CN208971561U - A kind of high intensity shatter-resistant handset structure - Google Patents

A kind of high intensity shatter-resistant handset structure Download PDF

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Publication number
CN208971561U
CN208971561U CN201821634652.0U CN201821634652U CN208971561U CN 208971561 U CN208971561 U CN 208971561U CN 201821634652 U CN201821634652 U CN 201821634652U CN 208971561 U CN208971561 U CN 208971561U
Authority
CN
China
Prior art keywords
fuselage cover
sealing
mounting bar
spring
sides
Prior art date
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
Application number
CN201821634652.0U
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Chinese (zh)
Inventor
张志宏
金星磊
桑建
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHENZHEN ZHENHUA COMMUNICATION EQUIPMENT CO Ltd
Original Assignee
SHENZHEN ZHENHUA COMMUNICATION EQUIPMENT CO Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SHENZHEN ZHENHUA COMMUNICATION EQUIPMENT CO Ltd filed Critical SHENZHEN ZHENHUA COMMUNICATION EQUIPMENT CO Ltd
Priority to CN201821634652.0U priority Critical patent/CN208971561U/en
Application granted granted Critical
Publication of CN208971561U publication Critical patent/CN208971561U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Studio Devices (AREA)

Abstract

The utility model discloses a kind of high-intensitive shatter-resistant handset structures, including a fuselage cover, fuselage cover surface is provided with a display screen, the two sides of fuselage cover open up a cushion chamber respectively, cushion chamber bottom surface is bonded one group or more of the first spring, a sealing is packed into each cushion chamber, in the two sides of fuselage cover, the sealing medial surface is adhesively fixed the lateral surface dimpling of sealing with the first spring outwards end face;A pre-buried chamber, the mounting bar of one lift of pre-buried intracavitary installation are opened up at the top of fuselage cover.The utility model structure is simple, can effectively increase the safety of whole mobile phone fuselage, increases drop resistant ability, and can realize the lifting of front camera by fashion of extrusion, preferably protects privacy of user, and have the function of camera automated cleaning.

Description

A kind of high intensity shatter-resistant handset structure
Technical field
The utility model relates to field of mobile phones, in particular to a kind of high-intensitive shatter-resistant handset structure.
Background technique
Handset intensity determines the drop resistant performance of mobile phone, and when mobile phone lands, mobile phone bears whole impacts, because This intensity for improving handset is the key that promote mobile phone drop resistant performance;Front camera can be all arranged in current mobile phone, preceding Portraiture right and individual privacy that camera directly affects user are set, but front camera can be invaded and oneself by criminal It is dynamic to open, the infringement to user is caused, how to hide front camera is the key that solve the above problems.
Summary of the invention
The technical problem to be solved by the utility model is to provide a kind of high-intensitive shatter-resistant handset structures, can be effective Increase the drop resistant ability of fuselage, increases buffer capacity and service life, front camera can be hidden, preferably protect user Privacy.
The utility model is achieved through the following technical solutions: a kind of high intensity shatter-resistant handset structure, including One fuselage cover, fuselage cover surface are provided with a display screen, and the two sides of fuselage cover open up a cushion chamber, cushion chamber respectively Bottom surface is bonded one group or more of the first spring, is packed into a sealing in each cushion chamber, the lateral surface dimpling of sealing is in machine The two sides of body shell, the sealing medial surface are adhesively fixed with the first spring outwards end face;
A pre-buried chamber, the mounting bar of one lift of pre-buried intracavitary installation, mounting bar two sides phase are opened up at the top of fuselage cover One the first inclined surface is respectively opened up to sealing side, the sealing top surface of the first inclined surface of face opens up one second inclination Face, the first inclined surface and the second inclined surface smooth contact, mounting bar engage assembly with the sealing of two sides, before the mounting bar End face insertion one front camera of setting, the front camera access the mobile phone master inside fuselage cover by camera wiring Plate.
The bottom surface of the pre-buried chamber opens up cavity as a preferred technical solution, and the of one group or more is equipped in cavity Two springs, the bottom surface of second spring top bonding mounting bar, the bottom surface of the bottom bonding cavity of second spring, the outside of mounting bar Face and fuselage cover either flush.
Camera wiring interlude is provided with one section of spring section as a preferred technical solution, and camera wiring passes through machine Aperture on body shell is inserted into the mainboard installation cavity inside fuselage cover Nei and connects cell phone mainboard.
The two sides of pre-buried chamber are bonded one layer of cleaning cotton layer respectively as a preferred technical solution, cleaning cotton layer with it is preposition The camera lens of camera contacts.
The beneficial effects of the utility model are: the utility model structure is simple, whole mobile phone fuselage can be effectively increased Safety increases drop resistant ability, and can realize the lifting of front camera by fashion of extrusion, preferably protects privacy of user, And has the function of camera automated cleaning.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor Under, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is the overall structure diagram of the utility model;
Fig. 2 is the partial enlarged view in Fig. 1 at A.
Specific embodiment
All features disclosed in this specification or disclosed all methods or in the process the step of, in addition to mutually exclusive Feature and/or step other than, can combine in any way.
Any feature disclosed in this specification (including any accessory claim, abstract and attached drawing), except non-specifically chatting It states, can be replaced by other alternative features that are equivalent or have similar purpose.That is, unless specifically stated, each feature is only It is an example in a series of equivalent or similar characteristics.
As depicted in figs. 1 and 2, including a fuselage cover 11,11 surface of fuselage cover is provided with a display screen 12, outside fuselage The two sides of shell 11 open up a cushion chamber 3 respectively, and 3 bottom surface of cushion chamber is bonded one group or more of the first spring 2, each cushion chamber 3 It is inside packed into a sealing 4, the lateral surface dimpling of sealing 4 is in the two sides of fuselage cover 11,4 medial surface of sealing and the first bullet 2 end face outside of spring is adhesively fixed;
The top of fuselage cover 11 opens up a pre-buried chamber, the mounting bar 5 of one lift of pre-buried intracavitary installation, and 5 liang of mounting bar Side opposing seal portion side respectively opens up first inclined surface 2, and 4 top surface of sealing of the first inclined surface of face 2 opens up one Two inclined surface (not shown), the first inclined surface 2 and the second inclined surface smooth contact, mounting bar engage dress with the sealing of two sides Match, front end face insertion one front camera 6 of setting of mounting bar 5, the front camera 6 accesses machine by camera wiring 13 The cell phone mainboard 1 of body interior of shell.
When fuselage cover falls, if impact is in the two sides of fuselage cover, the sealing of two sides can receive impact, First spring is pressurized, and realizes buffering, increases the drop resistant ability of fuselage cover.And mounting bar then passes through second spring when not in use Retraction is in pre-buried intracavitary, therefore front camera cannot image when not in use.Accordingly even when open front camera also without Method is shot, and the privacy of user is preferably protected.
When using front camera, as long as the sealing of two sides is squeezed with hand, so that the second inclined surface at the top of sealing The first inclined surface of mounting bar is squeezed, so that mounting bar realizes mounting bar by skidding off outward under the action of inclined surface with this It is flexible, it is very simple and convenient.
Wherein, the bottom surface of pre-buried chamber opens up cavity 9, and one group or more of second spring 7, second spring 7 are equipped in cavity 9 Top is bonded the bottom surface of mounting bar, the bottom surface of the bottom bonding cavity 9 of second spring 7, the lateral surface and fuselage cover of mounting bar Either flush.
As shown in Fig. 2, 13 interlude of camera wiring is provided with one section of spring section, camera wiring is passed through on fuselage cover Aperture be inserted into the mainboard installation cavity inside fuselage cover Nei and connect cell phone mainboard 1.Realize that camera connects using spring section The stretching of line meets flexible require so that mounting bar, after being ejected, camera wiring can be stretched.
Wherein, the two sides of pre-buried chamber are bonded one layer of cleaning cotton layer (not shown), cleaning cotton layer and front camera respectively Camera lens contact.Mounting bar is gone up and down every time, and contact friction of the front camera with cleaning cotton layer can be realized, and realization is taken the photograph to preposition As the cleaning of head.
The beneficial effects of the utility model are: the utility model structure is simple, whole mobile phone fuselage can be effectively increased Safety increases drop resistant ability, and can realize the lifting of front camera by fashion of extrusion, preferably protects privacy of user, And has the function of camera automated cleaning.
Above description is only a specific implementation of the present invention, but the protection scope of the utility model is not limited to In this, any change or replacement expected without creative work be should be covered within the scope of the utility model. Therefore, the protection scope of the utility model should be determined by the scope of protection defined in the claims.

Claims (4)

1. a kind of high intensity shatter-resistant handset structure, it is characterised in that: including a fuselage cover, fuselage cover surface is provided with One display screen, the two sides of fuselage cover open up a cushion chamber respectively, and cushion chamber bottom surface is bonded one group or more of the first spring, often A sealing is packed into a cushion chamber, the lateral surface dimpling of sealing is in the two sides of fuselage cover, the sealing medial surface It is adhesively fixed with the first spring outwards end face;
Open up a pre-buried chamber at the top of fuselage cover, the mounting bar of one lift of pre-buried intracavitary installation, mounting bar two sides are relatively close Envelope portion side respectively opens up first inclined surface, and the sealing top surface of the first inclined surface of face opens up second inclined surface, the One inclined surface and the second inclined surface smooth contact, mounting bar engage assembly, the front end face of the mounting bar with the sealing of two sides Insertion one front camera of setting, the front camera access the cell phone mainboard inside fuselage cover by camera wiring.
2. high intensity shatter-resistant handset structure as described in claim 1, it is characterised in that: the bottom surface of the pre-buried chamber opens up Cavity is equipped with one group or more of second spring in cavity, the bottom surface of bonding mounting bar, the bottom of second spring at the top of second spring Portion is bonded the bottom surface of cavity, the lateral surface and fuselage cover either flush of mounting bar.
3. high intensity shatter-resistant handset structure as described in claim 1, it is characterised in that: the setting of camera wiring interlude There is one section of spring section, the aperture that camera wiring passes through on fuselage cover is inserted into the mainboard installation cavity inside fuselage cover simultaneously Connect cell phone mainboard.
4. high intensity shatter-resistant handset structure as described in claim 1, it is characterised in that: glue respectively the two sides of pre-buried chamber One layer of cleaning cotton layer is connect, cleaning cotton layer is contacted with the camera lens of front camera.
CN201821634652.0U 2018-10-09 2018-10-09 A kind of high intensity shatter-resistant handset structure Expired - Fee Related CN208971561U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821634652.0U CN208971561U (en) 2018-10-09 2018-10-09 A kind of high intensity shatter-resistant handset structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821634652.0U CN208971561U (en) 2018-10-09 2018-10-09 A kind of high intensity shatter-resistant handset structure

Publications (1)

Publication Number Publication Date
CN208971561U true CN208971561U (en) 2019-06-11

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110324517A (en) * 2019-06-13 2019-10-11 维沃移动通信(杭州)有限公司 Terminal device and its control method and control device, computer readable storage medium
CN111327738A (en) * 2020-01-11 2020-06-23 夏天 Cell-phone safety lift camera

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110324517A (en) * 2019-06-13 2019-10-11 维沃移动通信(杭州)有限公司 Terminal device and its control method and control device, computer readable storage medium
CN110324517B (en) * 2019-06-13 2021-04-06 维沃移动通信(杭州)有限公司 Terminal device, control method and control device thereof, and computer-readable storage medium
CN111327738A (en) * 2020-01-11 2020-06-23 夏天 Cell-phone safety lift camera
CN111327738B (en) * 2020-01-11 2021-08-17 浙江联永移动终端设备制造有限公司 Cell-phone safety lift camera

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190611

Termination date: 20191009