Anti-vibration and anti-glare fixed seat industrial computer

Abstract

The utility model provides a kind of anti-vibration anti-dazzle seat fixed industrial computer, belong to aviation airborne equipment structure field.The problem of not fixed, inconvenient operation and potential safety hazard caused by vibration, glare and cable mess of industrial computer in the cabin of aircraft is solved.It includes clamping component, fixed table and folding light shield, the clamping component quantity is two groups, two groups of clamping component are symmetrically arranged in the left and right sides of fixed table, the clamping component includes ball screw and clamping plate, the clamping plate is connected on ball screw, the ball screw is connected with fixed table, the clamping plate is clamped between fixed table, and the aircraft seat armrest is clamped, folding light shield is rotatably connected on the fixed table, and operating equipment is provided on the fixed table.It is mainly used for anti-vibration anti-dazzle seat fixed industrial computer.

Description

Technical Field

[0001] This utility model belongs to the field of airborne equipment structure, and in particular relates to a seat-fixed industrial control computer with vibration resistance and anti-glare properties. Background Technology

[0002] In the field of avionics, industrial control computer (ICS) systems used in aircraft cockpits are critical equipment supporting various missions, especially in special mission aircraft such as patrol, reconnaissance, and rescue operations. Operators need to control optoelectronic payload pods and other airborne equipment via ICS. These ICS typically need to be brought into the cabin and secured in a suitable location so that operators can operate them effectively during flight. However, traditional securing methods have many limitations, affecting equipment performance and operator efficiency. Currently, the common practice is to bring portable ICS into the cabin and place them on the operator's lap or on a simple stand. This method has significant drawbacks: First, the continuous vibrations generated by the aircraft during flight can cause the ICS to shake, leading to accidental screen or button presses by the operator, affecting operational accuracy and equipment safety; second, the complex lighting conditions inside the cabin can cause glare on the screen, interfering with the operator's observation of target images; furthermore, exposed cables not only make the cabin cluttered but also pose risks of entanglement and impact.

[0003] To address the vibration issue, existing technologies involve removing the aircraft seat and installing a mounting bracket. While this method reduces swaying, the modification process is complex, damages the original seat structure, and lacks flexibility, hindering rapid assembly and disassembly. Therefore, there is an urgent need for an industrial control computer mounting solution that effectively reduces vibration and glare, allows for rapid installation, and does not damage the original aircraft structure. Utility Model Content

[0004] In view of this, the present invention aims to propose a vibration-resistant and anti-glare seat-mounted industrial control computer to solve the problems of unstable fixation, inconvenient operation, and safety hazards caused by vibration, glare, and messy cables in industrial control computers in aircraft cabins.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: a vibration-resistant and anti-glare seat-fixed industrial control computer, comprising clamping components, a fixed table, and a folding sunshade. The clamping components are arranged in two sets, symmetrically on the left and right sides of the fixed table. Each clamping component includes a ball screw and a clamping plate. The clamping plate is connected to the ball screw, and the ball screw is connected to the fixed table. The clamping plate clamps the aircraft seat armrest between itself and the fixed table. A folding sunshade is rotatably connected to the fixed table, and operating equipment is provided on the fixed table.

[0006] Furthermore, the two sides of the folding sunshade are connected to the fixed table via hinges.

[0007] Furthermore, the fixed table is provided with an adapter plate, and the adapter plate has several cavity channels.

[0008] Furthermore, the side of the fixed table has threading holes at the corresponding positions of the cavity cable channels.

[0009] Furthermore, cables are arranged inside the cavity channel.

[0010] Furthermore, the cable is fixed inside the cavity cable channel by a clamp.

[0011] Furthermore, the operating device includes a handle, a trackball, and a keyboard.

[0012] Furthermore, the fixed table is provided with an upper table surface and a lower table surface, which are respectively located on the upper and lower sides of the adapter plate.

[0013] Furthermore, the handle is mounted on the upper platform, while the trackball and keyboard are mounted on the lower platform.

[0014] Furthermore, the folding sunshade is made of a dark-colored flame-retardant composite material.

[0015] Compared with existing technologies, the advantages of this invention are as follows: This invention achieves a rigid connection with the aircraft seat through a clamping component. A ball screw drives a clamping plate, clamping the two aircraft seat armrests between the fixed table and the clamping plate, thus making the industrial computer and the aircraft a unified whole. This significantly reduces the risk of swaying and accidental touches caused by vibration, effectively suppressing vibration. The folding sunshade effectively blocks ambient light, improving screen visibility under complex lighting conditions, eliminating screen glare, and without occupying extra space. The internal cavity wiring channels conceal all cables within the table, preventing cable bumps and wear, maintaining a clean and safe cabin environment, and achieving neat cable management. The integrated physical operating device fundamentally avoids accidental touches on the touchscreen, improving operational accuracy and efficiency. The structure adapts to seat armrests with different spacing, requiring no modification to the aircraft, enabling rapid disassembly and flexible deployment. It provides an integrated aircraft seat industrial computer fixing structure that allows for rapid and non-destructive installation. Attached Figure Description

[0016] The accompanying drawings, which form part of this utility model, are used to provide a further understanding of the utility model. The illustrative embodiments of the utility model and their descriptions are used to explain the utility model and do not constitute an undue limitation of the utility model. In the drawings: Figure 1 This is a schematic diagram of a vibration-resistant and anti-glare seat-fixed industrial control computer structure according to the present invention.

[0017] In the picture: 1-Clamping component, 2-Fixed table, 3-Hinge, 4-Folding sunshade, 5-Handle, 6-Trajectory ball, 7-Cavity cable, 8-Adapter plate, 9-Keyboard. Detailed Implementation

[0018] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. It should be noted that, unless otherwise specified, the embodiments and features in the embodiments of the present utility model can be combined with each other, and the described embodiments are only some embodiments of the present utility model, not all embodiments.

[0019] See Figure 1 This embodiment describes a vibration-resistant and anti-glare seat-mounted industrial control computer, which includes clamping components 1, a fixed table 2, and a folding sunshade 4. There are two sets of clamping components 1, symmetrically arranged on the left and right sides of the fixed table 2. Each clamping component 1 includes a ball screw and a clamping plate. The clamping plate is connected to the ball screw, which is connected to the fixed table 2. The clamping plate clamps the aircraft seat armrest between itself and the fixed table 2. The folding sunshade 4 is rotatably connected to the fixed table 2, and operating equipment is provided on the fixed table 2.

[0020] The folding light shield 4 described in this embodiment is connected to the fixed table 2 on both sides by hinges 3. The fixed table 2 is provided with a transition plate 8, and the transition plate 8 has a plurality of hollow cable channels 7. The side of the fixed table 2 has wire holes at the corresponding positions of the hollow cable channels 7. Cables are arranged in the hollow cable channels 7 and the cables are fixed in the hollow cable channels 7 by cable clamps. The operating device includes a handle 5, a trackball 6 and a keyboard 9. The fixed table 2 is provided with an upper table surface and a lower table surface, which are respectively located on the upper and lower sides of the transition plate 8. The handle 5 is located on the upper table surface, and the trackball 6 and keyboard 9 are located on the lower table surface. The folding light shield 4 is made of dark-colored flame-retardant composite material.

[0021] A vibration-resistant and anti-glare seat-mounted industrial control computer includes clamping components 1, a fixed table 2, and a folding sunshade 4. Two sets of clamping components 1 are symmetrically arranged on the left and right sides of the fixed table 2. Each clamping component 1 includes a ball screw and a clamping plate, with the clamping plate connected to the ball screw, which is connected to the fixed table 2. The folding sunshade 4 is rotatably connected to the fixed table 2, and operating devices are mounted on the fixed table 2.

[0022] The folding sunshade 4 is connected to the fixed table 2 on both sides via hinges 3. The fixed table 2 has an adapter plate 8 with several hollow cable channels 7. Cable guide holes are provided on the sides of the fixed table 2 at corresponding positions within the hollow cable channels 7. Cables pass through these holes and are then routed within the hollow cable channels 7, where they are secured by cable clamps. The operating devices include a handle 5, a trackball 6, and a keyboard 9. The fixed table 2 has an upper and lower tabletop, located on the upper and lower sides of the adapter plate 8, respectively. The handle 5 is located on the upper tabletop, while the trackball 6 and keyboard 9 are located on the lower tabletop. The folding sunshade 4 is made of a dark-colored flame-retardant composite material.

[0023] The working process and principle of this solution are as follows: During installation, the fixed table 2 is placed between the two armrests of the aircraft seats. The operator rotates the ball screws of the clamping components 1 on both sides, causing the clamping plates to move linearly until the clamping plates and the fixed table 2 together clamp the aircraft seat armrests. Through the preload of the ball screws on both sides, friction is used to rigidly lock the entire device onto the seat, making the industrial control computer and the aircraft a whole, thereby significantly reducing the risk of swaying and accidental touch caused by flight vibrations. The adjustable stroke of the ball screws allows it to adapt to armrests of various widths, enabling non-destructive and rapid installation and removal.

[0024] When complex cabin lighting may cause screen glare, the operator can rotate the folding sunshade 4 upwards to unfold it. Made of dark-colored flame-retardant composite material, this sunshade effectively blocks ambient light such as sunlight entering through the side windows, eliminating screen glare and improving screen visibility. When not in use, it can be folded down for storage, saving space.

[0025] All cables connecting the industrial control computer host, operating equipment, and external devices are threaded through the cable entry holes on the side of the fixed table 2 into the internal hollow cable channel 7 during installation. The cables are secured within the hollow cable channel 7 using cable clamps, achieving concealment and centralized management. This avoids messy exposed cables within the machine compartment, effectively reducing the risk of cable bumps, wear, and entanglement, and maintaining a clean and safe machine compartment environment.

[0026] The operating devices, including a handle 5, a trackball 6, and a keyboard 9, are fixed to the upper and lower surfaces of the adapter plate 8, respectively. This integration of physical operating devices fundamentally avoids the accidental touch problems that are prone to occur with touchscreen operation, and improves the accuracy and efficiency of operators in controlling photoelectric loads and other equipment.

[0027] The specific embodiments of this utility model disclosed above are merely illustrative of the present utility model. These specific embodiments do not exhaustively describe all details, nor do they limit the utility model to only the described embodiments. Many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of this utility model, thereby enabling those skilled in the art to better understand and utilize it.

Claims

1. A vibration-resistant and anti-glare seat-mounted industrial control computer, characterized in that: It includes clamping components (1), a fixed table (2), and a folding sunshade (4). There are two sets of clamping components (1), which are symmetrically arranged on the left and right sides of the fixed table (2). Each clamping component (1) includes a ball screw and a clamping plate. The clamping plate is connected to the ball screw, and the ball screw is connected to the fixed table (2). The clamping plate clamps the aircraft seat armrest between the fixed table (2). The fixed table (2) is rotatably connected to the folding sunshade (4), and the fixed table (2) is equipped with operating devices.

2. The anti-vibration and anti-glare seat-mounted industrial control computer according to claim 1, characterized in that: The two sides of the folding light shield (4) are connected to the fixed table (2) by hinges (3).

3. The anti-vibration and anti-glare seat-mounted industrial control computer according to claim 1, characterized in that: The fixed table (2) is provided with a transition plate (8), and the transition plate (8) has several cavity channels (7).

4. The anti-vibration and anti-glare seat-fixed industrial control computer according to claim 3, characterized in that: The side of the fixed table (2) has a threading hole at the corresponding position of the cavity cable channel (7).

5. A vibration-resistant and anti-glare seat-mounted industrial control computer according to claim 3, characterized in that: Cables are arranged inside the cavity channel (7).

6. A vibration-resistant and anti-glare seat-mounted industrial control computer according to claim 5, characterized in that: The cable is fixed in the cavity channel (7) by a clamp.

7. A vibration-resistant and anti-glare seat-mounted industrial control computer according to claim 3, characterized in that: The operating device includes a handle (5), a trackball (6), and a keyboard (9).

8. The anti-vibration and anti-glare seat-mounted industrial control computer according to claim 7, characterized in that: The fixed table (2) is provided with an upper table surface and a lower table surface, which are respectively located on the upper and lower sides of the adapter plate (8).

9. A vibration-resistant and anti-glare seat-mounted industrial control computer according to claim 8, characterized in that: The handle (5) is mounted on the upper platform, and the trackball (6) and keyboard (9) are mounted on the lower platform.

10. A vibration-resistant and anti-glare seat-mounted industrial control computer according to claim 1, characterized in that: The folding sunshade (4) is made of dark-colored flame-retardant composite material.

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