Angle-adjustable aero seat table board

Abstract

The utility model discloses an angle-adjustable aero seat table board which comprises a table board body, the table board body is connected with a handrail through a supporting assembly, and a height adjusting mechanism capable of adjusting the height of the table board body and an angle adjusting mechanism capable of adjusting the inclination angle of the table board body are arranged on the table board body. The desk is simple in structure and reasonable in design, the angle adjusting mechanism is arranged, the desk plate is pulled out and rotated to drive the angle adjusting gear to rotate so as to adjust the inclination angle, the desk plate is pushed in, the angle fixing ring is matched with the angle adjusting gear so as to fix the inclination angle, and the inclination angle of the desk plate can be adjusted and fixed. The height adjusting mechanism is arranged, an adjusting rod can move up and down in an adjusting groove to adjust the height, the adjusting rod can move left and right to fix the height, the height of the table board can be matched with the heights and figures of different passengers, and the supporting assembly can enable the table board to be supported more stably.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation accessories, in particular to an aviation seat table with adjustable angles. Background Art

[0002] Airline seat tables are usually installed behind the front seats, and airline seats with multiple rows of seats also have them installed behind them, on which food, laptops, etc. can be placed. However, some tables have a single function and can only be used as tables to place things. When passengers want to use electronic products, the seat table cannot provide the desired angle support for the electronic products used by the passengers, affecting the user experience of the passengers. At the same time, the height cannot be adjusted, and it is not very convenient to use. Utility Model Content

[0003] The purpose of the present invention is to provide an aviation seat table with adjustable angle to solve the problems raised in the above background technology.

[0004] To achieve the above-mentioned object, the present invention provides the following technical solution: an angle-adjustable aviation seat table, comprising a table, characterized in that: the table is connected to an armrest via a support assembly, and a height adjustment mechanism and an angle adjustment mechanism are provided on the table;

[0005] The height adjustment mechanism includes:

[0006] An adjustment slot is provided on a side of the armrest;

[0007] An adjusting rod, the adjusting rod being movably connected to the adjusting slot, and a rotating shaft being provided at one end of the adjusting rod;

[0008] A rotating rod, one end of which is penetrated by a circular hole for passing through the rotating shaft, and the other end of which is connected to the angle adjustment mechanism.

[0009] Preferably, a sliding cavity for sliding is provided inside the rotating rod.

[0010] Preferably, the angle adjustment mechanism includes:

[0011] A fixed plate, the fixed plate being fixedly arranged at the bottom of the table top;

[0012] A tilting rod, one end of which passes through a hole on the fixed plate and is fixedly connected to the fixed plate, and the other end of which is disposed in the sliding cavity and is slidably connected to the sliding cavity;

[0013] An angle adjustment gear, the angle adjustment gear passes through the tilt rod and is fixed on the tilt rod;

[0014] An angle fixing ring is fixedly arranged on the rotating rod.

[0015] Preferably, the support assembly includes:

[0016] A support shaft, the support shaft being arranged on a side surface of the armrest;

[0017] A support rod, the support rod being rotatably connected to the support shaft;

[0018] The support groove is arranged on the back side of the table top at one end away from the armrest.

[0019] Preferably, a groove matching the angle adjustment gear is provided in the angle fixing ring.

[0020] Preferably, a water cup groove is provided on the table top.

[0021] Preferably, a mobile phone slot is provided on the table top.

[0022] Compared with the prior art, the beneficial effects of the present invention are:

[0023] 1. This angle-adjustable aviation seat table is equipped with an angle adjustment mechanism, which includes a fixed plate, a tilt rod, an angle adjustment gear, and an angle fixing ring. The angle adjustment gear adjusts the tilt angle, and the angle fixing ring fixes the tilt angle, so that the table can adjust the tilt angle and be fixed, which is convenient for passengers to use in different scenarios.

[0024] 2. This kind of aviation seat table with adjustable angle is equipped with a height adjustment mechanism. The height adjustment mechanism includes an adjustment slot and an adjustment rod. The adjustment rod can be moved up and down in the adjustment slot to adjust the height, and the adjustment rod can be moved left and right to fix the height, so that the height of the table can be matched with the height and body shape of different passengers. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 This is a schematic diagram of the front structure of the utility model;

[0026] Figure 2 It is a side structural diagram of the utility model;

[0027] Figure 3 This is a schematic diagram of the bottom surface of the table top of the present invention;

[0028] Figure 4 This is a schematic diagram of angle adjustment of the present utility model;

[0029] Figure 5 This is a detailed schematic diagram of the angle adjustment gear and angle fixing ring of the utility model;

[0030] Figure 6 This is a schematic diagram of the upper surface of the table top of the present invention.

[0031] In the figure: 1. Table top; 101. Support shaft; 102. Support rod; 103. Support slot; 104. Cup slot; 105. Mobile phone slot; 2. Armrest; 3. Height adjustment mechanism; 301. Adjustment slot; 302. Adjustment rod; 303. Rotational shaft; 304. Rotational rod; 305. Sliding cavity; 4. Angle adjustment mechanism; 401. Fixed plate; 402. Tilt rod; 403. Angle adjustment gear; 404. Angle fixing ring. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0033] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise" and the like to indicate orientations or positional relationships based on the orientations or positional relationships 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 should not be understood as a limitation on the present invention.

[0034] In the description of this patent, it should be noted that, unless otherwise expressly specified or limited, the terms "installed," "connected," and "disposed" should be understood broadly. For example, they can refer to fixed connection or disposition, detachable connection or disposition, or integrated connection or disposition. Those skilled in the art will understand the specific meanings of the above terms in this patent based on the specific circumstances.

[0035] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of the technical features being referred to. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of such features. In the description of this utility model, "several" means two or more, unless otherwise specifically defined.

[0036] Example 1

[0037] See also Figure 1-6As shown, the utility model provides a technical solution for an aviation seat table with adjustable angle: an aviation seat table with adjustable angle, comprising a table 1, the table 1 is connected to an armrest 2 by setting a supporting assembly, and a height adjustment mechanism 3 and an angle adjustment mechanism 4 are set on the table 1.

[0038] The height adjustment mechanism 3 includes: an adjustment slot 301, an adjustment rod 302, a rotating shaft 303, a rotating rod 304, and a sliding cavity 305. The adjustment slot 301 is opened on the side of the armrest 2, and the adjustment rod 302 is movably connected to the adjustment slot 301. A rotating shaft 303 is fixed to the end of the adjustment rod 302 close to the table top 1. A circular hole is passed through one end of the rotating rod 304, which passes through the rotating shaft 303 and is rotatably connected to the rotating shaft. The other end of the rotating rod 304 is connected to the angle adjustment mechanism 4, and a sliding cavity 305 for sliding is opened inside the rotating rod 304.

[0039] The angle adjustment mechanism 4 includes: a fixed plate 401, a tilting rod 402, an angle adjustment gear 403, and an angle fixing ring 404. The fixed plate 401 is fixedly set at the bottom of the table top 1. One end of the tilting rod 402 passes through the hole on the fixed plate 401 and is fixedly connected to the fixed plate 401. The other end of the tilting rod 402 is set in the sliding cavity 305 and is slidably connected to the sliding cavity 305. The angle adjustment gear 403 passes through the tilting rod 402 and is fixed on the tilting rod 402. The angle fixing ring 404 is fixedly set on the rotating rod 304.

[0040] The support assembly includes: a support shaft 101, a support rod 102, and a support groove 103. The support shaft 101 is arranged on the side of the armrest 2, and the support rod 102 is rotatably connected to the support shaft 101; the support groove 103 is arranged on the back of the table top 1 at one end away from the armrest 2.

[0041] A groove matching the angle adjustment gear 403 is provided in the angle fixing ring 404 .

[0042] A cup groove 104 for placing cups is provided on the table top 1 .

[0043] A mobile phone slot 105 for placing a mobile phone is provided on the table top 1 .

[0044] The working principle of this utility model is as follows:

[0045] When using an angle-adjustable aviation seat table in this embodiment, the height of the table 1 is adjusted through the height adjustment mechanism 3, the table 1 is lifted, the rotating rod 304 is rotated around the rotating axis 303, the adjustment rod 302 is toggled, and the position of the adjustment rod 302 in the adjustment slot 301 can be adjusted to adjust the height of the table 1. The tilt angle of the table 1 is adjusted through the angle adjustment mechanism 4, the table 1 is pulled away from the armrest 2, the angle adjustment gear 403 is turned to tilt the table 1 to a suitable angle, the table 1 is pushed back to make the angle fixing ring 404 and the angle fixing gear fit together to fix the tilt angle, and after the adjustment is completed, the support rod 102 is pulled up so that the support rod 102 is supported at the support slot 103.

[0046] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely preferred examples of the present invention and are not intended to limit the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.

Claims

1. An angle-adjustable aviation seat table, comprising a table (1), characterized in that: The table top (1) is connected to an armrest (2) by providing a support assembly, and a height adjustment mechanism (3) and an angle adjustment mechanism (4) are provided on the table top (1); The height adjustment mechanism (3) comprises: An adjustment slot (301), the adjustment slot (301) being provided on a side surface of the armrest (2); An adjusting rod (302), the adjusting rod (302) being movably connected to the adjusting slot (301), and a rotating shaft (303) being provided on one end of the adjusting rod (302) close to the table top (1); A rotating rod (304) is provided at one end with a circular hole passing through the rotating shaft (303), and the other end of the rotating rod (304) is connected to the angle adjustment mechanism (4).

2. The angle-adjustable aircraft seat table according to claim 1, characterized in that: A sliding cavity (305) for sliding is provided inside the rotating rod (304).

3. The angle-adjustable aircraft seat table according to claim 1, characterized in that: The angle adjustment mechanism (4) comprises: A fixed plate (401), the fixed plate (401) being fixedly arranged on the bottom of the table top (1); a tilting rod (402), one end of the tilting rod (402) passing through a hole on the fixed disk (401) and fixedly connected to the fixed disk (401), and the other end of the tilting rod (402) being disposed in the sliding cavity (305) and slidably connected to the sliding cavity (305); An angle adjustment gear (403), the angle adjustment gear (403) passes through the tilt rod (402) and is fixed on the tilt rod (402); An angle fixing ring (404), wherein the angle fixing ring (404) is fixedly arranged on the rotating rod (304).

4. The angle-adjustable aircraft seat table according to claim 1, characterized in that: The support assembly includes: A support shaft (101), wherein the support shaft (101) is arranged on a side surface of the handrail (2); A support rod (102), the support rod (102) being rotatably connected to the support shaft (101); A support groove (103) is provided at an end of the back of the table top (1) away from the armrest (2).

5. The angle-adjustable aircraft seat table according to claim 3, characterized in that: A groove matching the angle adjustment gear (403) is provided in the angle fixing ring (404).

6. The angle-adjustable aircraft seat table according to claim 1, characterized in that: A water cup groove (104) is provided on the table top (1).

7. The angle-adjustable aircraft seat table according to claim 1, characterized in that: A mobile phone slot (105) is provided on the table top (1).

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