CN103792547A - Satellite navigator - Google Patents

Satellite navigator Download PDF

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Publication number
CN103792547A
CN103792547A CN201210583669.9A CN201210583669A CN103792547A CN 103792547 A CN103792547 A CN 103792547A CN 201210583669 A CN201210583669 A CN 201210583669A CN 103792547 A CN103792547 A CN 103792547A
Authority
CN
China
Prior art keywords
main frame
junction surface
lid
satellite navigator
navigator
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.)
Pending
Application number
CN201210583669.9A
Other languages
Chinese (zh)
Inventor
付勇峰
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.)
BEIJING FOUNDER TECHNOLOGY INFORMATION PRODUCT Co Ltd
FOUNDER TECHNOLOGY GROUP Corp SUZHOU PRODUCT Co Ltd
Shanghai Founder Technology Computer System Co Ltd
Original Assignee
FOUNDER TECHNOLOGY GROUP Corp SUZHOU PRODUCT 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 FOUNDER TECHNOLOGY GROUP Corp SUZHOU PRODUCT Co Ltd filed Critical FOUNDER TECHNOLOGY GROUP Corp SUZHOU PRODUCT Co Ltd
Priority to CN201210583669.9A priority Critical patent/CN103792547A/en
Publication of CN103792547A publication Critical patent/CN103792547A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • G01S19/35Constructional details or hardware or software details of the signal processing chain

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Signal Processing (AREA)
  • Casings For Electric Apparatus (AREA)

Abstract

The invention discloses a satellite navigator. The navigator comprises a host and a cover body located on a front end of the host. The cover body is provided with a joint portion which is connected with the host and an entablature which is extended forwardly from the joint portion. The host is provided with a butt joint portion which is cooperated with the joint portion so that replacement of the cover body is realized. The navigator of the invention has the following advantages that dismounting of the cover body is convenient; the cover bodies with different colors and shapes can be used according to hobbies; sunlight can be prevented from directly irradiating an interface and a problem that a presenting effect of a frame is not good because of irradiation of the sunlight is avoided.

Description

Satellite navigator
Technical field
The present invention relates to a kind of satellite navigator, more particularly, is a kind of satellite navigator with detachable lid.
Background technology
In life now, " convenience " becomes one of most important demand in people's life, to such an extent as to many electronic equipments are constantly released for people's life provides service easily, as Satellite Navigation Set, mobile phone etc.And along with the continuous progress of science and technology, many increases are lived, and electronic product is also simultaneously constantly progressive easily, the technology of satellite navigation is also advanced by leaps and bounds thereupon, and satellite navigation manufacturer is in order to attract the function of the continuous improving product of consumer demand, as adjusted for aspects such as navigation quality, operation interface, display frame, body sizes, this wherein, compact satellite navigator has obtained popular welcome.
But in recent years, along with constantly bringing forth new ideas of technology, how the space that the technology of satellite navigator own can be upgraded again, with not quite, can show one's talent in the cut-throat competition of various brands, manufacturers find that the moulded of satellite navigator is also the key of a triumph.At present, the shell of satellite navigator on the market, in when assembling, is all to adopt the coated main frame of fixed engagement, mostly with protecgulum and bonnet fixed engagement to be coated main frame.During fabrication, the shape-designing of selecting color matching, selection to present via manufacturer, and user cannot be selected according to the hobby of oneself color of the lid of collocation, or improved in moulding.
Summary of the invention
Due to the problems referred to above that prior art exists, the present invention proposes a kind of satellite navigator, and it can address the above problem.
To achieve these goals, the present invention has adopted following technical scheme:
A kind of satellite navigator, comprises that a main frame and is positioned at the lid of main frame front end, and described lid is provided with the junction surface being connected with described main frame, and the eaves portion of extending forward from junction surface; Described main frame is provided with the docking section coordinating with junction surface in order to realize the replacing of lid.
As further feature of the present invention, described lid comprises a protecgulum, a bonnet, and described eaves portion is positioned at protecgulum upside, and described main frame both sides are provided with docking section corresponding to described junction surface.
As further feature of the present invention, described docking section be draw-in groove to drawing, described junction surface is that snap fit engages, this snap fit engages in separable mode and is arranged in draw-in groove docking.
As further feature of the present invention, described docking section is magnetic docking, and described junction surface is magnetic engagement, and this magnetic engagement is arranged on magnetic to connecting in separable mode.
As further feature of the present invention, on described lid, be also provided with input block.
With respect to prior art, the invention has the advantages that: lid convenient disassembly, can be according to the hobby collocation different colours of oneself and the lid of moulding, separately can block sunlight direct projection interface, prevent that picture from presenting poor effect because of the irradiation of sunlight.
[accompanying drawing explanation]
Fig. 1 is the schematic perspective view of embodiments of the invention;
Fig. 2 is the perspective exploded view of embodiments of the invention;
Fig. 3 is the perspective exploded view of another embodiment of the present invention.
[embodiment]
As depicted in figs. 1 and 2, satellite navigator of the present invention, has lid 2 and main frame 1, on this lid 2, is evenly provided with some junction surfaces 4 with the joining place of main frame 1, and these lid 2 upsides are outward extended with an eaves portion 3; Main frame 1 is being provided with docking section 5 with the joining place of lid 2 corresponding to junction surface 4.
Junction surface 4 can be made as snap fit joint, magnetic engagement, be threadedly engaged with or fastener joint, and 5 of docking sections are made as draw-in groove docking, magnetic docking, screw docking and fastener docking accordingly.
Lid 2 can be located at main frame 1 also can be located at above main frame 1 after, the corresponding rear side that only docking section on main frame 15 need be located to main frame 1.
Shown in Fig. 3 is the perspective exploded view of another embodiment of the present invention.Figure Satellite navigation schematic diagram comprises protecgulum 7, bonnet 6 and main frame 1, be all evenly provided with some junction surfaces 4, and protecgulum 7 upsides is outward extended with an eaves portion 3 on protecgulum 7 He on bonnet 6 with the joining place of main frame 1; The convergence part of main frame 1 both sides and protecgulum 7 and bonnet 6 is provided with docking section 5 corresponding to junction surface 4.On protecgulum 7, be also provided with some input blocks 8.
Eaves portion 3 extends to main frame 1 is outside, and and main frame 1 between there is suitable distance.In the time that user uses satellite navigator and be subject to sunlight direct irradiation, can be by eaves portion 3 block sunlight.To prevent that picture is because being subject to solar radiation to cause picture to present not good problem.The input signal of input block 8 can transfer to main frame 1 via transport interface and use.
Owing to dismantling, user can carry out according to the hobby of oneself collocation of color and moulding, neither affects the normal use of satellite navigator, has tried to please again the vision of oneself.
But above-mentioned embodiment is exemplary, be to be the restriction that this patent is comprised to scope in order better to make those skilled in the art can understand this patent, can not to be interpreted as; As long as any being equal to done according to spirit that this patent discloses changes or modify, all fall into the scope that this patent comprises.

Claims (5)

1. a satellite navigator, is characterized in that: comprise that a main frame and is positioned at the lid of main frame front end, described lid is provided with the junction surface being connected with described main frame, and the eaves portion of extending forward from junction surface; Described main frame is provided with the docking section coordinating with junction surface in order to realize the replacing of lid.
2. satellite navigator as claimed in claim 1, is characterized in that: described lid comprises a protecgulum, a bonnet, and described eaves portion is positioned at protecgulum upside, and described main frame both sides are provided with docking section corresponding to described junction surface.
3. satellite navigator as claimed in claim 1, is characterized in that: described docking section be draw-in groove to drawing, described junction surface is that snap fit engages, this snap fit engages in separable mode and is arranged in draw-in groove docking.
4. satellite navigator as claimed in claim 1, is characterized in that: described docking section is magnetic docking, and described junction surface is magnetic engagement, and this magnetic engagement is arranged on magnetic to connecting in separable mode.
5. satellite navigator as claimed in claim 1, is characterized in that: on described lid, be also provided with input block.
CN201210583669.9A 2012-12-30 2012-12-30 Satellite navigator Pending CN103792547A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210583669.9A CN103792547A (en) 2012-12-30 2012-12-30 Satellite navigator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210583669.9A CN103792547A (en) 2012-12-30 2012-12-30 Satellite navigator

Publications (1)

Publication Number Publication Date
CN103792547A true CN103792547A (en) 2014-05-14

Family

ID=50668405

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210583669.9A Pending CN103792547A (en) 2012-12-30 2012-12-30 Satellite navigator

Country Status (1)

Country Link
CN (1) CN103792547A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3145719U (en) * 2008-08-06 2008-10-16 徐鉦鑑 Satellite navigator
CN202305815U (en) * 2011-11-08 2012-07-04 邓伟廷 Industrial gps navigator
CN202502251U (en) * 2012-01-20 2012-10-24 上海达鑫电子有限公司 Satellite navigator with detachable cover body

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3145719U (en) * 2008-08-06 2008-10-16 徐鉦鑑 Satellite navigator
CN202305815U (en) * 2011-11-08 2012-07-04 邓伟廷 Industrial gps navigator
CN202502251U (en) * 2012-01-20 2012-10-24 上海达鑫电子有限公司 Satellite navigator with detachable cover body

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
ASS Succession or assignment of patent right

Owner name: BEIDA FANGZHENG SCIENCE + TECHNOLOGY COMPUTER SYST

Free format text: FORMER OWNER: FOUNDER TECHNOLOGY GROUP CORPORATION SUZHOU PRODUCT CO., LTD.

Effective date: 20150410

Owner name: BEIJING FOUNDER SCIENTIFIC AND TECHNOLOGICAL INFOR

Effective date: 20150410

C41 Transfer of patent application or patent right or utility model
COR Change of bibliographic data

Free format text: CORRECT: ADDRESS; FROM: 215026 SUZHOU, JIANGSU PROVINCE TO: 200120 JING AN, SHANGHAI

TA01 Transfer of patent application right

Effective date of registration: 20150410

Address after: 200120, A, room 091, block 1250, Xin Kai Road, Shanghai, Jingan District

Applicant after: Beida Fangzheng Science & Technology Computer System Co., Ltd., Shanghai

Applicant after: BEIJING FOUNDER TECHNOLOGY INFORMATION PRODUCT CO., LTD.

Applicant after: Founder Technology Group Corporation Suzhou Product Co., Ltd.

Address before: Suzhou City, Jiangsu province 215026 Suhong Suzhou Industrial Park Road No. 188

Applicant before: Founder Technology Group Corporation Suzhou Product Co., Ltd.

C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140514