CN108701897A - Directional aerial rotating mechanism and gateway device - Google Patents
Directional aerial rotating mechanism and gateway device Download PDFInfo
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- CN108701897A CN108701897A CN201680082046.XA CN201680082046A CN108701897A CN 108701897 A CN108701897 A CN 108701897A CN 201680082046 A CN201680082046 A CN 201680082046A CN 108701897 A CN108701897 A CN 108701897A
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- directional aerial
- rotary shaft
- omnidirectional antenna
- rotating disk
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
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- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
This application provides a kind of directional aerial rotating mechanisms, including directional aerial, omnidirectional antenna, rotating disk, transmission component and actuator.The rotating disk includes the top and bottom being oppositely arranged, and in the bottom surface, the transmission component is set to the top surface for the directional aerial and omnidirectional antenna setting.The transmission component is connected between the rotating disk and the actuator.The actuator drives the rotating disk to rotate by the transmission component, to adjust the radiation direction of the directional aerial.Present invention also provides a kind of gateway devices.The application drives rotating disk shaft by actuator, controls the radiation direction of directional aerial, avoids and manually adjusts inconvenient problem.
Description
This application involves fields of communication technology, and in particular to a kind of directional aerial rotating mechanism and gateway.
With the fast development of mobile Internet and smart phone in recent years, the usage amount of WLAN (WIFI) is increasingly frequently in daily life, usage scenario is increasingly sophisticated and household area increases that all more stringent requirements are proposed to the signal covering quality of gateway.
Currently on the market, user is exactly that WIFI signal covering quality is poor to most problems that wireless gateway device is complained, i.e., signal covering surface is small, signal strength is weak, influences online experience.Two kinds, i.e. omnidirectional antenna and directional aerial are generally divided into applied to the antenna on wireless gateway device.Omnidirectional antenna 360 degree of all homogeneous radiations in the horizontal plane, non-directional, so the signal cover of the gateway of mounting omnidirectional antenna is big, but gain is low, and distance is close.Directional aerial shows as having directionality with certain angle radiation scope in the horizontal plane, so the signal coverage distance of the gateway of installation directional aerial is remote, high gain, but coverage area is small.The combined use of directional aerial and omnidirectional antenna can improve the area coverage and gain of signal to a certain extent.And higher gain could only be obtained in the case where the antenna alignment with user terminal by orienting antenna direction, the aerial position of user terminal can change with the movement of user in practical situations, so the WIFI signal of user is limited using quality by directional aerial direction.
In the prior art, the position that the mode manually adjusted adjusts directional aerial is generallyd use, this adjustment mode is extremely inconvenient.
How the directional aerial adjust automatically direction of gateway is realized, the direction persistently studied for industry.
Summary of the invention
The embodiment of the present application provides a kind of directional aerial rotating mechanism and gateway, to solve the problems, such as that directional aerial adjustment is inconvenient in the prior art, realizes the adjust automatically of directional aerial, to improve the signal covering quality of gateway.
The application first aspect provides a kind of directional aerial rotating mechanism, comprising: directional aerial, omnidirectional antenna, rotating disk, transmission component and actuator, the rotating disk includes the top and bottom being oppositely arranged, described fixed
It is arranged to antenna and the omnidirectional antenna in the bottom surface, the transmission component is set to the top surface, the transmission component is connected between the rotating disk and the actuator, and the actuator drives the rotating disk to rotate by the transmission component, to adjust the radiation direction of the directional aerial.
With reference to first aspect, in the first possible embodiment, the omnidirectional antenna includes the first omnidirectional antenna and the second omnidirectional antenna, and first omnidirectional antenna and second omnidirectional antenna are set to the directional aerial two sides.The radiation length of directional aerial is long, but angle is small；Omnidirectional antenna angle of radiation is big, but apart from short.In present embodiment, directional aerial is located between two omnidirectional antennas, and the omnidirectional antenna of directional aerial two sides can make up the small deficiency of directional antenna radiation angle, increases the signal radiation angle of directional aerial rotating mechanism.
The possible embodiment of with reference to first aspect the first, in second of possible embodiment, the rotating disk is in the form of annular discs, the directional aerial, first omnidirectional antenna and second omnidirectional antenna are located at the marginal position of the rotating disk, first omnidirectional antenna and second omnidirectional antenna are symmetrically distributed in the two sides of the rotating disk rotation center, and first omnidirectional antenna and second omnidirectional antenna are also symmetrically distributed in the two sides of the directional aerial.Further, the line at the center of the first omnidirectional antenna and second omnidirectional antenna center can center Jing Guo rotating disk.In present embodiment, the layout type of first omnidirectional antenna and second omnidirectional antenna makes the spacing of the first omnidirectional antenna and the second omnidirectional antenna on the rotating pan maximum, to reduce signal interference between the two.
With reference to first aspect, in the third possible embodiment, the directional aerial includes radiator and reflecting plate, the reflecting plate is arc panel or folded structure, the radiator is set at the reflection kernel of the reflecting plate, and to increase the signal radiation directionality of the radiator, while reflecting plate makes the concentration of radiator radiation signal in the same direction, so that the antenna gain of directional aerial increases, the signal of radiation reaches farther away transmission range.
The third possible embodiment with reference to first aspect, in 4th kind of possible embodiment, the bottom surface of the rotating disk is equipped with the first buckle, first buckle is equipped with card slot, the card slot is for accommodating the radiator, so that the radiator is removably attachable in the rotating disk, radiator is conveniently replaceable or safeguarded.
With reference to first aspect, in 5th kind of possible embodiment, the transmission component includes the first gear and second gear being meshed, the first gear is fixed to the rotating disk, the second gear is connected to the actuator, the actuator drives the first gear to rotate by driving the second gear rotation, to drive the rotating disk to rotate, to realize 360 degree of rotations of directional aerial in rotating disk.
It with reference to first aspect, further include fixed bracket in the 6th kind of possible embodiment, the fixed branch
Frame is opposite with the top surface of the rotating disk, orthographic projection of the rotating disk on the fixed bracket is located at the fixed internal stent, the actuator is embedded in the fixed bracket, and specific inline mode is that the fixed bracket is equipped with groove, and the groove is for installing the actuator.Actuator is installed on fixed internal stent, takes full advantage of the space in fixed bracket, promotes directional aerial rotating mechanism small design.
The 6th kind of possible embodiment with reference to first aspect further includes rotary shaft, the rotating disk is fixedly connected with the rotary shaft and is rotated centered on the rotary shaft, and the fixed holder pivots are connected to the rotary shaft in the 7th kind of possible embodiment.Rotary shaft can be with fixed bracket and rotating disk is vertical connect.Specifically, in the case where fixed bracket is fixed, rotary shaft can be to fix bracket as support frame, by rotating connecting part vertical hanging on fixed bracket, 360 degree of rotations in the plane being parallel to where fixed bracket, and the rotating disk vertical with rotary shaft is driven to do 360 degree of rotations together in the plane being parallel to where fixed bracket.
The 7th kind of possible embodiment with reference to first aspect, in 8th kind of possible embodiment, the rotating disk is in the form of annular discs, the rotary shaft is through the center of the rotating disk, the support bracket fastened center includes an axis hole, and the rotary shaft passes through the axis hole and connect with the fixed holder pivots.When rotating disk is rotated around rotary shaft for center axis, if rotary shaft is through the center of the rotating disk, rotating disk horizontal surface area required for rotary shaft rotation is minimum at this time.Present embodiment is more conducive to the volume occupied when reducing directional aerial rotating mechanism working condition, convenient for reducing the space that directional aerial rotating mechanism occupies.Rotary shaft and support bracket fastened center are rotatablely connected, so that fixed bracket is identical as the central axis of rotating disk, promote the miniaturization of directional aerial rotating mechanism.
The 7th kind of possible embodiment with reference to first aspect, in 9th kind of possible embodiment, the transmission component includes the first gear and second gear being meshed, the first gear is centered on the rotary shaft and is fixed to the rotary shaft, the second gear is connected to the actuator, the actuator drives the first gear to rotate by driving the second gear rotation, to drive the rotating disk to rotate, to realize 360 degree of rotations of directional aerial in rotating disk.
The 7th kind of possible embodiment with reference to first aspect, it further include circuit board in tenth kind of possible embodiment, the circuit board is located at the side of the rotating disk, and face the bottom surface of the rotating disk, the rotary shaft is in hollow structure, it is electrically connected between the actuator and the circuit board by electric connection line, the electric connection line is passed through from the hollow space of the rotary shaft, realizes that the circuit board is electrically connected with the actuator.
The tenth kind of possible embodiment with reference to first aspect, in a kind of the tenth possible embodiment, institute
Rotary shaft is stated equipped with first through hole, the first through hole is arranged radially along the rotary shaft, it is electrically connected between the directional aerial and the circuit board by the first connecting line, first connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and the rotary shaft is stretched out from the first through hole, to be electrically connected with the directional aerial.
A kind of possible embodiment of the tenth with reference to first aspect, in the 12nd kind of possible embodiment, the omnidirectional antenna includes the first omnidirectional antenna and the second omnidirectional antenna, and first omnidirectional antenna and second omnidirectional antenna are set to the directional aerial two sides.
The 12nd kind of possible embodiment with reference to first aspect, in 13rd kind of possible embodiment, the rotary shaft is equipped with the second through-hole being arranged radially along the rotary shaft, it is electrically connected between first omnidirectional antenna and the circuit board by the second connecting line, second connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and the rotary shaft is stretched out from second through-hole, to be electrically connected with first omnidirectional antenna.
The 13rd kind of possible embodiment with reference to first aspect, in 14th kind of possible embodiment, the rotary shaft is equipped with the third through-hole being arranged radially along the rotary shaft, it is electrically connected between second omnidirectional antenna and the circuit board by third connecting line, the third connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and the rotary shaft is stretched out from the third through-hole, to be electrically connected with second omnidirectional antenna.
The 14th kind of possible embodiment with reference to first aspect, in the 15th kind of possible embodiment, on the axial direction of the rotary shaft, the first through hole, second through-hole and the third through-hole are spaced apart from each other.
The 15th kind of possible embodiment with reference to first aspect, in 16th kind of possible embodiment, in the circumferential direction of the rotary shaft, it is separated by 90 degree between the first through hole and second through-hole, it is separated by 90 degree between the first through hole and the third through-hole, the first through hole is between second through-hole and the third through-hole.
During directional aerial and omnidirectional antenna rotate, the connecting line being connected with them can also be rotated with.In order to avoid connecting line is wound into antenna structure or other equipment in rotary course, the application is by combing the trend of connecting line so that connecting line is separated with antenna assembly for hollow cylindrical configuration for rotating shaft designs.Via design being pierced by for connecting line in rotary shaft, and connected with corresponding antenna, it can avoid winding between connecting line.
The application second aspect provides a kind of gateway, comprising: directional aerial rotating mechanism, the orientation
The directional aerial rotating mechanism that antenna turning unit is any of the above-described kind, the gateway further includes rotational control assemblies, and the rotational control assemblies drive the rotation of the rotating disk and the directional aerial by controlling the actuator.
In conjunction with second aspect, in the first possible embodiment, the gateway further includes signal detection component, and the signal for detecting the gateway surrounding uses position；The probe assembly is electrically connected with the rotational control assemblies, and after the signal detection component detection goes out the signal using position, the rotational control assemblies, which will control the directional aerial and turn to the signal, uses position.
The combination design of directional aerial and omnidirectional antenna is ensured that gateway has biggish signal cover and higher antenna gain by directional aerial rotating mechanism provided by the present application and gateway；Directional aerial is driven to rotate by control actuator, with the radiation direction of adjust automatically directional aerial.This directional aerial rotating mechanism and gateway under trigger condition can adjust automatically directional aerial radiation direction to optimal position, meet user for the use demand of wireless network, overcome and manually adjust not convenient problem.
In ord to more clearly illustrate embodiments of the present application or technical solution in the prior art, the drawings to be used in the embodiments are briefly described below, apparently, the drawings in the following description are only some examples of the present application, for those of ordinary skill in the art, without creative efforts, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is the directional aerial rotating mechanism structural schematic diagram that the application embodiment provides；
Fig. 2 is the directional aerial rotating mechanism partial structural diagram that the application embodiment provides；
Fig. 3 is the directional aerial rotating mechanism partial structural diagram that the application embodiment provides；
Fig. 4 is the directional aerial rotating mechanism partial structural diagram that the application embodiment provides；
Fig. 5 is the gateway structural schematic diagram that the application embodiment provides.
To keep the purposes, technical schemes and advantages of the embodiment of the present application clearer, below in conjunction with the attached drawing in the embodiment of the present application, the technical scheme in the embodiment of the application is clearly and completely described, obviously, described embodiment is some embodiments of the present application, instead of all the embodiments.Based on the embodiment in the application, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, shall fall in the protection scope of this application.
Also referring to Fig. 1 and Fig. 2, directional aerial rotating mechanism 01 provided by the present application, including directional aerial 1, omnidirectional antenna 2, rotating disk 3, transmission component 4 and actuator 5.The rotating disk 3 includes the top surface 31 and bottom surface 32 being oppositely arranged, and in the bottom surface 32, the transmission component 4 is set to the top surface 31 for the directional aerial 1 and the setting of the omnidirectional antenna 2.In a kind of embodiment, the structure in the form of a circular plate of rotating disk 3, top surface 31 is parallel to bottom surface 32, is connected by columned side therebetween.It when 3 structure in the form of a circular plate of rotating disk, is rotated in the horizontal plane around center location, the other spatial position being not necessarily to, present embodiment can reduce taking up space in directional aerial rotating mechanism horizontal plane.
The transmission component 4 is connected between the rotating disk 3 and the actuator 5, and the actuator 5 drives the rotating disk 3 to rotate by the transmission component 4, to adjust the radiation direction of the directional aerial 1.In a kind of embodiment, transmission component 4 is driven to rotate under the driving effect of actuator 5, the rotation of transmission component 4 drives rotating disk 3 to rotate, to realize 360 degree of rotating disk rotations.
Referring to Fig. 2, the omnidirectional antenna 2 includes the first omnidirectional antenna 21 and the second omnidirectional antenna 22, first omnidirectional antenna 21 and second omnidirectional antenna 22 are set to 1 two sides of directional aerial.The radiation length of directional aerial 1 is long, but angle is small；2 angle of radiation of omnidirectional antenna is big, but apart from short.In present embodiment, directional aerial 1 is located between two omnidirectional antennas 2, the omnidirectional antenna 2 of 1 two sides of directional aerial can make up the small deficiency of 1 angle of radiation of directional aerial, the gateway formed by the combination of directional aerial and omnidirectional antenna, its signal radiation angle is big, and the pointing direction antenna gain of directional aerial is big, signal strength is high, signal quality is good.In addition, when the avoidable User Activity of antenna combination design in present embodiment goes out directional antenna radiation range and the case where directional aerial turns in time not yet, causes the signal catastrophic failure of user.In other embodiments, directional aerial rotating mechanism 01 includes multiple directional aerials 1 and multiple omnidirectional antennas 2.
The directional aerial 1 includes radiator 11 and reflecting plate 12, and the reflecting plate 12 is arc panel or folded structure.In other words, reflecting plate 12 is in semi-surrounding structure, and radiator 11 is located at the side of reflecting plate 12, and reflecting plate 12 is looped around around 11 side of radiator.In a kind of specific embodiment, radiator 11 is located at the center of arc-shaped reflecting plate 12, this center is similar at the reflector focus of arc-shaped reflecting plate 12.In 1 course of work of directional aerial, radiator 11 emits signal around, after the reflection of reflecting plate 12, all towards the same direction, to increase the signal radiation directionality of the radiator 11, radiation signal in the same direction is concentrated simultaneously, increases the antenna gain of directional aerial 1, the signal of radiation reaches farther away transmission range.The opening direction of reflecting plate 12 can be the direction for facing away from 3 center of rotating disk, so that towards user at radiation signal concentration.
In a kind of embodiment, the rotating disk 3 is in the form of annular discs, the directional aerial 1, first omnidirectional
Antenna 21 and second omnidirectional antenna 22 are located at the marginal position of the rotating disk.
In a kind of embodiment, first omnidirectional antenna 21 and second omnidirectional antenna 22 are symmetrically distributed in the two sides of 3 rotation center of rotating disk.First omnidirectional antenna 21 and second omnidirectional antenna 22 are also symmetrically distributed in the two sides of directional aerial 1.Further, the line at the center of the first omnidirectional antenna 21 and 22 center of the second omnidirectional antenna can center Jing Guo rotating disk 3.In present embodiment, the layout type of first omnidirectional antenna and second omnidirectional antenna makes the spacing of the first omnidirectional antenna and the second omnidirectional antenna on the rotating pan maximum, to reduce signal interference between the two.
In a kind of embodiment, rotating disk 3 is in the form of annular discs.On 3 circumferencial direction of rotating disk, 90 degree are differed between directional aerial 1 and the first omnidirectional antenna 21, also differs 90 degree between directional aerial 1 and second omnidirectional antenna 22.
Please refer to Fig. 2, the bottom surface 32 of the rotating disk 3 is equipped with first the 321, second buckle 322 of buckle, the 323, the 4th buckle 324 of third buckle, it is respectively used to that the radiator 11, the reflecting plate 12, first omnidirectional antenna 21 and second omnidirectional antenna 22 are installed, so that directional aerial 1 and omnidirectional antenna 2 are fixed in rotating disk 3.Specifically, the first buckle 321 can be integrally formed with rotating disk 3, it is also possible to split type structure therebetween, is assembled and fixed by screw.First buckle 321 is equipped with card slot, can accommodate radiator 11, and radiator 11 is inserted into card slot and is fixed to the first buckle 321.In this way, being dismountable connection relationship between radiator 11 and rotating disk 3, radiator 11 is convenient for changing or safeguarded.Equally, between the second buckle 322 and reflecting plate 12, third buckle 323 and first between omnidirectional antenna 21, all can be dismountable connection relationship between the 4th buckle 324 and the second omnidirectional antenna 22.
The directional aerial 1 and omnidirectional antenna 2 can be linear or planar or other shapes.
Referring to Fig. 1, the transmission component 4 includes the first gear 41 and second gear 42 being meshed.The first gear 41 is fixed to the rotating disk 3, and in a kind of embodiment, first gear 41 is set to the perimeter side edge of rotating disk 3.The second gear 42 is connected to the actuator 5, the second gear 42 and the actuator 5 are coaxially connected, second gear 42 and first gear 41 are intermeshed, the actuator 5 drives the first gear 41 to rotate by driving the rotation of second gear 42, to drive the rotating disk 3 to rotate, to realize 360 degree of rotations of directional aerial 1 in rotating disk 3.In other embodiments, transmission component 4 is also possible to belt transmission or other modes realized actuator 5 and drive 3 360 degree of rotations of energy of rotating disk.
Referring to Fig. 3, directional aerial rotating mechanism 01 further includes fixed bracket 6, fixed bracket 6 is located at the side of rotating disk 3, and opposite with the top surface 31 of the rotating disk 3, the rotating disk 3 is described solid
Orthographic projection on fixed rack 6 is located inside the fixed bracket 6.The actuator 5 is embedded in the fixed bracket 6, and specific embedded mode is that the fixed bracket 6 is equipped with groove 61, and the groove 61 is for installing the actuator 5.Groove 61 is set to install actuator 5 in fixed bracket 6, takes full advantage of the space in fixed bracket 6, promotes directional aerial rotating mechanism small design.
Directional aerial rotating mechanism 01 further includes rotary shaft 7, and the rotating disk 3 is fixedly connected with the rotary shaft 7 and is rotated centered on the rotary shaft 7, the fixed rotation connection of bracket 6 to the rotary shaft 7.Rotary shaft 7 can be with fixed bracket 6 and rotating disk 3 is vertical connect.Specifically, in the case where fixed bracket 6 is fixed, rotary shaft 7 can be to fix bracket 6 as support frame, by rotating connecting part vertical hanging on fixed bracket 6,360 degree of rotations in the plane being parallel to where fixed bracket 6, and the rotating disk 3 vertical with rotary shaft 7 is driven to do 360 degree of rotations together in the plane being parallel to where fixed bracket 6.
In a kind of embodiment, referring to Figure 2 together and Fig. 3, the rotating disk 3 is in the form of annular discs, and the rotary shaft 7 is through the center of the rotating disk 3, the center of the fixed bracket 6 includes an axis hole 62, and the rotary shaft 3 passes through the axis hole 62 and is rotatablely connected with the fixed bracket 6.When rotating disk 3 is rotated around rotary shaft 7 for center axis, if rotary shaft 7 is through the center of the rotating disk 3, rotating disk 3 rotates required horizontal surface area minimum around rotary shaft 7 at this time.In the case where meeting other demands, present embodiment is more conducive to the volume occupied when reducing 01 working condition of directional aerial rotating mechanism, convenient for reducing the space that directional aerial rotating mechanism occupies.Rotary shaft and support bracket fastened center are rotatablely connected, so that fixed bracket is identical as the central axis of rotating disk, promote the miniaturization of directional aerial rotating mechanism.In this embodiment, the radiation direction of directional aerial 1 can face away from the rotary shaft 7 of rotating disk 3, directional aerial 1 and omnidirectional antenna 2 can be distributed around the rotary shaft 7, as shown in Figure 1, this mode may insure that 01 surrounding of directional aerial rotating mechanism has radiation signal, and have on directional aerial pointing direction compared with intense radiation signal.
A kind of embodiment, the transmission component 4 include the first gear 41 and second gear 42 being meshed.The second gear 42 is connected to the actuator 5, and the first gear 41 is centered on the rotary shaft 7 and is fixed to the rotary shaft 7, and the second gear 42 and the actuator 5 are coaxially connected.First gear 41 can be set to the perimeter side edge of rotating disk 3, i.e. second gear 42 and rotating disk 3 be in the same plane, or, first gear 41 can be set in rotary shaft 7, i.e. second gear 42 and rotating disk 3 be not in the same plane, alternatively, other first gears 41 rotate the mode that rotating disk 3 can be driven to rotate.Preferably, first gear 41 is set in rotary shaft 7, as shown in figure 4, second gear 42 and rotating disk 3
Not in the same plane.Space in 3 occupancy level plane of rotating disk is larger and takes up space in vertical plane small, second gear 42 is arranged in the vertical space of rotating disk 3, such design can make full use of vertical spatial position, reduce the volume of directional aerial rotating mechanism 01, be convenient for device miniaturization.By above several embodiments, the actuator 5 can drive the first gear 41 to rotate by driving the rotation of second gear 42, so that the rotating disk 3 rotates, to realize 360 degree of rotations of directional aerial in rotating disk.
Please refer to Fig. 1, directional aerial rotating mechanism 01 further includes circuit board 9, the circuit board 9 is located at the side of the rotating disk 3, and face the bottom surface 32 of the rotating disk 3, the rotary shaft 7 is in hollow structure, it is electrically connected between the actuator 5 and the circuit board 9 by electric connection line (not shown), the electric connection line is passed through from the hollow space of the rotary shaft 7.The circuit board 9 is used to power for the directional aerial 1, the first omnidirectional antenna 21, the second omnidirectional antenna 22, actuator 5.
Please refer to Fig. 2, the rotary shaft 7 is equipped with first through hole 71, the first through hole 71 is arranged radially along the rotary shaft 7, the direction of the first through hole 71 corresponds to the direction where the directional aerial 1, it is electrically connected between the directional aerial 1 and the circuit board 9 by the first connecting line 81, first connecting line 81 protrudes into the hollow space of the rotary shaft 7 from the side of the circuit board 9, and the rotary shaft 7 is stretched out from the first through hole 71, to be electrically connected with the directional aerial 1, to realize circuit board 9 for the power supply of directional aerial 1.
The omnidirectional antenna 2 includes the first omnidirectional antenna 21 and the second omnidirectional antenna 22., first omnidirectional antenna 21 and second omnidirectional antenna 22 are set to 1 two sides of directional aerial.The second through-hole 72 being arranged radially along the rotary shaft 7 is additionally provided in the rotary shaft 7, it is electrically connected between first omnidirectional antenna 21 and the circuit board 9 by the second connecting line 81, second connecting line 81 protrudes into the hollow space of the rotary shaft 7 from the side of the circuit board 9, and the rotary shaft 7 is stretched out from second through-hole 72, to be electrically connected with first omnidirectional antenna 21.
The third through-hole 83 being arranged radially along the rotary shaft 7 is additionally provided in the rotary shaft 7, it is electrically connected between second omnidirectional antenna 22 and the circuit board 9 by third connecting line 73, the third connecting line 73 protrudes into the hollow space of the rotary shaft 7 from the side of the circuit board 9, and the rotary shaft 7 is stretched out from the third through-hole 83, to be electrically connected with second omnidirectional antenna 22.
On the axial direction of the rotary shaft 7, the first through hole 81, second through-hole 82 and the third through-hole 83 are spaced apart from each other.In the circumferential direction of the rotary shaft 7, it is separated by 90 degree between the first through hole 81 and second through-hole 82, the first through hole 81 and the third through-hole 83
Between be separated by 90 degree, the first through hole 81 is between second through-hole 82 and the third through-hole 83.
During directional aerial 1 and omnidirectional antenna 2 rotate, the connecting line being connected with them can also be rotated with.In order to avoid connecting line is wound into antenna structure or other equipment in rotary course, the application is by being designed as hollow cylindrical configuration for rotary shaft 7, so that connecting line is separated with antenna assembly, combs the trend of connecting line.Via design being pierced by for connecting line in rotary shaft 7, and connected with corresponding antenna, it can avoid connecting line and wind.
Referring to Fig. 5, a kind of gateway 00 provided by the embodiments of the present application further includes rotational control assemblies (not shown) including directional aerial rotating mechanism 01 described in any one of the above embodiment.The rotational control assemblies are located on circuit board 9, and are electrically connected with circuit board 9, while the rotational control assemblies are electrically connected with the actuator 5, and connecting line may pass through the hollow channel setting of rotary shaft 7.The rotational control assemblies drive the rotation of the rotating disk 3 and the directional aerial 1 by controlling the actuator 5.In present embodiment, gateway 00 is wireless router.
After a trigger condition is given in the external world, the trigger condition gives rotational control assemblies one rotation command, and rotational control assemblies pass through the driving of actuator 5, and directional aerial 1 is driven to rotate around rotary shaft 7, change antenna gain radiation direction, to meet user to the use demand of wireless network.
Above-mentioned trigger condition can be completed by an independent controller, i.e. user is by operating the key for controlling router rotation on the controller, form a trigger condition, rotational control assemblies receive " router rotation " instruction of controller transmission, and control actuator 5 drives rotary shaft 7, rotating disk 3, directional aerial 1 and omnidirectional antenna 2 to rotate together.When user thinks to have rotated into the optimal direction of wireless network or terminal notifying by directional aerial 1 wireless network is best at this time when, user can make directional aerial 1 maintain the direction constant by operating the key for controlling router on the controller and stopping rotating.When user is moved to other positions, directional aerial 1 can also be controlled through the above way and rotates to user using the optimal direction of wireless network.Gateway 00 provided by the present application solves the problems, such as that manual adjustment directional aerial 1 is not convenient, meets wireless network demand when user moves everywhere in a certain range.
Above-mentioned trigger condition can also be completed by application program.I.e. user installs the application program at the terminal, user controls directional aerial 1 by the application triggers rotational control assemblies and rotates, when user thinks to have rotated into the optimal direction of wireless network or terminal notifying by directional aerial 1, wireless network is best at this time, user can be stopped rotating by operating the application program controlling router, and directional aerial 1 is made to maintain the direction constant.
In a kind of embodiment, gateway 00 further includes signal detection component (not shown), and the signal for detecting 00 surrounding of gateway uses position.The probe assembly is electrically connected with the rotational control assemblies, the signal detection component is located on circuit board 9, and be electrically connected with circuit board 9, while the rotational control assemblies are electrically connected with the actuator 5, connecting line may pass through the hollow channel setting of rotary shaft 7.After the signal detection component detection goes out the signal using position, the rotational control assemblies, which will control the directional aerial 1 and turn to the signal, uses position.Specifically, trigger condition can be passed through, trigger signal probe assembly starts to detect the wireless network signal of the router surrounding using position, and when detecting wireless network signal using position, automatic trigger rotational control assemblies control directional aerial 1 rotates to the position.After the completion of rotation, user can stop the detection of trigger signal probe assembly, convenient for saving energy.The trigger condition can be completed by independent controller, application program or other modes.
A kind of gateway 00 provided by the present application further includes top shell 02, bottom case 03 and connects and supports shell 04 between the top shell and the bottom case.The top shell 02 is located at the side of the fixed bracket 6, is fixedly connected with the fixed bracket 6, the fixed bracket 6 separates the top shell 02 and the rotating disk 3.The bottom case 03 is located at the side of the circuit board 9, is fixedly connected with the circuit board 9, the circuit board 9 separates the bottom case 03 and the rotating disk 3.The shell 04 is used for the directional aerial rotating mechanism 01, the rotational control assemblies, the signal detection component package between the top shell 02 and the bottom case 03.In a kind of embodiment, which is wireless router, including directional aerial rotating mechanism 01, can adjust automatically optimal wireless network signal direction, enable users to use optimal wireless network more conveniently.
Directional aerial rotating mechanism and gateway provided by the embodiment of the present application are described in detail above, specific examples are used herein to illustrate the principle and implementation manner of the present application, the description of the example is only used to help understand the method for the present application and its core ideas；At the same time, for those skilled in the art, according to the thought of the application, there will be changes in the specific implementation manner and application range, in conclusion the contents of this specification should not be construed as limiting the present application.
Claims (19)
- A kind of directional aerial rotating mechanism, it is characterized in that, including directional aerial, omnidirectional antenna, rotating disk, transmission component and actuator, the rotating disk includes the top and bottom being oppositely arranged, the directional aerial and the omnidirectional antenna are arranged in the bottom surface, the transmission component is set to the top surface, the transmission component is connected between the rotating disk and the actuator, the actuator drives the rotating disk to rotate by the transmission component, to adjust the radiation direction of the directional aerial.
- Directional aerial rotating mechanism as described in claim 1, which is characterized in that the omnidirectional antenna includes the first omnidirectional antenna and the second omnidirectional antenna, and first omnidirectional antenna and second omnidirectional antenna are set to the directional aerial two sides.
- Directional aerial rotating mechanism as claimed in claim 2, it is characterized in that, the rotating disk is in the form of annular discs, the directional aerial, first omnidirectional antenna and second omnidirectional antenna are located at the marginal position of the rotating disk, first omnidirectional antenna and second omnidirectional antenna are symmetrically distributed in the two sides of the rotating disk rotation center, and first omnidirectional antenna and second omnidirectional antenna are also symmetrically distributed in the two sides of the directional aerial.
- Directional aerial rotating mechanism as described in claim 1, it is characterized in that, the directional aerial includes radiator and reflecting plate, the reflecting plate is arc panel or folded structure, the radiator is set at the reflection kernel of the reflecting plate, to increase the signal radiation directionality of the radiator.
- Directional aerial rotating mechanism as claimed in claim 4, it is characterized in that, the bottom surface of the rotating disk is equipped with the first buckle, first buckle is equipped with card slot, the card slot is removably attachable to the radiator in the rotating disk for accommodating the radiator.
- Directional aerial rotating mechanism as described in claim 1, which is characterized in that the transmission component includes the first gear and second gear being meshed, and the first gear is fixed to the rotating disk, and the second gear is connected to the actuator.
- Directional aerial rotating mechanism as described in claim 1, it is characterized in that, it further include fixed bracket, the fixed bracket is opposite with the top surface of the rotating disk, orthographic projection of the rotating disk on the fixed bracket is located at the fixed internal stent, and the actuator is embedded in the fixed bracket.
- Directional aerial rotating mechanism as claimed in claim 7, which is characterized in that further include rotary shaft, the rotating disk is fixedly connected with the rotary shaft and is rotated centered on the rotary shaft, and the fixed holder pivots are connected to the rotary shaft.
- Directional aerial rotating mechanism as claimed in claim 8, it is characterized in that, the rotating disk is in the form of annular discs, the rotary shaft is through the center of the rotating disk, the support bracket fastened center includes an axis hole, and the rotary shaft passes through the axis hole and connect with the fixed holder pivots.
- Directional aerial rotating mechanism as claimed in claim 8, it is characterized in that, the transmission component includes the first gear and second gear being meshed, and the first gear is centered on the rotary shaft and is fixed to the rotary shaft, and the second gear is connected to the actuator.
- Directional aerial rotating mechanism as claimed in claim 8, it is characterized in that, it further include circuit board, the circuit board is located at the side of the rotating disk, and face the bottom surface of the rotating disk, the rotary shaft is in hollow structure, is electrically connected between the actuator and the circuit board by electric connection line, the electric connection line is passed through from the hollow space of the rotary shaft.
- Directional aerial rotating mechanism as claimed in claim 11, it is characterized in that, the rotary shaft is equipped with first through hole, the first through hole is arranged radially along the rotary shaft, it is electrically connected between the directional aerial and the circuit board by the first connecting line, first connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and stretches out the rotary shaft from the first through hole, to be electrically connected with the directional aerial.
- Directional aerial rotating mechanism as claimed in claim 12, which is characterized in that the omnidirectional antenna includes the first omnidirectional antenna and the second omnidirectional antenna, and first omnidirectional antenna and second omnidirectional antenna are set to the directional aerial two sides.
- Directional aerial rotating mechanism as claimed in claim 13, it is characterized in that, the rotary shaft is equipped with the second through-hole being arranged radially along the rotary shaft, it is electrically connected between first omnidirectional antenna and the circuit board by the second connecting line, second connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and the rotary shaft is stretched out from second through-hole, to be electrically connected with first omnidirectional antenna.
- Directional aerial rotating mechanism as claimed in claim 14, it is characterized in that, the rotary shaft is equipped with the third through-hole being arranged radially along the rotary shaft, it is electrically connected between second omnidirectional antenna and the circuit board by third connecting line, the third connecting line protrudes into the hollow space of the rotary shaft from the side of the circuit board, and the rotary shaft is stretched out from the third through-hole, to be electrically connected with second omnidirectional antenna.
- Directional aerial rotating mechanism as claimed in claim 15, which is characterized in that on the axial direction of the rotary shaft, the first through hole, second through-hole and the third through-hole are spaced apart from each other.
- Directional aerial rotating mechanism as claimed in claim 16, it is characterized in that, in the circumferential direction of the rotary shaft, it is separated by 90 degree between the first through hole and second through-hole, it is separated by 90 degree between the first through hole and the third through-hole, the first through hole is between second through-hole and the third through-hole.
- A kind of gateway, which is characterized in that including directional aerial rotating mechanism and rotational control assemblies described in claim 1-17 any one, the rotational control assemblies drive the rotation of the rotating disk and the directional aerial by controlling the actuator.
- Gateway as claimed in claim 18, which is characterized in that further include signal detection component, the signal for detecting the gateway surrounding uses position；The probe assembly is electrically connected with the rotational control assemblies, and after the signal detection component detection goes out the signal using position, the rotational control assemblies, which will control the directional aerial and turn to the signal, uses position.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2016/104788 WO2018082072A1 (en) | 2016-11-04 | 2016-11-04 | Directional antenna rotation mechanism and gateway device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108701897A true CN108701897A (en) | 2018-10-23 |
Family
ID=62075458
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680082046.XA Pending CN108701897A (en) | 2016-11-04 | 2016-11-04 | Directional aerial rotating mechanism and gateway device |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN108701897A (en) |
| WO (1) | WO2018082072A1 (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111130656A (en) * | 2019-12-25 | 2020-05-08 | 深圳市宏电技术股份有限公司 | Terminal antenna adjusting method, gateway antenna adjusting method and related equipment |
| CN111856513A (en) * | 2020-07-31 | 2020-10-30 | 中国南方电网有限责任公司 | Satellite observation value acquisition method and device, computer equipment and storage medium |
| CN112333561A (en) * | 2020-10-28 | 2021-02-05 | Oppo广东移动通信有限公司 | Network device |
| CN112713401A (en) * | 2020-12-22 | 2021-04-27 | 孙齐凯 | 5G new system antenna circuit board |
| WO2023160255A1 (en) * | 2022-02-28 | 2023-08-31 | 荣耀终端有限公司 | Wireless router and control method therefor |
| CN117907978A (en) * | 2024-03-07 | 2024-04-19 | 沈阳才誉科技有限公司 | Adjustable laser radar antenna |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108993247B (en) * | 2018-09-18 | 2024-04-26 | 东莞市琅菱机械有限公司 | Inside and outside reversal agitating unit that single actuating mechanism drove |
| CN110838622B (en) * | 2019-01-30 | 2023-02-28 | 新华三技术有限公司 | Antenna system and network equipment |
| CN113659313A (en) * | 2021-08-27 | 2021-11-16 | 上海移远通信技术股份有限公司 | Antenna mechanical scanning device and user terminal equipment |
| CN113825261A (en) * | 2021-09-06 | 2021-12-21 | Oppo广东移动通信有限公司 | Gateway device |
| CN115473844B (en) * | 2022-09-14 | 2023-10-13 | 河南捷茂电子科技有限公司 | Router assembly for communication network connection |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2571003Y (en) * | 2002-07-22 | 2003-09-03 | 王郑发 | Double-antenna controller |
| CN201199546Y (en) * | 2008-05-09 | 2009-02-25 | 上海良友（集团）有限公司 | Rotary assembly antenna |
| CN103037383A (en) * | 2011-08-25 | 2013-04-10 | 快美思科技有限公司 | Wireless cable |
| CN203289427U (en) * | 2013-04-25 | 2013-11-13 | 浙江工业大学 | Wireless communication device with self-tracking and self-adapting functions |
| CN105593065A (en) * | 2013-05-17 | 2016-05-18 | Fybr有限责任公司 | Distributed remote sensing system gateway |
| CN205488551U (en) * | 2016-04-12 | 2016-08-17 | 刘萍 | Adjustable shortwave broadcasting antenna who turns to |
-
2016
- 2016-11-04 WO PCT/CN2016/104788 patent/WO2018082072A1/en active Application Filing
- 2016-11-04 CN CN201680082046.XA patent/CN108701897A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2571003Y (en) * | 2002-07-22 | 2003-09-03 | 王郑发 | Double-antenna controller |
| CN201199546Y (en) * | 2008-05-09 | 2009-02-25 | 上海良友（集团）有限公司 | Rotary assembly antenna |
| CN103037383A (en) * | 2011-08-25 | 2013-04-10 | 快美思科技有限公司 | Wireless cable |
| CN203289427U (en) * | 2013-04-25 | 2013-11-13 | 浙江工业大学 | Wireless communication device with self-tracking and self-adapting functions |
| CN105593065A (en) * | 2013-05-17 | 2016-05-18 | Fybr有限责任公司 | Distributed remote sensing system gateway |
| CN205488551U (en) * | 2016-04-12 | 2016-08-17 | 刘萍 | Adjustable shortwave broadcasting antenna who turns to |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111130656A (en) * | 2019-12-25 | 2020-05-08 | 深圳市宏电技术股份有限公司 | Terminal antenna adjusting method, gateway antenna adjusting method and related equipment |
| CN111856513A (en) * | 2020-07-31 | 2020-10-30 | 中国南方电网有限责任公司 | Satellite observation value acquisition method and device, computer equipment and storage medium |
| CN112333561A (en) * | 2020-10-28 | 2021-02-05 | Oppo广东移动通信有限公司 | Network device |
| CN112713401A (en) * | 2020-12-22 | 2021-04-27 | 孙齐凯 | 5G new system antenna circuit board |
| CN112713401B (en) * | 2020-12-22 | 2022-11-29 | 西安新里技术有限公司 | 5G new system antenna circuit board |
| WO2023160255A1 (en) * | 2022-02-28 | 2023-08-31 | 荣耀终端有限公司 | Wireless router and control method therefor |
| CN117907978A (en) * | 2024-03-07 | 2024-04-19 | 沈阳才誉科技有限公司 | Adjustable laser radar antenna |
| CN117907978B (en) * | 2024-03-07 | 2024-05-14 | 沈阳才誉科技有限公司 | Adjustable laser radar antenna |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018082072A1 (en) | 2018-05-11 |
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