Operating platform for aircraft assembly

Abstract

The utility model discloses an operation platform for aircraft assembly, and relates to the technical field of aircraft assembly. Four groups of penetrating type circular through groove structures are formed in the periphery of the top of the base in a rectangular array shape; a piston cylinder of a cylindrical structure is fixedly arranged in the middle of the bottom of the base. A connecting cylinder of a cylindrical structure is fixedly arranged on one side of the bottom of the base. A blocking plate of a circular-plate-shaped structure is arranged in the connecting cylinder in a sliding mode. According to the utility model, workers can be effectively reminded, the assembly quality is improved, and left parts can be found in time.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the technical field of aircraft assembly, more specifically, especially relate to an operating platform for aircraft assembly. BACKGROUND

[0002] In the process of assembling aircraft parts, it is usually necessary to assemble on the corresponding assembly platform. Aircraft assembly requires high precision, and the operation platform needs to have excellent stability to ensure the accurate positioning and connection of parts during assembly.

[0003] The current aircraft assembly platform still has the following shortcomings:

[0004] During the assembly of aircraft parts, the assembly parts may be left due to the negligence of the staff, which may lead to a decline in the overall assembly quality of the equipment. The current assembly platform lacks the necessary auxiliary monitoring function and cannot monitor and remind the assembly status in a timely manner, so the functionality is relatively single. INVENTION CONTENTS

[0005] In order to at least solve the above technical problems to some extent, the utility model provides an operating platform for aircraft assembly.

[0006] The purpose and function of the operating platform for aircraft assembly are achieved by the following specific technical means:

[0007] An operating platform for aircraft assembly, comprising: a base; the base adopts a rectangular plate structure, and four groups of through circular through-slots are arranged in a rectangular array around the top of the base, and a through circular through-slot is arranged in the middle of the top of the base; a piston cylinder of a cylindrical structure is fixedly arranged in the middle of the bottom of the base; a connecting cylinder of a cylindrical structure is fixedly arranged on one side of the bottom of the base, and the connecting cylinder is in communication with the piston cylinder, the connecting cylinder is made of transparent material, and a scale value is arranged on the outer wall of the connecting cylinder; a plug plate of a circular plate structure is slidably arranged in the connecting cylinder.

[0008] Further, a first sliding rod of a cylindrical structure is slidably arranged in each of the circular through-slots around the top of the base; a rectangular groove structure operating table is fixedly arranged on the top of the four first sliding rods, and a through rectangular through-slot structure is arranged in a rectangular array on the top of the operating table; a second sliding rod of a cylindrical structure is fixedly arranged in the middle of the bottom of the operating table, and a spring is sleeved on the outer side of the second sliding rod; a piston plate of a circular plate structure is fixedly arranged at the bottom end of the second sliding rod, and the piston plate is slidably arranged in the piston cylinder, and the outer wall of the piston plate is attached to the inner wall of the piston cylinder.

[0009] Further, the top of the operation table is fixedly provided with a clamp seat; the bottom of the clamp seat is fixedly and connectively provided with a clamping block in a rectangular block structure, and the size of the clamping block is matched with the size of the rectangular through slot at the top of the operation table; the bottom of the clamping block is fixedly and connectively provided with a screw rod; and the outer side of the screw rod is rotatably provided with a nut through thread cooperation.

[0010] Compared with the prior art, the utility model has the beneficial effects that:

[0011] In the application, after assembly is completed, the product is transported away, the operation table is lifted up under the action of the spring, the piston plate collects the gas in the connecting cylinder into the piston cylinder, and the baffle plate falls back to the bottom of the inner side of the connecting cylinder. If there are residual components on the operation table, the weight of the operation table is higher than before assembly, and the piston plate and the baffle plate cannot be reset. The operator can know whether there are residual components not installed on the operation table by observing the position of the baffle plate, so that it is avoided that residual components cannot be found in time due to too many clamp seats, work personnel are effectively reminded, assembly quality is improved, and residual components can be found in time.

[0012] In the assembly process, the clamping block at the bottom of the clamp seat can be inserted into the rectangular through slot at the corresponding position of the operation table, then the nut is installed to the outer side of the screw rod, the clamp seat is fixed and limited in position, the number and position of the clamp seat can be adjusted according to different use requirements, the installation process is greatly facilitated, and installation efficiency is improved. BRIEF DESCRIPTION OF DRAWINGS

[0013] Figure 1 is the overall front view structural schematic diagram of the utility model.

[0014] Figure 2 is the overall axial view structural schematic diagram of the utility model.

[0015] Figure 3 is the overall front view structural schematic diagram of the utility model under the condition that the piston cylinder and the connecting cylinder are cut open.

[0016] Figure 4 is the split structure schematic diagram of the operation table and the clamp seat of the utility model.

[0017] In the drawings, the corresponding relationship between the component names and the drawing numbers is as follows:

[0018] 1, base; 101, piston cylinder; 102, connecting cylinder; 103, baffle plate; 104, first sliding rod; 105, operation table; 106, second sliding rod; 107, piston plate; 108, clamp seat; 109, clamping block; 110, screw rod; 111, nut. DETAILED DESCRIPTION

[0019] The embodiment of the utility model will be further described in detail below in combination with the drawings and examples.

[0020] Example 1:

[0021] As Figures 1 to 4 shown:

[0022] The embodiment provides an operating platform for aircraft assembly, which comprises a base 1; the base 1 adopts a rectangular plate structure, four groups of through circular through-slots are arranged in a rectangular array on the top of the base 1, and a through circular through-slot is arranged in the middle of the top of the base 1; a piston cylinder 101 in a cylindrical structure is fixedly arranged in the middle of the bottom of the base 1; a connecting cylinder 102 in a cylindrical structure is fixedly arranged on one side of the bottom of the base 1 and communicates with the piston cylinder 101, the connecting cylinder 102 is made of transparent material, and a scale value is arranged on the outer wall of the connecting cylinder 102; a plug plate 103 in a circular plate structure is slidably arranged in the connecting cylinder 102, and the outer wall of the plug plate 103 is attached to the inner wall of the connecting cylinder 102.

[0023] The outer side of the top of the base 1 is slidably provided with a group of first sliding rods 104 in a cylindrical structure; a rectangular recess structure operating table 105 is fixedly arranged on the top of the four groups of first sliding rods 104, and a through rectangular through-slot structure is arranged on the top of the operating table 105 in a rectangular array; a second sliding rod 106 in a cylindrical structure is fixedly arranged in the middle of the bottom of the operating table 105, and a spring is sleeved on the outer side of the second sliding rod 106; a piston plate 107 in a circular plate structure is fixedly arranged at the bottom end of the second sliding rod 106, and the piston plate 107 is slidably arranged in the piston cylinder 101, and the outer wall of the piston plate 107 is attached to the inner wall of the piston cylinder 101.

[0024] The specific use mode and role of the embodiment are as follows:

[0025] In use, all parts waiting to be assembled are placed on the operating table 105, under the action of their own weight, the weight of the operating table 105 can be increased, thereby pressing the operating table 105 and each group of first slide rod 104 and second slide rod 106 to slide downward along the circular through slot on the base 1, thereby synchronously driving the piston plate 107 to slide downward along the inside of the piston cylinder 101 by a distance, and through the piston plate 107, the gas pressure in the piston cylinder 101 is extruded into the connecting cylinder 102, and through this part of the gas pressure, the baffle plate 103 is pushed upward along the inside of the connecting cylinder 102 by a distance, at this time, the scale value on the connecting cylinder 102 can be observed to observe and determine the height of the baffle plate 103 rising; after assembly is completed, the assembled product is transported from the operating table 105, and after the operating table 105 loses weight, under the action of the spring outside the second slide rod 106, the operating table 105 is raised along the base 1, thereby making the piston plate 107 collect the gas in the connecting cylinder 102 into the piston cylinder 101, and making the baffle plate 103 fall back to the inside bottom of the connecting cylinder 102, if there are still residual parts on the operating table 105, the weight of the operating table 105 will still be higher than that before assembly, so that the piston plate 107 and the baffle plate 103 cannot be reset, the operator can know whether there are residual parts on the operating table 105 by observing the position of the baffle plate 103, avoiding the phenomenon that too many clamp seats 108 on the operating table 105 cannot find residual parts in time, thereby effectively reminding the workers, which is conducive to improving the assembly quality.

[0026] Embodiment 2:

[0027] Based on embodiment 1, as shown in the accompanying drawings: Figure 1 to Figure 4 :

[0028] Among them, the top of the operating table 105 is fixedly provided with a clamp seat 108; the bottom of the clamp seat 108 is fixedly and connectively provided with a rectangular block structure of a clamping block 109, and the size of the clamping block 109 matches the size of the rectangular through slot on the top of the operating table 105; the bottom of the clamping block 109 is fixedly and connectively provided with a screw rod 110; the outside of the screw rod 110 is rotatably provided with a nut 111 through thread cooperation.

[0029] The specific use mode and effect of the embodiment:

[0030] The utility model discloses a plurality of clamp seats 108 are arranged on the operation table 105, and the clamp seat 108 is provided with the screw rod 110 and the nut 111, and the screw rod 110 is arranged on the clamp seat 108, and the nut 111 is arranged on the outer side of screw rod 110, and the clamp seat 108 is fixed and limited on the operation table 105 through the screw rod 110 and the nut 111.

Claims

1. An access platform for use in the assembly of an aircraft, characterised in that, Include: Base (1); the base (1) adopts rectangular plate structure, and four groups of through type circular through slot structure are arranged in rectangular array on the top of the base (1), and a through type circular through slot structure is arranged in the middle of the top of the base (1); the piston cylinder (101) of cylindrical structure is fixedly arranged in the middle of the bottom of the base (1); the connecting cylinder (102) of cylindrical structure is fixedly arranged on one side of the bottom of the base (1), and the connecting cylinder (102) is communicated with the piston cylinder (101), the connecting cylinder (102) is made of transparent material, and the scale value is arranged on the outer wall of the connecting cylinder (102); the plug plate (103) of circular plate structure is slidably arranged in the connecting cylinder (102), and the outer wall of the plug plate (103) is attached to the inner wall of the connecting cylinder (102).

2. An aircraft assembly operation platform as claimed in claim 1, characterised in that: A group of first slide rods (104) of cylindrical structure are slidably arranged in the circular through slot on the outer side of the top of the base (1); the operation table (105) of rectangular groove structure is fixedly arranged on the top of the four groups of first slide rods (104), and the through type rectangular through slot structure is arranged in the top of the operation table (105) in rectangular array.

3. An aircraft assembly operation platform as claimed in claim 2, wherein: The second slide rod (106) of cylindrical structure is fixedly arranged in the middle of the bottom of the operation table (105), and the spring is sleeved on the outer side of the second slide rod (106).

4. The aircraft assembly platform of Claim 3, wherein: The piston plate (107) of circular plate structure is fixedly arranged on the bottom end of the second slide rod (106), and the piston plate (107) is slidably arranged in the piston cylinder (101), and the outer wall of the piston plate (107) is attached to the inner wall of the piston cylinder (101).

5. An aircraft assembly platform as claimed in any one of claims 2 to 4 wherein: The clamp seat (108) is fixedly arranged on the top of the operation table (105); the clamping block (109) of rectangular block structure is fixedly connected on the bottom of the clamp seat (108), and the size of the clamping block (109) is matched with the size of the rectangular through slot on the top of the operation table (105).

6. An aircraft assembly platform as claimed in claim 5, wherein: The screw rod (110) is fixedly connected on the bottom of the clamping block (109).

7. An aircraft assembly platform as claimed in claim 6, wherein: The nut (111) is rotatably arranged on the outer side of the screw rod (110) through thread cooperation.

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