Rotary hinge device for installing solar panel
By designing the solar windsurfing plate to install a rotary hinge device, the traditional expansion mechanism is solved, the problems of large size, heavy weight, complex structure and easy damage are solved, and the windsurfing plate is stable, safe and efficiently deployed, and the secondary expansion and good heat dissipation are supported.
Patent Information
- Application Number
- CN202411769705.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-04
- Publication Date
- 2025-02-11
- Estimated Expiration
- 2044-12-04
AI Technical Summary
Traditional solar windsurfing panel deployment mechanisms have problems such as huge size, heavy weight, complex structure, high cost, and easy damage caused by interference when unfolding windsurfing panels.
Design a solar windsurfing plate installation rotary hinge device, including a hinge body and a windsurfing plate fixture, which forms a hinge fit with the hinge body through a rotary joint to support the secondary expansion of the windsurfing plate, and prevent interference during the expansion process through a time-sequential torsion spring. collision.
It realizes stable installation of solar windsurfing, strong bearing capacity and simple structure, avoids interference damage during windsurfing, and supports the secondary expansion needs of windsurfing, and provides exhaust or liquid discharge channels to achieve good heat dissipation.
Smart Images

Figure CN119408734A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of hinges, and in particular to a solar panel mounting rotary hinge device. Background Art
[0002] With the continuous development of aerospace technology, the demand for energy of spacecraft is increasing day by day. As the main energy supply device of spacecraft, the performance of solar panels directly affects the operating efficiency and life of spacecraft. Traditional solar panel deployment mechanisms often have problems such as large size, heavy weight, complex structure, high cost, and the panels are easily damaged due to mutual interference during deployment.
[0003] Therefore, developing a new type of solar panel secondary deployment hinge to achieve a safer, more efficient and economical solar panel deployment process has become a technical problem that needs to be urgently solved in the current aerospace technology field. Summary of the invention
[0004] In view of the defects in the prior art, the purpose of the present invention is to provide a solar panel mounting rotary hinge device, which can stably mount the solar panel, has the characteristics of strong bearing capacity and simple structure, and can avoid damage due to interference when the panel is unfolded. It can also be connected to the exhaust or drainage pipeline to implement good heat dissipation.
[0005] The technical solution adopted by the present invention is: a solar panel installation rotary hinge device, comprising a hinge body and a panel holder; hinge platforms are provided at both ends of the hinge body, connecting platforms are provided at both ends of the panel holder, the hinge platforms and the connecting platforms are connected by a rotary joint, so that the panel holder can rotate around the hinge platform, and a hinge torsion spring cooperating with the hinge platform and the connecting platform is sleeved on the rotary joint; a timing torsion spring is also provided at the outer end of one of the connecting platforms, and a control section fixed to the panel holder is provided at the end of the timing torsion spring;
[0006] An exhaust valve is provided on the end face of one of the articulated platforms, and an exhaust channel and a connecting channel are interconnected inside the exhaust valve. The connecting channel is connected to the connecting platform through a rotating joint, and an exhaust groove is provided on the side wall of the exhaust channel. A sealing screw is screwed on the opening of the exhaust channel, and the sealing screw can close the exhaust channel. When the sealing screw rotates, the exhaust groove, the connecting channel and the exhaust channel can be connected.
[0007] In the present technical solution, the panel holder for installing the solar panel is hingedly matched with the hinge body through a rotating joint, and the solar panel can be rotated around the rotating joint to be unfolded or folded, thereby realizing a flexible rotational connection between the solar panel and the satellite body, and supporting the secondary unfolding requirement of the solar panel; because a timing torsion spring is provided on one of the connecting platforms, torque control can be used to ensure that the first layer of the panel is fully unfolded and reaches the predetermined position before the second layer of the panel is allowed to start unfolding, thereby preventing interference and collision during the unfolding process.
[0008] The present technical solution also has a preset exhaust structure, and the exhaust valve is installed on a hinged platform. The connecting platform can be used to connect the exhaust pipe of the satellite heat dissipation radiation panel. Since precise exhaust channels, connecting channels and exhaust grooves are provided in the exhaust valve body, when exhausting, the sealing screw is turned to the left to connect the exhaust groove, connecting channel and exhaust channel. The operation is simple, ensuring smooth discharge of gas and smooth flow of liquid and gas.
[0009] Preferably, mounting heads are provided at both ends of the rotary joint, one of which is connected to a hinge hole provided on the hinge platform, and the other is connected to a connection hole provided on the connection platform. The connection heads are hollow so that the connecting channel of the exhaust valve is connected to the rotary joint.
[0010] Preferably, the exhaust valve has an end away from the exhaust groove provided with an insertion section inserted into a hinge hole on the end face of the hinge platform, the exhaust valve has a sealing ring bulge arranged around the insertion section on its outer periphery, the sealing ring bulge has a side wall corresponding to the insertion section on one side thereof provided with an annular groove arranged around the insertion section, and an outer sealing ring is provided in the annular groove.
[0011] Preferably, an inner sealing ring is provided in the exhaust passage, and when the sealing screw seals the exhaust passage, its end face contacts the inner sealing ring.
[0012] Preferably, the outer end of the connecting platform on which the timing torsion spring is installed is connected to a torsion spring bracket, the timing torsion spring is sleeved on a mounting portion provided at the end of the torsion spring bracket, and a movable clamp for fixing the timing torsion spring is provided at the end of the mounting portion.
[0013] Preferably, fixing holes for fixing spring feet of hinge torsion springs are provided on the outer sides of the hinge platform and the connecting platform.
[0014] Preferably, fixing plates are provided at both ends of the hinge body.
[0015] Preferably, a connecting portion for connecting to the solar panel is provided on a side of the sailboard fixture away from the hinge body.
[0016] Preferably, it also includes a limiter, which includes a limit block fixed to the outside of the hinge body, and the limit block is penetrated by a limit rod arranged along the length of the windsurfing board holder, and after the windsurfing board holder is unfolded around the hinge platform, the windsurfing board holder can be against the limit rod.
[0017] The beneficial effects of the present invention are as follows: the present invention has a compact structure and can be fixedly installed on the side of the satellite structure frame to be reliably connected to the sailboard; at the same time, the rotary joint used to rotate and connect the sailboard is built into the hinge body, realizing a flexible rotation connection between the sailboard and the satellite body, and supporting the secondary deployment requirements of the sailboard. A timing control structure is also provided in the hinge to prevent interference and collision during the deployment process. When installing the sailboard, the device can limit the deployment angle of the sailboard to ensure that the deployment angle of the sailboard meets the design requirements and prevent the occurrence of over-expansion or under-expansion. The device also has a prefabricated drainage or exhaust passage inside the hinge, which can be used to connect the satellite heat dissipation radiation panel and the thermal control system to achieve efficient transmission and dissipation of heat or discharge the air in the pipeline to ensure the smoothness of liquid flow; it can be applied in the field of satellite manufacturing; it has high practical value. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] In order to more clearly illustrate the specific embodiments of the present invention or the technical solutions in the prior art, the following is a brief introduction to the drawings required for the specific embodiments or the description of the prior art. In all the drawings, similar elements or parts are generally identified by similar reference numerals. In the drawings, the elements or parts are not necessarily drawn according to the actual scale.
[0019] Figure 1 It is a schematic diagram of the assembly of a solar panel mounting rotary hinge device provided in an embodiment of the present invention.
[0020] Figure 2 A cross-sectional view of an exhaust valve of a solar panel mounting rotary hinge device provided in an embodiment of the present invention.
[0021] Figure 3 A closed stereoscopic view of a solar panel mounting rotary hinge device provided in an embodiment of the present invention.
[0022] Figure 4 It is an unfolded stereoscopic view of a solar panel mounting rotary hinge device provided in an embodiment of the present invention.
[0023] Figure numerals: hinge body 100, hinge platform 110, hinge hole 111, fixing plate 120, windsurfing board holder 200, connecting platform 210, connecting hole 211, connecting part 220, rotating joint 300, hinge torsion spring 400, timing torsion spring 500, control section 510, mounting head 600, fixing hole 700, limit block 800, torsion spring bracket 900, movable clamp 1000, exhaust valve 1200, exhaust channel 1210, connecting channel 1220, exhaust groove 1230, insertion section 1240, sealing ring convex 1250, ring groove 1260, sealing screw 1300, outer sealing ring 1400, inner sealing ring 1500. DETAILED DESCRIPTION
[0024] The following embodiments of the technical solution of the present invention are described in detail in conjunction with the accompanying drawings. The following embodiments are only used to more clearly illustrate the technical solution of the present invention, and are therefore only used as examples, and cannot be used to limit the protection scope of the present invention.
[0025] It should be noted that, unless otherwise specified, the technical terms or scientific terms used in this application should have the common meanings understood by those skilled in the art to which the present invention belongs.
[0026] like Figures 1 to 3 As shown, a specific embodiment of the present invention provides a solar panel mounting rotary hinge device, which is used to connect a satellite and a solar panel to ensure that the solar panel can be stably unfolded or folded; it specifically includes a hinge body 100 and a panel holder 200; hinge bodies 110 are provided at both ends of the hinge body 100, connecting platforms 210 are provided at both ends of the panel holder 200, and the hinge bodies and connecting platforms 210 are connected by a rotary joint 300, so that the panel holder 200 can rotate around the hinge bodies 110, and the rotary joint 300 is provided with a hinge torsion spring 400 that cooperates with the hinge bodies 110 and the connecting platforms 210; a timing torsion spring 500 is also provided at the outer end of one of the connecting platforms 210, and a control section 510 fixed to the panel holder 200 is provided at the end of the timing torsion spring 500.
[0027] like Figures 1 to 3As shown, through the above arrangement, the panel holder 200 for installing the solar panel in this embodiment is hingedly matched with the hinge body 100 through the rotating joint 300, and the solar panel can be rotated around the rotating joint 300 to be unfolded or folded, thereby realizing a flexible rotation connection between the solar panel and the satellite body, and supporting the secondary unfolding requirement of the solar panel. Since a timing torsion spring 500 is provided on one of the connecting platforms 210, the control section 510 of the timing torsion spring 500 is connected to the windsurfing board holder 200, and can generate a certain torque for the hinge to unfold, thereby ensuring through torque control that the first layer of windsurfing board is fully unfolded and reaches a predetermined position before the second layer of windsurfing board is allowed to begin to unfold, thereby preventing interference and collision during the unfolding process. In order to install the timing torsion spring 500 on the connecting platform 210, a torsion spring bracket 900 is connected to the outer end of the connecting platform 210 on which the timing torsion spring 500 is installed, and the timing torsion spring 500 is sleeved on a mounting portion provided at the end of the torsion spring bracket 900, and a movable clamp 1000 for fixing the timing torsion spring is provided at the end of the mounting portion, so that the timing torsion spring can be installed through the torsion spring bracket, and it is prevented from falling off under the fixing action of the movable clamp.
[0028] like Figures 1 to 3 As shown, in actual application, the hinge body 100 and each structure on the sailboard fixture 200 are made of light and high-strength materials, so that the device can be reliably connected to the solar sailboard after being fixedly installed on the side of the satellite structure frame.
[0029] like Figures 1 to 3 As shown, in order to connect the rotary joint 300 with the hinged platform 110 and the connecting platform 210, the present embodiment has mounting heads 600 at both ends of the rotary joint 300, one mounting head 600 is connected to the hinged hole 111 provided on the hinged platform 110, and the other mounting head 600 is connected to the connecting hole 211 provided on the connecting platform 210. In this way, the rotary joint 300 can be connected to the hinged hole 111 and the connecting hole 211 through the mounting heads 600.
[0030] like Figures 1 to 3 As shown, the hinge torsion spring 400 provided on the rotary joint 300 needs to cooperate with the hinge platform 110 and the connecting platform 210. In this embodiment, a fixing hole 700 for fixing the spring foot of the hinge torsion spring 400 is provided on the outer side of the hinge platform 110 and the connecting platform 210. In this way, the spring foot of the hinge torsion spring 400 can be inserted into a corresponding fixing hole 700, thereby generating a torsion force to ensure that the hinge body 100 and the windsurfing fixture 200 form a hinged assembly.
[0031] like Figures 1 to 3As shown, this embodiment also provides fixing plates 120 at both ends of the hinge body 100, and the hinge body 100 can be installed on the outside of the satellite body through the fixing plates 120; at the same time, this embodiment also provides a connecting part 220 for connecting the solar panel on the side of the panel holder 200 away from the hinge body 100; the connecting part 220 can be used to connect the solar panel structure to ensure that the panel is stably installed.
[0032] like Figures 1 to 3 As shown, in actual application, the solar panel needs to be unfolded and rotated to a fixed position. This embodiment also provides a limiter for limiting the unfolding angle of the solar panel. The limiter includes a limit block 800 fixed to the outside of the hinge body 100. The limit block 800 is provided with a limit rod arranged along the length of the sailboard fixture 200. After the sailboard fixture 200 is unfolded around the hinge platform 110, the sailboard fixture 200 can be against the limit rod. In this way, when the solar panel is unfolded, the sailboard fixture 200 can be against the limit rod. The angle limiter structure ensures the accuracy of the unfolding angle of the sailboard and prevents equipment damage caused by over-expansion or under-expansion. The limiter is specially designed to control the unfolding angle of the sailboard. Limiters of different specifications can be replaced according to the unfolding needs.
[0033] Embodiment 2
[0034] like Figures 1 to 4 As shown, the present embodiment further optimizes the solar panel mounting rotary hinge device and integrates an exhaust structure, so that the pipeline can be connected to implement efficient heat dissipation or exhaust action; specifically, an exhaust valve 1200 is provided on the end face of one of the hinged platforms 110, and the exhaust valve 1200 has an exhaust channel 1210 and a connecting channel 1220 that are interconnected. The connecting channel 1220 is connected to the connecting platform 210 through a rotary joint 300, and an exhaust groove 1230 is provided on the side wall of the exhaust channel 1210. The opening of the exhaust channel 1210 is screwed with a sealing screw 1300, and the sealing screw 1300 can close the exhaust channel 1210. When the sealing screw 1300 rotates, the exhaust groove 1230, the connecting channel 1220 and the exhaust channel 1210 can be connected.
[0035] In order to make the rotary joint 300 communicate with the communication channel 1220, the connector installed at the end of the rotary joint 300 in this embodiment is arranged hollow; in order to install the exhaust valve 1200 on the end face of the hinged platform 110, an insertion section 1240 is provided at the end of the exhaust valve 1200 away from the exhaust groove 1230, which is inserted into one of the hinge holes 111 on the end face of the hinged platform 110. The outer periphery of the exhaust valve 1200 is provided with a sealing ring protrusion 1250 arranged around the insertion section 1240. The side wall of the sealing ring protrusion 1250 corresponding to the side of the insertion section 1240 is provided with an annular groove 1260 arranged around the insertion section 1240, and an outer sealing ring is provided in the annular groove 1260. In this way, when the insertion section 1240 is inserted into the installation hole, the outer sealing ring plays a role in sealing and installing. At the same time, an inner sealing ring is provided in the exhaust channel 1210. When the sealing screw 1300 seals the exhaust channel 1210, its end face contacts the inner sealing ring. Ensure that the sealing screw 1300 has a better sealing effect when sealing the exhaust channel 1210; in production applications, the exhaust valve 1200 is made of high-strength, high-temperature-resistant polyimide material, which not only has excellent mechanical properties and thermal stability, and can maintain structural stability at extreme temperatures (-200°C to +300°C), but also because of its translucent properties, allows light to penetrate, making it easy to observe the internal state of the pipeline, improving maintenance efficiency and troubleshooting speed. The outer sealing ring and the inner sealing ring 7 are both made of highly elastic, aging-resistant silicone rubber or similar materials to ensure that good sealing performance is maintained under extreme temperature and pressure changes. The sealing screw 1300 is a device for opening and closing the exhaust channel 1210. It controls gas emissions through rotation adjustment, and uses high-strength alloy materials to ensure that it has sufficient strength.
[0036] When the whole device is in use, the hinge structure is connected to the exhaust or liquid discharge pipeline on the satellite heat radiation plate through the connection hole 211 on the connection platform 210, so as to realize the efficient transmission and dissipation of heat and exhaust the air in the pipeline to ensure the smooth flow of liquid. The design of the exhaust valve 1200 improves the thermal management efficiency of the satellite and ensures that the internal equipment of the satellite operates at a suitable temperature.
[0037] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or replace some or all of the technical features therein by equivalents. These modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions of the embodiments of the present invention, and they should all be included in the scope of the claims and specification of the present invention.
Claims
1. A solar panel mounting rotary hinge device, characterized in that: It comprises a hinge body (100) and a windsurfing board fixing device (200); The hinge body (100) is provided with hinged platforms (110) at both ends, and the windsurfing fixture (200) is provided with connecting platforms (210) at both ends. The hinged platform (110) and the connecting platform (210) are connected via a rotating joint (300) so that the windsurfing fixture (200) can rotate around the hinged platform (110). The rotating joint (300) is provided with a hinge torsion spring (400) that cooperates with the hinged platform (110) and the connecting platform (210). A timing torsion spring (500) is fixed to the outer end of one of the connecting platforms (110), and a control section (510) fixed to the windsurfing fixture (200) is provided at the end of the timing torsion spring (500). An exhaust valve (1200) is provided on the end surface of one of the hinged platforms (110), wherein the exhaust valve (1200) has an exhaust channel (1210) and a communication channel (1220) that are interconnected, wherein the communication channel (1220) is connected to the connection platform (210) via a rotary joint (300), an exhaust groove (1230) is provided on the side wall of the exhaust channel (1210), and a sealing screw (1300) is screwed to the opening of the exhaust channel (1210), wherein the sealing screw (1300) can close the exhaust channel (1210), and when the sealing screw (1300) is rotated, the exhaust groove (1230), the communication channel (1220) and the exhaust channel (1210) can be connected.
2. The solar panel mounting rotary hinge device according to claim 1, characterized in that: Mounting heads (600) are provided at both ends of the rotary joint (300), one of the mounting heads (600) being connected to a hinge hole (111) provided on a hinge platform (110), and the other mounting head (600) being connected to a connection hole (211) provided on a connection platform (210), and the connection heads are arranged hollow so that a communication channel (1220) of the exhaust valve (1200) is connected to the rotary joint (300).
3. The solar panel mounting rotary hinge device according to claim 2, characterized in that: An insertion section (1240) is provided at one end of the exhaust valve (1200) away from the exhaust groove (1230) and is inserted into a hinge hole (111) on the end face of one of the hinge platforms (110); a sealing ring protrusion (1250) arranged around the insertion section (1240) is provided on the outer periphery of the exhaust valve (1200); a ring groove (1260) arranged around the insertion section (1240) is provided on the side wall of the sealing ring protrusion (1250) corresponding to the insertion section (1240); an outer sealing ring (1400) is provided in the ring groove (1260).
4. The solar panel mounting rotary hinge device according to claim 1, characterized in that: An inner sealing ring (1500) is provided in the exhaust passage (1210); when the sealing screw (1300) seals the exhaust passage (1210), its end surface contacts the inner sealing ring (1500).
5. The solar panel mounting rotary hinge device according to claim 1, characterized in that: The outer sides of the hinge platform (110) and the connecting platform (210) are provided with fixing holes (700) for fixing the spring feet of the hinge torsion spring (400).
6. The solar panel mounting rotary hinge device according to claim 1, characterized in that: The outer end of the connection platform (110) on which the timing torsion spring (500) is installed is connected to a torsion spring bracket (900); the timing torsion spring (500) is sleeved on a mounting portion provided at the end of the torsion spring bracket (900); and a movable clamp (1000) for fixing the timing torsion spring (500) is provided at the end of the mounting portion.
7. The solar panel mounting rotary hinge device according to claim 1, characterized in that: Fixed plates (120) are provided at both ends of the hinge body (100).
8. The solar panel mounting rotary hinge device according to claim 1, characterized in that: A connecting portion (220) for connecting to a solar panel is provided on a side of the sailboard fixing device (200) away from the hinge body (100).
9. The solar panel mounting rotary hinge device according to any one of claims 1 to 8, characterized in that: The invention also comprises a limiter, wherein the limiter comprises a limit block (800) fixed to the outside of the hinge body (100), and the limit block (800) is provided with a limit rod arranged along the length direction of the windsurfing board holder (200). After the windsurfing board holder (200) is unfolded around the hinge platform (110), the windsurfing board holder (200) can abut against the limit rod.
Citation Information
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