Aircraft take-off and landing platform tracing solar power generation curtain wall

Abstract

The utility model discloses an aircraft take-off and landing platform tracing solar power generation curtain wall which comprises a curtain wall body, limiting assemblies are installed at the tops and the bottoms of the left side and the right side of the curtain wall body, and a driving assembly is installed at the bottom of the curtain wall body. The curtain wall body comprises a hollow curtain wall plate, a mounting frame is movably connected to the interior of the hollow curtain wall plate, and a solar panel is fixedly mounted in the mounting frame; the limiting assembly comprises a mounting base fixedly connected with the surface of the hollow curtain wall plate, and the front side of the mounting base is rotationally connected with a rotating clamping pin. The device has the advantage of being convenient to maintain, and the problems that in the using process of an existing aircraft take-off and landing platform tracing solar power generation curtain wall, solar panels on curtain wall plates are inconvenient to disassemble and clean, efficient maintenance of workers on the curtain wall is affected, and the convenience of the curtain wall is reduced are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of new energy industry, in particular to an aircraft take-off and landing platform tracing solar power generation curtain wall. Background Art

[0002] The aircraft landing platform tracking solar power curtain wall is an advanced facility that combines solar energy utilization technology with aircraft landing and take-off functions. This design usually involves a platform that serves as an aircraft landing area and integrates solar power generation technology to supply its own energy needs. Specifically, this curtain wall refers to an array of solar panels installed on or around the landing platform. These panels can track the movement of the sun to maximize the absorption of solar energy and convert it into electrical energy.

[0003] Tracking refers to the automatic adjustment mechanism of solar panels, ensuring that the panels always face the sun, even if the position of the sun changes with time and season. This can significantly improve the power generation efficiency of solar systems, and can capture sunlight more effectively than fixed-mounted solar panels, especially when the angle of light varies greatly during the day. When tracking, photoelectric sensors or sun tracking sensors are used to detect the direction and intensity of sunlight and feed back to the controller for precise adjustment.

[0004] The Chinese patent application number is 201921085503.8, which is an automatically adjustable solar panel, comprising a photovoltaic panel, a semicircular track, a rotating disk and a fixed disk. The rear end face of the photovoltaic panel is symmetrically provided with semicircular tracks on both sides, and a semicircular sliding groove is provided on the semicircular track. The center position of the rear end face of the photovoltaic panel is provided with a first fixed plate, and a rotating column is fixedly sleeved at the center position of the first fixed plate. The top center position of the rotating disk is fixedly connected with a support column, and the top two sides of the support column are symmetrically provided with second fixed plates, and the rotating column is slidably sleeved on the second fixed plate. A single-chip microcomputer is fixedly installed on the top surface of the rotating disk on one side of the support column, and the rotating disk is slidably engaged in the fixed disk. The utility model is provided with a limit column, a second limit plate, a single-chip microcomputer, a first limit plate, a reflector, a shading sleeve and a light sensor.

[0005] The existing aircraft landing and take-off platform traces the process of using the solar power curtain wall, which is not convenient for disassembling and cleaning the solar panels on the curtain wall panels, affecting the efficient maintenance of the curtain wall by the staff and reducing the convenience of the curtain wall. Utility Model Content

[0006] The utility model aims to provide an aircraft landing and take-off platform tracing solar power generation curtain wall, which has the advantage of being easy to maintain and solves the problem that the existing aircraft landing and take-off platform tracing solar power generation curtain wall is not convenient to disassemble and clean the solar panels on the curtain wall panels during use, which affects the efficient maintenance of the curtain wall by the staff and reduces the convenience of the curtain wall.

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aircraft take-off and landing platform traceable solar power generation curtain wall, comprising a curtain wall main body,

[0008] Limiting components are installed on the top and bottom of the left and right sides of the curtain wall body, and a driving component is installed on the bottom of the curtain wall body;

[0009] The curtain wall body comprises a hollow curtain wall panel, a mounting frame is movably connected inside the hollow curtain wall panel, and a solar panel is fixedly installed inside the mounting frame;

[0010] The limit assembly includes a mounting seat fixedly connected to the surface of the hollow curtain wall panel, a rotating bayonet is rotatably connected to the front side of the mounting seat, the rotating bayonet penetrates the hollow curtain wall panel and the mounting frame, one end of the rotating bayonet is fixedly connected to a handle, one side of the handle is fixedly connected to a spring, and the end of the spring away from the handle is fixedly connected to the surface of the hollow curtain wall panel;

[0011] The driving assembly comprises a box body, the inner cavity of the box body is rotatably connected with a driving rod, and the top of the driving rod is fixedly connected to the bottom of the hollow curtain wall panel.

[0012] As a preferred aircraft take-off and landing platform tracing solar power generation curtain wall of the utility model, a sun tracking sensor is fixedly installed on the top of the front side of the curtain wall body.

[0013] As a preferred aircraft take-off and landing platform tracing solar power generation curtain wall of the utility model, a connecting rod is fixedly connected to the top of the curtain wall body, and the connecting rod is rotatably connected to the first curtain wall keel through a bearing.

[0014] As a preferred aircraft landing platform tracing solar power generation curtain wall of the utility model, the hollow curtain wall panel and the installation frame are both provided with a slot used in conjunction with a rotating bayonet, and the surface of the rotating bayonet is movably connected to the inner wall of the slot.

[0015] As a preferred embodiment of the utility model of an aircraft take-off and landing platform tracing solar power generation curtain wall, the surface of the driving rod is rotatably connected to a second curtain wall keel through a bearing.

[0016] As an aircraft take-off and landing platform tracing solar power generation curtain wall preferred in the utility model, an angle sensor is fixedly installed at the bottom of the driving rod, and the bottom of the driving rod surface is rotatably connected to a support seat through a bearing, and the support seat is fixedly installed at the bottom of the box body cavity.

[0017] As a preferred aircraft take-off and landing platform tracing solar power generation curtain wall of the utility model, the inner cavity of the box is also fixedly installed with a self-locking motor and a controller, the output shaft of the self-locking motor is fixedly connected with a rotating rod, the top of the rotating rod is rotatably connected to the top of the inner wall of the box, the rotating rod surface fixed sleeve is provided with a small gear, and the driving rod surface fixed sleeve is provided with a large gear meshing with the small gear.

[0018] Compared with the prior art, the beneficial effects of the utility model are as follows:

[0019] 1. The utility model can facilitate the disassembly, cleaning and maintenance of the solar panel by setting a limit assembly. The staff turns the handle outward, and the handle drives the rotating pin to rotate at the front side of the mounting seat and stretches the spring. At this time, the rotating pin rotates downward to disengage from the slot. Then the staff takes the mounting frame out of the hollow curtain wall panel to disassemble the mounting frame and the solar panel. When the maintenance is completed, the rotating pin is reset to the slot, and the spring pulls the handle downward to limit the rotating pin to prevent the rotating pin from disengaging from the inside of the slot.

[0020] 2. The sun tracking sensor of the utility model is responsible for monitoring the position and angle of the sun. Through the data input of the sun tracking sensor, the controller can determine the best angle to which the solar panel should be adjusted to ensure that it receives the maximum amount of direct sunlight. When the controller receives the detection data, it will control the self-locking motor to rotate, and then drive the curtain wall body to rotate through the small gear, rotating rod, large gear and driving rod to adjust the angle. The angle sensor detects the rotation angle, and the detection data is transmitted to the controller. When the set rotation angle is reached, the controller turns off the self-locking motor. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 This is the front view of the utility model;

[0022] Figure 2 This is a front cross-sectional view of the drive assembly of the utility model;

[0023] Figure 3 It is a partial sectional view of the main view of the limiting assembly and the curtain wall body of the utility model.

[0024] In the figure: 1. curtain wall body; 101. hollow curtain wall panel; 102. solar panel; 103. slot; 104. installation frame; 2. limit assembly; 201. installation seat; 202. rotating latch; 203. handle; 204. spring; 3. drive assembly; 301. box; 302. controller; 303. large gear; 304. drive rod; 305. rotating rod; 306. small gear; 307. self-locking motor; 308. support seat; 309. angle sensor; 4. first curtain wall keel; 5. connecting rod; 6. sun tracking sensor; 7. second curtain wall keel. DETAILED DESCRIPTION

[0025] See also Figure 1-Figure 3 A solar power generation curtain wall for aircraft take-off and landing platforms includes a curtain wall body 1, and limit components 2 are installed on the top and bottom of the left and right sides of the curtain wall body 1, and a driving component 3 is installed at the bottom of the curtain wall body 1.

[0026] Furthermore, a sun tracking sensor 6 is fixedly installed on the top of the front side of the curtain wall body 1 .

[0027] Furthermore, a connecting rod 5 is fixedly connected to the top of the curtain wall body 1, and the connecting rod 5 is rotatably connected to the first curtain wall keel 4 through a bearing.

[0028] Furthermore, the curtain wall body 1 includes a hollow curtain wall panel 101 , an installation frame 104 is movably connected inside the hollow curtain wall panel 101 , and a solar panel 102 is fixedly installed inside the installation frame 104 .

[0029] Furthermore, the limiting assembly 2 includes a mounting base 201 fixedly connected to the surface of the hollow curtain wall panel 101, a rotating pin 202 is rotatably connected to the front side of the mounting base 201, the rotating pin 202 penetrates into the hollow curtain wall panel 101 and the mounting frame 104, one end of the rotating pin 202 is fixedly connected to a handle 203, one side of the handle 203 is fixedly connected to a spring 204, and one end of the spring 204 away from the handle 203 is fixedly connected to the surface of the hollow curtain wall panel 101.

[0030] Furthermore, both the hollow curtain wall panel 101 and the installation frame 104 are provided with a slot 103 for use with the rotating bayonet 202 , and the surface of the rotating bayonet 202 is movably connected to the inner wall of the slot 103 .

[0031] By setting the limit assembly 2, the solar panel 102 can be easily disassembled, cleaned and maintained. The staff turns the handle 203 outward, and the handle 203 drives the rotating pin 202 to rotate on the front side of the mounting seat 201 and stretches the spring 204. At this time, the rotating pin 202 rotates downward to disengage from the slot 103. Then the staff takes the installation frame 104 out of the hollow curtain wall panel 101 to disassemble the installation frame 104 and the solar panel 102. When the maintenance is completed, the rotating pin 202 is reset to the slot 103, and the spring 204 pulls the handle 203 downward to limit the rotating pin 202 to prevent the rotating pin 202 from escaping from the inside of the slot 103.

[0032] Furthermore, the driving assembly 3 includes a box body 301 , the inner cavity of the box body 301 is rotatably connected with a driving rod 304 , and the top of the driving rod 304 is fixedly connected to the bottom of the hollow curtain wall panel 101 .

[0033] Furthermore, the surface of the driving rod 304 is rotatably connected to the second curtain wall keel 7 via a bearing.

[0034] Furthermore, an angle sensor 309 is fixedly installed at the bottom of the driving rod 304 , and a support seat 308 is rotatably connected to the bottom of the surface of the driving rod 304 through a bearing, and the support seat 308 is fixedly installed at the bottom of the inner cavity of the box body 301 .

[0035] Furthermore, a self-locking motor 307 and a controller 302 are fixedly installed in the inner cavity of the box 301, and the output shaft of the self-locking motor 307 is fixedly connected to a rotating rod 305, the top of the rotating rod 305 is rotatably connected to the top of the inner wall of the box 301, a small gear 306 is fixedly sleeved on the surface of the rotating rod 305, and a large gear 303 meshing with the small gear 306 is fixedly sleeved on the surface of the driving rod 304.

[0036] The sun tracking sensor 6 is responsible for monitoring the position and angle of the sun. Through the data input from the sun tracking sensor 6, the controller 302 can determine the optimal angle to which the solar panel 102 should be adjusted to ensure that it receives the maximum amount of direct sunlight. When the controller 302 receives the detection data, it will control the self-locking motor 307 to rotate, and then drive the curtain wall body 1 to rotate through the small gear 306, the rotating rod 305, the large gear 303 and the driving rod 304 to adjust the angle. The angle sensor 309 detects the rotation angle, and the detection data is transmitted to the controller 302. When the set rotation angle is reached, the controller 302 turns off the self-locking motor 307.

[0037] The electric energy generated by the solar panel 102 is transmitted to the solar charge controller inside the building. The solar charge controller stores the electric energy in the energy storage system and converts the direct current into alternating current through the inverter for use when in use.

[0038] The sun tracking sensor 6 is responsible for monitoring the position and angle of the sun. Through the data input from the sun tracking sensor 6, the controller 302 can determine the optimal angle to which the solar panel 102 should be adjusted to ensure that it receives the maximum amount of direct sunlight. When the controller 302 receives the detection data, it will control the self-locking motor 307 to rotate, and then drive the curtain wall body 1 to rotate through the small gear 306, the rotating rod 305, the large gear 303 and the driving rod 304 to adjust the angle. The angle sensor 309 detects the rotation angle, and the detection data is transmitted to the controller 302. When the set rotation angle is reached, the controller 302 turns off the self-locking motor 307.

[0039] The first curtain wall keel 4 and the second curtain wall keel 7 are installed on the outer wall of the building. The first curtain wall keel 4 is connected to the top of the curtain wall body 1 through the connecting rod 5 and the bearing to support the top of the curtain wall body 1. The second curtain wall keel 7 limits the driving rod 304, which increases the flexibility and stability of the entire structure and helps to reduce resistance and wear when adjusting the angle.

[0040] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An aircraft take-off and landing platform retrospective solar power generation curtain wall, comprising a curtain wall body (1), characterized in that: Limiting components (2) are installed at the top and bottom of the left and right sides of the curtain wall body (1), and a driving component (3) is installed at the bottom of the curtain wall body (1); The curtain wall body (1) comprises a hollow curtain wall panel (101), a mounting frame (104) is movably connected inside the hollow curtain wall panel (101), and a solar panel (102) is fixedly mounted inside the mounting frame (104); The limiting assembly (2) comprises a mounting seat (201) fixedly connected to the surface of the hollow curtain wall panel (101); a rotating bayonet (202) is rotatably connected to the front side of the mounting seat (201); the rotating bayonet (202) penetrates the hollow curtain wall panel (101) and the mounting frame (104); one end of the rotating bayonet (202) is fixedly connected to a handle (203); one side of the handle (203) is fixedly connected to a spring (204); and one end of the spring (204) away from the handle (203) is fixedly connected to the surface of the hollow curtain wall panel (101); The driving assembly (3) comprises a box (301), the inner cavity of the box (301) is rotatably connected to a driving rod (304), and the top of the driving rod (304) is fixedly connected to the bottom of the hollow curtain wall panel (101).

2. The aircraft take-off and landing platform retroactive solar power generation curtain wall according to claim 1, characterized in that: A sun tracking sensor (6) is fixedly mounted on the top of the front side of the curtain wall body (1).

3. The aircraft take-off and landing platform traceable solar power generation curtain wall according to claim 1, characterized in that: A connecting rod (5) is fixedly connected to the top of the curtain wall body (1), and the connecting rod (5) is rotatably connected to the first curtain wall keel (4) via a bearing.

4. The aircraft take-off and landing platform retroactive solar power generation curtain wall according to claim 1, characterized in that: The hollow curtain wall panel (101) and the installation frame (104) are both provided with a slot (103) for use with a rotating bayonet (202), and the surface of the rotating bayonet (202) is movably connected to the inner wall of the slot (103).

5. The aircraft take-off and landing platform traceable solar power generation curtain wall according to claim 1, characterized in that: The surface of the driving rod (304) is rotatably connected to a second curtain wall keel (7) via a bearing.

6. The aircraft take-off and landing platform traceable solar power generation curtain wall according to claim 1, characterized in that: An angle sensor (309) is fixedly mounted on the bottom of the driving rod (304); a support seat (308) is rotatably connected to the bottom of the surface of the driving rod (304) via a bearing; and the support seat (308) is fixedly mounted on the bottom of the inner cavity of the box body (301).

7. The aircraft take-off and landing platform traceable solar power generation curtain wall according to claim 1, characterized in that: A self-locking motor (307) and a controller (302) are also fixedly installed in the inner cavity of the box body (301); the output shaft of the self-locking motor (307) is fixedly connected to a rotating rod (305); the top of the rotating rod (305) is rotatably connected to the top of the inner wall of the box body (301); a small gear (306) is fixedly sleeved on the surface of the rotating rod (305); and a large gear (303) meshing with the small gear (306) is fixedly sleeved on the surface of the driving rod (304).

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