A new architecture for space solar energy conversion and transmission

Abstract

The present invention discloses a new architecture for realizing space solar energy conversion and transmission, the top surface of the mounting seat is connected to the unfolding and storing assembly through a connecting assembly, side spring hinges are installed on both sides of the main frame and the auxiliary frame, and mounting frames are symmetrically installed on both sides of the top spring hinge, the outer sides of the main frame and the auxiliary frame are wrapped with a silver-plated layer, a hemisphere is movably placed inside the polytetrafluoroethylene tube, the opposite sides of the heat conducting plate on the same side are bonded with polyethylene clips, and a protective receiving assembly is arranged inside the mounting seat. The polyethylene clip of the present invention melts at high temperature, and the main frame, the auxiliary frame and the mounting frame automatically unfold after the main frame is separated from the clamping plate, which is easy to fold and transport, and the wire is clamped in the wire clamping groove of the hemisphere, and the hemisphere slides in the polyethylene clip. During use, there is a gap between the outer side of the wire and the inner wall of the main frame and the auxiliary frame, and the wire does not directly contact the main frame and the auxiliary frame. The silver-plated layer blocks heat radiation, reduces the influence of heat on the wire, and ensures normal power generation.

Description

Technical Field

[0001] The present invention relates to the field of space solar energy technology, and in particular to a new architecture for realizing space solar energy conversion and transmission. Background Art

[0002] Solar energy is generated by the continuous nuclear fusion reactions of sunspots within and on the surface of the sun. Space solar power stations, built in unobstructed space, are unaffected by atmospheric conditions, seasonal variations, and diurnal fluctuations, resulting in a high specific energy density. If constructed in geosynchronous orbit, space solar power stations offer the most efficient use of solar energy.

[0003] Most of the existing space solar power station plans considered placing the power station in synchronous Earth orbit and using microwaves to transmit energy to the ground. This has the disadvantages of difficult construction, high launch costs, low transmission efficiency, huge temperature differences in space, and the solar power station wires and other structures are easily damaged by temperature differences, affecting the power generation effect, among other technical issues. Summary of the Invention

[0004] The present invention provides a new architecture for realizing space solar energy conversion and transmission, which can effectively solve the problems proposed in the above background technology that the power station is deployed in the synchronous earth orbit and uses microwaves to transmit energy to the ground. The construction is difficult, the launch cost is high, the transmission efficiency is low, and the temperature difference in space is huge. The structures such as the wires of the solar power station are easily damaged by the temperature difference, which affects the power generation effect.

[0005] To achieve the above object, the present invention provides the following technical solutions, including:

[0006] Connecting assembly, the mounting bar is installed inside the disassembly frame and can be disassembled by loosening the positioning screws. The disassembly is convenient. The main frame rotates in the guide hole under the action of the torsion spring, and the limit card is embedded in the limit groove and fixed, and is used in conjunction with the unfolding storage assembly;

[0007] The storage assembly is unfolded. The main frame, auxiliary frame, and installation frame automatically unfold after the main frame is detached from the clamping plate. The wires are clamped in the wire clamping grooves in the hemisphere. The hemisphere slides in the polyethylene clamping strip. During use, there is a gap between the outer side of the wires and the inner walls of the main frame and auxiliary frame. The silver-plated layer blocks heat radiation.

[0008] Protective receiving component, the converter is installed inside the embedded slot. When the device enters space, the internal and external air pressures are different, the sealing plug slides along the pressure-stabilizing hole, and the connecting spring deforms until the internal and external air pressures are the same. The sealing plug will return to its original position and continue to block the pressure-stabilizing hole.

[0009] Preferably, the top surface of the mounting seat is connected to an unfolding and storing assembly via a connecting assembly, and the unfolding and storing assembly includes a main frame, a secondary frame, a side spring hinge, a top spring hinge, a mounting frame, a solar cell panel, a silver-plated layer, a polytetrafluoroethylene tube, a hemisphere, a wire clip groove, an anti-slip gasket, a snap groove, a snap strip, a snap plate, a heat conducting plate, a polyethylene clip strip, and a wire hole;

[0010] The top surface of the mounting seat is symmetrically mounted with a main frame through a connecting assembly, and one side of the main frame is connected to the sub-frame in sequence, and side spring hinges are installed on both sides of the main frame and the sub-frame, and a top spring hinge is symmetrically mounted on the top of the sub-frame, and wire holes are opened in the middle of the side spring hinge and the top spring hinge, and the mounting frames are symmetrically mounted on both sides of the top spring hinge, and the solar cell panel is fixedly clamped inside the mounting frame, and the outer sides of the main frame and the sub-frame are wrapped with a silver-plated layer. A polytetrafluoroethylene tube is inlaid inside the main frame and the sub-frame, and a hemisphere is movably placed inside the polytetrafluoroethylene tube, and a wire clamping groove is opened in the middle of the hemisphere, and an anti-slip gasket is bonded inside the wire clamping groove, a clamping groove is opened at one end of the hemisphere, and a clamping strip is welded on the other end of the hemisphere, and a clamping plate is symmetrically bonded at the top surface of the mounting seat corresponding to the main frame, a heat conducting plate is bonded on one side of the clamping plate, and polyethylene clamping strips are bonded on the opposite sides of the heat conducting plate on the same side.

[0011] Preferably, the main frame and the sub-frame have the same size and are both rectangular frames formed by folding hollow tubes.

[0012] Preferably, the snap-fit ​​groove and the snap-fit ​​strip fit together, and the two hemispheres are a round sphere with a central opening.

[0013] Preferably, the clamping plate and the heat conducting plate have the same size, and the end face of the polyethylene clamping strip is a right triangle.

[0014] Preferably, the connecting assembly includes a disassembly frame, screw holes, positioning screws, a mounting bar, positioning holes, guide holes, a support bar, a support spring, a limit card, a limit slot and a torsion spring;

[0015] A disassembly frame is symmetrically welded on the top surface of the mounting seat, screw holes are evenly opened on the side surfaces of the disassembly frame, positioning screws are installed inside the screw holes, a mounting bar is movably connected to the inside of the disassembly frame, a positioning hole is opened on the mounting bar near the screw hole, a guide hole is opened in the middle of the mounting bar, a support bar is slidably installed inside the guide hole, a support spring is evenly spot-welded on the top surface of the support bar, the top surface of the support bar fits the bottom end of the main frame, a limit card is welded on the top end of the positioning hole, a limit slot is opened at the bottom end of the main frame corresponding to the limit card, and torsion springs are fixedly sleeved on both ends of the main frame near the disassembly frame.

[0016] Preferably, the inner wall of the disassembly frame fits the outer side of the mounting bar, and the diameter of the screw hole is equal to the diameter of the positioning hole.

[0017] Preferably, the width of the guide hole is equal to the outer diameter of the main frame, the bottom end of the torsion spring is overlapped with the top end of the main frame, the limit card fits into the limit groove, and the end face of the limit card is an isosceles triangle.

[0018] Preferably, a protective receiving assembly is provided inside the mounting seat, and the protective receiving assembly includes an embedding groove, a sealing ring, a pressure-stabilizing hole, a sealing plug, a connecting spring, an outer plate, a buffer layer, an inner plate and a converter;

[0019] An embedding groove is provided at the bottom end of the mounting seat, a sealing ring is welded to the bottom edge of the embedding groove, pressure-stabilizing holes are evenly provided on the bottom surface of the sealing ring, a sealing plug is movably installed inside the pressure-stabilizing hole, the top surface of the sealing plug is welded to the bottom end of the connecting spring, the top of the connecting spring is spot-welded to the top surface of the embedding groove, an outer plate is inlaid at the bottom end of the sealing ring, a buffer layer is bonded to the top surface of the outer plate, an inner plate is bonded to the top surface of the buffer layer, and a converter is clamped between the top surface of the inner plate and the top surface of the embedding groove.

[0020] Preferably, the edge of the top surface of the sealing plug is rounded, and the diameter of the sealing plug is equal to the diameter of the pressure-stabilizing hole.

[0021] Compared with the prior art, the present invention has the following beneficial effects:

[0022] 1. It is equipped with an unfolding and storage component. The polyethylene clip melts at high temperature. The main frame, sub-frame and installation frame automatically unfold after the main frame is separated from the clamping plate, making it easy to fold and transport. The wires are clamped in the wire clamping groove in the hemisphere. The hemisphere slides in the polyethylene clip. During use, there is a gap between the outer side of the wire and the inner wall of the main frame and sub-frame. The wires do not directly contact the main frame and sub-frame. The silver plating layer blocks heat radiation, reducing the impact of heat on the wires and ensuring normal power generation.

[0023] Low-Earth orbit space solar power stations can be combined with traditional communications and earth observation satellites, which can effectively reduce the construction cost of low-Earth orbit space solar power stations and improve resource utilization efficiency; medium-Earth orbit solar power stations mainly focus on energy forwarding and have relatively low construction costs; in the future, according to needs, a certain number of stratospheric airship receiving stations can be built on the ground, and a space solar photovoltaic station can be used to correspond to several airship receiving stations. According to the different time and geographical needs of human energy, distributed deployment can be carried out in time and space, which can effectively reduce construction costs and improve the utilization efficiency of solar power stations.

[0024] 2. A connecting component is provided, and the mounting bar is installed inside the disassembly frame. It can be disassembled by loosening the positioning screws. It is easy to disassemble, so that it is easy to disassemble and install and change its position. The main frame rotates in the guide hole under the action of the torsion spring, and the limit card is embedded in the limit groove and fixed. It is used in conjunction with the unfolding storage component to fix its position, making the unfolding storage component more stable after unfolding.

[0025] 3. A protective receiving component is provided, and the converter is installed inside the embedded slot. When the device enters space, the air pressure inside and outside is different. The sealing plug slides along the pressure-stabilizing hole, and the connecting spring deforms until the air pressure inside and outside is the same. The sealing plug will return to its original position and continue to block the pressure-stabilizing hole. The outer plate, buffer layer and inner plate protect the internal structure.

[0026] In summary, the unfolding and storage component is the main power generation component of the power station, the connecting component is used in conjunction with the unfolding and storage component to make it more stable after unfolding, and the protective receiving component is used to balance the air pressure and protect the internal structure to enable it to operate normally. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] The accompanying drawings are used to provide further understanding of the present invention and constitute a part of the specification. They are used to explain the present invention together with the embodiments of the present invention and do not constitute a limitation of the present invention.

[0028] In the attached figure:

[0029] Figure 1 It is a structural schematic diagram of the present invention;

[0030] Figure 2 It is a structural schematic diagram of the connection assembly of the present invention;

[0031] Figure 3 This invention Figure 1 Schematic diagram of the A region structure;

[0032] Figure 4 This is a schematic diagram of the installation structure of the polytetrafluoroethylene tube of the present invention;

[0033] Figure 5 This invention Figure 4 Schematic diagram of the structure of region B;

[0034] Figure 6 It is a structural schematic diagram of the connection assembly of the present invention;

[0035] Figure 7 It is a structural diagram of the protective receiving assembly of the present invention;

[0036] Numbers in the figure: 1, mounting seat;

[0037] 2. Connecting assembly; 201. Disassembly frame; 202. Screw hole; 203. Positioning screw; 204. Mounting bar; 205. Positioning hole; 206. Guide hole; 207. Support bar; 208. Support spring; 209. Limiting card; 210. Limiting slot; 211. Torsion spring;

[0038] 3. Expandable storage assembly; 301. Main frame; 302. Sub-frame; 303. Side spring hinge; 304. Top spring hinge; 305. Mounting frame; 306. Solar panel; 307. Silver coating; 308. PTFE tube; 309. Hemisphere; 310. Wire slot; 311. Anti-slip pad; 312. Snap-in slot; 313. Snap-in strip; 314. Snap-in plate; 315. Heat conducting plate; 316. Polyethylene snap-in strip; 317. Wire hole;

[0039] 4. Protective receiving assembly; 401. Embedded groove; 402. Sealing ring; 403. Voltage-stabilizing hole; 404. Sealing plug; 405. Connecting spring; 406. Outer plate; 407. Buffer layer; 408. Inner plate; 409. Converter. DETAILED DESCRIPTION

[0040] The preferred embodiments of the present invention are described below with reference to the accompanying drawings. It should be understood that the preferred embodiments described herein are only used to illustrate and explain the present invention, and are not used to limit the present invention.

[0041] Example: Figure 1 As shown, the present invention provides a new architecture technology solution for realizing space solar energy conversion and transmission, including:

[0042] Connecting assembly 2, the mounting bar 204 is installed inside the disassembly frame 201, and can be disassembled by loosening the positioning screw 203. The disassembly is convenient. The main frame 301 rotates in the guide hole 206 under the action of the torsion spring 211, and the limit card 209 is embedded in the limit groove 210 for fixation, and is used in conjunction with the unfolding storage assembly 3;

[0043] The storage assembly 3 is unfolded. The main frame 301, the sub-frame 302, and the installation frame 305 are automatically unfolded after the main frame 301 is separated from the clamping plate 314. The wires are clamped in the wire clamping groove 310 in the hemisphere 309. The hemisphere 309 slides in the polyethylene clamping strip 316. During use, there is a gap between the outer side of the wires and the inner walls of the main frame 301 and the sub-frame 302. The silver coating 307 blocks heat radiation.

[0044] The protective receiving component 4 and the converter 409 are installed inside the embedded slot 401. When the device enters space, the air pressure inside and outside is different. The sealing plug 404 slides along the pressure-stabilizing hole 403, and the connecting spring 405 deforms until the air pressure inside and outside is the same. The sealing plug 404 will return to its original position and continue to block the pressure-stabilizing hole 403.

[0045] like Figure 2-5 As shown, the top surface of the mounting base 1 is connected to the unfolding and storing assembly 3 through the connecting assembly 2. The unfolding and storing assembly 3 includes a main frame 301, a secondary frame 302, a side spring hinge 303, a top spring hinge 304, a mounting frame 305, a solar cell panel 306, a silver-plated layer 307, a polytetrafluoroethylene tube 308, a hemisphere 309, a wire clamping groove 310, an anti-slip gasket 311, a clamping groove 312, a clamping strip 313, a clamping plate 314, a heat conducting plate 315, a polyethylene clamping strip 316, and a wire hole 317.

[0046] The top surface of the mounting base 1 is symmetrically mounted with a main frame 301 through a connecting assembly 2, and a sub-frame 302 is connected to one side of the main frame 301 in turn. The main frame 301 and the sub-frame 302 are of the same size and are both rectangular frames folded from hollow tubes, which are convenient for passing wires inside. Side spring hinges 303 are mounted on both sides of the main frame 301 and the sub-frame 302, and a top spring hinge 304 is symmetrically mounted on the top of the sub-frame 302. Wire holes 317 are provided in the middle of the side spring hinge 303 and the top spring hinge 304, and mounting frames 305 are symmetrically mounted on both sides of the top spring hinge 304. A solar cell panel 306 is fixedly connected to the mounting frame 305. The outside of the main frame 301 and the sub-frame 302 are wrapped with a silver-plated layer 307. Polytetrafluoroethylene tubes 308 are inlaid inside the main frame 301 and the sub-frame 302, and the polytetrafluoroethylene tubes 308 are movable inside. A hemisphere 309 is placed, a wire clamping groove 310 is opened in the middle of the hemisphere 309, and an anti-slip gasket 311 is bonded inside the wire clamping groove 310, a clamping groove 312 is opened at one end of the hemisphere 309, and a clamping strip 313 is welded to the other end of the hemisphere 309, the clamping groove 312 and the clamping strip 313 fit together, the two hemispheres 309 are a round ball with a central opening, which is convenient for placing the hemisphere 309 for fixing the wires into the polytetrafluoroethylene tube 308, and a clamping plate 314 is symmetrically bonded to the top surface of the mounting seat 1 corresponding to the main frame 301, and a heat conducting plate 315 is bonded to one side of the clamping plate 314. The clamping plate 314 and the heat conducting plate 315 are the same size, and the end face of the polyethylene clamping strip 316 is a right triangle, which is convenient for clamping the main frame 301 and the sub-frame 302, and the opposite sides of the heat conducting plate 315 on the same side are bonded with polyethylene clamping strips 316.

[0047] like Figure 6 As shown, the connection assembly 2 includes a disassembly frame 201, a screw hole 202, a positioning screw 203, a mounting bar 204, a positioning hole 205, a guide hole 206, a support bar 207, a support spring 208, a limit card 209, a limit slot 210 and a torsion spring 211;

[0048] The top surface of the mounting seat 1 is symmetrically welded with a disassembly frame 201, and screw holes 202 are evenly opened on the side of the disassembly frame 201. Positioning screws 203 are installed inside the screw holes 202. A mounting strip 204 is movably connected to the inside of the disassembly frame 201. A positioning hole 205 is opened on the mounting strip 204 near the screw hole 202. The inner wall of the disassembly frame 201 fits the outer side of the mounting strip 204. The diameter of the screw hole 202 is equal to the diameter of the positioning hole 205, which is convenient for the positioning screw 203 to pass through the screw hole 202 and squeeze the positioning hole 205. A guide hole 206 is opened in the middle of the mounting strip 204, and a support is slidably installed inside the guide hole 206. The top surface of the support strip 207 is evenly spot-welded with a support spring 208. The top surface of the support strip 207 fits the bottom end of the main frame 301. The top of the positioning hole 205 is welded with a limit card 209. The bottom end of the main frame 301 is provided with a limit slot 210 corresponding to the limit card 209. The width of the guide hole 206 is equal to the outer diameter of the main frame 301. The bottom end of the torsion spring 211 is overlapped with the top end of the main frame 301. The limit card 209 fits the limit slot 210, and the end face of the limit card 209 is an isosceles triangle, which is convenient for the limit card 209 to clamp and fix the main frame 301. The torsion springs 211 are fixedly sleeved at both ends of the main frame 301 near the disassembly frame 201.

[0049] like Figure 7 As shown, a protective receiving assembly 4 is provided inside the mounting base 1, and the protective receiving assembly 4 includes an embedding groove 401, a sealing ring 402, a pressure-stabilizing hole 403, a sealing plug 404, a connecting spring 405, an outer plate 406, a buffer layer 407, an inner plate 408 and a converter 409;

[0050] An embedding groove 401 is provided at the bottom end of the mounting seat 1, and a sealing ring 402 is welded to the bottom edge of the embedding groove 401. Pressure-stabilizing holes 403 are evenly provided on the bottom surface of the sealing ring 402. A sealing plug 404 is movably installed inside the pressure-stabilizing hole 403. The edge of the top surface of the sealing plug 404 is rounded, and the diameter of the sealing plug 404 is equal to the diameter of the pressure-stabilizing hole 403, so that the sealing plug 404 can close the pressure-stabilizing hole 403. The top surface of the sealing plug 404 is welded to the bottom end of the connecting spring 405, and the top end of the connecting spring 405 is spot-welded to the top surface of the embedding groove 401. The bottom end of the sealing ring 402 is inlaid with an outer plate 406, and a buffer layer 407 is bonded to the top surface of the outer plate 406. The top surface of the buffer layer 407 is bonded to an inner plate 408, and a converter 409 is clamped between the top surface of the inner plate 408 and the top surface of the embedding groove 401.

[0051] The working principle and use process of the present invention are as follows: when the mounting base 1 is installed at the bottom of the main frame 301, it is a medium earth orbit space solar power station (20,000 kilometers), and a laser receiver and transmitter are installed inside the mounting base 1. When the mounting base 1 is installed at the top of the main frame 301, it is a low earth orbit space solar power station (such as 1,000 kilometers), and a device for converting electricity into laser is installed inside the mounting base 1. The outer side of the wire is sleeved with a sphere formed by the merger of two hemispheres 309. The wire passes through the wire clamping groove 310 and is squeezed and fixed by the anti-slip gasket 311. The wire and the hemisphere 309 are sent into the polytetrafluoroethylene tube 308 of the main frame 301 and the sub-frame 302, and are straightened so that the wire does not directly contact the inner wall of the polytetrafluoroethylene tube 308. The frame 301 passes through the guide hole 206, the mounting bar 204 is embedded in the disassembly frame 201, the positioning screw 203 passes through the screw hole 202 and squeezes the inside of the positioning hole 205 to fix the mounting bar 204, then the solar panel 306 in the mounting frame 305 is rotated and folded into the sub-frame 302 with the top spring hinge 304 as the center, and then the multiple sub-frames 302 and the main frame 301 are folded with the side spring hinge 303 as the center, and then the edges of the stacked sub-frames 302 and main frame 301 are embedded between the polyethylene clip 316 in the clamping plate 314 and the heat conducting plate 315. At this time, the bottom end of the main frame 301 moves downward along the guide hole 206, the limit clip 209 disengages from the limit slot 210, and the support spring 208 contracts;

[0052] After being sent into space, the air pressure inside and outside are different, the sealing plug 404 slides along the pressure-stabilizing hole 403, and the connecting spring 405 deforms until the air pressure inside and outside is the same. The sealing plug 404 will return to its original position and continue to block the pressure-stabilizing hole 403. The outer plate 406, the buffer layer 407 and the inner plate 408 protect the internal structure. The polyethylene card strip 316 melts under high temperature. After the main frame 301, the sub-frame 302 and the installation frame 305 are separated from the clamping plate 314, the side spring hinge 303 and the top spring The hinge 304 automatically unfolds, and at this time the torsion spring 211 drives the main frame 301 to rotate, the support spring 208 pushes the support bar 207 upward, and the limit card 209 is engaged with the inside of the limit slot 210 until it bends and unfolds. During use, there is a gap between the outer side of the wire and the inner wall of the main frame 301 and the sub-frame 302, and the wire does not directly contact the main frame 301 and the sub-frame 302. The silver-plated layer 307 blocks heat radiation, reducing the impact of heat on the wire and ensuring normal power generation.

[0053] A solar power station operating in low Earth orbit (1,000 km) converts solar energy into laser energy through an energy converter. This energy is then transmitted to a transponder at a space solar power station in medium Earth orbit (20,000 km). The medium Earth orbit space solar power station then transmits its own generated energy and the energy it transmits via laser to an airship in the stratosphere (e.g., 15 km). The laser energy collector on the airship then uses microwaves to transmit the energy to a ground-based distribution station, which converts the microwaves into electrical energy. This electricity then enters the national power grid. Low Earth orbit space solar power stations can be integrated with traditional communications and Earth observation satellites, effectively reducing the construction cost of low Earth orbit space solar power stations and improving resource utilization efficiency. Medium Earth orbit solar power stations primarily rely on energy forwarding, making them relatively inexpensive to build. In the future, a certain number of stratospheric airship receiving stations could be built on the ground, based on needs. This could be achieved by pairing one space solar photovoltaic station with several airship receiving stations. This distributed deployment, tailored to the varying temporal and regional needs of human energy, would effectively reduce construction costs and improve the efficiency of solar power stations.

[0054] In summary, the unfolding and storing component 3 is the main power generation component of the power station, the connecting component 2 is used in conjunction with the unfolding and storing component 3 to make it more stable after unfolding, and the protective receiving component 4 is used to balance the air pressure and protect the internal structure to enable it to operate normally.

[0055] Finally, it should be noted that the above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art will be able to modify the technical solutions described in the aforementioned embodiments or substitute equivalents for some of the technical features. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of the present invention shall be included within the scope of protection of the present invention.

Claims

1. A new architecture for space solar energy conversion and transmission, characterized by: include: A connecting assembly (2), the connecting assembly (2) comprising a disassembly frame (201); A disassembly frame (201) is symmetrically welded on the top surface of the mounting seat (1), screw holes (202) are evenly opened on the side of the disassembly frame (201), positioning screws (203) are installed inside the screw holes (202), and a mounting bar (204) is movably connected inside the disassembly frame (201), and a positioning hole (205) is opened near the screw hole (202) on the mounting bar (204), and a guide hole (206) is opened in the middle of the mounting bar (204), and the guide hole (20 6) A support bar (207) is slidably installed inside, and a support spring (208) is evenly spot-welded on the top surface of the support bar (207). The top surface of the support bar (207) is in contact with the bottom end of the main frame (301). A limit card (209) is welded on the top end of the positioning hole (205). A limit slot (210) is provided at the bottom end of the main frame (301) corresponding to the limit card (209). Torsion springs (211) are fixedly sleeved at both ends of the main frame (301) near the disassembly frame (201); The mounting bar (204) is installed inside the disassembly frame (201) and can be disassembled by loosening the positioning screw (203). The disassembly is convenient. The main frame (301) rotates in the guide hole (206) under the action of the torsion spring (211). The limit card (209) is embedded in the limit groove (210) and fixed, and is used in conjunction with the unfolding storage component (3). An unfolding and storing component (3), wherein the top surface of the mounting seat (1) is connected to the unfolding and storing component (3) via a connecting component (2), and the unfolding and storing component (3) comprises a main frame (301); A main frame (301) is symmetrically mounted on the top surface of the mounting seat (1) through a connecting assembly (2), a sub-frame (302) is sequentially connected to one side of the main frame (301), side spring hinges (303) are mounted on both sides of the main frame (301) and the sub-frame (302), a top spring hinge (304) is symmetrically mounted on the top of the sub-frame (302), a wire hole (317) is provided in the middle of the side spring hinge (303) and the top spring hinge (304), mounting frames (305) are symmetrically mounted on both sides of the top spring hinge (304), a solar cell panel (306) is fixedly connected to the inside of the mounting frame (305), the outer sides of the main frame (301) and the sub-frame (302) are both wrapped with a silver-plated layer (307), and the main frame (301) and the sub-frame (302) are both symmetrically mounted on the top of the sub-frame (302). A polytetrafluoroethylene tube (308) is embedded inside the frame (301) and the sub-frame (302), a hemisphere (309) is movably placed inside the polytetrafluoroethylene tube (308), a wire clamping groove (310) is provided in the middle of the hemisphere (309), an anti-slip gasket (311) is bonded inside the wire clamping groove (310), a clamping groove (312) is provided at one end of the hemisphere (309), a clamping strip (313) is welded at the other end of the hemisphere (309), a clamping plate (314) is symmetrically bonded to the top surface of the mounting seat (1) corresponding to the main frame (301), a heat conducting plate (315) is bonded to one side of the clamping plate (314), and polyethylene clamping strips (316) are bonded to the opposite sides of the heat conducting plates (315) on the same side; The main frame (301), the auxiliary frame (302) and the installation frame (305) are automatically unfolded after the main frame (301) is separated from the clamping plate (314), the wire is clamped in the clamping groove (310) in the hemisphere (309), the hemisphere (309) slides in the polyethylene clamping strip (316), and during use, there is a gap between the outer side of the wire and the inner wall of the main frame (301) and the auxiliary frame (302), and the silver-plated layer (307) blocks heat radiation; The protective receiving component (4) and the converter (409) are installed inside the embedded groove (401). When the device enters space, the internal and external air pressures are different, the sealing plug (404) slides along the pressure-stabilizing hole (403), and the connecting spring (405) is deformed until the internal and external air pressures are the same. The sealing plug (404) will return to its original position and continue to block the pressure-stabilizing hole (403).

2. A new architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: The main frame (301) and the sub-frame (302) have the same size and are both rectangular frames formed by folding hollow tubes.

3. The novel architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: The snap-fit ​​groove (312) and the snap-fit ​​strip (313) fit together, and the two hemispheres (309) are a sphere with a central opening.

4. The novel architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: The clamping plate (314) and the heat conducting plate (315) have the same size, and the end face of the polyethylene clamping strip (316) is a right triangle.

5. The novel architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: The inner wall of the disassembly frame (201) is in contact with the outer side of the installation strip (204), and the diameter of the screw hole (202) is equal to the diameter of the positioning hole (205).

6. The novel architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: The width of the guide hole (206) is equal to the outer diameter of the main frame (301), the bottom end of the torsion spring (211) is overlapped with the top end of the main frame (301), the limit card (209) fits into the limit groove (210), and the end face of the limit card (209) is an isosceles triangle.

7. The novel architecture for realizing space solar energy conversion and transmission according to claim 1, characterized in that: A protective receiving assembly (4) is provided inside the mounting seat (1), and the protective receiving assembly (4) includes an embedding groove (401), a sealing ring (402), a pressure-stabilizing hole (403), a sealing plug (404), a connecting spring (405), an outer plate (406), a buffer layer (407), an inner plate (408), and a converter (409); An embedding groove (401) is provided at the bottom end of the mounting seat (1), a sealing ring (402) is welded to the bottom edge of the embedding groove (401), a pressure stabilizing hole (403) is uniformly provided on the bottom surface of the sealing ring (402), a sealing plug (404) is movably installed inside the pressure stabilizing hole (403), the top surface of the sealing plug (404) is welded to the bottom end of the connecting spring (405), the top of the connecting spring (405) is spot-welded to the top surface of the embedding groove (401), an outer plate (406) is inlaid at the bottom end of the sealing ring (402), a buffer layer (407) is bonded to the top surface of the outer plate (406), an inner plate (408) is bonded to the top surface of the buffer layer (407), and a converter (409) is clamped between the top surface of the inner plate (408) and the top surface of the embedding groove (401).

8. The novel architecture for realizing space solar energy conversion and transmission according to claim 7, characterized in that: The top edge of the sealing plug (404) is rounded, and the diameter of the sealing plug (404) is equal to the diameter of the pressure-stabilizing hole (403).

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