A civil aviation control seat cabinet

Abstract

The utility model relates to the field of aviation management technology, and discloses a civil aviation control seat cabinet, including a main cabinet and a base, wherein the lower end surface of the main cabinet is fixedly provided with a base, and an outer table top is fixedly installed on the upper side of the rear end surface of the main cabinet, and driving motors are provided at both left and right ends of the inner side of the lower end of the main cabinet, and also includes: an adjustment component, which is provided at the output end of the driving motor and is located inside the main cabinet; a support component, which is respectively installed at the left and right ends of the lower side of the front end of the adjustment component. The civil aviation control seat cabinet can make a more convenient height adjustment to the internal table top while maintaining a consistent appearance, so that a more comfortable left height adjustment can be made for each different staff member, making the staff more comfortable when checking in.

Description

Technical Field

[0001] The utility model relates to the field of aviation management, in particular to a civil aviation control seat cabinet. Background Art

[0002] An airline refers to an enterprise that uses various aircraft as transportation tools to carry people or goods by air. With the continuous progress of today's society, traveling by plane, transporting goods, etc. has become one of the choices for the general public and is an indispensable means of transportation in today's society.

[0003] When taking a plane, you need to go to a designated workplace to check in. Since the staff handling the business are of different shapes and sizes, the check-in cabinets need to have the same appearance but meet the needs of the staff who need to sit for a long time as much as possible inside, so that the staff can have a better sitting experience as much as possible when working for a long time. However, some check-in cabinets on the market are all integrated fixed cabinets, which are not friendly to the staff who sit for a long time. Therefore, a civil aviation control seat cabinet is proposed. Utility Model Content

[0004] 1. Technical issues to be resolved

[0005] In view of the deficiencies in the prior art, the utility model provides a civil aviation control seat cabinet, which can make convenient height adjustments to the internal desktop while maintaining a consistent appearance, thereby making it possible to make more comfortable left-side height adjustments for each different staff member, making the staff more comfortable when checking in.

[0006] Technical Solution

[0007] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0008] A civil aviation control seat cabinet comprises a main cabinet and a base, wherein the base is fixedly arranged on the lower end surface of the main cabinet, and an outer table is fixedly installed on the upper side of the rear end surface of the main cabinet, and driving motors are arranged on both left and right ends of the inner side of the lower end of the main cabinet, and further comprises:

[0009] A regulating component, which is arranged at the output end of the driving motor and is located inside the main cabinet;

[0010] The supporting components are respectively installed at the left and right ends of the lower front end of the adjusting component.

[0011] As a preferred technical solution of the utility model, the adjustment assembly includes a connecting rod, a connecting block, a first fixing block, a second fixing block and an inner table top;

[0012] A connecting rod, which is arranged at the output end of the driving motor;

[0013] A connecting block, which is installed on the outer side of the lower end of the connecting rod and is located on the inner side of the main cabinet;

[0014] A first fixing block, which is fixedly arranged at the middle of the rear end surface of the connecting block;

[0015] A second fixing block, which is fixedly installed at the middle of the front end surface of the connecting block;

[0016] The inner table top is fixedly arranged on the front end surface of the second fixing block.

[0017] As a preferred technical solution of the utility model, the support assembly includes an upper fixing rod, a lower fixing rod and a fixing bolt;

[0018] Upper fixing rods, which are respectively fixedly mounted on the left and right ends of the front side of the lower end of the inner table top;

[0019] A lower fixing rod, which is arranged on the inner side of the upper fixing rod;

[0020] The fixing bolts are arranged in groups of two at the front and rear sides of the lower end of the upper fixing rod.

[0021] As a preferred technical solution of the utility model, the connecting block forms an integrated structure with the first fixed block and the second fixed block respectively, and the connecting block is externally threadedly connected to the connecting rod, the first fixed block is engaged with the main cabinet, and a groove structure is provided on the inner side of the rear end of the main cabinet for the first fixed block to slide.

[0022] As a preferred technical solution of the utility model, the upper fixing rod is slidably connected to the lower fixing rod, and the upper fixing rod is internally threadedly connected to the fixing bolt.

[0023] As a preferred technical solution of the utility model, the fixing bolt is tightly abutted against the lower fixing rod.

[0024] Beneficial Effects

[0025] Compared with the prior art, the utility model provides a civil aviation control seat cabinet, which has the following

[0026] Beneficial effects:

[0027] The civil aviation control seat cabinet can control the connecting block through the connecting rod to drive the inner table top to adjust the height more conveniently, and at the same time, the fixing bolt can provide a more stable fastening function for the lower fixing rod, so that the front end of the inner table top has better stability. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] Figure 1 It is a schematic diagram of the side cross-sectional structure of the utility model;

[0029] Figure 2 This is a schematic diagram of the front view structure of the utility model;

[0030] Figure 3 This is a schematic diagram of the cross-sectional structure of the utility model from top view;

[0031] Figure 4 For this utility model Figure 1 Enlarged structural diagram at A in the middle.

[0032] In the figure: 1, main cabinet; 2, base; 3, outer table; 4, drive motor; 51, connecting rod; 52, connecting block; 53, first fixing block; 54, second fixing block; 55, inner table; 61, upper fixing rod; 62, lower fixing rod; 63, fixing bolt. DETAILED DESCRIPTION

[0033] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0034] In the description of the present invention, it should be understood that the terms "center", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc., indicating the orientation or position relationship are based on the orientation or position relationship shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention.

[0035] See also Figure 1-4

[0036] In this embodiment, a civil aviation control seat cabinet includes a main cabinet 1 and a base 2, wherein the base 2 is fixedly arranged on the lower end surface of the main cabinet 1, and an outer table 3 is fixedly installed on the upper side of the rear end surface of the main cabinet 1, and a driving motor 4 is arranged on both left and right ends of the inner side of the lower end of the main cabinet 1;

[0037] It should be noted that the main cabinet 1 is the main structure of the cabinet, which is a complete cabinet for accommodating and protecting the internal electronic equipment and circuits. The base 2 is the base or foot of the cabinet, which is used to support the entire cabinet and ensure that it is stably placed on the ground or other planes. The external table 3 is used as a workbench for people from outside to handle business. It is fixed to the upper side of the rear end surface of the main cabinet 1 with a triangular support frame. The drive motor 4 is an existing drive motor, which is fixedly installed on the inner side of the main cabinet 1 using an existing installation method, and is arranged symmetrically based on the lower inner end of the main cabinet 1.

[0038] In this embodiment, the adjustment assembly is composed of a connecting rod 51, a connecting block 52, a first fixing block 53, a second fixing block 54 and an inner desktop table 55. The connecting rod 51 is arranged at the output end of the driving motor 4, the connecting block 52 is installed on the outer side of the lower end of the connecting rod 51 and is located on the inner side of the main cabinet 1, the first fixing block 53 is fixedly arranged in the middle of the rear end surface of the connecting block 52, the second fixing block 54 is fixedly arranged in the middle of the front end surface of the connecting block 52, and the inner desktop table 55 is fixedly arranged on the front end surface of the second fixing block 54;

[0039] It should be noted that the connecting rod 51 is installed on the output end of the driving motor 4 in an existing fixing manner, and the connecting rod 51 is externally threadedly connected to the connecting block 52, so that when the connecting rod 51 rotates, it can drive the connecting block 52 to rotate, and the connecting block 52 forms an integrated structure with the first fixed block 53 and the second fixed block 54. At the same time, the first fixed block 53 and the second fixed block 54 form a sliding structure inside the main cabinet 1, thereby providing a limiting function for the connecting block 52, so that when the connecting block 52 rotates through the connecting rod 51, it moves up and down based on the limiting of the first fixed block 53 and the second fixed block 54. A groove structure for the first fixed block 53 to slide is provided at the inner rear end of the main cabinet 1, and the first fixed block 53 is engaged with the main cabinet 1, and the inner desktop 55 is used to provide a working platform for the staff.

[0040] In this embodiment, the support assembly is composed of an upper fixing rod 61, a lower fixing rod 62 and a fixing bolt 63. The upper fixing rod 61 is fixedly mounted on the left and right ends of the front side of the lower end of the inner table 55. In addition, the lower fixing rod 62 is arranged on the inner side of the upper fixing rod 61. Furthermore, the fixing bolts 63 are arranged in pairs at the front and rear sides of the lower end of the upper fixing rod 61.

[0041] It should be noted that the upper fixing rod 61 is symmetrically arranged based on the vertical center axis of the inner table top 55. At the same time, the upper fixing rod 61 is slidably connected to the lower fixing rod 62. The upper fixing rod 61 is connected to the internal thread of the fixing bolt 63. In addition, the fixing bolt 63 is tightly pressed against the lower fixing rod 62. When the fixing bolt 63 is rotated, the fixing bolt 63 will move left and right through the threaded connection with the upper fixing rod 61, thereby providing kinetic energy for the lower fixing rod 62 to be pressed and stabilized, so that the upper fixing rod 61 provides support function for the front ends of the inner table top 55.

[0042] Working principle: The main cabinet 1 is stably placed in the designated position through the base 2. When the height of the inner desktop 55 needs to be adjusted, the fixing bolt 63 is first rotated to release the tight state of the lower fixing rod 62, so that the upper fixing rod 61 can slide outside the lower fixing rod 62. Then, the driving motors 4 on the left and right sides of the main cabinet 1 that are electrically connected to the electric control switch using existing technology are used to drive the connecting rod 51 to rotate, and then the connecting block 52 drives the inner desktop 55 to be raised and lowered through the second fixing block 54. Finally, when the height of the inner desktop 55 is adjusted to a suitable position, the fixing bolt 63 is rotated to provide a tight fit to the lower fixing rod 62, so that the front end of the inner desktop 55 has a better stable manufacturing function.

[0043] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A civil aviation control seat cabinet, comprising a main cabinet (1) and a base (2), wherein the base (2) is fixedly arranged on the lower end surface of the main cabinet (1), and an outer table (3) is fixedly installed on the upper side of the rear end surface of the main cabinet (1), and driving motors (4) are arranged on both left and right ends of the inner side of the lower end of the main cabinet (1), characterized in that: Also includes: An adjustment component, which is arranged at the output end of the drive motor (4) and is located inside the main cabinet (1); Support components, which are respectively installed at the left and right ends of the lower side of the front end of the adjustment component; The adjustment assembly comprises a connecting rod (51), a connecting block (52), a first fixing block (53), a second fixing block (54) and an inner table top (55); A connecting rod (51) disposed at an output end of the driving motor (4); A connecting block (52) is mounted on the outer side of the lower end of the connecting rod (51) and is located on the inner side of the main cabinet (1); A first fixing block (53) fixedly disposed at the middle portion of the rear end surface of the connecting block (52); A second fixing block (54) fixedly mounted on the middle portion of the front end surface of the connecting block (52); The inner table top (55) is fixedly arranged on the front end surface of the second fixing block (54).

2. A civil aviation control seat cabinet according to claim 1, characterized in that: The support assembly comprises an upper fixing rod (61), a lower fixing rod (62) and a fixing bolt (63); Upper fixing rods (61) are respectively fixedly mounted on the left and right ends of the front side of the lower end of the inner table top (55); A lower fixing rod (62) disposed on the inner side of the upper fixing rod (61); The fixing bolts (63) are arranged in groups of two at the front and rear sides of the lower end of the upper fixing rod (61).

3. A civil aviation control seat cabinet according to claim 2, characterized in that: The connecting block (52) respectively forms an integrated structure with the first fixing block (53) and the second fixing block (54), and the connecting block (52) is externally threadedly connected to the connecting rod (51), the first fixing block (53) is engaged with the main cabinet (1), and a groove structure for the first fixing block (53) to slide is provided on the inner side of the rear end of the main cabinet (1).

4. The civil aviation control seat cabinet according to claim 3, characterized in that: The upper fixing rod (61) is slidably connected to the lower fixing rod (62), and the upper fixing rod (61) is internally threadedly connected to the fixing bolt (63).

5. The civil aviation control seat cabinet according to claim 3, characterized in that: The fixing bolt (63) is tightly pressed against the lower fixing rod (62).

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