Airplane seat part facing adjusting device

Abstract

The utility model discloses an aircraft seat spare and accessory part orientation adjusting device which comprises a fixing base plate, the fixing base plate is provided with a connecting mechanism, the connecting mechanism comprises a limiting assembly arranged in the middle section of the fixing base plate, the upper section of the limiting assembly is connected with an adjusting assembly, and the front face of the limiting assembly is connected with a connecting assembly. The outer wall of the connected sliding rod is sleeved with a first limiting spring, the connected first limiting spring pushes a moving block sliding on the outer wall of the sliding rod to move, the front face of a fixing base fixedly connected to the front face of the moving block is fixedly connected with a fixing sleeve, and a second limiting spring fixedly connected to the inner wall of the fixing sleeve pushes a push sleeve fixedly connected to the inner side to move. The movable push sleeve slides on the inner wall of the fixing sleeve, a third limiting spring fixedly connected to the inner wall of the push sleeve pushes a fixedly-connected push rod to move, a limiting block fixedly connected to the inner side of the movable push rod moves, the connected limiting block limits a to-be-machined part, and facing adjustment of spare and accessory parts is facilitated.

Description

Technical Field

[0001] The utility model belongs to the technical field of aircraft seat component orientation adjustment devices, in particular to an aircraft seat component orientation adjustment device. Background Art

[0002] Because airplane seats are passengers' first impression of a flight, an airline's image is largely determined by their appearance and comfort. Aircraft seats are assembled from a variety of parts and components. Parts and components are the indivisible, individual components that make up an aircraft seat and serve as the basic mechanical unit. Aircraft seat parts and components are categorized as general-purpose and specialized. General-purpose parts are widely used in various machines, while mechanical parts and components require adaptive adjustments during processing.

[0003] However, during use, traditional aircraft seat component orientation adjustment devices require manual adjustment of the component orientation, which affects the convenience of multi-directional adjustment of the component orientation and increases the labor workload of personnel. Based on this, a device for adjusting the component orientation of an aircraft seat is proposed to solve the above problems. Utility Model Content

[0004] The purpose of the utility model is to provide an aircraft seat component orientation adjustment device to solve the technical problems raised in the background technology.

[0005] To achieve the above-mentioned object, the specific technical solution of the present invention is as follows: A facing adjustment device for an aircraft seat component includes a fixed base plate, the fixed base plate is provided with a connecting mechanism, the connecting mechanism includes a limit assembly provided in the middle section of the fixed base plate, the upper section of the limit assembly is connected to an adjustment assembly, and the front face of the limit assembly is connected to a connecting assembly;

[0006] The adjusting assembly includes a rotating shaft, the front face of the rotating shaft is fixedly connected to a turntable, the inner wall of the limiting sliding groove provided on the turntable is fixedly connected to a sliding rod, the outer wall of the sliding rod is sleeved with a limiting spring 1, the outer wall of the sliding rod is slidably connected to a moving block, the front face of the moving block is fixedly connected to a fixed seat, the front face of the fixed seat is fixedly connected to a fixed sleeve, the inner wall of the fixed sleeve is fixedly connected to a limiting spring 2, the inner side of the limiting spring 2 is fixedly connected to a push sleeve, the inner wall of the push sleeve is fixedly connected to a limiting spring 3, the inner side of the limiting spring 3 is fixedly connected to a push rod, and the inner side of the push rod is fixedly connected to the limiting block.

[0007] Preferably, the limiting assembly includes a fixing frame fixedly mounted on the top of the fixed base plate, the inner wall of the limiting sliding opening opened in the middle section of the fixing frame is slidably connected to the sliding frame, the top of the sliding frame is fixedly connected to the insertion rod, the top of the middle section of the fixed base plate is fixedly connected to the vertical pole, and the outer wall of the lower section of the vertical pole is sleeved with a connecting spring.

[0008] Preferably, the connecting assembly includes a telescopic rod, the outer wall of the telescopic rod is fixedly connected to a connecting rod 1, the connecting rod 1 is fixedly installed with a connecting rod 2 by a bolt, the connecting rod 2 is fixedly connected to a connecting rod 3, and the inner side of the connecting rod 3 is fixedly connected to a receiving block.

[0009] Preferably, the rotating shaft is rotatably connected to the inner wall of the fixed frame, and the rotating shaft is evenly provided with limiting holes, and the turntable is provided with a limiting slide groove; a sliding rod is fixedly connected to the inner wall of the limiting slide groove provided on the turntable, and a limiting spring 1 is sleeved on the outer wall of the connected sliding rod, and the connected limiting spring 1 pushes the moving block sliding on the outer wall of the sliding rod to move.

[0010] Preferably, the insertion rod is slidably connected to the inner wall of the limiting hole opened on the rotating shaft, and the outer wall of the vertical rod is slidably connected to the insertion rod and the inner wall of the sliding frame; a fixed frame is fixedly installed on the top of the connected fixed base plate, and a limiting sliding mouth opened in the middle section of the connected fixed frame is slidably connected to the sliding frame, the outer wall of the vertical rod fixed on the top of the middle section of the fixed base plate is sleeved with the vertical rod, the top of the connected sliding frame is connected with the insertion rod, and the connected sliding frame and the insertion rod are slidably connected to the outer wall of the vertical rod.

[0011] Preferably, the telescopic rod is fixedly connected to the front of the fixing frame, and the inner outer wall of the bolt is slidably connected to the inner wall of the limiting sliding groove opened on the turntable; the outer wall of the telescopic rod fixedly connected to the front of the fixing frame is fixedly connected to the connecting rod 1, the connected connecting rod 1 is fixedly connected to the connecting rod 2 by a bolt, and the inner side of the connecting rod 3 fixedly connected to the connecting rod 2 is fixedly connected to the receiving block.

[0012] The utility model provides an aircraft seat component orientation adjustment device with the following advantages:

[0013] 1. The aircraft seat spare parts facing adjustment device has a sliding rod fixedly connected to the inner wall of the limiting slide groove provided on the turntable, and the outer wall of the connected sliding rod is sleeved with a limiting spring 1, and the connected limiting spring 1 pushes the moving block sliding on the outer wall of the sliding rod to move, and the front side of the fixed seat fixedly connected to the front side of the moving block is fixedly connected to a fixed sleeve, and the limiting spring 2 fixedly connected to the inner wall of the fixed sleeve pushes the push sleeve fixedly connected on the inner side to move, and the moving push sleeve slides on the inner wall of the fixed sleeve, and the limiting spring 3 fixedly connected to the inner wall of the push sleeve pushes the fixedly connected push rod to move, and the limiting block fixedly connected to the inner side of the moving push rod moves, and the connected limiting block limits the parts to be processed and is convenient for adjusting the facing of the spare parts.

[0014] 2. The aircraft seat spare part faces the adjustment device, and the outer wall of the telescopic rod fixedly connected to the front of the fixing frame is fixedly connected to the connecting rod 1, and the connecting rod 1 is fixedly connected to the connecting rod 2 by a bolt. The inner side of the connecting rod 3 fixedly connected to the connecting rod 2 is fixedly connected to the receiving block. The connected receiving block limits the position of the limited spare part, which facilitates the overall part processing. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following is a brief introduction to the drawings required for use in the embodiments. It should be understood that the following drawings only show certain embodiments of the present invention and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without creative work.

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0017] Figure 2 This is a schematic diagram of the back structure of the utility model;

[0018] Figure 3 It is a schematic diagram of the local structure of the utility model;

[0019] Figure 4 It is a partial enlarged structural schematic diagram of the utility model;

[0020] Explanation of the marks in the figure: 1. Fixed base plate; 2. Connecting mechanism; 21. Limiting assembly; 211. Fixed frame; 212. Sliding frame; 213. Inserting rod; 214. Vertical rod; 215. Connecting spring; 22. Adjusting assembly; 221. Rotating shaft; 222. Turntable; 223. Sliding rod; 224. Limiting spring one; 225. Moving block; 226. Fixed seat; 227. Fixed sleeve; 228. Limiting spring two; 229. Push sleeve; 2210. Limiting spring three; 2211. Push rod; 2212. Limiting block; 23. Connecting assembly; 231. Telescopic rod; 232. Connecting rod one; 233. Bolt; 234. Connecting rod two; 235. Connecting rod three; 236. Supporting block. DETAILED DESCRIPTION

[0021] Hereinafter, only certain exemplary embodiments are briefly described. As will be appreciated by those skilled in the art, the described embodiments may be modified in various ways without departing from the spirit or scope of the embodiments of the present invention. Therefore, the drawings and description are to be regarded as illustrative in nature and not restrictive.

[0022] In the description of the embodiments of the present invention, it should be understood that the terms "length", "vertical", "horizontal", "top", "bottom", 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 embodiments of the present invention and simplifying the description, rather than indicating or implying 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 embodiments of the present invention.

[0023] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be understood to indicate or imply relative importance or implicitly specify the number of the technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of the features. In the description of the embodiments of the present invention, "plurality" means two or more, unless otherwise specifically defined.

[0024] In the embodiments of the present invention, unless otherwise expressly specified or limited, the terms "installed," "connected," "connected," "fixed," etc. should be understood in a broad sense. For example, they can refer to fixed connection, detachable connection, or integration; mechanical connection, electrical connection, or communication; direct connection or indirect connection through an intermediate medium; internal communication between two components or interaction between two components. Those skilled in the art will understand the specific meanings of the above terms in the embodiments of the present invention based on specific circumstances.

[0025] The disclosure below provides many different embodiments or examples for implementing different structures of the embodiments of the present invention. In order to simplify the disclosure of the embodiments of the present invention, the components and settings of specific examples are described below. Of course, these are merely examples and are not intended to limit the embodiments of the present invention. In addition, the embodiments of the present invention may repeat reference numbers and / or reference letters in different examples. Such repetition is for the purpose of simplicity and clarity and does not in itself indicate the relationship between the various embodiments and / or settings discussed.

[0026] In order to better understand the purpose, structure and function of the present invention, the following is a further detailed description of the aircraft seat component orientation adjustment device of the present invention in conjunction with the accompanying drawings.

[0027] like Figure 1-4As shown, an aircraft seat spare part facing adjustment device of the present invention includes a fixed base plate 1, the fixed base plate 1 is provided with a connecting mechanism 2, the connecting mechanism 2 includes a limiting component 21 arranged in the middle section of the fixed base plate 1, the upper section of the limiting component 21 is connected to the adjustment component 22, and the front of the limiting component 21 is connected to the connecting component 23; the adjustment component 22 includes a rotating shaft 221, the front of the rotating shaft 221 is fixedly connected to a turntable 222, the inner wall of the limiting slide groove provided by the turntable 222 is fixedly connected to a sliding rod 223, the outer wall of the sliding rod 223 is sleeved with a limiting spring 1 224, the outer wall of the sliding rod 223 is slidably connected to a moving block 225, the front of the moving block 225 is fixedly connected to a fixing seat 226, the front of the fixing seat 226 is fixedly connected to a fixing sleeve 227, the inner wall of the fixing sleeve 227 is fixedly connected to a limiting spring 228, the inner side of the limiting spring 228 is fixedly connected to a pushing sleeve 229, and the inner wall of the pushing sleeve 229 is fixedly connected to a limiting spring 3 221 0, the inner side of the limit spring 2210 is fixedly connected to a push rod 2211, and the inner side of the push rod 2211 is fixedly connected to a limit block 2212; the limit assembly 21 includes a fixed frame 211 fixedly mounted on the top of the fixed base plate 1, the inner wall of the limit sliding opening opened in the middle section of the fixed frame 211 is slidably connected to a sliding frame 212, the top of the sliding frame 212 is fixedly connected to an insertion rod 213, the top of the middle section of the fixed base plate 1 is fixedly connected to a vertical rod 214, and the outer wall of the lower section of the vertical rod 214 is sleeved with a connecting rod. Connecting spring 215; connecting assembly 23 includes telescopic rod 231, the outer wall of which is fixedly connected to connecting rod 1 232. Connecting rod 1 232 is fixedly mounted to connecting rod 234 via bolt 233. Connecting rod 234 is fixedly connected to connecting rod 3 235. Connecting rod 3 235 is fixedly connected to the inner wall of connecting rod 3 235. The inner side of connecting rod 3 235 is fixedly connected to a receiving block 236; rotating shaft 221 is rotatably connected to the inner wall of fixed frame 211, and rotating shaft 221 is evenly provided with limiting holes, and rotating disk 222 is provided with a limiting slot. Insertion rod 213 is slidably connected to the inner wall of the limiting hole provided in rotating shaft 221, and the outer wall of vertical rod 214 is slidably connected to insertion rod 213 and the inner wall of sliding frame 212; telescopic rod 231 is fixedly connected to the front of fixed frame 211, and the inner outer wall of bolt 233 is slidably connected to the inner wall of the limiting slot provided in rotating disk 222.

[0028] The working principle of the aircraft seat spare part facing adjustment device: when the aircraft seat spare part facing adjustment device is actually used, the fixed base plate 1 is fixedly installed with a fixed frame 211 on the top, and the limiting sliding mouth opened in the middle section of the connected fixed frame 211 is slidably connected with the sliding frame 212. The outer wall of the vertical rod 214 fixed to the top of the middle section of the fixed base plate 1 is sleeved with the vertical rod 214, and the top of the connected sliding frame 212 is connected with the insertion rod 213. The connected sliding frame 212 and the insertion rod 213 are slidably connected to the outer wall of the vertical rod 214, so that the connected insertion rod 213 can be moved upward, and the rotating shaft 221 connected to the inner wall of the fixed frame 211 is evenly provided with limiting holes. The connected insertion rod 213 slides into the inner wall of the limiting hole to limit the connected rotating shaft 221, and the turntable 222 fixedly connected to the front face of the rotating shaft 221 is limited accordingly, which is convenient for overall angle adjustment;

[0029] The inner wall of the limiting slide groove provided on the turntable 222 is fixedly connected with a slide rod 223, and the outer wall of the connected slide rod 223 is sleeved with a limiting spring 1 224. The connected limiting spring 1 224 pushes the moving block 225 that slides on the outer wall of the slide rod 223 to move. The front side of the fixed seat 226 fixedly connected to the front side of the moving block 225 is fixedly connected with a fixed sleeve 227. The limiting spring 228 fixedly connected to the inner wall of the fixed sleeve 227 pushes the push sleeve 229 fixedly connected on the inner side to move. The moving push sleeve 229 slides on the inner wall of the fixed sleeve 227. The limiting spring 3 2210 fixedly connected to the inner wall of the push sleeve 229 pushes the fixedly connected push rod 2211 to move. The limiting block 2212 fixedly connected to the inner side of the moving push rod 2211 moves. The connected limiting block 2212 limits the parts to be processed and is convenient for adjusting the orientation of the spare parts.

[0030] The outer wall of the telescopic rod 231 fixedly connected to the front of the fixed frame 211 is fixedly connected with a connecting rod 1 232, and the connected connecting rod 1 232 is fixedly connected to the connecting rod 2 234 through a bolt 233. The inner side of the connecting rod 3 235 fixedly connected to the connecting rod 2 234 is fixedly connected with a receiving block 236. The connected receiving block 236 limits the limited spare parts to facilitate the overall parts processing.

[0031] It is understood that the present invention is described by way of certain embodiments, and those skilled in the art will appreciate that various changes or equivalent substitutions may be made to these features and embodiments without departing from the spirit and scope of the present invention. Furthermore, under the guidance of the present invention, these features and embodiments may be modified to suit specific circumstances and materials without departing from the spirit and scope of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed herein, and all embodiments falling within the scope of the claims of this application are intended to be protected by the present invention.

Claims

1. An aircraft seat component orientation adjustment device, comprising a fixed base plate (1), characterized in that: The fixed base plate (1) is provided with a connecting mechanism (2), the connecting mechanism (2) comprising a limiting component (21) provided in the middle section of the fixed base plate (1), an adjusting component (22) being connected to the upper section of the limiting component (21), and a connecting component (23) being connected to the front side of the limiting component (21); The adjustment assembly (22) includes a rotating shaft (221), the front face of the rotating shaft (221) is fixedly connected to a turntable (222), the inner wall of the limiting sliding groove provided in the turntable (222) is fixedly connected to a slide rod (223), the outer wall of the slide rod (223) is sleeved with a limiting spring (224), the outer wall of the slide rod (223) is slidably connected to a moving block (225), the front face of the moving block (225) is fixedly connected to a fixing seat (226), and the fixing seat The front side of (226) is fixedly connected with a fixed sleeve (227), the inner wall of the fixed sleeve (227) is fixedly connected with a limiting spring 2 (228), the inner side of the limiting spring 2 (228) is fixedly connected with a push sleeve (229), the inner wall of the push sleeve (229) is fixedly connected with a limiting spring 3 (2210), the inner side of the limiting spring 3 (2210) is fixedly connected with a push rod (2211), and the inner side of the push rod (2211) is fixedly connected with a limiting block (2212).

2. The aircraft seat component orientation adjustment device according to claim 1, characterized in that: The limiting assembly (21) comprises a fixing frame (211) fixedly mounted on the top of the fixed base plate (1); a sliding frame (212) is slidably connected to the inner wall of a limiting sliding opening opened in the middle section of the fixing frame (211); an inserting rod (213) is fixedly connected to the top of the sliding frame (212); a vertical rod (214) is fixedly connected to the top of the middle section of the fixed base plate (1); and a connecting spring (215) is sleeved on the outer wall of the lower section of the vertical rod (214).

3. The aircraft seat component orientation adjustment device according to claim 1, characterized in that: The connecting assembly (23) includes a telescopic rod (231), the outer wall of the telescopic rod (231) is fixedly connected to a connecting rod 1 (232), the connecting rod 1 (232) is fixedly mounted with a connecting rod 2 (234) via a bolt (233), the connecting rod 2 (234) is fixedly connected to a connecting rod 3 (235), and the inner side of the connecting rod 3 (235) is fixedly connected to a receiving block (236).

4. The aircraft seat component orientation adjustment device according to claim 1, characterized in that: The rotating shaft (221) is rotatably connected to the inner wall of the fixing frame (211), and the rotating shaft (221) is evenly provided with limiting holes, and the rotating disk (222) is provided with limiting sliding grooves.

5. The aircraft seat component orientation adjustment device according to claim 2, characterized in that: The insertion rod (213) is slidably connected to the inner wall of the limiting hole opened in the rotating shaft (221), and the outer wall of the vertical rod (214) is slidably connected to the insertion rod (213) and the inner wall of the sliding frame (212).

6. The aircraft seat component orientation adjustment device according to claim 3, characterized in that: The telescopic rod (231) is fixedly connected to the front of the fixing frame (211), and the inner outer wall of the bolt (233) is slidably connected to the inner wall of the limiting sliding groove provided on the rotating disk (222).

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