CN213043622U

CN213043622U - Satellite is with solar panel convenient to installation

Info

Publication number: CN213043622U
Application number: CN202021286056.5U
Authority: CN
Inventors: 黄静桦
Original assignee: Individual
Current assignee: Yan'an Baota Xingkong Application Technology Co ltd
Priority date: 2020-07-03
Filing date: 2020-07-03
Publication date: 2021-04-23
Anticipated expiration: 2030-07-03

Abstract

The utility model relates to a solar panel technical field just discloses a satellite is with solar panel convenient to installation, which comprises a supporting plate and i, one side of extension board is provided with the support, one side through connection of support has the storage pipe, the one end fixed mounting who stores the pipe has link an, link an keeps away from the one end fixed mounting who stores the pipe and has frame an, frame an's inside is provided with the solar panel body. The device can be through connecing bolt and screw hole soon, accomplish the fixed to the solar panel body, through connect threaded rod and nut soon, accomplish this device and satellite surface's fixed, and the satellite launches after the space, because the material of link an and link b is memory metal, link an and link b receive sun exposure, after the temperature reaches the certain degree, will be according to preset's shape, expand the solar panel body, the completion is to the collection and the power supply of solar energy, this application simple to operate, the practicality of prior art has effectively been improved.

Description

Satellite is with solar panel convenient to installation

Technical Field

The utility model relates to a solar panel technical field specifically is a satellite is with solar panel convenient to installation.

Background

The artificial satellite is an unmanned spacecraft which runs around the earth on a space orbit, basically moves around the earth according to the laws of celestial body mechanics, but is influenced by a non-spherical earth gravitational field, atmospheric resistance, solar attraction, lunar attraction and light pressure on different orbits, the actual movement situation is very complex, the artificial satellite is the spacecraft which has the largest emission quantity, the widest application and the fastest development, the emission quantity of the artificial satellite accounts for more than 90 percent of the total emission quantity of the spacecraft, and the solar panel is a device for collecting solar energy, is usually arranged on the surface of the satellite in the field of aviation and supplies power to the satellite by using the solar energy.

The prior art has the following technical problems:

1. when the existing satellite solar panel is used, a complex mechanical structure is required to be utilized to fold and unfold the solar support, so that the cost is high, and the installation is inconvenient.

2. When the existing satellite solar panel is used, the related wires connected with the solar panel are exposed outside, so that the wires are easily wound with other objects, and certain potential safety hazards exist.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a satellite is with solar panel convenient to installation possesses advantages such as simple to operate and be convenient for accomodate the wire, has solved the inconvenient problem that has the potential safety hazard of solar panel installation and wire exposure among the prior art.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a satellite is with solar panel convenient to installation, includes the extension board, one side of extension board is provided with the support, one side through connection of support has the storage tube, the one end fixed mounting who stores the tube has link a, link a keeps away from the one end fixed mounting who stores the tube has frame a, frame a's inside is provided with the solar panel body, the equal fixed mounting in both sides of solar panel body has a piece, two the both sides of a piece all are provided with the limiting plate, the equal activity through connection in both ends of limiting plate one side has the bolt, the screw hole that is located corresponding piece one side is seted up to the one end of bolt.

Preferably, the limiting plate is hinged to the frame a through hinges at two ends of one side, far away from the solar panel body.

Preferably, one end of the frame a is fixedly provided with a connecting frame b, the other end of the connecting frame b is fixedly provided with a frame b, and the frame b and the frame a have the same structure.

Preferably, the insides of the connecting frame a, the connecting frame b, the frame a and the frame b are all cavities, one end of the accommodating pipe is communicated with one side of the connecting frame a, the other side of the connecting frame a is communicated with one side of the frame a, two sides of the connecting frame b are respectively communicated with one side of the frame a and one side of the frame b, and the connecting frame a and the connecting frame b are made of memory metal.

Preferably, threaded rods are fixedly mounted at two ends of one side, away from the frame a, of the support, the threaded rods movably penetrate through one side to the other side of the support plate, and nuts are screwed on one sides, away from the support, of the outer surfaces of the threaded rods.

Preferably, the threaded hole extends from one side of the fulcrum to the other side.

Preferably, one end of the accommodating pipe, which is far away from the connecting frame a, is fixedly penetrated through one side of the support plate to the other side.

Compared with the prior art, the utility model provides a satellite is with solar panel convenient to installation possesses following beneficial effect:

1. when the solar panel is used, firstly, the threaded structure between the bolt and the support block is utilized to place the solar panel body in the frame a or the frame b, the bolt penetrates through the limiting plate and is screwed with the threaded hole to complete the fixation of the solar panel body, then, the threaded rod penetrates through the support plate, the support is fixed on the support plate by utilizing the nut, then, the support plate is fixed on the surface of the satellite, after the satellite is emitted to the space, because the material of the connection frame a and the connection frame b is memory metal, the connection frame a and the connection frame b are irradiated by the sun, and after the temperature reaches a certain degree, the frame a and the frame b are unfolded according to the preset shape, thereby expand the solar panel body, accomplish collection and the power supply to solar energy, this application simple to operate, simple structure has effectively improved prior art's practicality.

2. This solar panel for satellite installation of being convenient for, through, when using, when placing the circuit with the solar panel body promptly, can will accomodate the fixed surface that runs through the satellite of pipe in advance, then penetrate the circuit in accomodating, and enter into in frame an and the frame b through link an and link b, and wear out from frame an and frame b's interior week and be connected with the solar panel body, thereby reach the purpose of hiding the wire of accomodating, effectively improved prior art's practicality.

Drawings

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

fig. 2 is an expanded top view of the frame a of the present invention;

fig. 3 is a schematic perspective view of the solar panel body of the present invention.

Wherein: 1. a support plate; 2. a support; 3. receiving a tube; 4. a connecting frame a; 5. a frame a; 6. A solar panel body; 7. supporting a block; 8. a limiting plate; 9. a bolt; 10. a threaded hole; 11. a hinge; 12. a connecting frame b; 13. a frame b; 14. a threaded rod; 15. and a nut.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, a solar panel for satellite installation comprises a support plate 1, one side of extension board 1 is provided with support 2, one side through connection of support 2 has accomodate pipe 3, the one end fixed mounting who accomodates pipe 3 has link a4, accomodate pipe 3 and keep away from one side to the opposite side that link a 4's one end was fixed to run through extension board 1, link a4 keeps away from the one end fixed mounting who accomodates pipe 3 has frame a5, the equal fixed mounting in both ends that frame a5 one side was kept away from to support 2 has threaded rod 14, two equal activities of threaded rod 14 run through one side to the opposite side of extension board 1, the equal threaded connection in one side that support 2 was kept away from to two threaded rod 14 surfaces has nut 15, the inside of frame a5 is provided with solar panel body 6, the equal fixed mounting in both sides of solar panel body 6 has a piece 7, the both sides of two piece 7 all are provided with limiting plate 8, limiting plate 8 is articulated with frame a 5. Both ends of one side of the limiting plate 8 are movably connected with bolts 9 in a penetrating mode, one end of each bolt 9 is provided with a threaded hole 10 located on one side of the corresponding supporting block 7, the threaded holes 10 extend from one side of the supporting block 7 to the other side, one end of the frame a5 is fixedly provided with a connecting frame b12, the other end of the connecting frame b12 is fixedly provided with a frame b13, the frame b13 and the frame a5 are identical in structure, the interiors of the connecting frame a4, the connecting frame b12, the frame a5 and the frame b13 are all cavities, one end of the accommodating pipe 3 is communicated with one side of the connecting frame a4, the other side of the connecting frame a4 is communicated with one side of the frame a5, two sides of the connecting frame b12 are respectively communicated with one side of the frame a5 and one side of the frame b13, and the connecting frame a 58.

When the solar energy collecting and supplying device is used, firstly, the solar panel body 6 is placed in the frame a5 or the frame b13 by using the thread structure between the bolt 9 and the support block 7, then the bolt 9 penetrates through the limit plate 8 and is screwed with the thread hole 10 to complete the fixing of the solar panel body 6, then the thread rod 14 penetrates through the support plate 1, the bracket 2 is fixed on the support plate 1 by using the nut 15, then the support plate 1 is fixed on the surface of a satellite, after the satellite is launched into space, because the material of the connection frame a4 and the connection frame b12 is memory metal, the connection frame a4 and the connection frame b12 are irradiated by the sun, after the temperature reaches a certain degree, the frame a5 and the frame b13 are unfolded according to the preset shape, so that the solar panel body 6 is unfolded to complete the collection and the supplying of solar energy, and when a circuit with the solar panel body 6 is placed, the receiving pipe 3 can be fixed on the surface, then the circuit is penetrated into the containing pipe 3, enters into the frame a5 and the frame b13 through the connecting frame a4 and the connecting frame b12, and penetrates out from the inner peripheries of the frame a5 and the frame b13 to be connected with the solar panel body 6, so that the purpose of hiding and containing wires is achieved, and the practicability of the prior art is effectively improved.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a satellite is with solar panel convenient to installation, includes extension board (1), its characterized in that: one side of extension board (1) is provided with support (2), one side through connection of support (2) has accomodate pipe (3), the one end fixed mounting who accomodates pipe (3) has link a (4), the one end fixed mounting who accomodates pipe (3) is kept away from in link a (4) has frame a (5), the inside of frame a (5) is provided with solar panel body (6), the equal fixed mounting in both sides of solar panel body (6) has a piece (7), two the both sides of a piece (7) all are provided with limiting plate (8), the equal activity through connection in both ends of limiting plate (8) one side has bolt (9), screw hole (10) that are located corresponding piece (7) one side are seted up to the one end of bolt (9).

2. The solar panel for satellite easy installation according to claim 1, wherein: the limiting plate (8) is hinged with the frame a (5) through hinges (11) which are far away from two ends of one side of the solar panel body (6).

3. The solar panel for satellite easy installation according to claim 1, wherein: one end fixed mounting of frame a (5) has link b (12), the other end fixed mounting of link b (12) has frame b (13), frame b (13) is the same with the structure of frame a (5).

4. A solar panel for satellite easy installation according to claim 3, wherein: the inside of link a (4), link b (12), frame a (5) and frame b (13) is the cavity, the one end of accomodating pipe (3) and the one side intercommunication of link a (4), the opposite side of link a (4) and the one side intercommunication of frame a (5), the both sides of link b (12) communicate with the one side of frame a (5) and the one side of frame b (13) respectively, link a (4) and link b (12) are memory metal and make.

5. The solar panel for satellite easy installation according to claim 1, wherein: the support (2) keep away from the equal fixed mounting in both ends on one side of frame a (5) has threaded rod (14), two one side to the opposite side of extension board (1) is all run through in threaded rod (14) activity, two the equal threaded connection in one side that support (2) were kept away from to threaded rod (14) surface has nut (15).

6. The solar panel for satellite easy installation according to claim 1, wherein: the threaded hole (10) extends from one side of the support block (7) to the other side.

7. The solar panel for satellite easy installation according to claim 1, wherein: one end of the accommodating pipe (3) far away from the connecting frame a (4) is fixedly penetrated through one side to the other side of the support plate (1).