CN104683567B - The control method of mobile terminal and mobile terminal - Google Patents
The control method of mobile terminal and mobile terminal Download PDFInfo
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- CN104683567B CN104683567B CN201410743316.XA CN201410743316A CN104683567B CN 104683567 B CN104683567 B CN 104683567B CN 201410743316 A CN201410743316 A CN 201410743316A CN 104683567 B CN104683567 B CN 104683567B
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- rotatable parts
- fuselage body
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- mobile terminal
- shaft
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- 238000000034 method Methods 0.000 title claims abstract description 49
- 230000005540 biological transmission Effects 0.000 claims description 7
- 238000012544 monitoring process Methods 0.000 claims description 5
- 238000013016 damping Methods 0.000 claims description 3
- 238000003384 imaging method Methods 0.000 claims 1
- 238000000465 moulding Methods 0.000 claims 1
- 238000002360 preparation method Methods 0.000 claims 1
- 238000004891 communication Methods 0.000 description 10
- 230000009286 beneficial effect Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000001727 in vivo Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000010363 phase shift Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
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Abstract
The present invention is suitable for technical field of mobile terminals, discloses the control method of a kind of mobile terminal and mobile terminal.Mobile terminal includes fuselage body and is rotationally connected with the rotatable parts of fuselage body, antenna, the driving part that the signal strength values that fuselage body or/and rotatable parts are connected with that rotatable parts is driven to rotate and are received in antenna stop when reaching setting value are provided in rotatable parts.Control method comprises the following steps, prepare the fuselage body for being rotatably connected to rotatable parts, by driving part the rotatable parts on fuselage body is driven to be rotated relative to the fuselage body, the signal strength values that the rotatable parts internal antenna receives are monitored by control module, when the signal strength values that antenna receives are more than setting value or are the maximum in rotatable parts slewing area, rotatable parts stop.The control method of mobile terminal and mobile terminal provided by the invention can be such that the signal of mobile terminal adjusts to simultaneously preferable states, convenient for the use of user.
Description
Technical field
The invention belongs to technical field of mobile terminals more particularly to the control methods of a kind of mobile terminal and mobile terminal.
Background technology
Existing mobile terminal, antenna are fixed in fuselage body, in actual use, it is not good enough signal often occur
Situation, be not easy to the use of user.
The content of the invention
It is an object of the invention to overcome above-mentioned the deficiencies in the prior art, a kind of mobile terminal and mobile terminal are provided
Control method can be such that the signal of mobile terminal adjusts to simultaneously preferable states, convenient for the use of user.
In a first aspect, the present invention provides a kind of mobile terminals, including fuselage body, further include and be rotationally connected with the machine
The rotatable parts of body body are provided with antenna in the rotatable parts, and the fuselage body or/and the rotatable parts are connected with
For the driving that the rotatable parts is driven to rotate and are stopped when the signal strength values that the antenna receives reach setting value
Component.
With reference to first aspect, in the first possible realization method of first aspect, the fuselage body or/and described
It is provided with to monitor the signal strength values that the antenna receives and in the signal strength values received in rotatable parts
The control module for controlling the driving part out of service when reaching setting value.
The possible realization method of with reference to first aspect the first, in second of possible realization method of first aspect
In, circuit board is provided in the fuselage body, the control module is connected to the circuit board or is integrated in the circuit board,
The driving part is electrically connected with the circuit board or the control module.
With reference to first aspect or in the first or second of possible realization method of first aspect, the of first aspect
In three kinds of possible realization methods, the rotatable parts are camera parts, and the camera parts include roll-shell and company
It is connected to the image-forming block of the roll-shell.
With reference to first aspect or first aspect the first is possible to any one of the third possible realization method
Realization method, in the 4th kind of possible realization method of first aspect, the end of the fuselage body or side setting are useful
In the slot position for installing the rotatable parts, the both sides of the rotatable parts are connected to the opposite both sides in the slot position by shaft.
With reference to first aspect or first aspect the first is possible to any one of the 4th kind of possible realization method
Realization method, in the 5th kind of possible realization method of first aspect, the driving part includes motor.
With reference to first aspect or first aspect the first is possible to any one of the 5th kind of possible realization method
Realization method, in the 6th kind of possible realization method of first aspect, the antenna is WIFI antennas.
With reference to first aspect or first aspect the first is possible to any one of the 6th kind of possible realization method
Realization method, in the 7th kind of possible realization method of first aspect, the antenna includes the WIFI of at least two 2.4GHz
Antenna either the WIFI antennas of at least two 5GHz or, the antenna includes the WIFI antennas of at least one 60GHz.
With reference to first aspect or first aspect the first is possible to any one of the 7th kind of possible realization method
Realization method, in the 8th kind of possible realization method of first aspect, the antenna is connected to the machine by feeding network
The intrinsic circuit board of body.
With reference to first aspect or first aspect the first is possible to any one of the 8th kind of possible realization method
Realization method, in the 9th kind of possible realization method of first aspect, the fuselage body or/and the rotatable parts are set
With having antenna system, system connects the antenna with the antenna.
The 9th kind of possible realization method with reference to first aspect, in the tenth kind of possible realization method of first aspect
In, the antenna system be the metalwork for being embedded at the rotatable parts or the fuselage body.
With reference to first aspect or first aspect the first is possible to any one of the tenth kind of possible realization method
Realization method, in a kind of the tenth possible realization method of first aspect, the antenna is connected with phase shifter, the phase shifter
Controller is connected with, the controller is located in the rotatable parts or in the fuselage body.
With reference to first aspect or first aspect the first to a kind of any one of the tenth possible realization method may
Realization method, in the 12nd kind of possible realization method of first aspect, the mobile terminal be mobile phone or tablet computer.
Second aspect, the present invention provides a kind of control methods of mobile terminal, comprise the following steps, and prepare the company of rotation
The fuselage body of rotatable parts is connected to, the relatively described fuselage body of rotatable parts on fuselage body is driven to turn by driving part
It is dynamic, the signal strength values that the rotatable parts internal antenna receives are monitored by control module, when the signal strength values received
When more than setting value or being the maximum in rotatable parts slewing area, the rotatable parts stop.
With reference to second aspect, in the first possible realization method of second aspect, when the control module monitors institute
When stating the signal strength values that rotatable parts internal antenna receives and being less than lower limiting value, the driving part controls the rotatable parts to turn
It is dynamic, until when the signal strength values that antenna receives are more than setting value or are the maximum in rotatable parts slewing area, it is described
Rotatable parts stop.
The control method of a kind of mobile terminal and mobile terminal provided by the present invention, can be with by the way that antenna is arranged at
On the rotatable parts rotated relative to fuselage body, by adjusting the angles of rotatable parts the signal that antenna receives can be made strong
Angle value size changes, and then rotatable parts can be adjusted to antenna the larger or maximum angle of the signal strength received, can
So that the signal of mobile terminal keeps preferable states, beneficial to the communication efficiency for improving user, the hair of communication module can also be reduced
Power is penetrated, so as to increase battery durable ability, under equal conditions, can effectively extend the usage time of battery.
Description of the drawings
It to describe the technical solutions in the embodiments of the present invention more clearly, below will be to needed in the embodiment
Attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the present invention, for ability
For the those of ordinary skill of domain, without creative efforts, it can also be obtained according to these attached drawings other attached
Figure.
Fig. 1 is the floor map of mobile terminal provided in an embodiment of the present invention;
Fig. 2 is the partial schematic diagram of mobile terminal provided in an embodiment of the present invention;
Fig. 3 is the partial schematic diagram of mobile terminal provided in an embodiment of the present invention;
Fig. 4 is the floor map of antenna arrangement in mobile terminal provided in an embodiment of the present invention;
Fig. 5 is the floor map of antenna arrangement in mobile terminal provided in an embodiment of the present invention;
Fig. 6 is the floor map of antenna arrangement in mobile terminal provided in an embodiment of the present invention;
Fig. 7 is the reference flow sheet of the control method of mobile terminal provided in an embodiment of the present invention.
Specific embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to the accompanying drawings and embodiments, it is right
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, it can be directly another
On one element or it may be simultaneously present centering elements.When an element is known as " being connected to " another element, it can
To be directly to another element or may be simultaneously present centering elements.
Only it is relative concept each other it should also be noted that, the orientation term such as left and right, upper and lower in the embodiment of the present invention
Or using the normal operating condition of product as reference, and should not be regarded as restrictive.
As shown in FIG. 1 to 3, a kind of mobile terminal provided in an embodiment of the present invention including fuselage body 1, is further included and turned
The rotatable parts 2 for being connected to fuselage body 1 are moved, are provided with antenna 3 in rotatable parts 2, fuselage body 1 or/and rotatable parts 2 connect
It is connected to the driving portion that rotatable parts 2 is driven to rotate and stop when the signal strength values that antenna 3 receives reach setting value
Part (not shown).The signal strength values received can be yield value.Setting value can be default fixed value, work as rotation
For component 2 in rotation process, the signal strength values received of antenna 3 have reached default fixed value, you can it stops operating, with
It is quickly obtained preferable signal.Setting value or rotatable parts 2 are after the first limit point turns to another limit point, and institute is really
First the rotary scanning in maximum rotation section determines 3 energy of antenna for the signal strength values that fixed maximum receives, i.e. rotatable parts 2
The signal strength values that the maximum reached receives, then by rotatable parts 2 to turn to the maximum signal strength values institute received right
The angle answered, to obtain best signal strength.When rotating, the directional diagram lobe 301 of antenna 3 can revolve rotatable parts 2
It is scanned in the range of turning, antenna 3 is adjusted to the signal strength that receives is larger or maximum corresponding angle, by making antenna height
Signal strength direction changes, in this way, rotatable parts 2 can be made to stop operating and kept when 3 receiving and transmitting signal of antenna is most strong
Corresponding state makes the signal of mobile terminal keep preferable states, beneficial to the communication efficiency for improving user, can also reduce communication mould
The transmission power of block, so as to increase battery durable ability, under equal conditions, when can effectively extend the use of battery
Between.
Specifically, circuit board is provided in fuselage body 1, can be set in fuselage body 1 or/and rotatable parts 2 useful
In monitoring aerial 3 the signal strength values received and control driving part when the signal strength values received reach setting value
Control module (not shown) out of service.Control module can be individual devices, can also be integrated in fuselage body 1
In circuit board (not shown).
Specifically, control module may connect to circuit board or be integrated in circuit board, driving part and circuit board or control mould
Block is electrically connected, and control module can control rotatable parts 2 to be rotated by the rate of setting, and reach setting in the yield value of antenna 3
In time stop rotatable parts 2 during value.
Specifically, rotatable parts 2 can be that camera parts etc. can be relative to the component of the rotation of fuselage body 1, camera
Component may include roll-shell and be connected to the image-forming block of roll-shell.
Specifically, as shown in FIG. 1 to 3, the end of fuselage body 1 or side may be provided with to install rotatable parts 2
Slot position 101, the both sides of rotatable parts 2 can be connected to the opposite both sides in slot position 101 by shaft 21.One end of shaft 21 can
Rotatable parts 2 are fixedly connected on, the other end can be rotationally connected with fuselage body 1.Alternatively, one end of shaft 21 is rotatably connected
In rotatable parts 2, the other end can be fixedly connected on fuselage body 1;Alternatively, the both ends of shaft 21 are rotationally connected with rotation respectively
Component 2 and fuselage body 1.
Specifically, antenna 3 can be connected to fuselage body 1 by the structures such as conducting wire or flexible PCB (not shown)
Interior circuit board, shaft 21 can be hollow structure, and conducting wire or flexible PCB can be arranged in shaft 21 and stretch into fuselage body 1
It is interior.
Alternatively, shaft 21 is provided with conducting ring (not shown), antenna 3 is connected to conducting ring, is set in fuselage body 1
There is a brush (not shown) being in contact with conducting ring, brush is electrically connected to the circuit board in fuselage body 1, and conducting ring can be with
Shaft 21 is sheathed on, shaft 21 can be used insulating materials and be made, and conducting ring can be becket, may be provided at least two, respectively
Becket can be arranged at intervals along shaft 21 and stretch into the in vivo one end of body housing positioned at shaft 21.In this way, rotatable parts 2 can connect
It is continuous to rotate in a circumferential direction, convenient for the use of user.
Specifically, driving part may include motor (not shown), and the motor shaft of motor can be directly connected to shaft
21, alternatively, motor shaft is cased with driving gear (not shown), shaft 21 is cased with driven gear (not shown), driving tooth
Wheel is meshed with driven gear, alternatively, motor shaft also can be connected to shaft 21 by transmission belt etc..In concrete application, driving portion
Other suitable mode drive shafts 21 can also be used in part.
In concrete application, can also manually rotary motion component 2, rotatable parts 2 can also be made with respect to fuselage body 1
It rotates, it can be by showing the signal strength values received of antenna 3 on the screen of the mobile terminal, user can be according to display
Signal strength values rotatable parts 2 are manually adjusted to suitable angle, and the signal strength values for receiving antenna 3 are larger
(fixed value for reaching setting) or maximum (reaching maximum of the antenna 3 in the range of the maximum rotation of rotatable parts 2).It can also
Indicator light is set on fuselage body 1 or rotatable parts 2, when the signal strength values that antenna 3 receives are larger or maximum, instruction
Lamp lights or represents that user can stop rotating rotatable parts 2 with specific color (such as red or green etc.).
Specifically, damping, in the case of from external force, rotatable parts are provided between rotatable parts 2 and fuselage body 1
2 will not arbitrarily be rotated relative to fuselage body 1, so that rotatable parts 2 can keep corresponding angle between fuselage body 1
Degree.
Specifically, antenna 3 can be WIFI (WIreless-Fidelity, Wireless Fidelity) antennas or GPS (Global
Positioning System, global positioning system) antenna etc..
Specifically, antenna 3 can be provided at least two.
Specifically, antenna 3 includes the WIFI antennas of 31 or at least two 5GHz of WIFI antennas of at least two 2.4GHz
32.In Fig. 4, antenna 3 includes the WIFI antennas 31 of two 2.4GHz.In Fig. 5, antenna 3 includes WIFI days of four 5GHz
Line 32.Each antenna can be connected to feeding network 30 by cable respectively.
In concrete application, antenna 3 can be connected to the circuit board in fuselage body 1 by feeding network 30.
Specifically, fuselage body 1 or/and rotatable parts 2 with being provided with antenna system, system connects antenna 3 with antenna,
To ensure the performance of antenna 3.
Specifically, antenna system can be the metalwork for being embedded at rotatable parts 2 or fuselage body 1, such as be embedded at
Sheet metal in roll-shell etc..
Specifically, as shown in Fig. 1~Fig. 6, antenna 3 can be connected with phase shifter 34, and phase shifter 34 can be variable phase shift
Device, phase shifter 34 are connected with controller 35, and controller 35 is located in rotatable parts 2 or in fuselage body 1.In the present embodiment, often
A antenna 3 is all connected with there are one phase shifter 34, to further improve the performance of antenna 3.
Specifically, mobile terminal can be mobile phone or tablet computer etc..
Specifically, mobile terminal can also include memory, audio input output unit, SIM (Subscriber
Identity Module, client identification module) card connector, card connector etc., memory, audio input output unit,
Sim card connector, card connector can be connected on the circuit board in fuselage body 1.
The mobile terminal that the embodiment of the present invention is provided, by the way that antenna 3 to be arranged at and can be rotated relative to fuselage body 1
Rotatable parts 2 on, the signal strength size that antenna 3 receives can be changed by adjusting the angles of rotatable parts 2, into
And rotatable parts 2 can be adjusted to antenna 3 the larger or maximum angle of the signal strength received, mobile terminal can be made
Signal keeps preferable states, beneficial to the communication efficiency for improving user, can also reduce the transmission power of communication module, so as to
Increase battery durable ability, under equal conditions, can effectively extend the usage time of battery.Moreover, it is driven by setting
Component and control module make the adjustment of rotatable parts 2 that can automate progress, and setting value can be default fixed value, work as rotation
For component 2 in rotation process, the signal strength values that antenna 3 receives have reached default fixed value, you can stop operating, with fast
Speed obtains preferable signal.Setting value or rotatable parts 2 (rotate after turning to another limit point from the first limit point
Component 2 rotated its maximum section that can be rotated), the signal strength values that identified maximum can receive, i.e. rotatable parts 2
First rotary scanning determines the 3 attainable maxgain value of institute of antenna in maximum rotation section, then is turned to by rotatable parts 2
Angle corresponding to maxgain value, to obtain best signal strength.Rotatable parts 2 are when rotating, the directional diagram ripple of antenna 3
Valve 301 can scan in rotating range, and antenna 3 is adjusted to larger or maximum signal strength angle, by making antenna 3
High signal intensity direction changes, in this way, rotatable parts 2 can be made to stop operating and protected when 3 receiving and transmitting signal of antenna is most strong
Corresponding relative angle is held, facility is brought to user.
The embodiment of the present invention additionally provides a kind of control method of mobile terminal, and above-mentioned mobile terminal may be employed.
Comprise the following steps, prepare the fuselage body 1 for being rotatably connected to rotatable parts 2, driven by driving part on fuselage body 1
Rotatable parts 2 are rotated relative to fuselage body 1, and the signal strength received of 2 internal antenna 3 of rotatable parts is monitored by control module
Value, when the signal strength values received are more than setting value or are the maximum in 2 slewing area of rotatable parts, rotatable parts 2
Stop.Setting value can be default fixed value, and when rotatable parts 2 are in rotation process, the signal that discovery antenna 3 receives is strong
Angle value has reached default fixed value, you can stops operating, to be quickly obtained preferable signal.Antenna 3 is rotated in rotatable parts 2
Scope there are at least one maximum, i.e., rotatable parts 2 from the first limit point turn to another limit point after (i.e. rotatable parts
After 2 rotated maximum angle), the signal strength values that identified maximum receives, i.e., rotatable parts 2 are first in maximum rotation section
Interior rotary scanning determine antenna 3 the signal strength values that can receive of attainable maximum, it is then strong by turning to peak signal
Angle corresponding to angle value, to obtain best signal strength.Rotatable parts 2 are when rotating, the directional diagram lobe 301 of antenna 3
It can be scanned in rotating range, the signal strength values that antenna 3 receives can change, you can so that 3 high-gain of antenna
Direction changes, in this way, rotatable parts 2 can be made to stop operating and keep corresponding phase when 3 receiving and transmitting signal of antenna is most strong
To angle, the signal of mobile terminal can be made to keep preferable states, beneficial to the communication efficiency for improving user, communication can also be reduced
The transmission power of module so as to increase battery durable ability, under equal conditions, can effectively extend the use of battery
Time.
Specifically, when the signal strength values that control module monitoring 2 internal antenna 3 of rotatable parts receives are less than lower limiting value,
Driving part control rotatable parts 2 rotate, until the signal strength values that antenna receives are more than setting value or are 2 turns of rotatable parts
During maximum in dynamic scope, rotatable parts 2 stop, during the use of mobile terminal, timely automated can also adjust to
The preferable state of 3 signal strength of antenna.
Specifically, when the signal strength values of control module monitoring 2 internal antenna 3 of rotatable parts are higher than setting value, (setting value can
With identical with lower limiting value), rotatable parts 2 can remain stationary as, and antenna 3 can keep corresponding yield value.
In concrete application, refering to what is shown in Fig. 7, application (system automatically starting or the application of mobile terminal can be opened first
Family control starts) S101, the driving part driving scanning of rotatable parts 2 determines the direction S102 of peak signal, if mobile terminal moves
Dynamic S103, control module check that signal (signal strength values) whether less than setting value S104, if signal is less than setting value, performs
S102;If signal is higher than setting value, value S104 is kept, i.e. rotatable parts 2 remain stationary as.
The control method for the mobile terminal that the embodiment of the present invention is provided, by setting for 3 gain of monitoring aerial
Control module and the driving part for driving the rotation of rotatable parts 2 pass through control module and monitor 2 internal antenna 3 of rotatable parts
The signal strength values received, when the signal strength values received be more than setting value or in 2 slewing area of rotatable parts most
During big value, rotatable parts 2 stop, and the signal of mobile terminal can be made to keep preferable states, beneficial to the communication efficiency for improving user,
The transmission power of communication module can also be reduced, it, under equal conditions, can be effectively so as to increase battery durable ability
Extend the usage time of battery.
The foregoing is merely a prefered embodiment of the invention, is not intended to limit the invention, it is all the present invention spirit and
Any modification, equivalent substitution or improvement for being made within principle etc., should all be included in the protection scope of the present invention.
Claims (12)
1. a kind of mobile terminal, including fuselage body, which is characterized in that further include the rotation for being rotationally connected with the fuselage body
Component, antenna is provided in the rotatable parts, and the fuselage body or/and the rotatable parts are connected with to drive described
The driving part that rotatable parts are rotated and stopped when the signal strength values that the antenna receives reach setting value, the driving
Component includes motor;The rotatable parts are camera parts, and the camera parts include roll-shell and are connected to described
The image-forming block of roll-shell, the end or side of the fuselage body are provided with to install the slot position of the rotatable parts,
The both sides of the rotatable parts are connected to the opposite both sides in the slot position by shaft;
The motor shaft of the motor is connected to the shaft;Alternatively, the motor shaft of the motor is cased with driving gear, the shaft
Driven gear is cased with, the driving gear is meshed with the driven gear;Alternatively, the motor shaft of the motor passes through transmission belt
It is connected to the shaft;
Be arranged with conducting ring in the shaft, the antenna is connected to the conducting ring, be equipped in the fuselage body with it is described
The brush that conducting ring is in contact, the brush are electrically connected with the circuit board in the fuselage body;
Between the rotatable parts and the fuselage body be equipped with avoid the rotatable parts arbitrarily relatively described fuselage body into
The damping that row rotates.
2. mobile terminal as described in claim 1, which is characterized in that set in the fuselage body or/and the rotatable parts
It is equipped with to monitor the signal strength values that the antenna receives and when the signal strength values received reach setting value
The control module for controlling the driving part out of service.
3. mobile terminal as claimed in claim 2, which is characterized in that circuit board, the control are provided in the fuselage body
Molding block is connected to the circuit board or is integrated in the circuit board, the driving part and the circuit board or the control mould
Block is electrically connected.
4. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the antenna is WIFI antennas.
5. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the antenna includes at least two
The WIFI antennas of 2.4GHz either the WIFI antennas of at least two 5GHz or, the antenna include at least one 60GHz
WIFI antennas.
6. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the antenna is connected by feeding network
The circuit board being connected in the fuselage body.
7. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the fuselage body or/and described turn
Dynamic component with being provided with antenna system, system connects the antenna with the antenna.
8. mobile terminal as claimed in claim 7, which is characterized in that the antenna system to be embedded at the rotatable parts
Or the metalwork of the fuselage body.
9. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the antenna is connected with phase shifter, institute
It states phase shifter and is connected with controller, the controller is located in the rotatable parts or in the fuselage body.
10. mobile terminal as claimed any one in claims 1 to 3, which is characterized in that the mobile terminal is mobile phone or flat
Plate computer.
11. the control method of a kind of mobile terminal, which is characterized in that comprise the following steps, preparation is rotatably connected to rotation section
The fuselage body of part drives the rotatable parts on fuselage body to be rotated relative to the fuselage body, the drive by driving part
Dynamic component includes motor, and the signal strength values received of the rotatable parts internal antenna are monitored by control module, work as reception
When the signal strength values arrived are more than setting value or are the maximum in rotatable parts slewing area, the rotatable parts stop;Institute
Rotatable parts are stated as camera parts, the camera parts include roll-shell and are connected to the imaging section of the roll-shell
Part, the end or side of the fuselage body are provided with to install the slot position of the rotatable parts, and the two of the rotatable parts
Side is connected to the opposite both sides in the slot position by shaft;
The motor shaft of the motor is connected to the shaft;Alternatively, the motor shaft of the motor is cased with driving gear, the shaft
Driven gear is cased with, the driving gear is meshed with the driven gear;Alternatively, the motor shaft of the motor passes through transmission belt
It is connected to the shaft;
Be arranged with conducting ring in the shaft, the antenna is connected to the conducting ring, be equipped in the fuselage body with it is described
The brush that conducting ring is in contact, the brush are electrically connected with the circuit board in the fuselage body;
Between the rotatable parts and the fuselage body be equipped with avoid the rotatable parts arbitrarily relatively described fuselage body into
The damping that row rotates.
12. the control method of mobile terminal as claimed in claim 11, which is characterized in that when described in control module monitoring
When the signal strength values that rotatable parts internal antenna receives are less than lower limiting value, the driving part controls the rotatable parts to turn
It is dynamic, until when the signal strength values that antenna receives are more than setting value or are the maximum in rotatable parts slewing area, it is described
Rotatable parts stop.
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CN201410743316.XA CN104683567B (en) | 2014-12-05 | 2014-12-05 | The control method of mobile terminal and mobile terminal |
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CN201410743316.XA CN104683567B (en) | 2014-12-05 | 2014-12-05 | The control method of mobile terminal and mobile terminal |
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CN104683567B true CN104683567B (en) | 2018-05-25 |
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CN201410743316.XA Expired - Fee Related CN104683567B (en) | 2014-12-05 | 2014-12-05 | The control method of mobile terminal and mobile terminal |
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CN107809505A (en) * | 2017-11-16 | 2018-03-16 | 珠海市魅族科技有限公司 | Mobile terminal |
CN111049541A (en) * | 2018-10-11 | 2020-04-21 | 中兴通讯股份有限公司 | Wireless signal enhancement method, mobile terminal and computer readable storage medium |
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CN111049601B (en) * | 2019-12-23 | 2022-03-29 | Oppo广东移动通信有限公司 | Position prompting method and related equipment |
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