Convenient modular mobile aviation power supply cabinet

Abstract

The invention discloses a convenient modular mobile aviation power supply cabinet, which comprises a cabinet main body frame, a touch screen panel and a front air hole plate are arranged on the front surface of the cabinet main body frame, a rear wire inlet panel and a rear air hole plate are arranged on the rear surface of the cabinet main body frame, and side plates are arranged on the left side and the right side of the cabinet main body frame. Two front enlargement beams, two rear enlargement beams, four middle stand columns, a control system tray, eight L-shaped guide rails and four pin seat mounting plates are installed in the cabinet body frame, two pin seats are installed on each pin seat mounting plate, and four universal wheels are installed at the bottom of the cabinet body frame. Installation of a cabinet door can be avoided, certain convenience is achieved, and use is convenient; a modular control system can be built according to requirements, and a standard-size power supply plug-in box can be placed in the modular control system, so that the modular control system has certain universality; the whole structure is simple in design, high in practicability, low in cost and suitable for batch production.

Description

Technical Field

[0001] This invention relates to a power supply cabinet technology, and more particularly to a convenient, modular, mobile aviation power supply cabinet. Background Technology

[0002] Most existing power supply cabinets use a design with doors installed at both the front and back. This requires opening the doors to operate the cabinet, which places high demands on surrounding space and is not very convenient to use. Without doors, the power modules inside the cabinet would be exposed, affecting aesthetics and accumulating dust over time. In addition, most existing cabinets lack versatility; a single cabinet may only have certain specific functions. To output different power or perform different functions, the cabinet structure must be redesigned according to the size of the components.

[0003] In view of this, the present invention is hereby proposed. Summary of the Invention

[0004] The purpose of this invention is to provide a convenient, modular, mobile aviation power supply cabinet to solve the aforementioned technical problems in the prior art.

[0005] The objective of this invention is achieved through the following technical solution:

[0006] A convenient modular mobile aviation power supply cabinet includes a main cabinet frame. A touchscreen panel and a front air vent plate are mounted on the front of the main cabinet frame. A rear cable entry panel and a rear air vent plate are mounted on the rear of the main cabinet frame. Side panels are mounted on the left and right sides of the main cabinet frame. Inside the main cabinet frame are two front extension beams, two rear extension beams, four central columns, a control system tray, eight L-shaped guide rails, and four pin mounting plates. Each of the four pin mounting plates has two pins. Four casters are mounted on the bottom of the main cabinet frame for easy movement of the cabinet.

[0007] Compared with existing technologies, the convenient modular mobile aviation power cabinet provided by this invention has the following advantages: it can be installed without cabinet doors, which is convenient and easy to use; it can build a modular control system according to needs, and can accommodate standard-sized power supply boxes, which is versatile; the overall structure design is simple, practical, and low in cost, making it suitable for mass production. Attached Figure Description

[0008] Figure 1 This is a three-dimensional structural diagram of a convenient modular mobile aviation power supply cabinet for embodiments of the present invention.

[0009] Figure 2 This is a schematic diagram of the internal structure of a convenient modular mobile aviation power supply cabinet provided for embodiments of the present invention.

[0010] Figure 3 This is a schematic diagram of the main frame of the cabinet in an embodiment of the present invention, viewed from below.

[0011] Figure 4 This is a top view of the main frame of the cabinet according to an embodiment of the present invention.

[0012] Figure 5 This is a schematic diagram of the structure of a touch screen panel according to an embodiment of the present invention.

[0013] In the picture:

[0014] 1. Cabinet main frame; 2. Touch screen panel; 3. Front air vent plate; 4. Side plate; 5. Casters; 6. Rear cable entry panel; 7. Rear air vent plate; 8. Front extension beam; 9. Rear extension beam; 10. Central column; 11. Control system tray; 12. L-shaped guide rail; 13. Pin mounting plate; 14. Pin; 15. Bracket A; 16. Bracket B.

[0015] 61. Aviation connector, 62. Copper busbar, 63. Power input terminal, 64. Grounding post;

[0016] 101 Top plate, 102 Bottom plate, 103 Front column, 104 Rear column, 105 Rear entry beam, 106 Top reinforcement plate, 107 Top upper edge (front), 108 Top upper edge (rear), 109 Bottom beam, 110 Bottom lower edge (front), 111 Bottom lower edge (rear), 112 Caster reinforcement rib 1, 113 Caster reinforcement rib 2, 114 Rear entry beam 1, 115 Rear entry beam 2;

[0017] 201 Switch box, 202 Main power switch, 203 Bracket H, 204 Industrial control all-in-one computer, 205 Bracket G. Detailed Implementation

[0018] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of the present invention, and not all of them, and do not constitute a limitation on the present invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without creative effort are within the protection scope of the present invention.

[0019] First, the following explanations are provided for the terms that may be used in this article:

[0020] The terms “including,” “contains,” “comprising,” “having,” or other similar semantic descriptions shall be interpreted as non-exclusive inclusion.

[0021] The term "composed of" excludes any technical features not expressly listed. When used in a claim, it closes the claim to exclude all technical features other than those expressly listed, except for associated conventional impurities. If the term appears only in a clause of a claim, it limits the claim to the elements expressly listed in that clause; elements recited in other clauses are not excluded from the overall claim.

[0022] The technical solution provided by this invention will be described in detail below. Contents not described in detail in the embodiments of this invention are prior art known to those skilled in the art. Where specific conditions are not specified in the embodiments of this invention, they shall be performed according to conventional conditions in the art or conditions recommended by the manufacturer. Reagents or instruments used in the embodiments of this invention whose manufacturers are not specified are all conventional products that can be purchased commercially.

[0023] like Figures 1 to 5 As shown, a convenient modular mobile aviation power supply cabinet includes the following steps:

[0024] A convenient modular mobile aviation power supply cabinet includes a main cabinet frame. The front of the main cabinet frame is equipped with a touchscreen panel and a front air vent plate. The rear of the main cabinet frame is equipped with a rear cable entry panel and a rear air vent plate. Side panels are installed on the left and right sides of the main cabinet frame. Inside the main cabinet frame are two front extension beams, two rear extension beams, four central uprights, a control system tray, eight L-shaped guide rails, and four pin mounting plates. Each of the four pin mounting plates is equipped with two pins. The bottom of the main cabinet frame is equipped with four casters for easy movement of the cabinet.

[0025] Preferably, the main frame of the cabinet consists of a top plate, a bottom plate, two front uprights, two rear uprights, and a rear cable entry beam. Top reinforcing plates are welded to the left and right sides of the top plate, and top upper edge front and top upper edge rear are welded to the front and back. Bottom crossbeams are welded to the left and right sides above the bottom plate, and bottom lower edge front and bottom lower edge rear are welded to the front and back. Caster reinforcing ribs one and two are welded to the left and right sides below the bottom plate. The rear cable entry beam is welded to two parts: rear cable entry beam one and rear cable entry beam two. The rear cable entry beam is welded to the upper rear part of the main frame of the cabinet.

[0026] Preferably, the two front extension beams are fixed to the two front columns of the main frame of the cabinet with screws, and the two rear extension beams are fixed to the two rear columns of the main frame of the cabinet with screws. The four middle columns are symmetrically fixed to the left and right sides of the main frame of the cabinet with screws. The control system tray is fixed to the four middle columns and the two rear extension beams with screws and is used to house the control system of the power cabinet. The eight L-shaped guide rails are fixed to the two front extension beams, the four middle columns and the two rear extension beams with screws, arranged in groups of four on the left and right sides of the main frame of the cabinet, and are used to house standard-sized power supply boxes. The four pin mounting plates are fixed to the eight L-shaped guide rails with screws. The pins are used to insert positioning pins to limit the movement of the power supply boxes.

[0027] Preferably, the two front columns of the main frame of the cabinet are designed with two layers of mounting holes by sheet metal bending. The rear mounting holes are used for the fixed installation of a standard-sized power supply box, and the front mounting holes are used for the fixed installation of a touch screen panel and a front air vent plate. The touch screen panel is fixedly installed on the top of the two front columns by screws, and the front air vent plate is fixedly installed on the bottom of the two front columns by screws.

[0028] Preferably, a recessed switch box is welded to the left side of the touch screen panel for installing the main power switch. The main power switch is fixedly installed on the switch box by a bracket H. An industrial control computer is mounted on the right side of the touch screen panel. The industrial control computer is fixedly installed on the touch screen panel by a bracket G. The power cabinet can be conveniently used by operating the industrial control computer. Seven rows of ventilation holes are designed above the touch screen panel for ventilation and heat dissipation of the power cabinet.

[0029] Preferably, the rear entry panel is equipped with several aviation plugs, copper busbars, power input terminals and grounding posts for power cabinet and external communication. The remaining parts are designed as vents for ventilation and heat dissipation of the power cabinet. The rear entry panel is fixedly installed at the rear of the main frame of the cabinet by screws, and is located above the rear entry beam.

[0030] Preferably, both the front and rear air vents are designed with large-area air vents. The rear air vent is fixedly installed at the rear of the main frame of the cabinet by four brackets A, located below the rear cable entry beam. The front and rear air vents are aligned front to back for ventilation and heat dissipation of the power cabinet.

[0031] Preferably, the two side panels are fixedly installed on the left and right sides of the main frame of the cabinet by six brackets B.

[0032] Preferably, the four central columns are designed with multiple sets of equidistant mounting holes, and the two rear-mounted megabeams are also designed with multiple sets of equidistant mounting holes. The installation position of the control system tray can be adjusted according to the size of the control system.

[0033] In summary, the convenient modular mobile aviation power cabinet of this invention, by designing the front uprights with two layers of mounting holes, eliminates the need for a cabinet door. For cabinets that do not require frequent door opening for operation, a vent plate can be fixedly installed, ensuring good ventilation and heat dissipation while also improving the cabinet's appearance and reducing dust ingress. A touchscreen industrial control all-in-one computer installed on the front panel facilitates cabinet operation. Casters at the bottom allow for easy movement of the cabinet. The cabinet interior can accommodate a standard-sized power outlet box with limit functions. The control system tray is adjustable in height, suitable for control systems of different sizes.

[0034] The power cabinet designed in this invention can be installed without a cabinet door, which is convenient and easy to use; it can be equipped with a modular control system according to needs, and can accommodate standard-sized power socket boxes, which is versatile; the overall structure is simple, practical, and low in cost, making it suitable for mass production.

[0035] To more clearly demonstrate the technical solution and its effects provided by the present invention, the following detailed description of the convenient modular mobile aviation power cabinet provided by the embodiments of the present invention is provided with specific examples.

[0036] Example 1

[0037] like Figure 1 , Figure 2 As shown, an embodiment of the present invention provides a convenient modular mobile aviation power supply cabinet, including a cabinet main frame 1. The front of the cabinet main frame 1 is equipped with a touch screen panel 2 and a front air vent plate 3. The rear of the cabinet main frame 1 is equipped with a rear cable entry panel 6 and a rear air vent plate 7. Side panels 4 are installed on the left and right sides of the cabinet main frame 1. The cabinet main frame 1 is equipped with two front support beams 8, two rear support beams 9, four central columns 10, a control system tray 11, eight L-shaped guide rails 12, and four pin seat mounting plates 14. Each of the four pin seat mounting plates 14 is equipped with two pin seats 14. The bottom of the cabinet main frame 1 is equipped with four casters 5 for easy movement of the cabinet.

[0038] like Figure 3 , Figure 4As shown, the main frame 1 of the cabinet consists of a top plate 101, a bottom plate 102, two front uprights 103, two rear uprights 104, and a rear cable entry beam 105. The top plate 101 is welded with top reinforcing plates 106 on the left and right sides, and with top upper edge front 107 and top upper edge rear 108 welded at the front and back. The bottom plate 102 is welded with bottom crossbeams 109 on the left and right sides above, and with bottom lower edge front 110 and bottom lower edge rear 111 welded at the front and back. The bottom plate 102 is welded with caster reinforcing ribs 112 on the left and right sides below, and with caster reinforcing ribs 113 welded at the front and back. The rear cable entry beam 105 is welded together from two parts: rear cable entry beam 114 and rear cable entry beam 115. The rear cable entry beam 105 is welded to the upper rear part of the main frame 1 of the cabinet.

[0039] like Figure 2 As shown, the two front extension beams 8 are fixed to the two front uprights 103 of the main frame 1 of the cabinet with screws, and the two rear extension beams 9 are fixed to the two rear uprights 104 of the main frame 1 of the cabinet with screws. The four middle uprights 10 are symmetrically fixed to the left and right sides of the main frame 1 of the cabinet with screws. The control system tray 11 is fixed to the four middle uprights 10 and the two rear extension beams 9 with screws and is used to place the control system of the power cabinet. The eight L-shaped guide rails 12 are fixed to the two front extension beams 8, the four middle uprights 10 and the two rear extension beams 9 with screws. They are arranged in groups of four and symmetrically on the left and right sides of the main frame 1 of the cabinet and are used to place standard-sized power supply boxes. The four pin mounting plates 14 are fixed to the eight L-shaped guide rails 12 with screws. The pins 14 are used to insert positioning pins to limit the position of the power supply boxes.

[0040] like Figure 1 , Figure 4 As shown, the two front columns 103 of the main frame 1 of the cabinet have two layers of mounting holes designed by sheet metal bending. The rear mounting holes are used for the fixed installation of the standard size power socket box, and the front mounting holes are used for the fixed installation of the touch screen panel 2 and the front air vent plate 3. The touch screen panel 2 is fixedly installed on the top of the two front columns 103 by screws, and the front air vent plate 3 is fixedly installed on the bottom of the two front columns 103 by screws.

[0041] like Figure 5As shown, a recessed switch box 201 is welded to the left side of the touch screen panel 2 for installing the main power switch 202. The main power switch 202 is fixedly installed on the switch box 201 by a bracket H203. An industrial control all-in-one computer 204 is installed on the right side of the touch screen panel 2. The industrial control all-in-one computer 204 is fixedly installed on the touch screen panel 2 by a bracket G205. The power cabinet can be conveniently used by operating the industrial control all-in-one computer 204. Seven rows of ventilation holes are designed on the top of the touch screen panel 2 for ventilation and heat dissipation of the power cabinet.

[0042] like Figure 2 As shown, the rear cable entry panel 6 is equipped with several aviation plugs 61, copper busbars 62, power input terminals 63, and grounding posts 64 for power cabinet and external communication. The remaining parts are designed as vents for ventilation and heat dissipation of the power cabinet. The rear cable entry panel 6 is fixedly installed at the rear of the main frame 1 of the cabinet with screws, located above the rear cable entry beam 105. The front vent plate 3 and the rear vent plate 7 are both designed with large-area vents. The rear vent plate 7 is fixedly installed at the rear of the main frame 1 of the cabinet with four brackets A15, located below the rear cable entry beam 105. The front vent plate 3 and the rear vent plate 7 are corresponding to each other for ventilation and heat dissipation of the power cabinet. The two side plates 4 are fixedly installed on the left and right sides of the main frame 1 of the cabinet with six brackets B16 respectively. Multiple sets of equidistant mounting holes are designed above the four central columns 10, and multiple sets of equidistant mounting holes are also designed on the two rear extension beams 9. The installation position of the control system tray 11 can be adjusted according to the size of the control system.

[0043] The above description is merely a preferred embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the scope of the technology disclosed in the present invention should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be determined by the scope of the claims. The information disclosed in the background section is intended only to enhance the understanding of the overall background technology of the present invention and should not be construed as an admission or implication in any way that such information constitutes prior art known to those skilled in the art.

Claims

1. A convenient modular mobile aviation power supply cabinet, characterized in that, The cabinet includes a main frame (1), a touch screen panel (2) and a front air vent plate (3) on the front of the main frame (1), a rear cable entry panel (6) and a rear air vent plate (7) on the back of the main frame (1), side panels (4) on the left and right sides of the main frame (1), two front support beams (8), two rear support beams (9), four central columns (10), a control system tray (11), eight L-shaped guide rails (12) and four pin mounting plates (13) inside the main frame (1), two pins (14) on each of the four pin mounting plates (13), and four casters (5) on the bottom of the main frame (1).

2. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, The main frame (1) of the cabinet consists of a top plate (101), a bottom plate (102), two front columns (103), two rear columns (104), and a rear cable entry beam (105). The top plate (101) is welded with top reinforcing plates (106) on the left and right sides, and with top upper edge front (107) and top upper edge rear (108) welded at the front and back. The bottom plate (102) is welded with bottom crossbeams (109) on the left and right sides above, and with bottom lower edge front (110) and bottom lower edge rear (111) welded at the front and back. The bottom plate (102) is welded with caster reinforcing rib one (112) on the left and right sides below, and with caster reinforcing rib two (113) welded at the front and back. The rear cable entry beam (105) is welded from two parts: rear cable entry beam one (114) and rear cable entry beam two (115). The rear cable entry beam (105) is welded to the upper part of the rear of the main frame (1) of the cabinet.

3. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, The two front extension beams (8) are fixed to the two front uprights (103) of the main frame of the cabinet (1) by screws. The two rear extension beams (9) are fixed to the two rear uprights (104) of the main frame of the cabinet (1) by screws. The four middle uprights (10) are symmetrically fixed to the left and right sides of the main frame of the cabinet (1) by screws. The control system tray (11) is fixed to the four middle uprights (10) and the two rear extension beams (9) by screws. Above, there is a control system for placing the power supply cabinet. The eight L-shaped guide rails (12) are fixed to the two front support beams (8), four central columns (10) and two rear support beams (9) by screws. The four are arranged in a group and symmetrically on the left and right sides of the main frame (1) of the cabinet. They are used to place standard-sized power supply boxes. The four pin mounting plates (13) are fixed to the eight L-shaped guide rails (12) by screws. The pins (14) are used to insert positioning pins to limit the position of the power supply boxes.

4. The convenient modular mobile aviation power supply cabinet according to claim 2, characterized in that, The main frame (1) of the cabinet has two front columns (103) with two layers of mounting holes designed by sheet metal bending. The rear mounting holes are used for the fixed installation of the standard size power supply box, and the front mounting holes are used for the fixed installation of the touch screen panel (2) and the front air vent plate (3). The touch screen panel (2) is fixedly installed on the top of the two front columns (103) by screws, and the front air vent plate (3) is fixedly installed on the bottom of the two front columns (103) by screws.

5. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, A recessed switch box (201) is welded to the left side of the touch screen panel (2) for installing the main power switch (202). The main power switch (202) is fixedly installed on the switch box (201) by a bracket H (203). An industrial control computer (204) is installed on the right side of the touch screen panel (2). The industrial control computer (204) is fixedly installed on the touch screen panel (2) by a bracket G (205). The power cabinet can be conveniently used by operating the industrial control computer (204). Seven rows of ventilation holes are designed on the top of the touch screen panel (2) for ventilation and heat dissipation of the power cabinet.

6. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, The rear entry panel (6) is equipped with several aviation plugs (61), wiring copper busbars (62), power input terminals (63) and grounding posts (64) for power cabinet and external communication. The remaining parts are designed as air vents for ventilation and heat dissipation of the power cabinet. The rear entry panel (6) is fixedly installed on the rear part of the main frame (1) of the cabinet by screws, and is located above the rear entry beam (105).

7. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, Both the front air vent plate (3) and the rear air vent plate (7) are designed with large-area air vents. The rear air vent plate (7) is fixedly installed at the rear of the main frame (1) of the cabinet by four brackets A (15), and is located below the rear cable entry beam (105). The front air vent plate (3) and the rear air vent plate (7) are corresponding to each other and are used for ventilation and heat dissipation of the power cabinet.

8. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, The two side panels (4) are fixedly installed on the left and right sides of the main frame (1) of the cabinet by six brackets B (16).

9. The convenient modular mobile aviation power supply cabinet according to claim 1, characterized in that, The four central columns (10) are designed with multiple sets of equidistant mounting holes, and the two rear-mounted megabeams (9) are also designed with multiple sets of equidistant mounting holes. The control system tray (11) can be adjusted in installation position according to the size of the control system.

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