CN218762330U

CN218762330U - Shock-absorbing seat of satellite navigation equipment

Info

Publication number: CN218762330U
Application number: CN202223152710.5U
Authority: CN
Inventors: 王�华; 陆倩
Original assignee: Jiangsu Ruiwei Iot Technology Co ltd
Current assignee: Jiangsu Ruiwei Iot Technology Co ltd
Priority date: 2022-11-28
Filing date: 2022-11-28
Publication date: 2023-03-28
Anticipated expiration: 2032-11-28

Abstract

The utility model discloses a satellite navigation equipment cushion socket, comprising a supporting seat, swing joint has the movable rod on the supporting seat, the internally mounted that the bottom of movable rod stretched into the supporting seat has elevating system, the top fixedly connected with base of movable rod, the internally mounted of base has damper, the last fixedly connected with damper of damper, damper's internally mounted has rotary mechanism, fixedly connected with places the board in the pivot, it adds and holds the mechanism to add to install on holding the seat. The utility model discloses a satellite navigation equipment cushion socket is provided with damping and damping spring between base and surge bin, increases the shock attenuation effect, improves the stability of base, adjusts the movable rod, can change the height of cushion socket, and application scope is wide, through holding the seat with add the cooperation between the board, can satellite navigation equipment add and hold, can install the satellite navigation equipment of different specifications, has improved the availability factor of cushion socket.

Description

Shock-absorbing seat of satellite navigation equipment

Technical Field

The utility model relates to a satellite navigation equipment technical field, in particular to satellite navigation equipment shock attenuation seat.

Background

Satellite navigation refers to the continuous transmission of radio signals from satellites to provide navigation, positioning, time service and other functions for users on the ground, in the sea, in the air and in the space. Currently, the satellite navigation systems in the world mainly include the Global Positioning System (GPS) in the united states, the GLONASS global navigation satellite system (GLONASS) in russia, the galileo satellite positioning system (GALIEO) in the european space agency, and the beidou navigation satellite positioning system (BDS) in china.

Chinese patent application with application number CN201921520313.4 just discloses a satellite navigation's fixing device, including central vacuum chuck, the fixed plate, the center principal post, spacing anticreep dish, micro vacuum pump, the symmetry holding rod, the rubber protection pad, torsional spring and fixed column, the center principal post is installed to the bearing frame upside, the terminal surface is connected with spacing anticreep dish under the center principal post, the fixed plate is installed to center principal post up end, central vacuum chuck is installed to the fixed plate up end, terminal surface left side is equipped with micro vacuum pump under the fixed plate, the not enough convenient problem is dismantled in the installation of original satellite navigation ware to this design solution, the symmetry holding rod is installed to bilateral symmetry about the back of the body frame right-hand member face, symmetry holding rod and back of the body frame junction are connected with the torsional spring, torsional spring internally mounted has the fixed column, the rubber protection pad is installed on symmetry holding rod down end face right side, this design has solved the not enough perfect problem of original satellite navigation ware safeguard measure, the utility model discloses rational in infrastructure, be convenient for installation and disassembly, the protection is effectual, use is convenient for installation

However, the existing fixing device adopting the sucking disc still has some defects, is single in structure, can only be used for installing satellite navigation equipment with one specification, has no good anti-seismic effect, is easy to damage due to vibration, and shortens the service life.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides a satellite navigation equipment shock attenuation seat, its purpose is solved the structure singleness, can only install the satellite navigation equipment of a specification, does not have good antidetonation effect, receives vibrations and is impaired easily, has shortened life scheduling problem.

In order to achieve the above-mentioned objects of the utility model, the utility model adopts the technical proposal that: the shock absorption seat for the satellite navigation equipment comprises a supporting seat, wherein a movable rod is movably connected onto the supporting seat, a lifting mechanism is installed at the bottom end of the movable rod, the bottom end of the movable rod extends into the supporting seat, a base is fixedly connected to the top end of the movable rod, the base is of a cavity structure, a shock absorption mechanism is installed inside the base, a shock absorption bin is fixedly connected onto the shock absorption mechanism, cushion pads are installed on two sides of the shock absorption bin, a rotating mechanism is installed inside the shock absorption bin, a rotating shaft is connected onto the rotating mechanism, a placing plate is fixedly connected onto the rotating shaft, clamping seats are installed on two sides of the placing plate, and clamping mechanisms are installed on the clamping seats;

the damping mechanism comprises a first fixing seat arranged inside, damping is arranged on the first fixing seat, the bottom end of the damping is connected with a second fixing seat, a damping spring is sleeved on the damping, and a damping bin is fixedly connected to the second fixing seat.

Furthermore, the damping bin is internally provided with a rotating motor, the output end of the rotating motor is connected with a first gear, the bottom end of the rotating shaft extends into the damping bin and is internally provided with a second gear, and the first gear is meshed with the second gear.

Furthermore, elevating system is including installing the lifting rack in the movable rod bottom, be connected with spacing rack between the lifting rack, the one end of spacing rack is connected with the gag lever post, be connected with the regulating box between the gag lever post, install the limiting plate on the gag lever post, be connected with lifting spring between the limiting plate, install the regulation pole on the spacing rack.

Furthermore, a through hole is arranged on the supporting column, and the adjusting rod is inserted into the through hole.

Further, add and hold the mechanism including installing the mounting panel on adding the seat, be connected with the auxiliary rod on the mounting panel, the auxiliary rod passes to add and holds the seat and be connected with to add and hold the board, add and hold and install the shock pad on the board, install the lead screw on the mounting panel, the top of lead screw is passed the mounting panel and is installed the handle.

The utility model has the advantages that:

the utility model discloses a satellite navigation equipment shock attenuation seat, be provided with damping and damping spring between base and surge bin, increase the shock attenuation effect, improve the stability of base, adjust the movable rod, can change the height of shock attenuation seat, application scope is wide, start rotating electrical machines can autogiration satellite navigation equipment, it is convenient to adjust, through adding the seat and add the cooperation between holding the board, can satellite navigation equipment add and hold, can install the satellite navigation equipment of different specifications, the availability factor of shock attenuation seat is improved, the lead screw adds to hold and has replaced traditional bolt fastening simultaneously, simple to operate has effectually solved when maintaining or changing, consume a large amount of time, influence work efficiency.

Drawings

Fig. 1 is a sectional view of a shock mount of a satellite navigation device according to the present invention;

fig. 2 is an enlarged view of a position a in fig. 1 of the shock-absorbing seat of the satellite navigation device of the present invention.

Reference symbol comparison table:

1. a supporting seat; 101. a through hole; 2. a movable rod; 3. a lifting mechanism; 301. a lifting rack; 302. a limiting rack; 303. a limiting rod; 304. an adjusting box; 305. a limiting plate; 306. a lift spring; 307. adjusting a rod; 4. a base; 5. a damping mechanism; 501. a first fixed seat; 502. damping and damping; 503. a second fixed seat; 504. a damping spring; 6. a damping bin; 7. a cushion pad; 8. a rotation mechanism; 801. a rotating electric machine; 802. a first gear; 803. a second gear; 9. placing the plate; 10. a clamping seat; 11. a clamping mechanism; 1101. mounting a plate; 1102. an auxiliary lever; 1103. a holding plate; 1104. a shock pad; 1105. a screw rod; 1106. a handle; 12. a rotating shaft.

Detailed Description

The following describes the present invention with reference to the accompanying drawings. In which like parts are designated by like reference numerals.

It should be noted that the terms "front," "back," "left," "right," "upper" and "lower" used in the following description refer to directions in the drawings, and the terms "inner" and "outer" refer to directions toward and away from, respectively, the geometric center of a particular component.

In order to make the content of the present invention more clearly understood, the technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the attached drawings in the embodiment of the present invention.

As shown in fig. 1 to 2, the shock absorbing seat for the satellite navigation equipment comprises a supporting seat 1, wherein a movable rod 2 is movably connected to the supporting seat 1, a lifting mechanism 3 is installed inside the supporting seat 1, the bottom end of the movable rod 2 extends into the supporting seat 1, a base 4 is fixedly connected to the top end of the movable rod 2, the base 4 is of a cavity structure, a shock absorbing mechanism 5 is installed inside the base 4, a shock absorbing bin 6 is fixedly connected to the shock absorbing mechanism 5, cushion pads 7 are installed on two sides of the shock absorbing bin 6, a rotating mechanism 8 is installed inside the shock absorbing bin 6, a rotating shaft 12 is connected to the rotating mechanism 8, a placing plate 9 is fixedly connected to the rotating shaft 12, clamping seats 10 are installed on two sides of the placing plate 9, and clamping mechanisms 11 are installed on the clamping seats 10;

the damping mechanism 5 comprises a first fixing seat 501 arranged inside, a damping damper 502 is arranged on the first fixing seat 501, the bottom end of the damping damper 502 is connected with a second fixing seat 503, a damping spring 504 is sleeved on the damping damper 502, and a damping cabin 6 is fixedly connected to the second fixing seat 503.

Specifically, when receiving vibrations, the shock attenuation storehouse 6 can atress compress downwards to promote shock attenuation damping 502 displacement downwards, shock attenuation damping 502 atress compresses, thereby alleviates the impact force that shock attenuation storehouse 6 brought, and then weakens satellite navigation equipment and receives the shaking force, and blotter 7 adopts the rubber material, can play the effect of a buffering through blotter 7, prevents that satellite navigation equipment from receiving the shaking force and damaging.

The interior of the damping bin 6 is provided with a rotating motor 801, the output end of the rotating motor 801 is connected with a first gear 802, the bottom end of the rotating shaft 12 extends into the interior of the damping bin 6 and is provided with a second gear 803, and the first gear 802 is meshed with the second gear 803.

Specifically, the rotating motor 801 is started, and the first gear 802 rotates, so that the second gear 803 is driven to rotate, the placing plate 9 on the rotating shaft 12 is driven to rotate, and the adjustment is convenient.

Elevating system 3 is connected with spacing rack 302 including installing lifting rack 301 in 2 bottoms of movable rod between lifting rack 301, and the one end of spacing rack 302 is connected with gag lever post 303, is connected with regulating box 304 between the gag lever post 303, installs limiting plate 305 on the gag lever post 303, is connected with lifting spring 306 between the limiting plate 305, installs regulation pole 307 on the spacing rack 302.

The supporting seat 1 is provided with a through hole 101, and the adjusting rod 307 is inserted into the through hole 101.

Specifically, the adjusting rod 307 is pressed, the limiting rack 302 stretches, the limiting rod 303 extrudes the lifting spring 306, the lifting rack 301 is separated from the limiting rack 302, the adjusting movable rod 2 slides on the supporting seat 1 to adjust the height, the adjusting rod 307 is loosened after adjustment is completed, and the lifting spring 306 pushes the limiting plate 305, so that the lifting rack 301 is meshed with the limiting rack 302.

The clamping mechanism 11 comprises a mounting plate 1101 mounted on the clamping base 10, an auxiliary rod 1102 is connected to the mounting plate 1101, the auxiliary rod 1102 is connected with a clamping plate 1103 through the clamping base 10, a shock absorption pad 1104 is mounted on the clamping plate 1103, a lead screw 1105 is mounted on the mounting plate 1101, and a handle 1106 is mounted at the top end of the lead screw 1105 through the mounting plate 1101.

Specifically, rotating handle 1106, lead screw 1105 rotates, drives mounting panel 1101 displacement to drive auxiliary rod 1102 and add and hold board 1103 displacement, fix satellite navigation equipment, can install the satellite navigation equipment of different specifications, improved the availability factor of shock attenuation seat, replace traditional bolt fastening through adding satellite navigation equipment, simple to operate, effectual solution when maintaining or changing, consumed a large amount of time, improved work efficiency.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not intended to limit the present invention, and all modifications, equivalents, improvements and the like that are made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims

1. The shock absorption seat for the satellite navigation equipment comprises a support seat (1) and is characterized in that a movable rod (2) is movably connected onto the support seat (1), a lifting mechanism (3) is installed inside the support seat (1) and extends into the bottom end of the movable rod (2), a base (4) is fixedly connected to the top end of the movable rod (2), the base (4) is of a cavity structure, a shock absorption mechanism (5) is installed inside the base (4), a shock absorption bin (6) is fixedly connected onto the shock absorption mechanism (5), cushion pads (7) are installed on two sides of the shock absorption bin (6), a rotating mechanism (8) is installed inside the shock absorption bin (6), a rotating shaft (12) is connected onto the rotating mechanism (8), a placing plate (9) is fixedly connected onto the rotating shaft (12), clamping seats (10) are installed on two sides of the placing plate (9), and clamping mechanisms (11) are installed on the clamping seats (10);

damper (5) are including installing fixing base (501) in inside, install damping (502) on the fixing base (501), the bottom of damping (502) is connected with fixing base two (503), the cover is equipped with damping spring (504) on damping (502), fixedly connected with shock attenuation storehouse (6) on fixing base two (503).

2. The satellite navigation device damper of claim 1, wherein: shock attenuation storehouse (6) internally mounted has rotating electrical machines (801), the output of rotating electrical machines (801) is connected with gear one (802), the internally mounted that the bottom of pivot (12) stretched into shock attenuation storehouse (6) has gear two (803), gear one (802) and gear two (803) mesh mutually.

3. The satellite navigation device damper of claim 1, wherein: elevating system (3) is including installing lifting rack (301) in movable rod (2) bottom, be connected with spacing rack (302) between lifting rack (301), the one end of spacing rack (302) is connected with gag lever post (303), be connected with regulating box (304) between gag lever post (303), install limiting plate (305) on gag lever post (303), be connected with lifting spring (306) between limiting plate (305), install regulation pole (307) on spacing rack (302).

4. The satellite navigation equipment shock mount of claim 3, wherein: the supporting seat (1) is provided with a through hole (101), and the adjusting rod (307) is inserted into the through hole (101).

5. The satellite navigation device damper of claim 1, wherein: the clamping mechanism (11) comprises a mounting plate (1101) mounted on a clamping base (10), an auxiliary rod (1102) is connected to the mounting plate (1101), the auxiliary rod (1102) penetrates through the clamping base (10) to be connected with a clamping plate (1103), a shock absorption pad (1104) is mounted on the clamping plate (1103), a screw rod (1105) is mounted on the mounting plate (1101), and a handle (1106) is mounted on the top end of the screw rod (1105) through the mounting plate (1101).