Aircraft seat disassembling device

Abstract

The utility model discloses an aircraft seat dismantling device, which relates to the technical field of dismantling devices and comprises a base, a support plate is fixedly mounted at the top of the base, a sliding component is fixedly mounted on the inner wall of the support plate and comprises a first motor and a threaded rod, and the output end of the first motor is connected to the left side of the threaded rod. The outer surface of the threaded rod is in threaded connection with a first sliding block, the front side of the first sliding block is fixedly connected with a connecting rod, the front side of the connecting rod is fixedly connected with a gear, the front side of the gear is connected with a rotating rod, and the circumferential surface of the rotating rod is fixedly provided with a dismounting assembly. The first sliding block can move, so that the gear and the rotating rod are driven to rotate, the disassembling assembly is accurately moved to the position needing to be disassembled, the disassembling accuracy and efficiency are improved, errors and labor intensity of manual operation are reduced, and automatic position adjustment is achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of disassembling devices, in particular to an aircraft seat disassembling device. Background Art

[0002] In aircraft maintenance and overhaul, aircraft seat disassembly is an important task. Traditional aircraft seat disassembly methods often rely on manual operation, which is inefficient and labor-intensive. At the same time, due to the complex structure of aircraft seats and the diverse screw fastening positions, manual disassembly is difficult to ensure accuracy and consistency, and is prone to damage to the seats and surrounding components. To this end, we propose an aircraft seat disassembly device. Utility Model Content

[0003] The purpose of the utility model is to provide an aircraft seat disassembly device.

[0004] To achieve the above-mentioned objectives, the present invention provides the following technical solutions: an aircraft seat disassembly device, comprising a base, a support plate fixedly mounted on the top of the base, a sliding assembly fixedly mounted on the inner wall of the support plate, the sliding assembly comprising a first motor and a threaded rod, the output end of the first motor being connected to the left side of the threaded rod, the outer surface of the threaded rod being threadedly connected to a first slider, the front side of the first slider being fixedly connected to a connecting rod, the front side of the connecting rod being fixedly connected to a gear, the front side of the gear being connected to a rotating rod, a disassembly assembly fixedly mounted on the circumferential surface of the rotating rod, the disassembly assembly comprising a fixed block, a second motor, a screwdriver and a fixing frame, the output end of the second motor being connected to the top of the screwdriver, and the top of the screwdriver passing through the inner wall of the fixing block, and the bottom of the fixing block being fixedly connected to the top of the fixing frame.

[0005] As a further solution of the present invention: a rack is fixedly mounted on the inner wall of the support plate, and the gear and the rack are meshed and connected.

[0006] As a further solution of the present invention: a slide groove is provided on the front side of the base, and a slide rod is fixedly installed on the inner wall of the slide groove, and a second sliding block is slidably connected to the circumferential surface of the slide rod.

[0007] As a further solution of the present invention: a support rod is fixedly installed on the front side of the second sliding block, a clamping plate is fixedly installed on the front side of the support rod, and an anti-slip strip is fixedly installed on the front side of the clamping plate.

[0008] As a further solution of the present invention: a connecting block is fixedly installed on the circumferential surface of the support rod, and the inner wall of the connecting block is connected to the circumferential surface of the rotating rod.

[0009] As a further solution of the present invention: a limit plate is fixedly installed on the front side of the support plate, a groove is opened on the front side of the limit plate, and the groove is adapted to the rotating rod.

[0010] As a further solution of the present invention: a support block is fixedly installed on the top of the base, and the bottom of the first motor is connected to the top of the support block.

[0011] By adopting the above technical solution, compared with the prior art, the beneficial effects of the present invention are:

[0012] 1. The utility model provides a sliding assembly, and the first motor drives the threaded rod to rotate, so that the first slider can accurately move along the horizontal direction of the threaded rod, thereby driving the gear and the rotating rod to rotate, and can accurately move the disassembly assembly to the position where it needs to be disassembled, thereby improving the accuracy and efficiency of disassembly, reducing the error and labor intensity of manual operation, and realizing automatic position adjustment;

[0013] 2. The utility model provides a disassembly component, and uses a second motor to drive a screwdriver to remove the screws, which can quickly turn the screws and greatly improve the speed of disassembly. The fixing block and the fixing frame provide a stable support for the screwdriver, ensuring that the position of the screwdriver is stable during the disassembly process, avoiding shaking and displacement, thereby ensuring the quality and reliability of disassembly. At the same time, the splint and anti-slip strip can effectively fix and support the seat, adapt to aircraft seats of different sizes and shapes, and prevent the seat from shaking and displacement during the disassembly process.

[0014] Other advantages, objectives and features of the present invention will be described in part in the following description and will be apparent to those skilled in the art based on an examination of the following or may be learned from the practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is a three-dimensional schematic diagram of the overall structure in an embodiment of the present utility model;

[0016] Figure 2 This is a schematic diagram of the inner wall of the support plate in an embodiment of the present utility model;

[0017] Figure 3 This is a three-dimensional schematic diagram of a disassembled component in an embodiment of the present utility model;

[0018] Figure 4 This is a three-dimensional schematic diagram of a screwdriver in an embodiment of the present utility model;

[0019] Figure 5 It is a three-dimensional schematic diagram of the splint in the embodiment of the present utility model.

[0020] In the figure: 1. Base; 11. Sliding rod; 12. Second slider; 13. Support rod; 14. Clamp; 15. Connecting block; 2. Support plate; 21. Rack; 22. Limiting plate; 3. Sliding assembly; 31. First motor; 32. Threaded rod; 33. First slider; 34. Connecting rod; 35. Gear; 36. Rotating rod; 4. Disassembly assembly; 41. Fixing block; 42. Second motor; 43. Screwdriver; 44. Fixing bracket. DETAILED DESCRIPTION

[0021] The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings. It should be noted that the description of these embodiments is used to help understand the present invention, but does not constitute a limitation of the present invention.

[0022] In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0023] Please see the attached Figure 1 -Attached Figure 5 The utility model discloses an aircraft seat disassembly device, including a base 1, a support plate 2 is fixedly installed on the top of the base 1, a sliding assembly 3 is fixedly installed on the inner wall of the support plate 2, the sliding assembly 3 includes a first motor 31 and a threaded rod 32, the output end of the first motor 31 is connected to the left side of the threaded rod 32, the outer surface of the threaded rod 32 is threadedly connected to a first slider 33, the front side of the first slider 33 is fixedly connected to a connecting rod 34, the front side of the connecting rod 34 is fixedly connected to a gear 35, the front side of the gear 35 is connected to a rotating rod 36, and a disassembly assembly 4 is fixedly installed on the circumferential surface of the rotating rod 36. The disassembly assembly 4 includes a fixed block 41, a second motor 42, a screwdriver 43 and a fixing frame 44, the output end of the second motor 42 is connected to the top of the screwdriver 43, and the top of the screwdriver 43 passes through the inner wall of the fixing block 41, and the bottom of the fixing block 41 is fixedly connected to the top of the fixing frame 44.

[0024] In one embodiment of the present invention, a rack 21 is fixedly mounted on the inner wall of the support plate 2 , and the gear 35 is meshedly connected to the rack 21 .

[0025] In one embodiment of the present invention, a slide groove is provided on the front side of the base 1 , and a slide rod 11 is fixedly mounted on the inner wall of the slide groove. A second sliding block 12 is slidably connected to the circumferential surface of the slide rod 11 .

[0026] In one embodiment of the present invention, a support rod 13 is fixedly mounted on the front side of the second slider 12 , a clamping plate 14 is fixedly mounted on the front side of the support rod 13 , and an anti-slip strip is fixedly mounted on the front side of the clamping plate 14 .

[0027] In one embodiment of the present invention, a connecting block 15 is fixedly mounted on the circumferential surface of the support rod 13 , and an inner wall of the connecting block 15 is connected to the circumferential surface of the rotating rod 36 .

[0028] In one embodiment of the present invention, a limiting plate 22 is fixedly mounted on the front side of the support plate 2 . A groove is formed on the front side of the limiting plate 22 , and the groove is matched with the rotating rod 36 .

[0029] In one embodiment of the present invention, a support block is fixedly mounted on the top of the base 1 , and the bottom of the first motor 31 is connected to the top of the support block.

[0030] Example 1, please refer to the attached Figure 1 -Attached Figure 2 There are two bases 1 symmetrically arranged along the central axis, and support plates 2 are installed on the top of the two bases 1, which can more evenly share the various forces from the disassembly process, reduce the deformation and vibration of the device, and thus ensure the accuracy and reliability of the disassembly operation. At the same time, the first motor 31 is started to drive the threaded rod 32 to rotate, and the rotation speed and angle of the gear 35 can be accurately controlled to achieve precise adjustment of the position of the disassembly component 4, ensuring that the screwdriver 43 can accurately align with the screws on the aircraft seat, improving the accuracy and efficiency of disassembly, and providing more stable power output through the rotation of the gear 35 to ensure the smooth progress of the disassembly work.

[0031] Example 2, please refer to the attached Figure 3 -Attached Figure 5 The support rod 13 and the rotating rod 36 are connected by the connecting block 15, so that the support rod 13 and the splint 14 can move synchronously with the sliding assembly 3. The sliding assembly 3 drives the disassembly assembly 4 to move to different disassembly positions, and the splint 14 can follow synchronously, always maintaining effective fixation of the seat, preventing the seat from displacement and shaking when the screws are removed, thereby ensuring the accuracy and safety of the disassembly work. At the same time, the groove can provide a clear guide for the movement of the rotating rod 36, ensuring that the rotating rod 36 moves accurately along the predetermined trajectory during the movement, avoiding deviation, thereby ensuring the accuracy and stability of the movement of the entire disassembly assembly 4.

[0032] Specifically, by setting up a sliding component 3, the threaded rod 32 is driven to rotate by the first motor 31, so that the first slider 33 can move accurately in the horizontal direction along the threaded rod 32, thereby driving the gear 35 and the rotating rod 36 to rotate, and the disassembly component 4 can be accurately moved to the position where disassembly is required, thereby improving the accuracy and efficiency of disassembly, reducing the errors and labor intensity of manual operation, and realizing automatic position adjustment.

[0033] Specifically, by setting up the disassembly component 4, the screw is removed by driving the screwdriver 43 through the second motor 42, and the screw can be turned quickly, which greatly improves the speed of disassembly. The fixing block 41 and the fixing frame 44 provide a stable support for the screwdriver 43, ensuring that the position of the screwdriver 43 is stable during the disassembly process, avoiding shaking and displacement, thereby ensuring the quality and reliability of disassembly. At the same time, the splint 14 and the anti-slip strip can effectively fix and support the seat, adapt to aircraft seats of different sizes and shapes, and prevent the seat from shaking and displacement during the disassembly process.

[0034] Working principle:

[0035] First, the threaded rod 32 is driven to rotate by the first motor 31, so that the first slider 33 moves back and forth. The first slider 33 drives the gear 35 to move through the connecting rod 34. At the same time, the gear 35 is engaged with the rack 21 fixedly installed on the inner wall of the support plate 2. The gear 35 rotates through the rack 21, thereby driving the front rotating rod 36 to rotate. The connecting block 15 on the circumferential surface of the rotating rod 36 is connected to the support rod 13, thereby driving the support rod 13 and the splint 14 to move and fix the seat. At the same time, the rotating rod 36 drives the disassembly assembly 4 to move. The screwdriver 43 in the disassembly assembly 4 is driven to rotate by the second motor 42. Under the horizontal movement of the sliding assembly 3, the screwdriver 43 can accurately align with the screws on the aircraft seat for disassembly. At this point, the entire workflow is completed.

[0036] The above-mentioned front, back, left, right, up and down are all based on the Figure 1 As a benchmark, according to the person's observation perspective, the side of the device facing the observer is defined as the front, the left side of the observer is defined as the left, and so on.

[0037] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "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, 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 limiting the scope of protection of the present invention.

[0038] It should be noted that the equipment structure and drawings of the present invention mainly describe the principle of the present invention. In terms of the technology of the design principle, the settings of the device's power mechanism, power supply system and control system are not fully described. On the premise that those skilled in the art understand the principle of the above-mentioned utility model, they can clearly know the details of its power mechanism, power supply system and control system. The control method of the application document is automatic control through a controller, and the control circuit of the controller can be realized by simple programming by those skilled in the art.

[0039] The standard parts used can be purchased from the market and can be customized according to the description in the specification and drawings. The specific connection methods of each part adopt conventional means such as mature bolts, rivets, welding, etc. in the existing technology. The machinery, parts and equipment all adopt conventional models in the existing technology, and the components known to technical personnel in this field, their structures and principles can be known to these technical personnel through technical manuals or through conventional experimental methods.

[0040] The embodiments of the present invention are described in detail above with reference to the accompanying drawings, but the present invention is not limited to the described embodiments.

[0041] For those skilled in the art, it is possible to make various changes, modifications, substitutions and variations to these embodiments without departing from the principles and spirit of the present invention, and they still fall within the scope of protection of the present invention.

Claims

1. An aircraft seat disassembly device, comprising a base (1), characterized in that: A support plate (2) is fixedly mounted on the top of the base (1), a sliding assembly (3) is fixedly mounted on the inner wall of the support plate (2), the sliding assembly (3) comprises a first motor (31) and a threaded rod (32), the output end of the first motor (31) is connected to the left side of the threaded rod (32), the outer surface of the threaded rod (32) is threadedly connected to a first slider (33), the front side of the first slider (33) is fixedly connected to a connecting rod (34), the front side of the connecting rod (34) is fixedly connected to a gear ( 35), the front side of the gear (35) is connected to a rotating rod (36), a disassembly assembly (4) is fixedly installed on the circumferential surface of the rotating rod (36), the disassembly assembly (4) comprises a fixing block (41), a second motor (42), a screwdriver (43) and a fixing frame (44), the output end of the second motor (42) is connected to the top of the screwdriver (43), and the top of the screwdriver (43) passes through the inner wall of the fixing block (41), and the bottom of the fixing block (41) is fixedly connected to the top of the fixing frame (44).

2. The aircraft seat disassembly device according to claim 1, characterized in that: A rack (21) is fixedly mounted on the inner wall of the support plate (2), and the gear (35) and the rack (21) are meshed and connected.

3. The aircraft seat disassembly device according to claim 1, characterized in that: A sliding groove is provided on the front side of the base (1), and a sliding rod (11) is fixedly installed on the inner wall of the sliding groove. The circumferential surface of the sliding rod (11) is slidably connected to a second sliding block (12).

4. The aircraft seat disassembly device according to claim 3, characterized in that: A support rod (13) is fixedly mounted on the front side of the second sliding block (12), a clamping plate (14) is fixedly mounted on the front side of the support rod (13), and an anti-slip strip is fixedly mounted on the front side of the clamping plate (14).

5. The aircraft seat disassembly device according to claim 4, characterized in that: A connecting block (15) is fixedly mounted on the circumferential surface of the support rod (13), and the inner wall of the connecting block (15) is connected to the circumferential surface of the rotating rod (36).

6. The aircraft seat disassembly device according to claim 1, characterized in that: A limiting plate (22) is fixedly mounted on the front side of the support plate (2), and a groove is provided on the front side of the limiting plate (22), and the groove is adapted to the rotating rod (36).

7. The aircraft seat disassembly device according to claim 1, characterized in that: A support block is fixedly mounted on the top of the base (1), and the bottom of the first motor (31) is connected to the top of the support block.

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