CN111409826B - Electronic device - Google Patents

Abstract

The invention discloses electronic equipment which comprises an equipment main body and an unmanned aerial vehicle, wherein the equipment main body comprises a shell and a first connecting piece, the shell is provided with an inner cavity and an opening communicated with the inner cavity, and the first connecting piece is positioned in the inner cavity; the drone comprises a second connection, the drone having a first state and a second state, the drone being switchable between the first state and the second state upon application of an external force; when the unmanned aerial vehicle is in the first state, at least part of the unmanned aerial vehicle is located in the inner cavity, and the unmanned aerial vehicle is detachably connected with the shell through the matching of the first connecting piece and the second connecting piece; under the condition that the unmanned aerial vehicle is in the second state, the first connecting piece is separated from the second connecting piece, and at least part of the unmanned aerial vehicle extends out of the inner cavity through the opening. The scheme can solve the problem of large thickness of the electronic equipment.

Description

Electronic device

Technical Field

The invention relates to the technical field of communication equipment, in particular to electronic equipment.

Background

Along with the development of science and technology, the user can operate unmanned aerial vehicle through electronic equipment to realize taking photo by plane or other aviation operation. Present unmanned aerial vehicle and electronic equipment belong to two independent equipment, therefore unmanned aerial vehicle's portability is relatively poor.

In order to make unmanned aerial vehicle convenient to carry, can be with unmanned aerial vehicle integrated to electronic equipment on, electronic equipment's casing has the inner chamber and the opening that is linked together with the inner chamber, unmanned aerial vehicle accessible opening stretches out outside the inner chamber or retract to among the inner chamber. When the user uses unmanned aerial vehicle, can take out unmanned aerial vehicle from the inner chamber of casing to make unmanned aerial vehicle convenient to carry.

In the process of actual work, the unmanned aerial vehicle is realized by actuating mechanism from the operation of taking out of inner chamber. The driving mechanism often includes driving motor and drive mechanism, and driving motor and drive mechanism spare part are more, and the structure is complicated, therefore driving mechanism seriously occupies the inner space of casing, leads to electronic equipment's thickness great to make electronic equipment's frivolousness remain to be improved.

Disclosure of Invention

The invention discloses electronic equipment, which aims to solve the problem of large thickness of the electronic equipment.

In order to solve the technical problem, the invention is realized as follows:

the embodiment of the invention discloses an electronic device, which comprises:

the device comprises a device body and a control unit, wherein the device body comprises a shell and a first connecting piece, the shell is provided with an inner cavity and an opening communicated with the inner cavity, and the first connecting piece is positioned in the inner cavity;

a drone including a second connection, the drone having a first state and a second state, the drone being switchable between the first state and the second state upon application of an external force;

wherein, when the drone is in the first state, at least a portion of the drone is located in the internal cavity, and the drone is detachably connected to the housing through the mating of the first connector and the second connector;

under the condition that the unmanned aerial vehicle is in the second state, the first connecting piece is separated from the second connecting piece, and at least part of the unmanned aerial vehicle extends out of the inner cavity through the opening.

The technical scheme adopted by the invention can achieve the following beneficial effects:

in the embodiment of the invention, the shell is detachably connected with the unmanned aerial vehicle through the matching of the first connecting piece and the second connecting piece, and a user can apply acting force to the unmanned aerial vehicle, so that the unmanned aerial vehicle can be switched between the first state and the second state.

Simultaneously, unmanned aerial vehicle just exerts external force through the user and can accomplish at the in-process that first state and second state switch, consequently does not have power consumptive problem to can reduce electronic equipment's energy consumption.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments or the background art of the present invention, the drawings used in the description of the embodiments or the background art will be briefly described below, and it is obvious for those skilled in the art to obtain other drawings without any inventive exercise.

Fig. 1 is a schematic diagram of an unmanned aerial vehicle in a first state in an electronic device disclosed in an embodiment of the present invention;

fig. 2 is a schematic diagram of an electronic device disclosed in the embodiment of the present invention, in which an unmanned aerial vehicle is in a second state;

FIG. 3 is a schematic diagram of a first electronic device according to an embodiment of the disclosure;

FIG. 4 is a diagram of a second electronic device according to an embodiment of the disclosure;

fig. 5 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention when the unmanned aerial vehicle is magnetically connected to the housing;

fig. 6 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention when the unmanned aerial vehicle is in the first state when the unmanned aerial vehicle is connected to the housing in a snap-fit manner;

fig. 7 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention, when the unmanned aerial vehicle is clamped with the housing, the unmanned aerial vehicle is in a second state:

fig. 8 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention, when the pop-up assembly is an elastic expansion member, the unmanned aerial vehicle is in a first state;

fig. 9 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention, when the pop-up assembly is an elastic expansion member, the unmanned aerial vehicle is in a second state;

fig. 10 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention, when the pop-up assembly is a magnetic member, the unmanned aerial vehicle is in a first state;

fig. 11 is a cross-sectional view of the electronic device disclosed in the embodiment of the present invention, when the pop-up assembly is a magnetic member, the unmanned aerial vehicle is in a second state;

fig. 12 is a schematic structural diagram of an electronic device according to an embodiment of the disclosure, in which a slider of an eject mechanism is in a first position;

FIG. 13 is a schematic structural diagram of an electronic device according to an embodiment of the disclosure, in which a slider of an eject mechanism is in a second position;

FIG. 14 is a schematic structural diagram of a slider in an electronic device according to an embodiment of the disclosure;

fig. 15 is a schematic structural diagram of another guide rail disclosed in the embodiment of the present invention.

Description of reference numerals:

100-shell, 110-inner cavity, 120-opening,

200-unmanned plane, 210-second connecting piece,

300-an ejection mechanism, 310-a connecting rod, 320-a sliding block, 321-a guide track, 322-a first limit section, 323-an extension section, 324-a second limit section, 325-a retraction section, 326-a limit bulge, 330-an ejection assembly, 331-a third magnetic part, 332-a fourth magnetic part, 333-a fifth magnetic part, 334-a sixth magnetic part, 340-a guide rod,

400-first connector.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions of the present invention will be clearly and completely described below with reference to the specific embodiments of the present invention and the accompanying drawings. It is to be understood that the described embodiments are merely a few embodiments of the 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.

The technical solutions disclosed in the embodiments of the present invention are described in detail below with reference to the accompanying drawings.

Referring to fig. 1 to 15, an embodiment of the present invention discloses an electronic device, which includes a device main body and an unmanned aerial vehicle 200.

The main body of the device is a main body component of the electronic device, and the main body of the device may include the housing 100, the first connector 400, the display module, the circuit board, the electronic component, and other components. The housing 100 has an inner cavity 110 and an opening 120 communicating with the inner cavity 110, and the first connector 400 is located in the inner cavity 110.

The drone 200 comprises a second connection 210, the drone 200 having a first state and a second state, the drone 200 being switchable between the first state and the second state under the effect of an external force.

As shown in fig. 1, with the drone 200 in the first state, at least a portion of the drone 200 is located in the internal cavity, and the drone 200 is removably connected to the housing 100 by the mating of the first connector 400 and the second connector 210.

With the drone 200 in the second state, the first connector 400 is disconnected from the second connector 210 and at least a portion of the drone 200 protrudes out of the internal cavity through the opening 120. At this time, the drone 200 has two positions, the first position is that a part of the drone 200 is still located inside the inner cavity, and the other part of the drone 200 extends out of the inner cavity through the opening 120, as shown in fig. 7, 9 and 11; in the second position, the drone 200 is entirely outside the interior cavity, as shown in fig. 2.

Optionally, components such as a camera module and a mapping chip can be arranged on the unmanned aerial vehicle 200, so that aerial photography, mapping and other aerial operations can be completed. Equipment subject and unmanned aerial vehicle 200 radio connection to make equipment subject can carry out the remote control to unmanned aerial vehicle 200, unmanned aerial vehicle 200 also can transmit the information transmission of aviation operation to equipment subject simultaneously. When setting up the camera module on unmanned aerial vehicle, the electronic equipment shoots the function and does not receive the restriction of position and angle, and then has improved the function of camera module.

In the embodiment of the present invention, the housing 100 and the unmanned aerial vehicle 200 are detachably connected by the first connecting member 400 and the second connecting member 210 in a matching manner, and a user can apply an acting force to the unmanned aerial vehicle 200, so as to switch the unmanned aerial vehicle 200 between the first state and the second state, when the unmanned aerial vehicle 200 needs to work, the user can apply an acting force to the unmanned aerial vehicle 200 to separate the first connecting member 400 and the second connecting member 210, and further separate the unmanned aerial vehicle 200 from the housing 200, so that the unmanned aerial vehicle 200 can be taken down from the housing 100, at this time, the first connecting member 400 and the second connecting member 210 have simple structures and fewer parts, so that the first connecting member 400 and the second connecting member 210 occupy a smaller internal space of the housing 100, so as to reduce the thickness of the electronic device, and facilitate the development of lightness and thinness of the electronic device.

Meanwhile, in the process of switching between the first state and the second state, the unmanned aerial vehicle 200 can be completed only by applying external force through a user, so that the problem of power consumption does not exist, and the energy consumption of the electronic equipment can be reduced.

In addition, the electronic equipment disclosed by the invention does not need high-price components such as a driving motor, a transmission mechanism and the like, so that the production cost can be reduced.

As shown in fig. 5, in an alternative embodiment, one of the first connecting member 400 and the second connecting member 210 is a first magnetic member, and the other one is a magnetic member, and when the unmanned aerial vehicle 200 is in the first state, the first magnetic member and the magnetic member are magnetically attracted to each other. At this moment, unmanned aerial vehicle 200 and casing 100 inhale the cooperation through magnetism of first magnetism spare and magnetism and realize dismantling the connection, and this kind of connected mode is simple, convenient, easily operation. Optionally, the first magnetic member may be an electromagnet, and when the first magnetic member is powered on, the first magnetic member is magnetically connected with the magnetic attraction member; when the first magnetic member is powered off, the first magnetic member is separated from the magnetic member, so that the housing 100 can be inverted, and the drone 200 can slide out of the inner cavity 110 of the housing 100. At this time, when the drone 200 is in the first state, the drone 200 may be partially located in the inner cavity 110, or may be entirely located in the inner cavity 110. First magnetic part still can be the permanent magnet, and at this moment, unmanned aerial vehicle 200 part is located inner chamber 110 to unmanned aerial vehicle exposes partly convenience of customers operation.

Specifically, the magnetic part can be an iron part which is easy and convenient to process, so that the cost of the electronic equipment is lower. In order to make the first magnetic member and the magnetic member have a larger magnetic attraction force, in another embodiment, the magnetic member may also be a second magnetic member, and the second magnetic member is opposite to the first magnetic member in magnetism. At this moment, magnetism is inhaled the piece and is also magnetic structure spare, and first magnetic part is inhaled when a magnetism cooperates with magnetism, and first magnetic part is inhaled the magnetic attraction of piece great with magnetism to make the fastening more that unmanned aerial vehicle 200 and casing 100 are connected, make unmanned aerial vehicle 200 be difficult to drop from casing 100, and then can improve electronic equipment's security and reliability. Optionally, the second magnetic member may be an electromagnet, and when the second magnetic member is energized, the first magnetic member and the second magnetic member are magnetically attracted; when the second magnetic member is powered off, the first magnetic member is separated from the second magnetic member, so that the housing 100 can be inverted, and the drone 200 can slide out of the inner cavity 110 of the housing 100. At this time, when the drone 200 is in the first state, the drone 200 may be partially located in the inner cavity 110, or may be entirely located in the inner cavity 110. The second magnetism piece also can be the permanent magnet, and at this moment, unmanned aerial vehicle 200 part is located inner chamber 110 to unmanned aerial vehicle 200 exposes partly convenience of customers operation.

In the above embodiment, when the magnetic attraction force between the first magnetic member and the magnetic attraction member is large, a large force needs to be applied to the unmanned aerial vehicle 200 to separate the first magnetic member and the magnetic attraction member; when the magnetic attraction force of first magnetic part and magnetism piece is less, the unmanned aerial vehicle 200 is easy to follow the roll-off in inner chamber 110 to electronic equipment's security has been reduced. Therefore, the first magnetic member and the magnetic member have high processing precision, which may result in high manufacturing cost of the electronic device.

For this reason, the first connector 400 may be a first hook, and the second connector 210 may be a second hook, and the first hook and the second hook are connected by being fastened when the unmanned aerial vehicle 200 is in the first state. At this time, the first connector 400 and the second connector 210 are connected in a clamping manner, so that the processing precision of the first hook and the second hook is low, and further the manufacturing cost of the electronic device is low.

However, the inner cavity 110 needs to reserve an installation space for the first hook and the second hook, so that the first hook and the second hook occupy a larger space of the inner cavity 110 when being clamped, in an alternative embodiment, one of the first connecting piece 400 and the second connecting piece 210 is a clamping groove, and the other is a clamping protrusion, and when the unmanned aerial vehicle 200 is in the first state, the clamping groove is connected to the clamping protrusion in a clamping manner, as shown in fig. 6 and 7. At this time, when the first connector 400 is connected to the second connector 210, the clamping protrusion may be disposed in the clamping groove, so as to reduce the occupation of the first connector 400 and the second connector 210 on the inner cavity 110.

In the above-mentioned embodiment, the user need exert the effort for unmanned aerial vehicle 200 to can drive unmanned aerial vehicle 200 and remove outside inner chamber 110, partial unmanned aerial vehicle 200 this moment can set up in inner chamber 110, and the user can apply the effort to the part that unmanned aerial vehicle 200 is located outside inner chamber 110, thereby switches unmanned aerial vehicle 200 to the second state. However, with the drone 200 in the first state, when the volume of the drone 200 outside the internal cavity 110 is small, the user's fingers easily slip with the drone 200, making it difficult to transition the drone 200 to the second state; when the volume of the unmanned aerial vehicle 200 outside the inner cavity 110 is large, the external dimension of the electronic device is large, the external texture of the electronic device is poor, and therefore the user experience is poor. As shown in fig. 8 to 11, in an alternative embodiment, the apparatus main body may further include an eject mechanism 300, and the eject mechanism 300 may include a connecting rod 310, a slider 320, and an eject assembly 330.

The slider 320 has a limiting protrusion 326, and the drone 200 includes a limiting surface that is lapped over the limiting protrusion 326. At this moment, when the slider 320 moves, the slider 320 drives the limiting protrusion 326 to move, and the limiting protrusion 326 is matched with the limiting surface, so that the unmanned aerial vehicle 200 is pushed to move. When unmanned aerial vehicle 200 removed, unmanned aerial vehicle 200 drove spacing face and removes, spacing face and spacing protruding 326 because spacing cooperation to can promote the slider 320 and remove.

The slider 320 is provided with a guide track 321, and the guide track 321 includes a first limit section 322, an extending section 323, a second limit section 324 and a retracting section 325 which are sequentially connected in a ring shape. It should be noted that, in the present specification, the annular shape means that the first limiting section 322, the extending section 323, the second limiting section 324 and the retracting section 325 are sequentially connected to form a closed guide rail 321, so that the second end of the connecting rod 310, which will be described later, can sequentially pass through the first limiting section 322, the extending section 323, the second limiting section 324 and the retracting section 325 in the sliding process, thereby realizing the recyclable sliding.

The pop-up assembly 330 is disposed in the inner cavity 110, the pop-up assembly can drive the sliding block 320 to move toward the extending direction of the drone 200, and the drone 200 can move to the second state along with the sliding block 320 through the matching of the limiting protrusion 326 and the limiting surface.

The first end of the connecting rod 310 is hinged to the housing 100, the second end of the connecting rod 310 is in sliding fit with the guide track 321, the slider 320 has a first position and a second position, and the slider 320 is switchable between the first position and the second position under the action of external force. The first end of the connecting rod 310 is hinged to the housing 100, so that the connecting rod 310 can swing, and the second end of the connecting rod 310 can be adapted to the first limiting section 322, the extending section 323, the second limiting section 324 and the retracting section 325 in the sliding process.

With the slider 320 in the first position, at least a portion of the drone 200 protrudes out of the internal cavity 110 through the opening 120, and the second end of the connecting rod 310 mates with the second restraint segment 324.

At this moment, when first connecting piece 400 sets up on casing 100, the user presses unmanned aerial vehicle 200, unmanned aerial vehicle 200 retracts to inner chamber 110, unmanned aerial vehicle 200's spacing face drives the spacing protruding 326 of slider 320 and removes, thereby drive slider 320 removes, the second end of connecting rod 310 slides in from first spacing section 322 and stretches out section 323, the user removes the back of pressing force, pop out subassembly 330 drive slider 320 and remove, slider 320's spacing protruding 326 drives unmanned aerial vehicle 200 and removes outside inner chamber 110, thereby make first connecting piece 400 and second connecting piece 210 separation, and then pop out unmanned aerial vehicle 200, at this moment, connecting rod 310's second end is from stretching out section 323 and sliding in spacing section 324 of second. In this way, after the drone 200 is ejected, the first connector 400 and the second connector 210 are already separated, so the user only needs to take out the drone 200. It should be noted that the driving force of the pop-up assembly 330 is greater than the force between the first connecting member 400 and the second connecting member 210, so that the pop-up assembly 330 applies a force to the slider 320 to separate the first connecting member 400 and the second connecting member 210.

When first connecting piece 400 sets up on slider 320, the user presses unmanned aerial vehicle 200, unmanned aerial vehicle 200 retracts to inner chamber 110, spacing face on unmanned aerial vehicle 200 drives the spacing protruding 326 of slider 320 and removes, thereby drive slider 320 removes, the second end of connecting rod 310 slides in from first spacing section 322 and stretches out section 323, when the user withdraws the pressing force, pop out subassembly 330 drive slider 320 and remove, the spacing protruding 326 of slider 320 drives unmanned aerial vehicle 200 and removes outside the inner chamber, when slider 320 moves to the primary importance, most unmanned aerial vehicle 200 exposes, at this moment, first connecting piece 400 and second connecting piece 210 can also not separate, the user can hold the part that exposes of unmanned aerial vehicle 200 and exert the effort to unmanned aerial vehicle 200, thereby make first connecting piece 400 and second connecting piece 210 separate. In this manner, after the drone 200 is ejected, the user is required to apply force to the drone 200 again to cause the first connector 400 and the second connector 210 to separate.

With the slide block 320 in the second position, at least a portion of the drone 200 is retracted into the internal cavity 110 through the opening 120, and the first connector 400 and the second connector 210 are connected, and the second end of the connecting rod 310 is engaged with the first restraint section 322.

At this moment, when first connecting piece 400 sets up on casing 100, the user presses unmanned aerial vehicle 200, unmanned aerial vehicle 200 retracts to inner chamber 110, thereby make unmanned aerial vehicle 200's spacing face drive the spacing protruding 326 of slider 320 and remove, thereby drive slider 320 removes, the second end of connecting rod 310 slides in from the spacing section 324 of second and retracts section 325, when first connecting piece 400 is connected with second connecting piece 210, remove the pressing force, unmanned aerial vehicle 200 installs in casing 100, at this moment, the second end of connecting rod 310 slides in first spacing section 322 from retracting section 325, and with the spacing cooperation of first spacing section 322.

When first connecting piece 400 sets up on slider 320, the user presses unmanned aerial vehicle 200, unmanned aerial vehicle 200 retracts to inner chamber 110, at this moment, first connecting piece 400 and second connecting piece 210 are connected, then unmanned aerial vehicle 200's spacing face drives the spacing arch 326 removal of slider 320, thereby drive slider 320 removes, the second end of connecting rod 310 slides in from the spacing section 324 of second and retracts section 325, when the second end of connecting rod 310 slides in first spacing section 322 from retracting section 325, remove and press, unmanned aerial vehicle 200 installs in casing 100.

In the above scheme, the user is through pressing unmanned aerial vehicle 200 to trigger pop-up mechanism 300 work, thereby switch unmanned aerial vehicle 200 to the second state, the user indicates to be difficult to take place the phenomenon of skidding with unmanned aerial vehicle 200 this moment, thereby makes unmanned aerial vehicle 200 dismantle operating efficiency higher. Meanwhile, under the condition that the unmanned aerial vehicle 200 is in the first state, the volume of the unmanned aerial vehicle 200 outside the inner cavity 110 can be smaller, so that the appearance size of the electronic equipment is smaller, the appearance texture of the electronic equipment is better, and the user experience is effectively improved.

In a specific operation, when the drone 200 is in a normal state, i.e. the drone 200 is not in operation, at least a part of the drone 200 is located in the inner cavity 110, and the second end of the connecting rod 310 is connected to the break point (the point of intersection a shown in fig. 14) of the first limiting section 322.

When the drone 200 needs to be taken out of the casing 100, the first step: pressing unmanned aerial vehicle 200, unmanned aerial vehicle 200 drives slider 320 and moves along the direction of keeping away from opening 120, and when unmanned aerial vehicle 200 moved the minimum of inner chamber 110, the second end of connecting rod 310 was located the nodical (the nodical as the B that is shown in fig. 14) department of the first spacing section 322 and the section 323 that stretches out. The second step is that: withdraw the pressing force, pop out subassembly 330 and drive slider 320 and kick-back, slider 320 drives unmanned aerial vehicle 200 and removes towards the direction of opening 120 to push away unmanned aerial vehicle 200 opening 120, unmanned aerial vehicle 200 reaches a protruding position before not separating with casing 100, and the second end of connecting rod 310 is located the nodical (the nodical C shown in fig. 14) department of nodical with the section 323 that stretches out of second spacing section 324 this moment. Alternatively, when the driving force of the pop-up assembly 330 is large, the pop-up assembly 330 drives the slider to reach another protruding position, and at this time, the second end of the connecting rod 310 is located at the bottom-most end of the second limiting section 324 (as shown in fig. 14, point D is intersected), and at this time, the drone can be taken out. In case the drone is in an extended position before being detached from the housing, the second end of the connecting rod 310 is located at the intersection of the second limiting section 324 and the extension section 323 (intersection C as shown in fig. 14), a third step may be performed: when the drone 200 is in the extended position, under the condition that the second end of the connecting rod 310 is located at the intersection point (the intersection point C shown in fig. 14) of the second limiting section 324 and the extending section 323, the user can hold the exposed part of the drone 200, so as to take the drone 200 out of the housing 100, after the drone 200 is separated from the housing 100, the weight borne by the slider 320 is reduced, the pop-up assembly 330 drives the slider 320 to move again, and at this time, the second end of the connecting rod 310 is located at the bottommost end (the intersection point D shown in fig. 14) of the second limiting section 324. The first position of the slider 320 is the position where the slider 320 is located after the drone 200 extends out, so when the slider 320 is located at the first position, the second end of the connecting rod 310 may be located at the intersection point of the second limiting section 324 and the extending section 323 (e.g., the intersection point C shown in fig. 14), or the second end of the connecting rod 310 may also be located at the bottommost end of the second limiting section 324 (e.g., the intersection point D shown in fig. 14), and of course, the first position may also be other positions, which is not limited herein.

When the drone 200 is mounted to the casing 100, the first step: with unmanned aerial vehicle 200 stretching into opening 120, unmanned aerial vehicle 200's spacing face laps on the spacing arch 326 of slider 320, at this moment, the load of slider 320 is great, probably make the second end of connecting rod 310 move to the nodical (the nodical C that is shown in fig. 14) department of second spacing section 324 and stretch out section 323 from the lowest end (the nodical D that is shown in fig. 14) of second spacing section 324, or, because unmanned aerial vehicle fuselage gravity is not enough, when unmanned aerial vehicle's spacing face laps on the spacing arch 326 of slider 320, make the second end of connecting rod 310 probably still be located the bottommost (the nodical D that is shown in fig. 14) of second spacing section 324. In the second step, the user presses the drone 200, when the drone 200 reaches the bottom end of the inner cavity 110, the second end of the connecting rod 310 is located at the intersection point (E intersection point shown in fig. 14) of the first limiting section 322 and the retracting section 325, and at this time, the pressing force is removed, the pop-up assembly 330 drives the slider 320 to rebound, so that the slider 320 reaches the second position, the second end of the connecting rod 310 returns to the folding point (a intersection point shown in fig. 14) of the first limiting section 322, and the drone 200 is installed in the housing 100. In the above-mentioned first step and second step operation process, when unmanned aerial vehicle stretched into the opening under the condition that the user just applyed the thrust to unmanned aerial vehicle 200, the user directly pushed unmanned aerial vehicle 200 to the bottommost of inner chamber 110, and at this moment, the second end of connecting rod 310 was located the nodical department (the E nodical as shown in fig. 14) of first spacing section 322 and retraction section 325, and after the user loosed one's hand, the second end of connecting rod 310 finally can be in the breakpoint department of first spacing section 322.

In order to further improve user experience, the unmanned aerial vehicle 200 can be completely arranged in the inner cavity 110, only one side surface is exposed, a user can apply pressing force to the exposed surface of the unmanned aerial vehicle 200, at the moment, the unmanned aerial vehicle 200 is completely positioned in the inner cavity 110, the appearance size of the electronic device is further reduced, and user experience is further improved. The size of the exposed surface of the drone 200 may be sufficient for user operation.

In an alternative embodiment, as shown in fig. 8 and 9, the pop-up assembly 330 is an elastic telescopic member, one end of the elastic telescopic member is connected to the housing 100, the other end of the elastic telescopic member is connected to the slider 320, and the elastic telescopic member drives the slider 320 to switch to the first position. The scheme is simple, the parts are fewer, and the operation is easy to realize. Optionally. The resilient bellows may be a spring.

In the above embodiment, the electronic device is easy to generate heat during operation, so that the elastic expansion member is heated and aged, the service life of the elastic expansion member is short, and the reliability of the pop-up mechanism 300 is reduced. For this purpose, in an alternative embodiment, the pop-up assembly 330 may include a third magnetic member 331 and a fourth magnetic member 332, the third magnetic member 331 is disposed on the housing 100, the fourth magnetic member 332 is disposed at an end of the sliding block 320 facing away from the opening 120, the fourth magnetic member 332 is located between the third magnetic member 331 and the sliding block 320, polarities of the third magnetic member 331 and the fourth magnetic member 332 are the same, and a magnetic repulsion force between the third magnetic member 331 and the fourth magnetic member 332 drives the sliding block 320 to move to the first position, so that the sliding block 320 pushes the drone 200 to switch to the second state. At this time, the third magnetic member 331 and the fourth magnetic member 332 are not easily thermally deteriorated, so the life of the third magnetic member 331 and the fourth magnetic member 332 is long, thereby improving the reliability of the eject mechanism 300.

In another embodiment, one end of the fourth magnetic member 332 protrudes relative to the slider 320, and the protruding portion of the fourth magnetic member 332 is magnetically coupled to the second connector 210, and at this time, the protruding portion of the fourth magnetic member 332 is equivalent to the first connector 400, so that the fourth magnetic member 332 can also serve as the first connector 400, thereby simplifying the structure of the electronic device and making the structure of the electronic device more compact.

In the above embodiment, only one pair of magnetic members is provided, the driving force of the pop-up mechanism 300 is small, and the pop-up mechanism 300 is not easy to push the drone 200 to move, therefore, the pop-up assembly 330 may further include a fifth magnetic member 333 and a sixth magnetic member 334, the fifth magnetic member 333 is disposed in the housing 100, the sixth magnetic member 334 is disposed at one end of the slider 320 facing the opening 120, the sixth magnetic member 334 is located between the fifth magnetic member 333 and the slider 320, the polarities of the fifth magnetic member 333 and the sixth magnetic member 334 are opposite, and the magnetic attraction force between the fifth magnetic member 333 and the sixth magnetic member 334 drives the slider 320 to move to the first position, so that the slider 320 pushes the drone 200 to switch to the second state, as shown in fig. 10 and 11. At this moment, magnetic repulsion is generated between the third magnetic member 331 and the fourth magnetic member 332, and the fifth magnetic member 333 and the sixth magnetic member 334 generate magnetic attraction, so that the stress of the slider 320 is in the same direction, and the driving force of the pop-up mechanism 300 is increased, so that the unmanned aerial vehicle 200 is more easily switched to the second state.

In the above embodiment, the slider 320 is easy to shake during the moving process, so that the slider 320 collides with the side wall of the inner cavity 110, and the slider 320 is damaged or the slider 320 is jammed during the moving process. In an alternative embodiment, the pop-up mechanism 300 may further include a guiding rod 340, the sliding block 320 is provided with a sliding slot, one end of the guiding rod 340 is connected to the casing 100, the other end of the guiding rod 340 extends into the sliding slot, and the sliding slot is in sliding fit with the guiding rod 340 in the extending direction of the guiding rod 340. At this moment, the guide bar 340 can limit the moving direction of the slider 320, and reduce the shaking of the slider 320 during the moving process, thereby preventing the slider 320 from colliding with the side wall of the inner cavity 110, further preventing the slider 320 from being damaged easily, and meanwhile, the slider 320 is not easy to jam during the moving process.

In order to more reliably maintain the sliding block 320 at the first position or the second position, in an alternative embodiment, the second end of the connecting rod 310 is provided with a hanging part, when the unmanned aerial vehicle 200 is in the first state, the hanging part is in hanging fit with the first limiting section 322, and then the sliding block 320 is in the second position; under the condition that unmanned aerial vehicle 200 is in the second state, the hooking portion articulates the cooperation with spacing section 324 of second, and slider 320 is in the primary importance this moment. At this time, the second end of the connecting rod 310 is disposed between the opening 120 and the first end of the connecting rod 310, and the connecting rod 310 applies a pulling force to the slider 320, so as to restrict the slider 320 from moving in a direction in which the drone 200 protrudes, and further enable the slider 320 to be maintained at the first position or the second position.

However, in the above embodiment, the first end of the connecting rod 310 is located below the sliding block 320, so the connecting rod 310 is closer to the central area of the casing 100 as a whole, and since the central area of the casing 100 is disposed with the circuit board and more electronic components, the connecting rod 310 is easily interfered with the circuit board or the electronic components, for this reason, in another embodiment, the second end of the connecting rod 310 is provided with a collision portion, and when the unmanned aerial vehicle 200 is in the first state, the collision portion collides with the first limiting section 322, and at this time, the sliding block 320 is in the second position; when unmanned aerial vehicle 200 is in the condition of second state, the conflict portion is inconsistent with spacing section 324 of second, slider 320 is in the primary importance this moment, the first end of connecting rod 310 sets up between the second end of opening 120 and connecting rod 310, connecting rod 310 exerts thrust to slider 320, thereby restriction slider 320 removes towards the direction that unmanned aerial vehicle 200 stretched out, in this kind of mode, connecting rod 310 is more close to the edge of casing 100, because the electronic components of the edge distribution of casing 100 is less, consequently connecting rod 310 is difficult to take place to interfere with electronic components.

When the unmanned aerial vehicle 200 is in the first state, when a part of the unmanned aerial vehicle 200 is higher than the housing 100, the overall appearance size of the electronic device is increased, so that the user is inconvenient to carry, and the user experience is poor; when the partly unmanned aerial vehicle 200 that exceeds of casing 100, the sunken area can be left to the position that unmanned aerial vehicle 200 is connected with casing 100, and this sunken area gathers the dust easily to make unmanned aerial vehicle 200 appear the circumstances of jam when removing. In an alternative embodiment, the outer surface of the drone 200 is coplanar with the outer surface of the housing 100 with the drone 200 in the first state. At this moment, the hookup location department of unmanned aerial vehicle 200 and casing 100 is comparatively level and smooth to make electronic equipment's overall dimension less, consequently user convenient to carry improves the gripping and feels, and then improves user experience, simultaneously, unmanned aerial vehicle 200 does not have the depressed area with the hookup location department of casing 100, consequently is difficult to gather the dust, thereby makes unmanned aerial vehicle 200 the circumstances of jam can not appear, and then has improved electronic equipment's reliability.

In order to make the business turn over inner chamber 110 that unmanned aerial vehicle 200 can be more smooth, the size of inner chamber 110 can be greater than unmanned aerial vehicle 200's external dimension, however, when the user applys the effort to unmanned aerial vehicle 200, because the position of effort is not unmanned aerial vehicle 200's intermediate position, probably causes unmanned aerial vehicle 200 to incline to one side for unmanned aerial vehicle 200's surface and inner chamber 110's lateral wall take place the friction, thereby cause unmanned aerial vehicle 200's surface fish tail. In an alternative embodiment, the housing 100 may be provided with a first guide portion, and the drone 200 may be provided with a second guide portion, the first guide portion being a sliding fit with the second guide portion. At this time, the first guide portion and the second guide portion assist in restricting the movement locus of the drone 200, thereby preventing the drone 200 from inclining to one side. This scheme can play spacing and the effect of direction to unmanned aerial vehicle 200's removal orbit to prevent more reliably that unmanned aerial vehicle 200 from taking place to incline at the in-process that removes. Alternatively, one of the first guide portion and the second guide portion may be a guide groove, and the other may be a guide protrusion, the guide protrusion being slidably fitted with the guide groove. Of course, the first guide portion and the second guide portion may also be other guide structures, which is not limited herein.

In an alternative embodiment, the housing 100 may include a bezel, and the opening 120 may be opened on the bezel. At this moment, under the condition that unmanned aerial vehicle 200 is in the first state, partial unmanned aerial vehicle 200 hides in casing 100 to make electronic equipment's outward appearance feel better, thereby improved user experience, simultaneously, can also be used for protecting unmanned aerial vehicle 200, thereby prevent that unmanned aerial vehicle 200 from being by the fish tail. Further, when the drones 200 are located in the inner cavity 110, the drones 200 can block the opening 120, and the appearance surface of the housing 100 observed by the user is a whole, so that the user experience is further improved. Alternatively, the housing 100 may include a bezel, and the components forming the bezel of the housing 100 of different configurations may be different. For example, the case 100 may include a front case, a rear cover, and a middle frame disposed therebetween. The rim may be formed on the middle frame. In this case, the frame serves as a part of the middle frame. For another example, the housing 100 includes a front cover and a rear cover, and the bezel may be molded on the rear cover.

In the electronic device disclosed in the embodiment of the present invention, the structure of the guide rail 321 may be various, and in a specific implementation manner, the guide rail 321 may be a guide groove, that is, the first limiting section 322, the extending section 323, the second limiting section 324, and the retracting section 325 may be each groove section of the guide groove, that is, the first limiting section 322 is communicated with the extending section 323, the extending section 323 is communicated with the second limiting section 324, the second limiting section 324 is communicated with the retracting section 325, and the retracting section 325 is communicated with the first limiting section 322. In this case, the second end of the connecting rod 310 can slide in the guide groove, which certainly can improve the stability of the sliding fit and certainly also facilitates the slider 320 to be maintained in the first position or the second position.

Optionally, there is a height difference between the bottom wall of the protruding section 323 and the bottom wall of the second limiting section 324, so that the second end of the connecting rod 310 can only move to the second limiting section 324 from the protruding section 323, and cannot move reversely to the protruding section 323 from the second limiting section 324. Similarly, the bottom wall of the retracting section 325 and the bottom wall of the first position-limiting section 322 have a height difference, so that the second end of the connecting rod 310 can only move from the retracting section 325 to the first position-limiting section 322, and cannot move reversely from the first position-limiting section 322 to the retracting section 325.

In order to better realize the limit fit, the first limit section 322 may be a groove section bent away from the extending direction of the drone 200, for example, a penetrating axis of the first limit section 322 is a V-shaped broken line; similarly, the second limiting section 324 may also be a groove section bent away from the extending direction of the drone 200, for example, a penetrating axis of the second limiting section 324 is a V-shaped broken line; in this case, the first and second limiting sections 322 and 324 can be more stably and limitedly engaged with the second end of the connecting rod 310.

Of course, the guide rail 321 may have other structures, and is not limited to the groove-shaped structure. In one embodiment, the guide rail 321 may be a guide protrusion, and the first position-limiting section 322, the extending section 323, the second position-limiting section 324 and the retracting section 325 are all protrusion sections. The sliding formation of the second end of the connecting rod 310 may be as shown in fig. 15, and the direction in which the second end of the connecting rod 310 slides with respect to the guide rail 321 is schematically shown by a dotted arrow in fig. 15.

Similarly, the first limiting section 322 may be a strip-shaped protrusion bent away from the extending direction of the drone 200; the second limiting section 324 may be another strip-shaped protrusion bent away from the extending direction of the drone 200.

The electronic device disclosed in the embodiment of the present invention may be a smart phone, a tablet computer, an electronic book reader, a wearable device (e.g., a smart watch), an electronic game machine, or the like, and the specific type of the electronic device is not limited in the embodiment of the present invention.

In the above embodiments of the present invention, the difference between the embodiments is mainly described, and different optimization features between the embodiments can be combined to form a better embodiment as long as they are not contradictory, and further description is omitted here in view of brevity of the text.

The above description is only an example of the present invention, and is not intended to limit the present invention. Various modifications and alterations to this invention will become apparent to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims (10)

1. An electronic device, comprising:

a device body including a housing (100) and a first connector (400), the housing (100) having an inner cavity (110) and an opening (120) communicating with the inner cavity (110), the first connector (400) being located in the inner cavity (110);

a drone (200), the drone (200) comprising a second connection (210), the drone (200) having a first state and a second state, the drone (200) being switchable between the first state and the second state upon application of an external force;

wherein with the drone (200) in the first state, at least part of the drone (200) is located in the internal cavity (110), and the drone (200) is removably connected to the housing (100) by the mating of the first connector (400) and the second connector (210);

with the drone (200) in the second state, the first connector (400) is disconnected from the second connector (210) and at least part of the drone (200) protrudes outside the internal cavity (110) through the opening (120);

applying a force on the drone (200) to disengage the first connector (400) and the second connector (210).

2. The electronic device of claim 1, wherein the first connector (400) and the second connector (210) are magnetically attractive.

3. The electronic device of claim 1, wherein one of the first connector (400) and the second connector (210) is a clamping groove, and the other of the first connector and the second connector is a clamping protrusion, and when the unmanned aerial vehicle (200) is in the first state, the clamping groove is connected with the clamping protrusion in a clamping manner.

4. The electronic device according to claim 1, wherein the device body further comprises an ejection mechanism (300), the ejection mechanism (300) comprising a connecting rod (310), a slider (320), and an ejection assembly (330);

the sliding block (320) is provided with a limiting bulge (326), the unmanned aerial vehicle (200) comprises a limiting surface, and the limiting surface is lapped on the limiting bulge (326);

the sliding block (320) is provided with a guide track (321), and the guide track (321) comprises a first annular limiting section (322), an extending section (323), a second limiting section (324) and a retracting section (325) which are sequentially connected;

the ejection assembly (330) is arranged in the inner cavity (110), the ejection assembly (330) can drive the sliding block (320) to move towards the extending direction of the unmanned aerial vehicle (200), and the unmanned aerial vehicle (200) can move to the second state along with the movement of the sliding block (320) through the matching of the limiting protrusion (326) and the limiting surface;

the first end of the connecting rod (310) is hinged to the shell (100), the second end of the connecting rod (310) is in sliding fit with the guide track (321), the sliding block (320) has a first position and a second position, and the sliding block (320) can be switched between the first position and the second position under the action of external force;

with the sliding block (320) in the first position, at least part of the drone (200) protrudes out of the internal cavity (110) through the opening (120), the second end of the connecting rod (310) cooperating with the second restraint section (324);

under the condition that the sliding block (320) is located at the second position, at least part of the unmanned aerial vehicle (200) retracts into the inner cavity (110) through the opening (120), the first connecting piece (400) is connected with the second connecting piece (210), and the second end of the connecting rod (310) is matched with the first limiting section (322).

5. The electronic device of claim 4, wherein the ejecting assembly (330) comprises a third magnetic member (331) and a fourth magnetic member (332), the third magnetic member (331) is disposed on the housing (100), the fourth magnetic member (332) is disposed at an end of the slider (320) facing away from the opening (120), the fourth magnetic member (332) is disposed between the third magnetic member (331) and the slider (320), and the third magnetic member (331) and the fourth magnetic member (332) have the same polarity.

6. The electronic device of claim 5, wherein the pop-up assembly (330) further comprises a fifth magnetic member (333) and a sixth magnetic member (334), the fifth magnetic member (333) is disposed on the housing (100), the sixth magnetic member (334) is disposed on an end of the slider (320) facing the opening (120), the sixth magnetic member (334) is disposed between the fifth magnetic member (333) and the slider (320), and the fifth magnetic member (333) and the sixth magnetic member (334) have opposite polarities.

7. The electronic device according to claim 4, wherein the eject mechanism (300) further comprises a guide rod (340), the slider (320) is provided with a sliding slot, one end of the guide rod (340) is connected with the housing (100), the other end of the guide rod (340) extends into the sliding slot, and the sliding slot is in sliding fit with the guide rod (340) in the extending direction of the guide rod (340).

8. The electronic device of claim 4, wherein the second end of the connecting rod (310) is provided with an interference portion, and the interference portion is in interference with the first limiting section (322) or the second limiting section (324).

9. The electronic device of claim 4, wherein the guide rail (321) is a guide slot, and the first position-limiting section (322), the protruding section (323), the second position-limiting section (324), and the retracting section (325) are slot sections of the guide slot.

10. The electronic device of claim 1, wherein an outer surface of the drone (200) is coplanar with an outer surface of the housing (100) with the drone (200) in the first state.

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