CN110823231A - Adjusting mechanism for satellite navigator and using method thereof - Google Patents
Adjusting mechanism for satellite navigator and using method thereof Download PDFInfo
- Publication number
- CN110823231A CN110823231A CN201910955896.1A CN201910955896A CN110823231A CN 110823231 A CN110823231 A CN 110823231A CN 201910955896 A CN201910955896 A CN 201910955896A CN 110823231 A CN110823231 A CN 110823231A
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- China
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- adjustment mechanism
- mounting panel
- adjusting
- satellite navigator
- disc
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/26—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for navigation in a road network
- G01C21/265—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for navigation in a road network constructional aspects of navigation devices, e.g. housings, mountings, displays
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
The invention discloses an adjusting mechanism for a satellite navigator and a using method thereof. The rotation angle adjusting mechanism can adjust the rotation angle of the satellite navigator, and the pitching angle adjusting mechanism can adjust the pitching angle of the satellite navigator, so that people can observe the picture of the satellite navigator clearly, the practicability and the use effect are improved, and the adjusting operation is simple and convenient.
Description
Technical Field
The invention relates to the technical field of navigators, in particular to an adjusting mechanism for a satellite navigator and a using method thereof.
Background
Currently, with technological progress and economic development, more people increasingly pursue transportation tools for free and convenient travel, and an automobile is one of the most common transportation tools for people, and a road network developed increasingly enables various automobile navigators to be more and more popularized; although the folding leg supporting the navigator can complete the support of the navigator, the sight of a user is far away when the user installs and looks over, the driving attention is affected, the folding leg is inconvenient to adjust according to actual needs, and the folding leg is inconvenient to adjust, so that the use of people is inconvenient.
Disclosure of Invention
The present invention is directed to solving the above problems and providing an adjustment mechanism for a satellite navigator and a method for using the same.
The invention realizes the purpose through the following technical scheme:
the adjusting mechanism for the satellite navigator comprises a fixing mechanism and a corner adjusting mechanism, wherein the corner adjusting mechanism is arranged above the fixing mechanism and connected with the fixing mechanism and used for adjusting the rotation angle of the satellite navigator, and the pitch angle adjusting mechanism is arranged on the corner adjusting mechanism and used for adjusting the pitch angle of the satellite navigator.
Preferably: every single move angle adjustment mechanism includes first mounting panel, first ear seat, two be provided with between the first ear seat first mounting panel, the shaping has first louvre on the first mounting panel, the both sides of first louvre are in the front end of first mounting panel is provided with first stopper, the rear end shaping of first mounting panel has the spacing groove, one of them the spacing inslot is provided with the bracing piece, the other end of bracing piece is provided with the second ear seat, the second ear seat with the bracing piece is through round pin hub connection, the second ear seat first ear seat all connect in corner adjustment mechanism.
So set up, pitch angle adjustment mechanism is used for adjusting the pitch angle of satellite navigation appearance.
Preferably: every single move angle adjustment mechanism includes second mounting panel, second stopper, the second stopper sets up the front end of second mounting panel, the shaping has the second louvre on the second mounting panel, the rear end of second mounting panel is provided with the connection ear seat, the rear of second mounting panel is provided with the support column, be provided with adjusting screw on the support column, the support column with the connection ear seat passes through adjusting screw connects, the support column connect in corner adjustment mechanism.
So set up, thereby through adjusting screw is right the angle of second mounting panel is adjusted, and then realizes the regulation to satellite navigation appearance's every single move angle.
Preferably: the corner adjusting mechanism comprises a disc and an arc-shaped groove, the arc-shaped groove is formed in the disc, a fastening screw is arranged in the arc-shaped groove and connected with the fixing mechanism, a handle is formed on the side face of the disc, a rotating column is arranged at the lower end of the disc, and the rotating column and the disc are integrally formed.
According to the arrangement, the rotation angle adjusting mechanism is used for adjusting the rotation angle of the satellite navigator.
Preferably: the fixing mechanism comprises a fixing seat and a connecting column, the connecting column is arranged at the lower end of the fixing seat, a sucker is arranged in the connecting column, a convex column is arranged at the upper end of the fixing seat, and the convex column and the fixing seat are integrally formed.
So set up, fixed mechanism is used for supporting the effect of fixing.
Preferably: the first mounting plate is connected with the first ear seat through a pin shaft, and the first limiting block is integrally formed with the first mounting plate.
So set up, be convenient for through round pin hub connection first mounting panel with take place to rotate between the first ear seat, it is convenient right through integrated into one piece first stopper manufacturing.
Preferably: the second mounting panel with second stopper integrated into one piece, the connecting lug seat with second mounting panel integrated into one piece.
So set up, through the manufacturing between the two of integrated into one piece convenient connection, reduce the degree of difficulty of processing.
Preferably: the fixing seat and the connecting column are integrally formed, and the sucker is connected with the connecting column through threads.
So set up, the fixing base is used for supporting the effect of installation, and is convenient through threaded connection the installation and the fixed of sucking disc.
The use method of the adjusting mechanism for the satellite navigator comprises the following steps:
a. firstly, fixing the device on a center console of an automobile through a sucker, and then fixing a satellite navigator on a first mounting plate or a second mounting plate;
b. loosening the fastening screw, pulling the handle to rotate the disc, screwing the fastening screw after rotating for a certain angle, adjusting the pitching angle of the first mounting plate, and inserting one end of the support rod into the limiting groove to support and fix after reaching a proper position;
c. or directly unscrewing the adjusting screw, manually pulling the second mounting plate to a proper pitching angle, and then tightening the adjusting screw.
Compared with the prior art, the invention has the following beneficial effects:
the rotation angle of the satellite navigator can be adjusted through the rotation angle adjusting mechanism, the pitching angle of the satellite navigator can be adjusted by the pitching angle adjusting mechanism, people can clearly observe the picture of the satellite navigator conveniently, the practicability and the using effect are improved, and the adjustment operation is simple and convenient.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a first structural schematic diagram of a first embodiment of an adjusting mechanism for a satellite navigator according to the present invention;
FIG. 2 is a second schematic structural diagram of a first embodiment of an adjusting mechanism for a satellite navigator according to the present invention;
FIG. 3 is a front view of a first embodiment of an adjustment mechanism for a satellite navigator according to the present invention;
FIG. 4 is a schematic view of a first structure of a second embodiment of an adjusting mechanism for a satellite navigator according to the present invention;
FIG. 5 is a second schematic structural diagram of a second embodiment of an adjusting mechanism for a satellite navigator according to the present invention;
FIG. 6 is a front view of a second embodiment of an adjustment mechanism for a satellite navigator according to the present invention;
fig. 7 is a schematic structural diagram of an adjusting mechanism disc for a satellite navigator, provided by the invention.
The reference numerals are explained below:
1. a fixing mechanism; 101. a fixed seat; 102. connecting columns; 103. a suction cup; 104. a convex column; 2. a corner adjusting mechanism; 201. a disc; 202. an arc-shaped slot; 203. fastening screws; 204. a handle; 205. turning the column; 3. a pitch angle adjustment mechanism; 301. a first mounting plate; 302. a first ear mount; 303. a first stopper; 304. a first heat dissipation hole; 305. a support bar; 306. a second ear mount; 307. a limiting groove; 308. a second mounting plate; 309. a second limiting block; 310. a second heat dissipation hole; 311. a support pillar; 312. connecting the ear seat; 313. and adjusting the screw.
Detailed Description
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The invention will be further described with reference to the accompanying drawings in which:
example 1
As shown in fig. 1, 2, 3, and 7, the adjusting mechanism for a satellite navigator includes a fixing mechanism 1, a corner adjusting mechanism 2 installed above the fixing mechanism 1 and connected to the fixing mechanism 1 for adjusting a rotation angle of the satellite navigator, and a pitch angle adjusting mechanism 3 installed on the corner adjusting mechanism 2 for adjusting a pitch angle of the satellite navigator.
Preferably: the pitching angle adjusting mechanism 3 comprises a first mounting plate 301 and first ear seats 302, the first mounting plate 301 is arranged between the two first ear seats 302, a first heat dissipation hole 304 is formed in the first mounting plate 301, first limiting blocks 303 are arranged at the front ends of the first mounting plate 301 on the two sides of the first heat dissipation hole 304, a limiting groove 307 is formed at the rear end of the first mounting plate 301, a supporting rod 305 is arranged in one limiting groove 307, a second ear seat 306 is arranged at the other end of the supporting rod 305, the second ear seat 306 is connected with the supporting rod 305 through a pin shaft, the second ear seat 306 and the first ear seat 302 are both connected to the corner adjusting mechanism 2, and the pitching angle adjusting mechanism 3 is used for adjusting the pitching angle of the satellite navigator; the corner adjusting mechanism 2 comprises a disc 201 and an arc-shaped groove 202, the arc-shaped groove 202 is formed in the disc 201, a fastening screw 203 is arranged in the arc-shaped groove 202, the fastening screw 203 is connected to the fixing mechanism 1, a handle 204 is formed on the side face of the disc 201, a rotating column 205 is arranged at the lower end of the disc 201, the rotating column 205 and the disc 201 are integrally formed, and the corner adjusting mechanism 2 is used for adjusting the rotating angle of the satellite navigator; the fixing mechanism 1 comprises a fixed seat 101 and a connecting column 102, the connecting column 102 is arranged at the lower end of the fixed seat 101, a sucker 103 is arranged in the connecting column 102, a convex column 104 is arranged at the upper end of the fixed seat 101, the convex column 104 and the fixed seat 101 are integrally formed, and the fixing mechanism 1 is used for supporting and fixing; the first mounting plate 301 is connected with the first lug seat 302 through a pin shaft, the first limiting block 303 is integrally formed with the first mounting plate 301, the first mounting plate 301 and the first lug seat 302 can rotate conveniently through the pin shaft connection, and the first limiting block 303 can be processed and manufactured conveniently through integral forming; fixing base 101 and spliced pole 102 integrated into one piece, sucking disc 103 passes through threaded connection with spliced pole 102, and fixing base 101 is used for supporting the effect of installation, makes things convenient for the installation and the fixed of sucking disc 103 through threaded connection.
Example 2
As shown in fig. 4, 5, 6, and 7, the adjusting mechanism for a satellite navigator includes a fixing mechanism 1, a rotation angle adjusting mechanism 2 installed above the fixing mechanism 1 and connected to the fixing mechanism 1 for adjusting a rotation angle of the satellite navigator, and a pitch angle adjusting mechanism 3 installed on the rotation angle adjusting mechanism 2 for adjusting a pitch angle of the satellite navigator.
Preferably: the pitching angle adjusting mechanism 3 comprises a second mounting plate 308 and a second limiting block 309, the second limiting block 309 is arranged at the front end of the second mounting plate 308, a second heat dissipation hole 310 is formed in the second mounting plate 308, a connecting lug seat 312 is arranged at the rear end of the second mounting plate 308, a supporting column 311 is arranged behind the second mounting plate 308, an adjusting screw 313 is arranged on the supporting column 311, the supporting column 311 is connected with the connecting lug seat 312 through an adjusting screw 313, the supporting column 311 is connected to the corner adjusting mechanism 2, the angle of the second mounting plate 308 is adjusted by adjusting the adjusting screw 313, and further the pitching angle of the satellite navigator is adjusted; the corner adjusting mechanism 2 comprises a disc 201 and an arc-shaped groove 202, the arc-shaped groove 202 is formed in the disc 201, a fastening screw 203 is arranged in the arc-shaped groove 202, the fastening screw 203 is connected to the fixing mechanism 1, a handle 204 is formed on the side face of the disc 201, a rotating column 205 is arranged at the lower end of the disc 201, the rotating column 205 and the disc 201 are integrally formed, and the corner adjusting mechanism 2 is used for adjusting the rotating angle of the satellite navigator; the fixing mechanism 1 comprises a fixed seat 101 and a connecting column 102, the connecting column 102 is arranged at the lower end of the fixed seat 101, a sucker 103 is arranged in the connecting column 102, a convex column 104 is arranged at the upper end of the fixed seat 101, the convex column 104 and the fixed seat 101 are integrally formed, and the fixing mechanism 1 is used for supporting and fixing; the second mounting plate 308 and the second limiting block 309 are integrally formed, the connecting lug seat 312 and the second mounting plate 308 are integrally formed, and the two parts are conveniently connected through integral forming, so that the processing difficulty is reduced; fixing base 101 and spliced pole 102 integrated into one piece, sucking disc 103 passes through threaded connection with spliced pole 102, and fixing base 101 is used for supporting the effect of installation, makes things convenient for the installation and the fixed of sucking disc 103 through threaded connection.
The use method of the adjusting mechanism for the satellite navigator comprises the following steps:
a. firstly, the device is fixed on a center console of an automobile through a sucking disc 103, and then a satellite navigator is fixed on a first mounting plate 301 or a second mounting plate 308;
b. loosening the fastening screw 203, pulling the handle 204 to rotate the disc 201, screwing the fastening screw 203 after rotating for a certain angle, adjusting the pitch angle of the first mounting plate 301, inserting one end of the supporting rod 305 into the limiting groove 307 to support and fix after reaching a proper position;
c. or directly unscrewing the adjusting screw 313, manually pulling the second mounting plate 308 to a proper pitch angle, and then tightening the adjusting screw 313.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed.
Claims (9)
1. A adjustment mechanism for satellite navigation appearance, including fixed establishment (1), and install fixed establishment (1) the top and connect in fixed establishment (1) is used for adjusting satellite navigation appearance's turned angle adjustment mechanism (2), its characterized in that: the satellite navigation device also comprises a pitching angle adjusting mechanism (3) which is arranged on the corner adjusting mechanism (2) and is used for adjusting the pitching angle of the satellite navigation device.
2. The adjustment mechanism for a satellite navigator according to claim 1, characterized in that: every single move angle adjustment mechanism (3) include first mounting panel (301), first ear seat (302), two be provided with between first ear seat (302) first mounting panel (301), the shaping has first louvre (304) on first mounting panel (301), the both sides of first louvre (304) are in the front end of first mounting panel (301) is provided with first stopper (303), the rear end shaping of first mounting panel (301) has spacing groove (307), one of them be provided with bracing piece (305) in spacing groove (307), the other end of bracing piece (305) is provided with second ear seat (306), second ear seat (306) with bracing piece (305) are through round pin hub connection, second ear seat (306) first ear seat (302) all connect in corner adjustment mechanism (2).
3. The adjustment mechanism for a satellite navigator according to claim 1, characterized in that: every single move angle adjustment mechanism (3) include second mounting panel (308), second stopper (309) set up the front end of second mounting panel (308), the shaping has second louvre (310) on second mounting panel (308), the rear end of second mounting panel (308) is provided with connecting ear seat (312), the rear of second mounting panel (308) is provided with support column (311), be provided with adjusting screw (313) on support column (311), support column (311) with connecting ear seat (312) pass through adjusting screw (313) are connected, support column (311) connect in corner adjustment mechanism (2).
4. The adjustment mechanism for a satellite navigator according to claim 1, characterized in that: corner adjustment mechanism (2) include disc (201), arc wall (202) shaping in disc (201), be provided with fastening screw (203) in arc wall (202), fastening screw (203) connect in fixed establishment (1), the side shaping of disc (201) has handle (204), the lower extreme of disc (201) is provided with rotary column (205), rotary column (205) with disc (201) integrated into one piece.
5. The adjustment mechanism for a satellite navigator according to claim 1, characterized in that: the fixing mechanism (1) comprises a fixing seat (101) and a connecting column (102), wherein the connecting column (102) is arranged at the lower end of the fixing seat (101), a sucker (103) is arranged in the connecting column (102), a convex column (104) is arranged at the upper end of the fixing seat (101), and the convex column (104) and the fixing seat (101) are integrally formed.
6. The adjustment mechanism for a satellite navigator according to claim 2, characterized in that: first mounting panel (301) with first ear seat (302) are through the round pin hub connection, first stopper (303) with first mounting panel (301) integrated into one piece.
7. The adjustment mechanism for a satellite navigator according to claim 3, characterized in that: the second mounting plate (308) and the second limiting block (309) are integrally formed, and the connecting lug seat (312) and the second mounting plate (308) are integrally formed.
8. The adjustment mechanism for a satellite navigator according to claim 5, characterized in that: the fixing seat (101) and the connecting column (102) are integrally formed, and the sucker (103) is connected with the connecting column (102) through threads.
9. The use method of the adjusting mechanism for the satellite navigator is characterized by comprising the following steps:
a. firstly, the device is fixed on a center console of an automobile through a sucking disc (103), and then a satellite navigator is fixed on a first mounting plate (301) or a second mounting plate (308);
b. loosening the fastening screw (203), pulling the handle (204) to enable the disc (201) to rotate, screwing the fastening screw (203) after rotating for a certain angle, adjusting the pitch angle of the first mounting plate (301), and inserting one end of the supporting rod (305) into the limiting groove (307) to support and fix after reaching a proper position;
c. or directly unscrewing the adjusting screw (313), manually pulling the second mounting plate (308) to a proper pitch angle, and then tightening the adjusting screw (313).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910955896.1A CN110823231A (en) | 2019-10-09 | 2019-10-09 | Adjusting mechanism for satellite navigator and using method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910955896.1A CN110823231A (en) | 2019-10-09 | 2019-10-09 | Adjusting mechanism for satellite navigator and using method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110823231A true CN110823231A (en) | 2020-02-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910955896.1A Pending CN110823231A (en) | 2019-10-09 | 2019-10-09 | Adjusting mechanism for satellite navigator and using method thereof |
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| Country | Link |
|---|---|
| CN (1) | CN110823231A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111873914A (en) * | 2020-07-20 | 2020-11-03 | 深圳市云智易联科技有限公司 | Multifunctional vehicle-mounted navigator |
-
2019
- 2019-10-09 CN CN201910955896.1A patent/CN110823231A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111873914A (en) * | 2020-07-20 | 2020-11-03 | 深圳市云智易联科技有限公司 | Multifunctional vehicle-mounted navigator |
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Application publication date: 20200221 |