CN204407469U - Mobile terminal - Google Patents
Mobile terminal Download PDFInfo
- Publication number
- CN204407469U CN204407469U CN201420764281.3U CN201420764281U CN204407469U CN 204407469 U CN204407469 U CN 204407469U CN 201420764281 U CN201420764281 U CN 201420764281U CN 204407469 U CN204407469 U CN 204407469U
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- China
- Prior art keywords
- antenna
- fuselage body
- rotatable parts
- mobile terminal
- gap
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 239000002184 metal Substances 0.000 claims description 15
- 230000009286 beneficial effect Effects 0.000 abstract description 7
- 238000002955 isolation Methods 0.000 abstract description 3
- 238000004891 communication Methods 0.000 description 3
- 238000013016 damping Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
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Abstract
The utility model is applicable to technical field of mobile terminals, provides a kind of mobile terminal, comprises fuselage body, and described fuselage body is rotatably connected to rotatable parts, and described slot antenna is arranged at fuselage body and is positioned at the one or both sides of described rotatable parts.A kind of mobile terminal that the utility model provides, fuselage body is rotatably connected to rotatable parts, slot antenna is arranged at fuselage body and is positioned at the one or both sides of rotatable parts, slot antenna is not easy the impact being subject to rotatable parts rotation, and isolation between antennae is good, and each antenna not easily influences each other, and be beneficial to and reduce antenna the taking of space in fuselage body, be convenient to the arrangement of other antenna in fuselage body, to ensure the performance of each antenna, and be beneficial to the lightening design of product.
Description
Technical field
The utility model belongs to technical field of mobile terminals, particularly relates to a kind of mobile terminal.
Background technology
In current mobile terminal, along with product is to lightening future development, antenna need be arranged in narrow and small fuselage body, easily influences each other between antenna, and antenna performance is not good enough.
Utility model content
The purpose of this utility model is to overcome above-mentioned the deficiencies in the prior art, provides a kind of mobile terminal, the excellent performance of its antenna.
First aspect, provide a kind of mobile terminal, comprise fuselage body and slot antenna, described fuselage body is rotatably connected to rotatable parts, described slot antenna is arranged at fuselage body and is positioned at the one or both sides of described rotatable parts, is provided with electronic device in described rotatable parts.
In conjunction with first aspect, in the first possible implementation of first aspect, be provided with circuit board in described fuselage body, described electronic device is connected to the circuit board in described fuselage body by feeder line.
In conjunction with first aspect, in the implementation that the second of first aspect is possible, described fuselage body comprises housing, and described housing comprises metal edge frame, or described housing is metal shell and described metal edge frame is the part of described housing; Described slot antenna comprises the gap being arranged at described metal edge frame and the feed line being connected to described gap.
In conjunction with the implementation that the second of first aspect is possible, in the third possible implementation of first aspect, be provided with circuit board in described fuselage body, one end of described feed line strides across the sidewall that gap is connected to described gap, and the other end of described feed line is connected to described circuit board.
In conjunction with the implementation that the second of first aspect is possible, in the 4th kind of possible implementation of first aspect, described gap comprises from described metal edge frame sidewall transversely or oblique the first gap extended to opposite side direction, and described gap also comprises from described first gap end longitudinally or the second gap of oblique extension.
In conjunction with the first possible implementation of first aspect, in the 5th kind of possible implementation of first aspect, described fuselage body is provided with slot, and the both sides of described rotatable parts are connected to the both sides of described slot by axis of rotation.
In conjunction with the 5th kind of possible implementation of first aspect, in the 6th kind of possible implementation of first aspect, it is inner that described feeder line is arranged in described rotating shaft.
In conjunction with the first possible implementation of first aspect, in the 7th kind of possible implementation of first aspect, described rotatable parts and described feeder line form reception antenna or dual-mode antenna.
In conjunction with the 7th kind of possible implementation of first aspect, in the 8th kind of possible implementation of first aspect, described reception antenna is gps antenna.
In conjunction with the first of first aspect to any one possible implementation in the 8th kind, in the 9th kind of possible implementation of first aspect, described slot antenna is WIFI antenna or gps antenna or high frequency diversity antenna, and described slot antenna is divided into the both sides of described rotatable parts or is arranged at the side of described rotatable parts.
In conjunction with the first of first aspect to any one possible implementation in the 8th kind, in the tenth kind of possible implementation of first aspect, described rotatable parts are camera parts or audio amplifier parts or fingerprint recognition parts.
In conjunction with the first of first aspect to any one possible implementation in the 8th kind, in the 11 kind of possible implementation of first aspect, in described fuselage body, be provided with the driving element for driving described rotatable parts to rotate relative to described fuselage body.
In conjunction with the first of first aspect to any one possible implementation in the 8th kind, in the 12 kind of possible implementation of first aspect, described mobile terminal is mobile phone or panel computer.
A kind of mobile terminal that the utility model provides, fuselage body is rotatably connected to rotatable parts, slot antenna is arranged at fuselage body and is positioned at the one or both sides of rotatable parts, slot antenna is not easy the impact being subject to rotatable parts rotation, isolation between antennae is good, each antenna not easily influences each other, the excellent performance of each antenna.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, be briefly described to the accompanying drawing used required in embodiment below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the floor map of the mobile terminal that the utility model embodiment provides.
Embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
It should be noted that, when element is called as " being fixed on " or " being arranged at " another element, it can directly on another element or may there is centering elements simultaneously.When an element is known as " being connected to " another element, it can be directly connected to another element or may there is centering elements simultaneously.
Also it should be noted that, the orientation term such as left and right, upper and lower in the utility model embodiment, is only relative concept or be reference with the normal operating condition of product each other, and should not be regarded as have restrictive.
As shown in Figure 1, a kind of mobile terminal that the utility model embodiment provides, comprise fuselage body 100, fuselage body 100 is rotatably connected to rotatable parts 300, slot antenna 400 is arranged at fuselage body 100 and is positioned at the side of rotatable parts 300, or slot antenna 400 is arranged at fuselage body 100 and is arranged at the both sides of rotatable parts 300 respectively.Slot antenna 400 is not easy the impact being subject to rotatable parts 300 rotation, isolation between antennae is good, and is beneficial to and reduces antenna the taking of space in fuselage body 100, and is convenient to the arrangement of other antenna in fuselage body 100, to ensure the performance of each antenna, and be beneficial to the lightening design of product.
Particularly, fuselage body 100 comprises housing 110, and housing 110 comprises metal edge frame (not indicating in figure), or housing 110 is metal shell and metal edge frame is the part of housing 110.Slot antenna 400 comprises the gap 410 being arranged at metal edge frame and the feed line 420 being connected to gap 410.
Particularly, circuit board (not shown) can be provided with in fuselage body 100, one end of feed line 420 strides across gap 410 and is connected to the sidewall in gap 410, and the other end of feed line 420 can be connected to the communication module of circuit board, to ensure the performance of slot antenna 400.
Particularly, gap 410 comprises from metal edge frame sidewall transversely or the first gap 411 of extending, oblique or Qu Xiangxiang opposite side direction, and gap 410 also comprises or song longitudinal or oblique from the first gap 411 end to the second gap 412 extended.Gap 410 can the suitable shape such as L-shaped, " 7 " font, " Z " shape.In the present embodiment, the end in the second gap 412 can be positioned at the side of rotatable parts 300.In embody rule, the concrete shape in gap 410, structure, arrangement can set according to actual conditions.
Particularly, electronic device (not shown) is provided with in rotatable parts 300, electronic device can be connected to the communication module of the circuit board in fuselage body 100 by feeder line 310, like this, rotatable parts 300 and feeder line 310 can form an antenna structure, and rotatable parts 300, except the function of itself, also have antenna function, be beneficial to and reduce further antenna the taking of space in fuselage body 100, and be convenient to the arrangement of other antenna in fuselage body 100.Electronic device can be circuit board etc.Feeder line 310 accessible site is in the winding displacement (flexible circuit board or wire) etc. of rotatable parts 300.
Particularly, fuselage body 100 can be provided with slot 101, and the both sides of rotatable parts 300 are rotationally connected with the both sides of slot 101 by rotating shaft 320.Slot 101 can be arranged at the suitable place such as top or sidepiece or bottom etc. of fuselage body 100.Particularly, one end of rotating shaft 320 can be fixedly connected on rotatable parts 300, and the other end can be rotationally connected with fuselage body 100.Or one end of rotating shaft 320 is rotationally connected with rotatable parts 300, and the other end can be fixedly connected on fuselage body 100, or the two ends of rotating shaft 320 are rotationally connected with rotatable parts 300 and fuselage body 100 respectively.
Particularly, at least one rotating shaft 320 can be hollow structure, and it is inner that feeder line 310 can be arranged in rotating shaft 320, signal to be connected to the communication module of fuselage body 100 interior circuit board from rotatable parts 300.
Particularly, rotatable parts 300 and feeder line 310 can form reception antenna or dual-mode antenna, and in the present embodiment, rotatable parts 300 and feeder line 310 form reception antenna, to avoid affecting other antenna in fuselage body 100.
In the present embodiment, reception antenna can be gps antenna etc.
Particularly, can also antenna structure be provided with in the fuselage body 100 below rotatable parts 300, between itself and rotatable parts 300, can screen be provided with.
Particularly, slot antenna 400 can be WIFI antenna or gps antenna or high frequency diversity antenna (1710MHz-2700MHz) etc.Slot antenna 400 can be provided with two, two slot antennas 400 can be divided into the both sides of rotatable parts 300, or slot antenna 400 is provided with one and is arranged at the side of rotatable parts 300, in the present embodiment, slot antenna 400 is two WIFI antennas being divided into rotatable parts 300 both sides.
Particularly, rotatable parts 300 can be the parts that camera parts or audio amplifier parts or fingerprint recognition parts etc. can rotate relative to fuselage body 100.
Particularly, the driving element (not shown) for driving rotatable parts 300 to rotate relative to fuselage body 100 can be provided with in fuselage body 100.Driving element can be motor etc.In the present embodiment, for motor, the motor shaft of motor can be directly connected in rotating shaft 320, or motor shaft sleeve has driving gear, rotating shaft 320 cover has driven gear, driving gear is meshed with driven gear, or motor shaft is also connected to rotating shaft 320 by driving-belt etc.In embody rule, driving element also can adopt other suitable mode drive shaft 320.
In embody rule, also can manually rotary motion parts 300, rotatable parts 300 also can be made to rotate relative to fuselage body 100.
Particularly, between rotatable parts 300 and fuselage body 100, can damping being provided with, the rotational angle set can be kept to make rotatable parts 300 when not being subject to external force.
Particularly, mobile terminal can be mobile phone or panel computer etc.
The mobile terminal that the embodiment of the present invention provides, its rotatable parts 300 are except the function of itself, also there is antenna function, be beneficial to and reduce antenna the taking of space in fuselage body 100, and be convenient to the arrangement of other antenna in fuselage body 100, slot antenna 400 can be positioned at the side of rotatable parts 300, not by the impact that rotatable parts 300 rotate, each antenna not easily influences each other, the excellent performance of antenna, to ensure the performance of each antenna, and be beneficial to the lightening design of product.
These are only preferred embodiment of the present invention, not in order to limit the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement or improvement etc., all should be included within protection scope of the present invention.
Claims (13)
1. a mobile terminal, comprise fuselage body and slot antenna, it is characterized in that, described fuselage body is rotatably connected to rotatable parts, described slot antenna is arranged at fuselage body and is positioned at the one or both sides of described rotatable parts, is provided with electronic device in described rotatable parts.
2. mobile terminal as claimed in claim 1, it is characterized in that, described electronic device is connected to the circuit board in described fuselage body by feeder line.
3. mobile terminal as claimed in claim 1, it is characterized in that, described fuselage body comprises housing, and described housing comprises metal edge frame, or described housing is metal shell and described metal edge frame is the part of described housing; Described slot antenna comprises the gap being arranged at described metal edge frame and the feed line being connected to described gap.
4. mobile terminal as claimed in claim 3, it is characterized in that, be provided with circuit board in described fuselage body, one end of described feed line strides across the sidewall that gap is connected to described gap, and the other end of described feed line is connected to described circuit board.
5. mobile terminal as claimed in claim 3, it is characterized in that, described gap comprises from described metal edge frame sidewall transversely or oblique the first gap extended to opposite side direction, and described gap also comprises from described first gap end longitudinally or the second gap of oblique extension.
6. mobile terminal as claimed in claim 2, it is characterized in that, described fuselage body is provided with slot, and the both sides of described rotatable parts are connected to the both sides of described slot by axis of rotation.
7. mobile terminal as claimed in claim 6, is characterized in that, it is inner that described feeder line is arranged in described rotating shaft.
8. mobile terminal as claimed in claim 2, it is characterized in that, described rotatable parts and described feeder line form reception antenna or dual-mode antenna.
9. mobile terminal as claimed in claim 8, it is characterized in that, described reception antenna is gps antenna.
10. mobile terminal as claimed in any one of claims 1-9 wherein, it is characterized in that, described slot antenna is WIFI antenna or gps antenna or high frequency diversity antenna, and described slot antenna is divided into the both sides of described rotatable parts or is arranged at the side of described rotatable parts.
11. mobile terminals as claimed in any one of claims 1-9 wherein, is characterized in that, described rotatable parts are camera parts or audio amplifier parts or fingerprint recognition parts.
12. mobile terminals as claimed in any one of claims 1-9 wherein, is characterized in that, being provided with the driving element for driving described rotatable parts to rotate relative to described fuselage body in described fuselage body.
13. mobile terminals as claimed in any one of claims 1-9 wherein, it is characterized in that, described mobile terminal is mobile phone or panel computer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420764281.3U CN204407469U (en) | 2014-12-05 | 2014-12-05 | Mobile terminal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420764281.3U CN204407469U (en) | 2014-12-05 | 2014-12-05 | Mobile terminal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204407469U true CN204407469U (en) | 2015-06-17 |
Family
ID=53431306
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420764281.3U Expired - Fee Related CN204407469U (en) | 2014-12-05 | 2014-12-05 | Mobile terminal |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204407469U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105958184A (en) * | 2016-06-08 | 2016-09-21 | 广东欧珀移动通信有限公司 | Mobile terminal |
| CN106229627A (en) * | 2016-09-30 | 2016-12-14 | 北京小米移动软件有限公司 | A kind of antenna module and mobile terminal |
| CN108493576A (en) * | 2018-03-12 | 2018-09-04 | 广东欧珀移动通信有限公司 | Antenna module, electronic equipment and antenna switching method |
| CN108649335A (en) * | 2018-05-15 | 2018-10-12 | Oppo广东移动通信有限公司 | Antenna module, electronic equipment and antenna switching method |
| CN109005264A (en) * | 2018-08-30 | 2018-12-14 | 维沃移动通信有限公司 | A kind of mobile terminal |
| CN109167152A (en) * | 2018-08-29 | 2019-01-08 | Oppo广东移动通信有限公司 | Electronic equipment |
| WO2020000240A1 (en) * | 2018-06-27 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Antenna structure, remote control, and unmanned aerial vehicle system |
-
2014
- 2014-12-05 CN CN201420764281.3U patent/CN204407469U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105958184A (en) * | 2016-06-08 | 2016-09-21 | 广东欧珀移动通信有限公司 | Mobile terminal |
| CN106229627A (en) * | 2016-09-30 | 2016-12-14 | 北京小米移动软件有限公司 | A kind of antenna module and mobile terminal |
| CN108493576A (en) * | 2018-03-12 | 2018-09-04 | 广东欧珀移动通信有限公司 | Antenna module, electronic equipment and antenna switching method |
| CN108649335A (en) * | 2018-05-15 | 2018-10-12 | Oppo广东移动通信有限公司 | Antenna module, electronic equipment and antenna switching method |
| WO2020000240A1 (en) * | 2018-06-27 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Antenna structure, remote control, and unmanned aerial vehicle system |
| CN109167152A (en) * | 2018-08-29 | 2019-01-08 | Oppo广东移动通信有限公司 | Electronic equipment |
| CN109005264A (en) * | 2018-08-30 | 2018-12-14 | 维沃移动通信有限公司 | A kind of mobile terminal |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: Changan town in Guangdong province Dongguan 523860 usha Beach Road No. 18 Patentee after: GUANGDONG OPPO MOBILE TELECOMMUNICATIONS Corp.,Ltd. Address before: Changan town in Guangdong province Dongguan 523841 usha Beach Road No. 18 Patentee before: GUANGDONG OPPO MOBILE TELECOMMUNICATIONS Corp.,Ltd. |
|
| CP03 | Change of name, title or address | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150617 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |