Loading disc for aviation part machining

Abstract

The utility model discloses a material carrying disc for aviation part machining, relates to the field of aviation part auxiliary machining, solves the problem that an existing device is difficult to stably place and transfer parts of different specifications according to requirements, and adopts the following scheme that the material carrying disc comprises a material carrying disc body, and column nails are fixedly installed at the top of the material carrying disc body; the inner side of the material carrying disc is sleeved with a limiting assembly. The limiting assembly is formed by movably sleeving a sleeve seat and a sleeve plate, and a sleeve groove is formed in the side end face of the sleeve seat. An arc clamp is fixedly installed at the top of the material carrying disc, and a first spring column is assembled between the arc clamp and the outer wall of the sleeve base. According to the material carrying disc for machining the aviation parts, through arrangement of all assemblies on the limiting assembly, the parts can be clamped between the limiting assembly and the inner wall of the material carrying disc through rotation of the limiting assembly, the parts of different specifications can be placed, and synchronous limiting and clamping can be conducted on the parts; and follow-up transfer and stable placement of the parts are facilitated.

Description

Technical Field

[0001] The utility model relates to the technical field of auxiliary processing of aviation parts, in particular to a material loading tray used for processing aviation parts. Background Art

[0002] Aviation refers to aircraft that engage in flying activities, also known as aircraft, which are divided into two categories: lighter-than-air aircraft and heavier-than-air aircraft;

[0003] After searching, the application with patent number CN202221507049.2 discloses a loading tray for aviation parts processing, including a support base, a motor is fixedly mounted on the upper end of the support base, a threaded rod is fixedly mounted on the end of the motor output shaft, a connecting disk 2 is mounted on the surface of the threaded rod, and a loading tray body is rotatably mounted above the connecting disk 2. The utility model divides the loading tray body into two halves by a partition plate, so the parts can be separated, and at the same time, two rotating plates separate the loading tray body from the partition plate, so that the loading tray body is divided into four placement slots, and the user can separate and place multiple parts, and by using the partition plate and the rotating plate to separate the inside of the loading tray body, the parts can be placed in categories;

[0004] The above application document achieves the effect of separating and placing the parts by means of separation components, but it can only separate and place the parts but cannot limit the parts, and the parts also need to be transported, which makes it difficult to ensure the stability of the placement and transportation of the parts.

[0005] Therefore, we propose a carrier tray for aviation parts processing. Utility Model Content

[0006] In view of the deficiencies of the prior art, the utility model provides a loading tray for aviation parts processing, which solves the problem that the prior devices are difficult to stably place and transport parts of different specifications according to demand.

[0007] To achieve the above purpose, the utility model is implemented through the following technical solutions: a material loading tray for aviation parts processing, comprising a material loading tray, a stud is fixedly installed on the top of the material loading tray, and a limit assembly is sleeved on the inner side of the material loading tray;

[0008] The limit assembly is composed of a sleeve and a sleeve plate that are movably assembled together, and a sleeve groove is provided on the side end surface of the sleeve;

[0009] An arc clamp is fixedly installed on the top of the loading tray, and a first spring column is installed between the arc clamp and the outer wall of the sleeve.

[0010] Preferably, a support plate is fixedly mounted on the top side of the tail end of the sleeve, and a groove arranged on the top side of the sleeve is formed on the bottom side of the support plate;

[0011] Among them, the setting of the groove on the bottom side of the support plate can ensure that another set of sleeves can rotate inside it, thereby achieving the effect of funny clamping and limiting parts of different specifications.

[0012] Preferably, the tail end of the support plate is provided with a nail groove adapted to the specifications of the column nail;

[0013] Among them, the nail groove can be set on the column nail, so that the limiting component can be rotatably fitted on the column nail, so as to perform corresponding limiting clamping on different parts according to needs.

[0014] Preferably, the outer end of the sleeve is an arc-shaped end, and the sleeve is made of soft plastic;

[0015] The outer end of the sleeve plate is arranged so as to be closely attached to the inner wall of the loading tray.

[0016] Preferably, four groups of arc clips and column nails in opposite positions are fixedly installed on the top of the loading tray, and each group of column nails is covered with a limiting component.

[0017] Preferably, three groups of sleeve grooves are fixedly installed on the inner side wall of the sleeve plate, and the outer ends of the three groups of sleeve grooves are fixedly connected to the second spring columns.

[0018] The utility model provides a material loading tray for processing aviation parts, which has the following beneficial effects:

[0019] The material carrier for processing aviation parts can utilize the rotation of the limit assembly to clamp the parts between the limit assembly and the inner wall of the material carrier, through the arrangement of the components on the limit assembly. Not only can parts of different specifications be placed, but they can also be synchronously limited and clamped to facilitate the subsequent transportation and stable placement of the parts, thus solving the problem that existing devices are difficult to stably place and transport parts of different specifications as required. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 It is a structural schematic diagram of the utility model;

[0021] Figure 2 It is a structural schematic diagram of the limit assembly of the utility model;

[0022] Figure 3 It is a structural schematic diagram of the sleeve of the utility model;

[0023] Figure 4 It is a structural schematic diagram of the set plate of the utility model.

[0024] In the figure: 1, loading tray; 2, column nail; 3, limit assembly; 31, sleeve; 32, support plate; 33, nail groove; 34, arc clamp; 35, first spring column; 36, sleeve plate; 37, sleeve groove; 38, second spring column. DETAILED DESCRIPTION

[0025] 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.

[0026] Embodiment 1:

[0027] A material loading tray for processing aviation parts, comprising a material loading tray 1, a column nail 2 is fixedly installed on the top of the material loading tray 1, and a limit assembly 3 is sleeved on the inner side of the material loading tray 1; the limit assembly 3 is formed by a sleeve seat 31 and a sleeve plate 36 that are movably sleeved, and a sleeve groove 37 is opened on the side end surface of the sleeve seat 31; an arc clamp 34 is fixedly installed on the top of the material loading tray 1, and a first spring column 35 is installed between the arc clamp 34 and the outer wall of the sleeve seat 31;

[0028] Among them, the loading tray for processing aviation parts, through the settings of various components on the limit component 3, can utilize the rotation of the limit component 3 to clamp the parts between it and the inner wall of the loading tray 1, not only can it place parts of different specifications, but also can limit and clamp them synchronously, so as to facilitate the subsequent transportation and stable placement of the parts, solving the problem that the existing devices are difficult to stably place and transport parts of different specifications according to needs.

[0029] Embodiment 2:

[0030] A support plate 32 is fixedly installed on the top side of the rear end of the sleeve 31, and a groove is opened on the bottom side of the support plate 32 on the top side of the sleeve plate 36; wherein, the setting of the groove on the bottom side of the support plate 32 can ensure that another set of sleeve plates 36 can rotate inside it, thereby achieving the effect of funny clamping and limiting parts of different specifications.

[0031] The rear end of the support plate 32 is provided with a nail groove 33 that matches the specifications of the column nail 2; wherein, the setting of the nail groove 33 can be sleeved on the column nail 2, so that the limiting component 3 can be rotatably sleeved on the column nail 2, so as to facilitate corresponding limiting clamping of different components according to needs.

[0032] The outer end of the sleeve plate 36 is an arc-shaped end, and the sleeve plate 36 is made of soft plastic. The outer end of the sleeve plate 36 is arranged to be closely attached to the inner wall of the loading tray 1 .

[0033] Four sets of arc clips 34 and studs 2 are fixedly installed on the top of the loading tray 1, and each set of studs 2 is fitted with a limit assembly 3. Three sets of sleeve grooves 37 are fixedly installed on the inner side wall of the sleeve plate 36, and the outer ends of the three sets of sleeve grooves 37 are fixedly connected to the second spring column 38.

[0034] The working principle and use process of the utility model are as follows: when the device is required to work, the limit component 3 is rotated outward in advance, and the parts to be processed are placed between the limit component 3 and the inner wall of the loading tray 1, and then the limit component 3 is released, so as to achieve the effect of clamping and limiting parts of different specifications, and then the subsequent driving component performs subsequent processing and transportation on the loading tray 1 and the parts clamped by its inner side.

[0035] The above shows and describes the basic principles and main features of the utility model and the advantages of the utility model. For those skilled in the art, it is obvious that the utility model is not limited to the details of the above exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or basic features of the utility model. Therefore, no matter from which point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the utility model is limited by the attached claims rather than the above description, and it is intended to include all changes within the meaning and scope of the equivalent elements of the claims. Any figure mark in the claims should not be regarded as limiting the claims involved.

[0036] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. A material carrier for processing aviation parts, comprising a material carrier (1), characterized in that: A stud (2) is fixedly mounted on the top of the material loading tray (1), and a limiting component (3) is sleeved on the inner side of the material loading tray (1); The position limiting assembly (3) is formed by a sleeve seat (31) and a sleeve plate (36) that are movably assembled together, and a sleeve groove (37) is provided on the side end surface of the sleeve seat (31); An arc clamp (34) is fixedly mounted on the top of the material loading tray (1), and a first spring column (35) is mounted between the arc clamp (34) and the outer wall of the sleeve (31).

2. A material carrier for aviation parts processing according to claim 1, characterized in that: A support plate (32) is fixedly mounted on the top side of the rear end of the sleeve seat (31), and a groove arranged on the top side of the sleeve plate (36) is formed on the bottom side of the support plate (32).

3. A material carrier for aviation parts processing according to claim 2, characterized in that: The rear end of the support plate (32) is provided with a nail groove (33) matching the specifications of the column nail (2).

4. A material carrier for aviation parts processing according to claim 1, characterized in that: The outer end of the sleeve plate (36) is an arc-shaped end, and the sleeve plate (36) is entirely made of soft plastic.

5. The material carrier for aviation parts processing according to claim 1, characterized in that: Four sets of arc clips (34) and column nails (2) in opposite positions are fixedly installed on the top of the material loading plate (1), and each set of column nails (2) is fitted with a limiting component (3).

6. The material carrier for aviation parts processing according to claim 1, characterized in that: Three groups of sleeve grooves (37) are fixedly mounted on the inner side wall of the sleeve plate (36), and the outer ends of the three groups of sleeve grooves (37) are fixedly connected to second spring columns (38).

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