CN1584736A - Electronic device with mirror and image picking-up function - Google Patents
Electronic device with mirror and image picking-up function Download PDFInfo
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- CN1584736A CN1584736A CN 03154098 CN03154098A CN1584736A CN 1584736 A CN1584736 A CN 1584736A CN 03154098 CN03154098 CN 03154098 CN 03154098 A CN03154098 A CN 03154098A CN 1584736 A CN1584736 A CN 1584736A
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Abstract
An electronic device comprising a body, a mirror display and an image picking unit features that mirror display is set in the body, and the mirror display has a transparent baseplate and transparency reflecting layer as transparent baseplate is equipped with the first surface and the second surface being opposite to the first one, transparency reflecting layer is on the first or on the second surface and image picking unit is set on the body.
Description
Technical field
The present invention relates to a kind of electronic installation, be meant a kind of electronic installation especially with mirror face function and image acquisition function.
Background technology
Because infosystem is compact day by day, make portable electric device also be tending towards variation, for example mobile phone, PDA(Personal Digital Assistant), e-book, stock handset and digital camera or the like.With the mobile phone is example, and the mobile phone with digital camera functionality has become designer trends in recent years, and the mobile phone of this type is provided with a camera lens in fuselage, the reservoir of arranging in pairs or groups simultaneously, the photo that is filmed in order to storage.
The dealer is installed a metal convex mirror additional in order to allow the convenient image of taking self of user in mobile phone at present.Shown in Figure 1A and Figure 1B, mobile phone 9 has one first fuselage body 91, one second fuselage body 92, a display 93, an image acquisition unit 94, a metal convex mirror 95 and an input block 96, wherein, display 93, image acquisition unit 94, metal convex mirror 95 are arranged on first fuselage body 91, input block 96 is arranged on second fuselage body 92, and image acquisition unit 94 comprises a camera lens.When the user utilizes mobile phone 9 shootings self image, can utilize metal convex mirror 95 reflection users' self image, to determine own position in camera lens.Yet, because the precision of convex mirror focusing is not high, and the sharpness of institute's reflected image is also low, in this way only can rough affirmation oneself position (as self whether in the centre of whole image) in whole image, and can't really see the image that image acquisition unit 94 is captured.
In view of this, the dealer uses the design of rotating lens to solve above-mentioned problem.Shown in Fig. 2 A, mobile phone 10 has one first fuselage body 101, one second fuselage body 102, a display 103, an image acquisition unit 104 and an input block 105, wherein, display 103, image acquisition unit 104 are arranged on first fuselage body 101, and input block 105 is arranged on second fuselage body 102.In mobile phone 10, image acquisition unit 104 captured images directly are presented on the display 103.After the user utilizes mobile phone 10 to autodyne, can utilize the design of rotating hinge that first fuselage body 101 is overturn, and utilize display 103 to confirm the image of just having taken, shown in Fig. 2 B.Yet complex structure, the production cost of this kind mobile phone are higher, and operation simultaneously is also inconvenient, so be unfavorable for the application of actualsization.
Summary of the invention
Because above-mentioned problem, the purpose of this invention is to provide a kind of simple in structure, low production cost, operation is convenient and accurately the tool mirror face function of preview shooting image and the electronic installation of image acquisition function.
Electronic installation of the present invention comprises but is not defined as mobile phone, palmtop computer (hand-heldPC), personal digital assistant, e-book, stock handset, digital recording pen and digital camera or the like.
For reaching above-mentioned purpose, the electronic installation according to a kind of tool mirror face function of the present invention and image acquisition function comprises a fuselage body, a mirror display and an image acquisition unit.Wherein, mirror display is arranged in the fuselage body, and mirror display comprises a transparency carrier and a light transmissive reflecting layer, and transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit is arranged on the fuselage body.
For reaching above-mentioned purpose, the electronic installation according to a kind of tool mirror face function of the present invention and image acquisition function comprises a fuselage body, a mirror display and an image acquisition unit.Wherein, mirror display is arranged in the fuselage body, and mirror display comprises a transparency carrier and a light transmissive reflecting layer, and transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit is connected with the either side of fuselage body.
For reaching above-mentioned purpose, the electronic installation according to a kind of tool mirror face function of the present invention and image acquisition function comprises one first fuselage body, one second fuselage body, a mirror display and an image acquisition unit.Wherein, second fuselage body and first fuselage body interconnect; Mirror display is arranged in first fuselage body, and mirror display comprises a transparency carrier and a light transmissive reflecting layer, transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit is arranged on first fuselage body or second fuselage body.
For reaching above-mentioned purpose, the electronic installation according to a kind of tool mirror face function of the present invention and image acquisition function comprises one first fuselage body, a pivot, one second fuselage body, a mirror display and an image acquisition unit.Wherein, second fuselage body utilizes the pivot and first fuselage body to interconnect; Mirror display is arranged in first fuselage body, and mirror display comprises a transparency carrier and a light transmissive reflecting layer, transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit is arranged on the pivot.
Mirror display comprises but is not defined as an organic electric-excitation luminescent (OrganicElectroluminescence, OEL) display, inorganic electroluminescence (Electroluminescence, EL) display, light emitting diode (Light Emitting Diode, LED) display, LCD (Liquid Crystal Display, LCD), plasma display panel (Plasma Display Panel, PDP), vacuum fluorescent display (Vacuum Fluorescent Display, VFD), (Field Emission Display is FED) with electrochromic display device (ECD) (Electro-chromicDisplay) etc. for field-emitter display.
From the above, the electronic installation of tool mirror face function of the present invention and image acquisition function utilizes mirror display usefulness as preview when autodyning, particularly, when the user utilizes electronic installation shooting self image, can utilize the reflection function of mirror display to aim at, to determine the captured scope of camera lens.Compared with prior art, the present invention need not add any element (as metal convex mirror of the prior art) or increase the action of operation, can aim at when taking, and has not only saved the cost that adds element, more need not carry out complicated operational motion.Again, the present invention need not utilize display to show the image of shooting, scope that can accurate preview shooting.In addition, when mirror display was not luminous, the mirror display of electronic installation promptly had the function of mirror surface, as the purposes of mirror, can be used to reflect user's self image, when taking as the usefulness of auto heterodyne preview; On the other hand, when mirror display was luminous, the mirror display of electronic installation had the function of display message image, can be as the usefulness of general display.Moreover the present invention only is provided with light transmissive reflecting layer in mirror display, just can produce the function of minute surface, and not only processing procedure is simple, and the increase of whole cost is also not high, and is very suitable for the application of actualsization.
Description of drawings
Figure 1A and Figure 1B are one group of synoptic diagram of existing mobile phone;
Fig. 2 A and Fig. 2 B are one group of synoptic diagram of another existing mobile phone;
Fig. 3 is a synoptic diagram of the electronic installation of tool mirror face function and image acquisition function in the first embodiment of the invention;
Fig. 4 A and Fig. 4 B are one group of diagrammatic cross-section of mirror display in the first embodiment of the invention;
Fig. 5 A and Fig. 5 B are the concrete one group of synoptic diagram implementing of Fig. 3;
Fig. 6 A to Fig. 6 C is one group of synoptic diagram of the electronic installation of tool mirror face function and image acquisition function in the second embodiment of the invention;
Fig. 7 is a synoptic diagram of the electronic installation of tool mirror face function and image acquisition function in the third embodiment of the invention;
Fig. 8 is a synoptic diagram of the electronic installation of tool mirror face function and image acquisition function in the fourth embodiment of the invention.
Symbol description among the figure
5 electronic installations
51 fuselage bodies
52 mirror display
521 transparency carriers
5211 first surfaces
5212 second surfaces
522 light transmissive reflecting layer
53 image acquisition units
54 input blocks
6 electronic installations
61 fuselage bodies
62 mirror display
63 image acquisition units
64 input blocks
7 electronic installations
71 first fuselage bodies
72 second fuselage bodies
73 mirror display
74 image acquisition units
75 input blocks
8 electronic installations
81 first fuselage bodies
82 pivots
83 second fuselage bodies
84 mirror display
85 image acquisition units
86 input blocks
9 mobile phones
91 first fuselage bodies
92 second fuselage bodies
93 displays
94 image acquisition units
95 metal convex mirrors
96 input blocks
10 mobile phones
101 first fuselage bodies
102 second fuselage bodies
103 displays
104 image acquisition units
105 input blocks
Embodiment
Hereinafter with reference to relevant drawings, illustrate according to the tool mirror face function of preferred embodiment of the present invention and the electronic installation of image acquisition function.
To be example below, describe the electronic installation of tool mirror face function of the present invention and image acquisition function in detail with the mobile phone.
Shown in Fig. 3, Fig. 4 A and Fig. 4 B, a kind of tool mirror face function of first embodiment of the invention and the electronic installation 5 of image acquisition function comprise a fuselage body 51, a mirror display 52 and an image acquisition unit 53.Wherein, mirror display 52 is arranged in the fuselage body 51, and mirror display 52 comprises a transparency carrier 521 and a light transmissive reflecting layer 522, transparency carrier 521 has a first surface 5211 and a second surface 5212 relative with first surface 5211, and light transmissive reflecting layer 522 is formed on first surface 5211 or the second surface 5212; Image acquisition unit 53 is arranged on the fuselage body 51.
In present embodiment, fuselage body 51 is a housing, and the shape of fuselage body 51 and size can adjust on demand.
In present embodiment, mirror display 52 can be an organic electro-luminescent display.
The mirror display 52 of present embodiment is arranged in the fuselage body 51.Shown in Fig. 4 A, mirror display 52 comprises transparency carrier 521, light transmissive reflecting layer 522, one first electrode 523, a luminous zone 524 and one second electrode 525.Wherein, transparency carrier 521 have first surface 5211 and with first surface 5211 opposing second surface 5212; First electrode 523 is positioned on the first surface 5211 of transparency carrier 521; Second electrode 525 is formed on first electrode 523; Luminous zone 524 is between first electrode 523 and second electrode 525; Light transmissive reflecting layer 522 is formed on the second surface 5212.Wherein, luminous zone 524 its can be an organic functional layer.
In present embodiment, transparency carrier 521 can be a flexibility (flexible) substrate or a rigidity (rigid) substrate.Simultaneously, transparency carrier 521 can also be plastics (plastic) substrate or a glass substrate.Wherein, flexible base, board and plastic base can be a polycarbonate (polycarbonate, PC) substrate, a polyester (polyester, PET) substrate, a cyclenes copolymer (cyclic olefin copolymer, COC) substrate or a crome metal compound base material one cyclenes copolymer (metallocene-based cyclic olefin copolymer, mCOC) substrate.
Shown in Fig. 4 A, first electrode 523 utilizes sputter (sputtering) or ion plating modes such as (ion plating) is formed on the transparency carrier 521.At this, first electrode 523 is generally a transparent conductive metal oxide as anode and its material usually, for example tin indium oxide (ITO), aluminum zinc oxide (AZO) or indium zinc oxide (IZO) or the like.
In addition, the luminous zone 524 in the present embodiment is positioned on first electrode 523, and it can be an organic functional layer.Wherein, organic functional layer 524 comprises an electric hole input horizon, an electric hole transfer layer, a luminescent layer, an electron transfer layer and an electron injecting layer (not shown) usually.Organic functional layer 524 utilizes evaporation (evaporation), rotary coating (spin coating), ink jet printing (ink jet printing) or printing modes such as (printing) to be formed on first electrode 523.In addition, the light launched of organic functional layer 524 can be blue light, green glow, ruddiness, white light, other monochromatic light or the colorama that is combined into of monochromatic light.
Shown in Fig. 4 A, light transmissive reflecting layer 522 is formed on the second surface 5212.In this, light transmissive reflecting layer 522 utilizes evaporation, sputter or ion plating mode to be formed on the second surface 5212.In present embodiment, the material of light transmissive reflecting layer 522 is metal or dielectric material.And the transmittance of light transmissive reflecting layer 522 is about 10% to 90%.
Certainly, light transmissive reflecting layer 522 also can be formed on the first surface 5211, shown in Fig. 4 B.
In present embodiment, when the material of light transmissive reflecting layer 522 is metal, more be formed with an insulation course (not being shown among the figure) between the light transmissive reflecting layer 522 and first electrode 523.This insulation course is a light-permeable material, in order to the isolated light transmissive reflecting layer 522 and first electrode 523, avoids both to cause short circuit condition because of contact.
In present embodiment, when mirror display 52 was luminous, user's eyes are seen was the shown picture of mirror display 52, for example literal, numeral, pattern or image.On the one hand, when mirror display 52 was not luminous, the person of being to use that user's eyes are seen held the reflected image of background in addition, that is mirror display 52 is used as the mirror use.
In addition, the mirror display 52 of present embodiment can also be inorganic electroluminescence (Electroluminescence, EL) display, light emitting diode (Light Emitting Diode, LED) display, LCD (Liquid Crystal Display, LCD), plasma display panel (Plasma Display Panel, PDP), vacuum fluorescent display device (Vacuum FluorescentDisplay, VFD), field-emission display device (Field Emission Display, FED) or electrochromic display device (Electro-chromic Display) or the like.
Please refer to Fig. 3 again, the image acquisition unit 53 of present embodiment is arranged on the fuselage body 51.In this, image acquisition unit 53 comprises a camera lens and a charge coupled cell (CCD) or CMOS, wherein charge coupled cell is an inductor, by this charge coupled cell, can be with the image that camera lens was truncated to, convert digital image signal to, by the processing of electronic circuit, digital image signal is stored in the Storage Media (storer) again.
In addition, in present embodiment, electronic installation 5 more comprises an input block 54, and this input block 54 is arranged on the fuselage body 51.Wherein, input block 54 can be button input block, touch input block or or acoustic control formula input block or the like.In this, input block 54 is established with mirror display 52 neighbours; Certainly, input block 54 also can be arranged on the mirror display 52 and (not be shown among the figure).
In addition, the electronic installation 5 in the present embodiment more comprises a message processing module (not being shown among the figure), and wherein message processing module is arranged in the fuselage body 51.In this, message processing module comprises microprocessor, communication interface (transmitter and receiver), storer and signal processor or the like.
In addition, the electronic installation 5 in the present embodiment more comprises a power-supply unit, battery (not being shown among the figure) for example, and wherein power-supply unit is arranged in the fuselage body 51.
Fig. 5 A and Fig. 5 B are one group of synoptic diagram of the concrete enforcement of Fig. 3.Shown in Fig. 5 A, when mirror display 52 was luminous, mirror display 52 had the function of display message image, as incoming call number, time or other figure shelves or the like; On the other hand, shown in Fig. 5 B, when mirror display 52 is not luminous, mirror display 52 promptly has the function of mirror surface, as the purposes of mirror, so, when the user utilizes electronic installation 5 shootings self image (auto heterodyne), can be simultaneously see the reflected image of self background from mirror display 52, that is camera lens institute picked image, as the usefulness of auto heterodyne preview.
In addition, shown in Fig. 6 A, 6B and 6C, a kind of tool mirror face function of second embodiment of the invention and the electronic installation 6 of image acquisition function comprise a fuselage body 61, a mirror display 62 and an image acquisition unit 63.Wherein, mirror display 62 is arranged in the fuselage body 61, and mirror display 62 comprises a transparency carrier and a light transmissive reflecting layer, and transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit 63 is connected with the either side of fuselage body 61.
Shown in Fig. 6 A, Fig. 6 B and Fig. 6 C, the image acquisition unit 63 in the present embodiment is connected with the either side of fuselage body 61, and the set position of image acquisition unit 63 can be required and adjust according to reality.
In present embodiment, the feature of fuselage body 61, mirror display 62, transparency carrier and light transmissive reflecting layer is identical with similar elements among the function and first embodiment, also repeats no more at this.
In addition, the image acquisition unit 63 of present embodiment is connected with the either side of fuselage body 61, and in addition, image acquisition unit 63 remaining feature are identical with image acquisition unit 53 among the function and first embodiment, also repeat no more at this.
The electronic installation 6 of present embodiment more is provided with an input block 64, a message processing module (not being shown among the figure) and a power-supply unit (not being shown among the figure), the feature of these elements and the function element that is basically the same as those in the first embodiment is identical, also repeats no more at this.
In addition, as shown in Figure 7, a kind of tool mirror face function of third embodiment of the invention and the electronic installation 7 of image acquisition function comprise one first fuselage body 71, one second fuselage body 72, a mirror display 73 and an image acquisition unit 74.Wherein, second fuselage body 72 and first fuselage body 71 interconnect; Mirror display 73 is arranged in first fuselage body 71, and mirror display 73 comprises a transparency carrier and a light transmissive reflecting layer, transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit 74 is arranged on first fuselage body 71 or second fuselage body 72 (not being shown among the figure).
In present embodiment, first fuselage body 71 and second fuselage body 72 are housing, and the shape and the size of first fuselage body 71 and second fuselage body 72 can adjust on demand.As shown in Figure 7, first fuselage body 71 and second fuselage body 72 interconnect, and connected mode can be to articulate.Certainly, the pivot of present embodiment also can be arranged at one of remaining three limit (not being shown among the figure).In addition, also double replacement mutually of first fuselage body 71 and second fuselage body 72.
In addition, the feature of mirror display 73, transparency carrier, light transmissive reflecting layer and image acquisition unit 74 is identical with similar elements among the function and first embodiment, also repeats no more at this.
The electronic installation 7 of present embodiment more is provided with an input block 75, a message processing module (not being shown among the figure) and a power-supply unit (not being shown among the figure), the feature of these elements and the function element that is basically the same as those in the first embodiment is identical, also repeats no more at this.
Please refer to Fig. 7 again, in present embodiment, except image acquisition unit 74 was arranged on first fuselage body 71, all the other features of image acquisition unit 74 were identical with the image acquisition unit 13 of the function and first embodiment, also repeat no more at this.
In addition, as shown in Figure 8, a kind of tool mirror face function of fourth embodiment of the invention and the electronic installation 8 of image acquisition function comprise one first fuselage body 81, a pivot 82, one second fuselage body 83, a mirror display 84 and an image acquisition unit 85.Wherein, second fuselage body 83 utilizes the pivot 82 and first fuselage body 81 to interconnect; Mirror display 84 is arranged in first fuselage body 81, and mirror display 84 comprises a transparency carrier and a light transmissive reflecting layer, transparency carrier has a first surface and a second surface relative with first surface, and light transmissive reflecting layer is formed on first surface or the second surface; Image acquisition unit 85 is arranged on the pivot 82.
In present embodiment, first fuselage body 81, pivot 82, second fuselage body 83, mirror display 84, transparency carrier, light transmissive reflecting layer are identical with the similar elements among function and the 3rd embodiment with the feature of image acquisition unit 85, also repeat no more at this.
In addition, as shown in Figure 8, in present embodiment, except image acquisition unit 85 was arranged on the pivot 82, all the other features of image acquisition unit 85 were identical with the image acquisition unit 13 of the function and first embodiment, also repeat no more at this.
The electronic installation 8 of present embodiment more is provided with an input block 86, a message processing module (not being shown among the figure) and a power-supply unit (not being shown among the figure), the feature of these elements and the function element that is basically the same as those in the first embodiment is identical, also repeats no more at this.
Certainly, in the present invention, electronic installation comprises but is not defined as mobile phone, palmtop computer, personal digital assistant, e-book, stock handset, digital recording pen and digital camera or the like.
The electronic installation of tool mirror face function of the present invention and image acquisition function utilizes mirror display usefulness as preview when autodyning, particularly, when the user utilizes electronic installation shooting self image, can utilize the reflection function of mirror display to aim at, to determine the captured scope of camera lens.Compared with prior art, the present invention need not add any element (as metal convex mirror of the prior art) or increase the action of operation, can aim at when taking, and has not only saved the cost that adds element, more need not carry out complicated operational motion.Again, the present invention need not utilize display to show the image of shooting, scope that can accurate preview shooting.In addition, when mirror display was not luminous, the mirror display of electronic installation promptly had the function of mirror surface, as the purposes of mirror, can be used to reflect user's self image, when taking as the usefulness of auto heterodyne preview; On the other hand, when mirror display was luminous, the mirror display of electronic installation had the function of display message image, can be as the usefulness of general display.Moreover the present invention only is provided with light transmissive reflecting layer in mirror display, just can produce the function of minute surface, and not only processing procedure is simple, and the increase of whole cost is also not high, and is very suitable for the application of actualsization.
The above only is an illustrative, but not is restricted person.Anyly do not break away from spirit of the present invention and category, and, all should be contained in the scope of claims its equivalent modifications of carrying out or change.
Claims (26)
1. the electronic installation of tool mirror face function and image acquisition function is characterized in that, comprises:
One fuselage body;
One mirror display, it is arranged in this fuselage body, and this mirror display comprises a transparency carrier and a light transmissive reflecting layer, this transparency carrier has a first surface and a second surface relative with this first surface, and this light transmissive reflecting layer is formed on this first surface or this second surface; And
One image acquisition unit, it is arranged on this fuselage body.
2. the electronic installation of tool mirror face function as claimed in claim 1 and image acquisition function more comprises an input block, and this input block is arranged at this fuselage body.
3. the electronic installation of tool mirror face function as claimed in claim 1 and image acquisition function more comprises a message processing module, and this message processing module is arranged in this fuselage body.
4. the electronic installation of tool mirror face function as claimed in claim 1 and image acquisition function, wherein the material of this light transmissive reflecting layer is metal or is dielectric material.
5. the electronic installation of tool mirror face function as claimed in claim 1 and image acquisition function, wherein the transmittance of this light transmissive reflecting layer is 10% to 90%.
6. the electronic installation of tool mirror face function as claimed in claim 1 and image acquisition function, wherein this mirror display is organic electro-luminescent display or inorganic electroluminescence display or for light emitting diode indicator or for LCD or for plasma display panel or for vacuum fluorescent display or for field-emitter display or be electrochromic display device (ECD).
7. the electronic installation of tool mirror face function and image acquisition function is characterized in that, comprises:
One fuselage body;
One mirror display, it is arranged in this fuselage body, and this mirror display comprises a transparency carrier and a light transmissive reflecting layer, this transparency carrier has a first surface and a second surface relative with this first surface, and this light transmissive reflecting layer is formed on this first surface or this second surface; And
One image acquisition unit, it is connected with the either side of this fuselage body.
8. the electronic installation of tool mirror face function as claimed in claim 7 and image acquisition function more comprises an input block, and this input block is arranged at this fuselage body.
9. the electronic installation of tool mirror face function as claimed in claim 7 and image acquisition function more comprises a message processing module, and this message processing module is arranged in this fuselage body.
10. the electronic installation of tool mirror face function as claimed in claim 7 and image acquisition function, wherein the material of this light transmissive reflecting layer is metal or is dielectric material.
11. the electronic installation of tool mirror face function as claimed in claim 7 and image acquisition function, wherein the transmittance of this light transmissive reflecting layer is 10% to 90%.
12. the electronic installation of tool mirror face function as claimed in claim 7 and image acquisition function, wherein this mirror display is organic electro-luminescent display or inorganic electroluminescence display or for light emitting diode indicator or for LCD or for plasma display panel or for vacuum fluorescent display or for field-emitter display or be electrochromic display device (ECD).
13. the electronic installation of tool mirror face function and image acquisition function is characterized in that, comprises:
One first fuselage body;
One second fuselage body, itself and this first fuselage body interconnects;
One mirror display, it is arranged in this first fuselage body, and this mirror display comprises a transparency carrier and a light transmissive reflecting layer, this transparency carrier has a first surface and a second surface relative with this first surface, and this light transmissive reflecting layer is formed on this first surface or this second surface; And
One image acquisition unit, it is arranged on this first fuselage body or this second fuselage body.
14. the electronic installation of tool mirror face function as claimed in claim 13 and image acquisition function more comprises an input block.
15. the electronic installation of tool mirror face function as claimed in claim 14 and image acquisition function, wherein this input block is arranged at this first fuselage body or second fuselage body.
16. the electronic installation of tool mirror face function as claimed in claim 13 and image acquisition function more comprises a message processing module, this message processing module is arranged in this fuselage body.
17. the electronic installation of tool mirror face function as claimed in claim 13 and image acquisition function, wherein the material of this light transmissive reflecting layer is metal or is dielectric material.
18. the electronic installation of tool mirror face function as claimed in claim 13 and image acquisition function, wherein the transmittance of this light transmissive reflecting layer is 10% to 90%.
19. the electronic installation of tool mirror face function as claimed in claim 13 and image acquisition function, wherein this mirror display is organic electro-luminescent display or inorganic electroluminescence display or for light emitting diode indicator or for LCD or for plasma display panel or for vacuum fluorescent display or for field-emitter display or be electrochromic display device (ECD).
20. the electronic installation of tool mirror face function and image acquisition function is characterized in that, comprises:
One first fuselage body;
One pivot;
One second fuselage body, it utilizes this pivot and this first fuselage body to interconnect;
One mirror display, it is arranged in this first fuselage body, and this mirror display comprises a transparency carrier and a light transmissive reflecting layer, this transparency carrier has a first surface and a second surface relative with this first surface, and this light transmissive reflecting layer is formed on this first surface or this second surface; And
One image acquisition unit, it is arranged on this pivot.
21. the electronic installation of tool mirror face function as claimed in claim 20 and image acquisition function more comprises an input block.
22. the electronic installation of tool mirror face function as claimed in claim 21 and image acquisition function, wherein this input block is arranged at this first fuselage body or second fuselage body.
23. the electronic installation of tool mirror face function as claimed in claim 20 and image acquisition function more comprises a message processing module, this message processing module is arranged in this fuselage body.
24. the electronic installation of tool mirror face function as claimed in claim 20 and image acquisition function, wherein the material of this light transmissive reflecting layer is metal or is dielectric material.
25. the electronic installation of tool mirror face function as claimed in claim 20 and image acquisition function, wherein the transmittance of this light transmissive reflecting layer is 10% to 90%.
26. the electronic installation of tool mirror face function as claimed in claim 20 and image acquisition function, wherein this mirror display is organic electro-luminescent display or inorganic electroluminescence display or for light emitting diode indicator or for LCD or for plasma display panel or for vacuum fluorescent display or for field-emitter display or be electrochromic display device (ECD).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03154098 CN1584736A (en) | 2003-08-19 | 2003-08-19 | Electronic device with mirror and image picking-up function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 03154098 CN1584736A (en) | 2003-08-19 | 2003-08-19 | Electronic device with mirror and image picking-up function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1584736A true CN1584736A (en) | 2005-02-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 03154098 Pending CN1584736A (en) | 2003-08-19 | 2003-08-19 | Electronic device with mirror and image picking-up function |
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| CN (1) | CN1584736A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109040580A (en) * | 2018-07-17 | 2018-12-18 | 奇酷互联网络科技（深圳）有限公司 | Mobile terminal and its control method taken pictures and device |
-
2003
- 2003-08-19 CN CN 03154098 patent/CN1584736A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109040580A (en) * | 2018-07-17 | 2018-12-18 | 奇酷互联网络科技（深圳）有限公司 | Mobile terminal and its control method taken pictures and device |
| CN109040580B (en) * | 2018-07-17 | 2021-08-13 | 奇酷互联网络科技（深圳）有限公司 | Mobile terminal and photographing control method and device thereof |
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