CN213093282U

CN213093282U - Satellite navigation does not have magnetism battery

Info

Publication number: CN213093282U
Application number: CN202021586658.2U
Authority: CN
Inventors: 王立平; 赵志勇; 陈威
Original assignee: Shenzhen Powercom Electronics Co ltd
Current assignee: Shenzhen Powercom Electronics Co ltd
Priority date: 2020-07-31
Filing date: 2020-07-31
Publication date: 2021-04-30
Anticipated expiration: 2030-07-31

Abstract

The utility model relates to the technical field of batteries, in particular to a satellite navigation non-magnetic battery, which reduces the damage of vibration to the battery through the elasticity of a plurality of groups of springs, thereby reducing the failure rate of the non-magnetic battery; the battery comprises a battery and a plurality of groups of series plates, wherein the rear ends of the plurality of groups of series plates are connected with the front end of the battery, and the interior of the battery does not contain free nickel, cobalt and other magnetic substances; still include shell, multiunit spring, the first connecting plate of multiunit and multiunit second connecting plate, the shell covers the battery cage with the inside of shell, and the both ends of multiunit spring are connected with the surface of the lateral wall in the shell and battery respectively through the first connecting plate of multiunit and multiunit second connecting plate.

Description

Satellite navigation does not have magnetism battery

Technical Field

The utility model relates to a technical field of battery especially relates to a satellite navigation does not have magnetism battery.

Background

As is well known, with the development of economy and science and the trend of human beings to the space, the aerospace technology is rapidly developed, wherein the satellite occupies a very important position in the aerospace field, the artificial earth satellite has wide application and various varieties, and comprises a space communication satellite, a space remote sensing earth resource satellite, a space meteorological satellite, a space navigation satellite, a space reconnaissance satellite, a space broadcasting satellite, a space geodesic satellite, a space astronomical satellite and the like, and the satellite navigation nonmagnetic battery is an auxiliary device for providing energy for satellite navigation and is widely used in the field of batteries; the conventional satellite navigation non-magnetic battery comprises a battery and a plurality of groups of series plates, wherein the rear ends of the plurality of groups of series plates are connected with the front end of the battery, and the battery does not contain magnetic substances such as free nickel, cobalt and the like; when the non-magnetic battery for the existing satellite navigation is used, the non-magnetic battery for the existing satellite navigation is found in use, the vibration in a satellite is frequent, and the failure rate of the non-magnetic battery is high.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problem, the utility model provides a through the elasticity of multiunit spring, reduce the injury that vibrations caused to the battery to reduce the satellite navigation of the fault rate of no magnetic battery and do not have magnetic battery.

The utility model discloses a satellite navigation does not have magnetism battery, including battery and multiunit series connection board, the rear end of multiunit series connection board all is connected with the front end of battery to the inside of battery does not contain magnetic substance such as free nickel, cobalt; still include shell, multiunit spring, the first connecting plate of multiunit and multiunit second connecting plate, the shell covers the battery cage with the inside of shell, and the both ends of multiunit spring are connected with the surface of the lateral wall in the shell and battery respectively through the first connecting plate of multiunit and multiunit second connecting plate.

The utility model discloses a satellite navigation does not have magnetic battery, still includes the heat preservation shell, and the heat preservation shell is located the inside of shell to the heat preservation shell covers the battery cage with the inside of heat preservation shell, and the surface of heat preservation shell is connected with the side of the first connecting plate of multiunit.

The utility model discloses a no magnetic battery of satellite navigation still includes that the top of base is connected with the bottom of shell to the base is made for epoxy glass fiber material, and the top of base is provided with the multiunit fixed orifices.

The utility model discloses a no magnetism battery of satellite navigation still includes first rings, second rings, third rings and fourth rings, and the bottom of first rings, second rings, third rings and fourth rings all is connected with the top of shell.

The utility model discloses a satellite navigation does not have magnetic battery still includes multiunit welded plate, and the bottom of multiunit welded plate all is connected with the top of base, and the side of multiunit welded plate all is connected with the surface of shell.

The utility model discloses a no magnetic battery of satellite navigation still includes first fixed plate, the second fixed plate, first support, the second support, the third support, the fourth support, the first solar charging panel of multiunit and multiunit second solar charging panel, the side of first fixed plate and second fixed plate is respectively through first support, the second support, third support and fourth support are connected with the left end and the right-hand member of shell respectively, the rear end of the first solar charging panel of multiunit and multiunit second solar charging panel is connected with the front end of first fixed plate and second fixed plate respectively.

Compared with the prior art, the beneficial effects of the utility model are that: through the elasticity of multiunit spring, reduce the damage that vibrations caused to electric battery to reduce the fault rate of no magnetism battery.

Drawings

Fig. 1 is a schematic front sectional view of the present invention;

fig. 2 is a schematic front view of the present invention;

FIG. 3 is a schematic view of the front view section of the present invention;

in the drawings, the reference numbers: 1. a battery; 2. a series plate; 3. a housing; 4. a spring; 5. a first connecting plate; 6. a second connecting plate; 7. a heat preservation shell; 8. a base; 9. a first hanging ring; 10. a second hoisting ring; 11. a third hoisting ring; 12. a fourth hoisting ring; 13. welding the plate; 14. a first fixing plate; 15. a second fixing plate; 16. a first bracket; 17. a second bracket; 18. a third support; 19. a fourth bracket; 20. a first solar charging panel; 21. and a second solar charging panel.

Detailed Description

The following detailed description of the embodiments of the present invention is provided with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.

As shown in fig. 1 to 3, the satellite navigation non-magnetic battery of the present invention comprises a battery 1 and a plurality of series plates 2, wherein the rear ends of the plurality of series plates 2 are connected to the front end of the battery 1, and the battery 1 does not contain magnetic materials such as free nickel and cobalt; the battery pack is characterized by further comprising a shell 3, a plurality of groups of springs 4, a plurality of groups of first connecting plates 5 and a plurality of groups of second connecting plates 6, wherein the shell 3 covers the battery 1 and the inside of the shell 3, and two ends of the plurality of groups of springs 4 are respectively connected with the side wall in the shell 3 and the surface of the battery 1 through the plurality of groups of first connecting plates 5 and the plurality of groups of second connecting plates 6; through the elasticity of multiunit spring 4, reduce the damage that vibrations caused to battery 1 to reduce the fault rate of no magnetism battery.

The satellite navigation non-magnetic battery of the utility model also comprises a heat preservation shell 7, wherein the heat preservation shell 7 is positioned inside the shell 3, the heat preservation shell 7 covers the battery 1 and the heat preservation shell 7, and the surface of the heat preservation shell 7 is connected with the side ends of the plurality of groups of first connecting plates 5; through setting up heat preservation shell 7, reduce the loss of the inside temperature of heat preservation shell 7 to improve the practicality of no magnetism battery.

The satellite navigation non-magnetic battery of the utility model also comprises a base 8 whose top end is connected with the bottom end of the shell 3, and the base 8 is made of epoxy glass fiber material, and the top end of the base 8 is provided with a plurality of groups of fixing holes; through setting up base 8, conveniently be fixed in the working face with equipment on to improve equipment fixing's convenience.

The utility model discloses a satellite navigation does not have magnetism battery, still includes first rings 9, second rings 10, third rings 11 and fourth rings 12, and the bottom of first rings 9, second rings 10, third rings 11 and fourth rings 12 all is connected with the top of shell 3; through setting up first rings 9, second rings 10, third rings 11 and fourth rings 12, make things convenient for equipment and transportation equipment fixed connection to improve the convenience of equipment transportation.

The satellite navigation non-magnetic battery of the utility model also comprises a plurality of groups of welding plates 13, the bottom ends of the plurality of groups of welding plates 13 are all connected with the top end of the base 8, and the side ends of the plurality of groups of welding plates 13 are all connected with the surface of the shell 3; by providing a plurality of sets of welding plates 13, the stability of the housing 3 is increased, thereby improving the practicability of the device.

The utility model discloses a no magnetism battery of satellite navigation still includes first fixed plate 14, second fixed plate 15, first support 16, second support 17, third support 18, fourth support 19, multiunit first solar charging panel 20 and multiunit second solar charging panel 21, the side of first fixed plate 14 and second fixed plate 15 is connected with the left end and the right-hand member of shell 3 respectively through first support 16, second support 17, third support 18 and fourth support 19, the rear end of multiunit first solar charging panel 20 and multiunit second solar charging panel 21 is connected with the front end of first fixed plate 14 and second fixed plate 15 respectively; through setting up the first solar charging panel 20 of multiunit and multiunit second solar charging panel 21, charge for battery 1 with the electric energy of solar ray conversion to improve equipment's duration.

The utility model discloses a satellite navigation does not have magnetic battery, and it at the during operation at first reduces the loss of 7 inside temperatures of heat preservation shell through heat preservation shell 7, later through the elasticity of multiunit spring 4, reduces the injury that vibrations caused to the battery, then through the first solar charging panel 20 of multiunit and multiunit second solar charging panel 21, convert the solar ray into the electric energy and charge for the battery can.

The installation mode, the connection mode or the arrangement mode of the satellite navigation nonmagnetic battery are common mechanical modes, and the satellite navigation nonmagnetic battery can be implemented as long as the beneficial effects can be achieved; the utility model discloses a first solar charging panel of multiunit 20 and multiunit second solar charging panel 21 of no magnetic battery of satellite navigation are purchase on the market, and this technical staff only need install and operate according to its subsidiary service instruction in industry can.

The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.

Claims

1. A satellite navigation non-magnetic battery comprises a battery (1) and a plurality of groups of series plates (2), wherein the rear ends of the plurality of groups of series plates (2) are connected with the front end of the battery (1), and the battery (1) does not contain magnetic substances such as free nickel, cobalt and the like; the battery pack is characterized by further comprising a shell (3), a plurality of groups of springs (4), a plurality of groups of first connecting plates (5) and a plurality of groups of second connecting plates (6), wherein the shell (3) covers the battery (1) and the shell (3), and two ends of the plurality of groups of springs (4) are respectively connected with the inner side wall of the shell (3) and the surface of the battery (1) through the plurality of groups of first connecting plates (5) and the plurality of groups of second connecting plates (6).

2. The satellite navigation nonmagnetic battery according to claim 1, further comprising a heat preservation case (7), wherein the heat preservation case (7) is located inside the outer shell (3), and the heat preservation case (7) covers the battery (1) and the inside of the heat preservation case (7), and the surface of the heat preservation case (7) is connected with the side ends of the plurality of groups of first connection plates (5).

3. The satellite navigation nonmagnetic battery according to claim 2, further comprising a base (8) whose top end is connected with the bottom end of the shell (3), and the base (8) is made of epoxy glass fiber material, and the top end of the base (8) is provided with a plurality of groups of fixing holes.

4. The satellite navigation nonmagnetic battery according to claim 3, further comprising a first lifting ring (9), a second lifting ring (10), a third lifting ring (11) and a fourth lifting ring (12), wherein the bottom ends of the first lifting ring (9), the second lifting ring (10), the third lifting ring (11) and the fourth lifting ring (12) are all connected with the top end of the housing (3).

5. The satellite navigation nonmagnetic battery according to claim 4, further comprising a plurality of sets of welding plates (13), wherein the bottom ends of the plurality of sets of welding plates (13) are all connected with the top end of the base (8), and the side ends of the plurality of sets of welding plates (13) are all connected with the surface of the outer shell (3).

6. The satellite navigation non-magnetic battery according to claim 5, further comprising a first fixing plate (14), a second fixing plate (15), a first bracket (16), a second bracket (17), a third bracket (18), a fourth bracket (19), a plurality of sets of first solar charging plates (20) and a plurality of sets of second solar charging plates (21), wherein side ends of the first fixing plate (14) and the second fixing plate (15) are respectively connected with the left end and the right end of the housing (3) through the first bracket (16), the second bracket (17), the third bracket (18) and the fourth bracket (19), and rear ends of the plurality of sets of first solar charging plates (20) and the plurality of sets of second solar charging plates (21) are respectively connected with front ends of the first fixing plate (14) and the second fixing plate (15).