The present disclosure relates to unmanned aerial vehicle (UAV) technology field and, more particularly, to an antenna structure, a remote controller, and an unmanned aerial vehicle (UAV) system.
The current unmanned aerial vehicle (UAV) is controlled by a remote controller. Both the UAV and the remote controller include antennas for wireless communication. For the current remote controller, a structure with two antennas is configured to send and receive signals at different frequency bands, so that the UAV can be controlled in various ways. For the current remote controller with the structure with two antennas, a technical problem exists that the two antennas cannot be folded and stored, or can only be folded and opened separately, and when the remote controller is used, the opening angle of each antenna must be adjusted separately, which is inconvenient.
Embodiments of the present disclosure provide an antenna structure, including a base, a first radiator, and a second radiator. The base is configured to be rotatably connected to a remote controller body of a remote controller of an unmanned aerial vehicle (UAV) system. One ends of the first radiator and the second radiator are connected to the base, and other ends of the first radiator and the second radiator extend away from the base. The first radiator and the second radiator are fixedly connected to the base in a rotation direction relative to the remote controller body and are configured to rotate simultaneously with the base in the rotation direction.
Embodiments of the present disclosure provide a remote controller, including a remote controller body, and an antenna structure. The antenna structure includes a base, a first radiator, and a second radiator. The base is configured to be rotatably connected to a remote controller body of a remote controller of an unmanned aerial vehicle (UAV) system. One ends of the first radiator and the second radiator are connected to the base, and other ends of the first radiator and the second radiator extend away from the base. The first radiator and the second radiator are fixedly connected to the base in a rotation direction relative to the remote controller body and are configured to rotate simultaneously with the base in the rotation direction.
Technical solutions of the present disclosure will be described in connection with the reference drawings. The described embodiments are only some of embodiments not all embodiments of the present disclosure. In accordance with embodiments of the disclosure, all other embodiments obtained by those of ordinary skill in the art without any creative work are within the scope of the present disclosure.
When a component is referred to as “fixed to” another component, the component may be directly on the other component or may have a component therebetween. When a component is referred to as “connected to” another component, the component may be directly connected to the other component or may have a component therebetween.
All technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art, unless otherwise defined. The terminology used in the specification of the present disclosure is for the purpose of describing specific embodiments and is not intended to limit the disclosure. The term “and/or” as used herein includes any or all combinations of one or more of the associated listed items.
Some embodiments of the disclosure are described in detail in connection with the reference drawings. When no conflict exists, the features of the embodiments and the embodiments described below can be combined with each other.
With reference to
Consistent with the disclosure, the first radiator 13 and the second radiator 14 are connected to the base 11, and the first radiator 13 and the second radiator 14 rotate with the base 11 in the first rotation direction. Thus, when the first radiator 13 and the second radiator 14 need to be folded or opened, an external force can be applied to the first radiator 13, the second radiator 14, or the base 11 to realize the synchronous rotation of the first radiator 13 and the second radiator 14 to reach set positions, e.g., set orientations. Compared to the radiators which need to be adjusted individually, the antenna structure of the present disclosure can allow adjustment of the positions, e.g., orientations, of the first radiator 13 and the second radiator 14 synchronously. The structure is simple, and the operation is convenient. In this disclosure, the position of a radiator, e.g., the first radiator 13 or the second radiator 14, can refer to, e.g., the orientation of the radiator, and the position of the radiator towards an object, e.g., the UAV, can refer to, e.g., the orientation of the radiator towards the object.
The antenna structure also includes a first rotation shaft 12 and a second rotation shaft 16. The first rotation shaft 12 includes a first rotation member 122 and a first fixation member 121. The first rotation member 122 is rotatably connected to the first fixation member 121. The second rotation shaft 16 includes a second rotation member 162 and a second fixation member 161. The second rotation member 162 is rotatably connected to the second fixation member 161. The first fixation member 121 and the second fixation member 161 are fixedly connected to the remote controller body 20. The first rotation member 122 penetrates through the first end surface 112 of the base 11, and the second rotation member 162 penetrates through the second end surface 113 of the base 11. With the provision of the first rotation shaft 12 and the second rotation shaft 16, and the first end surface 112 and the second end surface 113 of the base 11 cooperate with the first rotation shaft 12 and the second rotation shaft 16, respectively, rotation of the base 11 relative to the remote controller body 20 can be realized. In some embodiments, the first end surface 112 of the base 11 is configured with a first shaft hole (not shown in the figure), and the second end surface 113 is configured with a second shaft hole 1131. The axes of the first shaft hole and the second shaft hole 1131 are collinear. The first rotation member 122 is in mating connection with the first shaft hole, and the second rotation member 162 is in mating connection with the second shaft hole 1131, so that the base 11 is mounted at the remote controller body 20. In an embodiment, the second rotation member 162 is fixedly connected to the second fixation member 161, and the second rotation member 162 is movably connected to the second shaft hole 1131, where the second rotation member 162 provides a support function. In another embodiment, the second rotation member 162 is rotatably connected to the second fixation member 161, and the structure of the second rotation shaft 16 is similar to the structure of the first rotation shaft 12. The second rotation member 162 cooperates with the second shaft hole 1131 to form a rigid structure.
In some embodiments, as shown in, e.g.,
The first rotation member 122 includes a first middle shaft 1221 and a first sleeve 1222. The first sleeve 1222 is sleeved outside the first middle shaft 1221. The first middle shaft 1221 and the first sleeve 1222 are rotatably connected to each other. One end of the first middle shaft 1221 is fixedly connected to the first connection plate 1211 of the first fixation member 121. An extension direction of the first middle shaft 1221 is perpendicular to an extension plane of the first connection plate 1211. The first fixation plate 1213 of the first fixation member 121 may protrude from the first extension plate 1212 to the side of the first rotation member 122, so that the projection of the first connection hole 1214 at a plane parallel to the first fixation plate 1213 at least partially overlaps with the projection of the first rotation member 122, more specifically the first sleeve 1222, at the plane parallel to the first fixation plate 1213. As such, the center of gravity of the entire first rotation member 12, after the first fixation member 121 is connected and fixed, is more biased toward the side of the first rotation member 122. In this way, when the first sleeve 1222 of the first rotation member 122 rotates relative to the first middle shaft 1221, the torque between the first middle shaft 1221 and the first connection plate 1211 is smaller, and the lifetime of the first rotation shaft 1211 may be extended.
The cross-section of the first middle shaft 1221 is circular, and the cross-section of the first sleeve 1222 may be circular, or the inner surface of the first sleeve 1222 may be circular and the outer surface of the first sleeve 1222 may be polygonal. The inner surface of the first sleeve 1222 and the first middle shaft 1221 cooperate and form a rotation pair. The shape of the first shaft hole of the base 11 corresponds to the shape of the outer surface of the first sleeve 1222. For example, when the cross-section of the outer surface of the first sleeve 1222 is polygonal, the shape of the cross-section of the first shaft hole is also correspondingly polygonal. The first shaft hole cooperates with the first sleeve 1222 to form a rigid structure. Compared to a circular cross-section of the outer surface of the first sleeve 1222, the polygonal structure can ensure no relative sliding between the outer surface of the first sleeve 1222 and the inner surface of the first shaft hole of the base 11 to improve accuracy. Therefore, in the embodiment, the first end surface 112 of the base is rotated through the relative rotation of the rotation pair of the first sleeve 1222 and the first middle shaft 1221.
In some embodiments, the first rotation shaft 12 also includes the following characteristics. To save material, the first extension plate 1212 may adopt a hollow structure, for example, the first extension plate 1212 is formed by, but is not limited to, combining three-strip plates, with certain gaps existing between the three-strip plates and two ends of each of the three-strip plates being connected with the first connection plate 1211 and the first fixation plate 1213, respectively. To ensure the structural strength of the first connection plate 1211, the size (i.e., thickness) of the first connection plate 1211 in the direction of the first middle shaft 1221 is configured to be larger than the size of the first extension plate 1212. Further, to strengthen the connection structure between the first extension plate 1212 and the first fixation plate 1213 and reduce the stress, a first rib plate 1216 may be provided, which may be connected to the position where the first extension plate 1212 and the first fixation plate 1213 are connected to each other. To increase the structural strength of the first fixation plate 1213, the edge thickness of the first fixation plate 1213 is configured to be thicker than the thickness of the center area.
As shown in, e.g.,
The base 11 may extend as a straight column, such as cylindrical, ellipsoidal, or rectangular column with rounded corners. That is, the side surface 114 of the base 11 may be a cylindrical surface, an elliptical cylindrical surface, or a combination of flat and rounded surfaces. The dimension of the cross-section of the base 11 is kept the same, so that the area when the base 11 rotates is the same, and the structure of the base 11 mounted at the remote controller body 20 can be conveniently designed. The first end surface 112 and the second end surface 113 of the base 11 may be flat, and the first end surface 112 and the second end surface 113 are perpendicular to a straight line in the extension direction of the base 11, and the first end surface 112 and the second end surface 113 are parallel, so that the structure of the base 11 is simpler and easier to facilitate the assembly of the first rotation shaft 12 and the second rotation shaft 16.
The first rotation direction in this disclosure refers to a circumferential direction about a straight line extending along the base 11. In some embodiments, the first rotation direction may be in the circumferential direction about the axis of the first shaft hole and the second shaft hole 1131, and maybe a counter-clockwise direction or a clockwise direction.
The first radiator 13, the second radiator 14, and the base 11 may be an integrated structure, that is, the first radiator 13, the second radiator 14, and the base 11 may be integrally formed by a single process. The manufacturing process may include casting, turning, milling, etc. The first radiator 13 and the second radiator 14 can also be separate parts mounted at the base 11. For example, a clip sleeve can be opened on the side surface 114 of the base 11 and the first radiator 13 and the second radiator 14 can be inserted into the clip sleeve to be fixed, or the first radiator 13 and the second radiator 14 can be mounted at the side surface 114 of the base 11 using connection pieces such as screws, rivets, etc.
The first radiator 13 and the second radiator 14 are both configured to radiate and receive electromagnetic wave signals. The object of wireless communication is the UAV. A corresponding antenna device is provided at the UAV to receive the electromagnetic wave signals from the first radiator 13 and the second radiator 14, or send the electromagnetic wave signals to the first radiator 13 and the second radiator 14. The electromagnetic wave signals sent by the remote controller to the UAV through the first radiator 13 and the second radiator 14 are control instructions, and the control instructions may include adjusting parameters such as flight speed, altitude, etc., of the UAV, and control a camera device carried by the UAV to photograph or change the photographing angle, lens focal length, etc. The first radiator 13 and the second radiator 14 are electrically connected to the chip of the remote controller and controlled by different control circuits of the chip. The electromagnetic wave signals radiated and received by the first radiator 13 and the second radiator 14 are not in the same frequency band. The frequency ranges of the electromagnetic wave signals radiated and received by the first radiator 13 and the second radiator 14 do not overlap, so that the electromagnetic wave signals radiated by the first radiator 13 and the electromagnetic wave signals radiated by the second radiator 14 do not interfere with each other and the electromagnetic wave signals can be accurately radiated to the UAV to control the UAV. When the electromagnetic wave signals are received from the UAV, similarly, the electromagnetic wave signals with different frequency bands can be received by the first radiator 13 and the second radiator 14 and be transmitted to the chip to be processed by different circuits. In this way, the flight parameter of the UAV, the photographed images, videos, etc., can be obtained. When the UAV is at a certain position, the positions, e.g., orientations, of the first radiator 13 and the second radiator 14 towards the UAV should be determined and change following the position of the UAV. When adjusting the positions of the first radiator 13 and the second radiator 14, the relative position between the first radiator 13 and the second radiator 14 is not changed. In embodiments of the disclosure, the structure of the antennas can realize the position pairing between the first radiator 13 and the second radiator 14 with the UAV at once.
In embodiments of the present disclosure, the types of the first radiator 13 and the second radiator 14 are not limited. The first radiator 13 and the second radiator 14 may be monopole antennas, inverted-F antennas, loop antennas, etc. The first radiator 13 and the second radiator 14 are made of metal. The metal may be iron, aluminum, copper, alloys, etc. To protect the metal and form a complete and uniform appearance, the outer surfaces of the first radiator 13 and the second radiator 14 are also covered with a non-metallic shell. The non-metallic shell can be made of plastic material. The use of the non-metallic shell can also prevent signal shielding of the first radiator 13 and the second radiator 14.
The first radiator 13 and the second radiator 14 are described here as an example. In some other embodiments, the base may also include a third radiator, a fourth radiator, etc. When one radiator rotates, other radiators are driven by the base 11 to also rotate together, so that the positions of the plurality of radiators can be adjusted at once.
The first radiator 13 and the second radiator 14 may be provided at any position on the side surface 114 of the base 11. The first radiator 13 is provided at one end of the base 11 near the first end surface 112. The second radiator 14 is provided at one end of the base 11 near the second end surface 113. In other words, the first radiator 13 and the second radiator 14 are positions at the base 11 that are farthest to each other, so that sufficient antenna isolation is provided between the first radiator 13 and the second radiator 14 to prevent the signals of the first radiator 13 and the second radiator 14 from cross-talking with each other and affecting the communication quality with the UAV.
In an embodiment, to simplify the overall structure of the antenna structure, the first radiator 13 and the second radiator 14 are fixedly connected to the base 11, and the extension directions of the first radiator 13 and the second radiators 14 are parallel to each other. The positions of the first radiator 13 and the second radiator 14 towards the UAV are determined, and a radiator generally has a stronger capability of radiating and receiving electromagnetic wave signals at a position corresponding to the direction to which the radiator points, i.e., the orientation of the radiator. Therefore, by configuring the extension directions of the first radiator 13 and the second radiator 14 to be parallel to each other, the orientations of the first radiator 13 and the second radiator 14 are the same, so that a higher antenna efficiency can be achieved.
In an embodiment, the first radiator 13 is rotatably connected to the base 11 in a second rotation direction, and the second rotation direction is perpendicular to the first rotation direction. Due to the increased requirements for the autonomous operability of the remote controller, in the antenna structure provided in the embodiment, the first radiator 13 is configured to rotate in the second rotation direction, so that the first radiator 13 can rotate in the second rotation direction in addition to rotate in the first rotation direction with the base 11. Since the two rotation directions are perpendicular to each other, when the first radiator 13 rotates in the second rotation direction, the rotation in the first rotation direction will not be affected. The second rotation direction refers to a direction that the first radiator 13 rotates relative to the first end surface 112 and the second end surface 113 of the base 11, with the connection position between the first radiator 13 and the side surface 114 of the base 11 as the center. In an extreme scenario, the first radiator 13 can rotate to a position parallel to the extension direction of the base 11. In this way, the first radiator 13 can be fine-tuned to achieve better wireless communication.
The second radiator 14 may be similar to the first radiator 13 and may be rotatably connected to the base 11 in the second rotation direction to adjust the position of the second radiator 14 to achieve better wireless communication. The second radiator 14 may also be fixedly connected to the base 11, which can also realize wireless communication.
As shown in
The second radiator 14 is similar to the first radiator 13 and includes a second connection member 141 and a second radiation member 142. The second connection member 141 is connected to the base 11. The second radiation member 142 and the second connection member 141 have a smooth transition. The thickness of the second radiation member 142 may be smaller than the thickness of the second connection member 141 in the first rotation direction.
In one embodiment, the extension directions of the first radiator 13 and the second radiator 14 are in the same plane. The connection line of the connection position between the first radiator 13 and the second radiator 14 at the base 11 is parallel to the extension straight line of the base 11. When the base 11 rotates, the distances of the first radiator 13 and the second radiator 14 relative to the remote controller body 20 are always the same. In other words, the first radiator 13 and the second radiator 14 can contact the remote controller body 20 at the same time to facilitate a better storage of the first radiator 13 and the second radiator 14.
In an embodiment, as shown in
The groove 111 is formed between the first radiator 13 and the second radiator 14, that is, located in a middle part of the base 11, so as to avoid occupying the positions of the first shaft hole at the first end surface 112 and the second shaft hole 1131 at the second end surface 113 of the base 11. In some embodiments, as shown in
As shown in
When the base 11 rotates to drive the first radiator 13 to the position with the smallest opening angle relative to the remote controller body 20, the first radiator 13 contacts the remote controller body 20, and the opening of the groove 111 faces the remote controller body 20. When the first radiator 13 is at the position with the smallest opening angle, for example 0°, the first radiator 13 is in the folded state, and the first radiator 13 contacts the remote controller body 20 to realize the storage of the first radiator 13. At this state, the opening of the groove 111 at the base 11 faces the remote controller body 20, the remote controller body 20 closes the opening of the groove 111 to prevent the joysticks from being dropped and lost.
The limitations of the opening angle of the first radiator 13 and the opening of the groove 111 are also applicable to the second radiator 14. In an embodiment, the extension directions of the second radiator 14 and the first radiator 13 are in the same plane, so that both the second radiator 14 and the first radiator 13 can have the largest opening angle or the smallest opening angle at the same time.
As shown in
As shown in
In an embodiment, the separator 152 is provided at a middle part of the main body 151, so that the separator 152 and the main body 151 enclose to form the first clip groove 153 and the second clip groove 154 symmetric to each other about the separator 152. The joysticks include a left joystick 21 and a right joystick 22, and the first clip groove 153 and the second clip groove 154 are configured for clamping the left joystick 21 and the right joystick 22, respectively. In general, the remote controller is provided with two joysticks, that is, the left joystick 21 and the right joystick 22, and the left joystick 21 and the right joystick 22 are configured to implement different operation controls. The clip member 15 can clamp the left joystick 21 and the right joystick 22, so that both the left joystick 21 and the right joystick 22 are stored in the groove 111 and do not fall.
As shown in
As shown in
In the embodiment with the first protrusion engaged with the first groove, to strengthen the connection between the connection piece 15 and the inner surface of the groove 111, a second protrusion 119 and a third protrusion 120 are also provided at the inner surface of the groove 111. A second groove 1514 and a third groove 1515 are formed at the main body 151 of the clip member 15. The second protrusion 119 is engaged with the second groove 1514 and the third protrusion 120 is engaged with the third groove 1515 to fix the clip member 15 to the inner surface of the groove 111.
In an embodiment, as shown in
In some embodiments, there are more than two shift positions, and each shift position is configured with a pre-compression angle. The first rotation member 122 rotates to realize the more than two shift positions of the base. Since the first radiator 13 and the second radiator 14 may have a plurality of preferable opening angles, by setting more than two shift positions, the base 11, the first radiator 13, and the second radiator 14 may be fixed at one of a plurality of fixed positions.
There is a shift position respectively when the first radiator 13 is at the smallest opening angle or at the largest opening angle, that is, the first radiator 13 is at the folded state or at the fully opened state. Each of the two operation states is configured with a shift position with a pre-compression angle. For example, when the opening angle of the first radiator 13 is 0°, the first radiator 13 is at the folded state, and the pre-compression angle is set to 5°, the first radiator 13 rotates to 0° position with the opening angle between 0°˜5° until being fixed at the 0° position. Similarly, when the opening angle of the first radiator 13 is 180°, the first radiator 13 is at the fully opened state, and the pre-compression angle is set to −5°, the first radiator 13 rotates to 180° position with the opening angle between 175°˜180° until being fixed at the 180° position.
The present disclosure further provides an unmanned aerial vehicle (UAV) system, which includes a UAV and various remote controllers provided in embodiments of the present disclosure. The remote controller of the UAV system is provided with a base 11, and a first radiator 13 and a second radiator 14 that can rotate synchronously. The structure is simple, and the operation is convenient.
Referring to
Referring to
In some embodiments, the back cover 25 is provided with a transition member 252 and two handheld members 251. The two handheld members 251 are located at two side edges of the back cover 25 that are opposite to each other, respectively, and the transition member 252 is provided between the two handheld members 251. The two handheld members 251 protrude from the transition member 252. When the base 11 rotates to cause the first radiator 13 of the base 11 to be at a position with the smallest opening angle relative to the remote controller body 20, the first radiator 13 contacts the transition member 252, and the protrusion height of the first radiator 13 in the direction perpendicular to the transition member 252 is not higher than the heights of the two handheld members 251. The cross-sections of the two handheld members 251 are arc-shaped and form grip handles, which are convenient for the users to hold with fingers of both hands. The two handheld members 251 protrude from the transition member 252, so that the transition member 252 forms a recess structure relative to the two handheld members 251. When the first radiator 13 rotates to have the smallest opening angle, the first radiator 13 contacts the transition member 252, and the height of the first radiator 13 does not exceed the heights of the two handheld members 251. As such, the first radiator 13 is accommodated. The remote controller may be placed on the desk with the back cover 25 facing the desk. Thus, the remote controller does not compress the first radiator 13 to deform, and is convenient to be packaged and transported. In some embodiments, since the second radiator 14 is in the same plane with the extension plane of the first radiator 13, the second radiator 14 and the first radiator 13 may rotate synchronously and contact the transition member 252.
The structure of the top cover 24 may also correspond to the back cover 25, that is, the middle portion of the top cover 24 are recessed relative to both sides. When the base 11 is mounted at the top cover 24, the first radiator 13 and the second radiator 14 are located in the edge area of the middle portion. As such, the first radiator 13 and the second radiator 14 may contact the transition member 252 to be accommodated corresponding to the position of the transition member 252.
Referring to
The remote controller further includes a front cover 26. The front cover is provided opposite to the back cover 25. The top cover 24 is away from a side of the back cover 25 and connected to the front cover 26. The front cover 26 is provided with an operation member (not shown in the figure), and the operation member is provided with a joystick. The joystick is configured to control the remote controller. The front cover 26 is provided with the operation member. Thus, operating the remote controller may be performed at the front cover 26. The operation of the remote controller is implemented by swinging the joystick, such that the antenna structure does not affect the control of the remote controller. Besides the joystick, the operation member may be further provided with an operation button, a display, etc.
The remote controller further includes a bottom cover. The bottom cover is connected to a position between the front cover 26 and the back cover 25. The bottom cover and the top cover 24 are provided opposite to each other. The bottom cover, the top cover 24, the front cover 26, and the back cover 25 are configured to form a complete structure of the remote controller body 20. A structure such as a chip, a circuit, a connection wire, etc. may be provided in the remote controller body 20. The remote operation of the remote controller may be realized through the cooperation of the various components of the remote controller body 20.
In some embodiments, the joystick is detachably connected to the operation member.
When the UAV is grounded, the groove 111 of the base 11 is configured to accommodate the joystick detached from the operation member. The joystick may be placed into and taken out the groove 111 through the opening. The joystick is detachably designed. The joystick may be accommodated to reduce a protrusion structure of the remote controller body 20 for convenient packaging and transportation.
Referring to
In general, the joystick includes a left joystick 21 and a right joystick 22. When the left joystick 21 and the right joystick 22 are accommodated in the groove 111, the left joystick 21 and the right joystick 22 are clamped in the first clip groove 153 and the second clip groove 154, respectively. The plug 211 of the left joystick 21 and the plug 221 of the right joystick 22 are oppositely provided. The extension directions of the left joystick and the right joystick are in a straight line. With this setup, the left joystick 21 and the right joystick 22 may be accommodated in the groove 111 and may not interfere with the rotation of the base 11.
The antenna structure, the remote controller, and the UAV of embodiments of the present disclosure are described in detail. Specific examples are used to describe the theory and embodiments of the present disclosure. The above embodiments are merely used to help to understand the methods and the core ideas of the present disclosure. Those of ordinary skill in the art can modify specific embodiments and application scope according to the spirit of the present disclosure. In summary, the specification should not be considered to limit the present disclosure.
This application is a continuation of International Application No. PCT/CN2018/093052, filed Jun. 27, 2018, the entire content of which is incorporated herein by reference.
Number | Date | Country | |
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Parent | PCT/CN2018/093052 | Jun 2018 | US |
Child | 17035362 | US |