transmitted data includes at least one of: flight data, taking pictures and upgrading the package.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2017/094671 WO2019019093A1 (en) | 2017-07-27 | 2017-07-27 | Unmanned aerial vehicle assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108513554A CN108513554A (en) | 2018-09-07 |
| CN108513554B true CN108513554B (en) | 2022-02-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780005152.2A Active CN108513554B (en) | 2017-07-27 | 2017-07-27 | Unmanned aerial vehicle subassembly |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN108513554B (en) |
| WO (1) | WO2019019093A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021087727A1 (en) * | 2019-11-05 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Positioning method and system, remote control device, and rtk module |
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| WO2014080409A1 (en) * | 2012-11-26 | 2014-05-30 | Wisec Ltd. | Safety apparatus for a multi-blade aircraft |
| CN204956923U (en) * | 2015-07-06 | 2016-01-13 | 刘琳 | Intelligent Mobile Terminal's flying suit and intelligence flight system thereof |
| CN105915249A (en) * | 2015-02-23 | 2016-08-31 | 金永权 | Mobile communication terminal having unmanned aerial vehicle |
| CN106218909A (en) * | 2016-09-23 | 2016-12-14 | 珠海格力电器股份有限公司 | Aircraft and system of taking photo by plane |
| CN106956772A (en) * | 2017-04-15 | 2017-07-18 | 上海量明科技发展有限公司 | Folding unmanned plane and its implementation |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9573683B2 (en) * | 2014-04-28 | 2017-02-21 | Arch-Aerial, Llc | Collapsible multi-rotor UAV |
| KR101725444B1 (en) * | 2016-03-29 | 2017-04-11 | 장민하 | Flat type drone |
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- 2017-07-27 WO PCT/CN2017/094671 patent/WO2019019093A1/en active Application Filing
- 2017-07-27 CN CN201780005152.2A patent/CN108513554B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014080409A1 (en) * | 2012-11-26 | 2014-05-30 | Wisec Ltd. | Safety apparatus for a multi-blade aircraft |
| CN105915249A (en) * | 2015-02-23 | 2016-08-31 | 金永权 | Mobile communication terminal having unmanned aerial vehicle |
| CN204956923U (en) * | 2015-07-06 | 2016-01-13 | 刘琳 | Intelligent Mobile Terminal's flying suit and intelligence flight system thereof |
| CN106218909A (en) * | 2016-09-23 | 2016-12-14 | 珠海格力电器股份有限公司 | Aircraft and system of taking photo by plane |
| CN106956772A (en) * | 2017-04-15 | 2017-07-18 | 上海量明科技发展有限公司 | Folding unmanned plane and its implementation |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019019093A1 (en) | 2019-01-31 |
| CN108513554A (en) | 2018-09-07 |
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