Aviation aircraft part cutting limiting device
By designing a combination of a limiting mechanism and a moving mechanism, the problem that the limiting device of existing aviation aircraft parts cutting equipment cannot move is solved, automatic limit adjustment is achieved, and cutting efficiency and accuracy are improved.
Patent Information
- Application Number
- CN202422745753.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-12
- Publication Date
- 2025-09-12
- Estimated Expiration
- 2034-11-12
AI Technical Summary
The limiting device of existing aircraft parts cutting equipment cannot be moved, resulting in frequent adjustments to the raw material position during the cutting process, which is inefficient.
A cutting limit device for aircraft parts is designed, which includes a limit mechanism and a moving mechanism. The automatic movement of the limit plate and the sliding of the I-bench are achieved through a combination of a bidirectional screw and a helical gear, reducing manual adjustment.
It improves the efficiency of parts cutting, avoids frequent limit adjustments, and ensures cutting accuracy and efficiency.
Smart Images
Figure CN223325584U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of cutting aviation aircraft parts, in particular to a cutting limiting device for aviation aircraft parts. Background Art
[0002] The cutting of aircraft parts is a crucial step in the aircraft manufacturing process. There are many kinds of aviation materials, including aluminum alloys, titanium alloys, composite materials, etc. Different materials require different cutting methods to ensure their performance is not damaged. Various parts of aircraft need to be cut to make the raw materials into the size people need.
[0003] When existing equipment is cutting component raw materials, it is necessary to limit the raw materials. After the existing equipment has limited the raw materials, the position of the raw materials relative to the limiting device is usually fixed, and the limiting device used for limiting is also in an immobile state. This leads to the situation that in actual use, when the cutting workload is large and the next section of raw materials needs to be cut after completing one cutting, the staff needs to frequently release the limit, adjust the position of the raw materials, and then limit them again, which is very cumbersome. Utility Model Content
[0004] In order to make up for the above deficiencies, the present invention provides an aircraft component cutting and limiting device that overcomes the above technical problems or at least partially solves the above problems.
[0005] The utility model is achieved in this way:
[0006] The utility model provides a cutting and limiting device for aircraft parts, comprising a work table and a cutting machine. A limiting mechanism is provided on the top of the work table. The limiting mechanism comprises:
[0007] An I-beam, which is arranged inside the workbench, has a limit slot on the top, and a bidirectional screw is rotatably installed inside the limit slot;
[0008] A limit plate, wherein the limit plate is slidably mounted inside the limit groove, and two limit plates are provided. The two limit plates are respectively sleeved on both sides of the bidirectional screw rod and are both threadedly connected to the bidirectional screw rod;
[0009] The limit blocks are provided with two, and the two limit blocks are respectively fixedly mounted on the top of the two limit plates, and duckbill grooves are provided on opposite sides of the two limit blocks, and the two limit blocks are mirror-imaged.
[0010] In a preferred solution, a first helical gear is rotatably mounted inside the I-bench, and the first helical gear is fixedly sleeved on the surface of the bidirectional screw rod.
[0011] In a preferred solution, a second helical gear is rotatably installed inside the I-beam, and the second helical gear is meshed and connected with the first helical gear.
[0012] In a preferred solution, a spline shaft is rotatably mounted inside the work table, and an internal fixed sleeve of the second helical gear is provided with a spline sleeve, and the spline sleeve is slidably sleeved on the surface of the spline shaft.
[0013] In a preferred solution, a first motor is fixedly installed on the right side of the work table, and an output end of the first motor is fixedly connected to the right side of the spline shaft.
[0014] In a preferred solution, a moving mechanism is provided inside the work table, and the moving mechanism includes a slide groove, the slide groove is opened on the top of the work table, and the I-beam is slidably sleeved inside the slide groove.
[0015] In a preferred embodiment, the spline shaft is rotatably sleeved inside the slide groove, a driving screw is rotatably installed inside the slide groove, a limiting rod is fixedly installed inside the slide groove, the driving screw and the limiting rod are both sleeved inside the I-beam, and the driving screw and the I-beam are threadedly connected.
[0016] In a preferred solution, a second motor is fixedly installed on the right side of the work table, and the output end of the second motor is fixedly connected to the right side of the driving screw.
[0017] The utility model provides a cutting limit device for aircraft parts, the beneficial effects of which include:
[0018] 1. By setting a limit mechanism and cooperating with the limit groove, the two limit plates respectively drive the two limit blocks to move in opposite directions, so that the component raw materials are clamped, and rubber pads can be installed on the opposite sides of the two limit blocks to prevent the limit blocks from damaging the component raw materials, so that the component raw materials are limited by the limit mechanism, avoiding the problem of inaccurate cutting accuracy caused by shaking of the component raw materials during cutting.
[0019] 2. By setting up a moving mechanism, since the sliding sleeve of the spline sleeve is arranged on the surface of the spline shaft, the spline shaft can always drive the spline sleeve to rotate without affecting the left and right movement of the I-beam. Therefore, when the staff finishes cutting a section of component raw materials and needs to cut the next section of raw materials, they no longer need to frequently release the limit of the component raw materials, adjust the position and then re-limit it. Compared with the existing technology, the efficiency of component cutting is higher. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] 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.
[0021] Figure 1 It is a schematic diagram of the overall structure provided by the embodiment of the utility model;
[0022] Figure 2 A partial cross-sectional view of a work table is provided for an embodiment of the present utility model;
[0023] Figure 3 A structural diagram of an I-bench is provided for the embodiment of the utility model;
[0024] Figure 4 A partial cross-sectional view of an I-bench is provided for an embodiment of the present utility model.
[0025] In the figure: 1. work table; 2. cutting machine; 301. I-beam; 302. limit groove; 303. bidirectional screw; 304. limit plate; 305. limit block; 306. duckbill groove; 307. first bevel gear; 308. second bevel gear; 309. spline shaft; 310. spline sleeve; 311. first motor; 401. slide; 402. driving screw; 403. limit rod; 404. second motor. DETAILED DESCRIPTION
[0026] To make the purpose, technical solutions, and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments 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.
[0027] Example 1
[0028] Reference Figure 1-4The utility model provides a technical solution: a cutting limit device for aircraft parts, including a work table 1 and a cutting machine 2. A limit mechanism is provided on the top of the work table 1. The limit mechanism includes an I-beam 301. The I-beam 301 is arranged inside the work table 1. A limit slot 302 is provided on the top of the I-beam 301. A two-way screw rod 303 is rotatably installed inside the limit slot 302. A limit plate 304 is slidably installed inside the limit slot 302. Two limit plates 304 are provided. The two limit plates 304 are respectively sleeved on both sides of the two-way screw rod 303 and are both threadedly connected to the two-way screw rod 303. Two limit blocks 305 are provided. The two limit blocks 305 are respectively fixedly installed on the top of the two limit plates 304. The two limit blocks 305 are relative to each other. A duckbill groove 306 is provided on one side of each of the two limit blocks 305, and the two limit blocks 305 are arranged in a mirror image. By setting a limit mechanism, the staff places the component raw material between the two limit blocks 305, and by rotating the bidirectional screw rod 303, the two limit plates 304 are respectively threadedly connected to the two ends of the bidirectional screw rod 303 in opposite directions, and through the cooperation of the limit groove 302, the two limit plates 304 respectively drive the two limit blocks 305 to move in opposite directions, so that the component raw material is clamped, and rubber pads can be installed on the opposite sides of the two limit blocks 305 to prevent the limit blocks 305 from damaging the component raw material, so that the component raw material is limited by the limit mechanism, avoiding the problem of inaccurate cutting accuracy caused by the shaking of the component raw material during cutting;
[0029] Reference Figure 1-4 The first bevel gear 307 is installed for rotation inside the I-beam 301. The first bevel gear 307 is fixedly sleeved on the surface of the bidirectional screw rod 303. The second bevel gear 308 is installed for rotation inside the I-beam 301. The second bevel gear 308 is meshed with the first bevel gear 307. By setting the first bevel gear 307 and the second bevel gear 308, when the second bevel gear 308 rotates, the meshing connection between the second bevel gear 308 and the first bevel gear 307 causes the first bevel gear 307 to rotate. Since the first bevel gear 307 is fixedly sleeved on the surface of the bidirectional screw rod 303, the first bevel gear 307 can drive the bidirectional screw rod 303 to rotate.
[0030] Reference Figure 1-4The work table 1 is internally rotatably installed with a spline shaft 309, and the internal fixed sleeve of the second helical gear 308 is provided with a spline sleeve 310. The spline sleeve 310 is slidably sleeved on the surface of the spline shaft 309. The right side of the work table 1 is fixedly installed with a first motor 311. The output end of the first motor 311 is fixedly connected to the right side of the spline shaft 309. By setting the spline shaft 309, the staff starts the first motor 311 to drive the spline shaft 309 to rotate. Due to the meshing between the spline shaft 309 and the spline sleeve 310, the spline shaft 309 and the spline sleeve 310 are engaged. , so that the spline shaft 309 drives the spline sleeve 310 to rotate. Since the spline sleeve 310 is fixedly sleeved inside the second helical gear 308, the second helical gear 308 is driven to rotate by the spline sleeve 310, so that the two limit blocks 305 move in relative directions to clamp the component raw material. Moreover, since the spline sleeve 310 is slidably sleeved on the surface of the spline shaft 309, the spline shaft 309 can drive the spline sleeve 310 to rotate without affecting the left and right movement of the spline sleeve 310.
[0031] Example 2
[0032] In the above embodiment, the relative movement of the two limiting blocks 305 can limit the position of the component material relative to the I-beam 301. However, since the I-beam 301 cannot be moved, when a large number of cutting processes are carried out, the staff needs to frequently adjust the position of the component material, which is very cumbersome and needs to be improved.
[0033] Reference Figure 1-4, this embodiment is different from the above-mentioned embodiment 1 in that a moving mechanism is provided inside the work table 1, and the moving mechanism includes a slide 401, the slide 401 is opened on the top of the work table 1, the I-beam 301 is slidably sleeved inside the slide 401, the spline shaft 309 is rotatably sleeved inside the slide 401, a driving screw 402 is rotatably installed inside the slide 401, a limit rod 403 is fixedly installed inside the slide 401, the driving screw 402 and the limit rod 403 are both sleeved inside the I-beam 301, the driving screw 402 and the I-beam 301 are threadedly connected, a second motor 404 is fixedly installed on the right side of the work table 1, and the output end of the second motor 404 is fixedly connected to the right side of the driving screw 402. By setting the moving mechanism , the staff starts the second motor 404 to drive the driving screw 402 to rotate. Due to the threaded connection between the driving screw 402 and the I-beam 301, and the sliding connection between the limit rod 403 and the I-beam 301, the I-beam 301 moves along the direction of the slide groove 401, and because the spline sleeve 310 is slidingly sleeved on the surface of the spline shaft 309, the spline shaft 309 can always drive the spline sleeve 310 to rotate without affecting the left and right movement of the I-beam 301. As a result, when the staff has cut a section of component raw material and needs to cut the next section of raw material, there is no need to frequently release the limit of the component raw material, adjust the position and then limit it again. Compared with the existing technology, the efficiency of component cutting is higher.
[0034] Specifically, the working process or working principle of the aircraft component cutting limit device is as follows: when in use, the staff places the component raw material between the two limit blocks 305, starts the first motor 311, drives the spline shaft 309 to rotate, and due to the engagement between the spline shaft 309 and the spline sleeve 310 key teeth, the spline shaft 309 drives the spline sleeve 310 to rotate, and since the spline sleeve 310 is fixedly sleeved inside the second bevel gear 308, the second bevel gear 308 is driven to rotate through the spline sleeve 310. When the second bevel gear 308 rotates, the second bevel gear 308 and the first bevel gear 307 are connected. The meshing connection causes the first bevel gear 307 to rotate. Since the first bevel gear 307 is fixedly sleeved on the surface of the bidirectional screw rod 303, the first bevel gear 307 can drive the bidirectional screw rod 303 to rotate, so that the two limit blocks 305 move in relative directions to clamp the component raw materials. When the lower section of the raw materials needs to be cut, the staff starts the second motor 404 to drive the driving screw rod 402 to rotate. Due to the threaded connection between the driving screw rod 402 and the I-beam 301, and the sliding connection between the limit rod 403 and the I-beam 301, the I-beam 301 moves along the direction of the slide groove 401.
Claims
1. A cutting and limiting device for aircraft parts, comprising a work table (1) and a cutting machine (2), characterized in that: A limiting mechanism is provided on the top of the work table (1), and the limiting mechanism comprises: An I-beam (301), the I-beam (301) being arranged inside the work table (1), a limiting groove (302) being provided on the top of the I-beam (301), a bidirectional screw rod (303) being rotatably installed inside the limiting groove (302); A limiting plate (304), wherein the limiting plate (304) is slidably mounted inside the limiting groove (302), and two limiting plates (304) are provided. The two limiting plates (304) are respectively sleeved on both sides of the bidirectional screw rod (303), and are both threadedly connected to the bidirectional screw rod (303); A limit block (305) is provided with two limit blocks (305), and the two limit blocks (305) are respectively fixedly installed on the top of the two limit plates (304), and a duckbill groove (306) is provided on the opposite side of the two limit blocks (305), and the two limit blocks (305) are arranged in a mirror image.
2. The cutting limit device for aircraft parts according to claim 1, characterized in that: A first bevel gear (307) is rotatably mounted inside the I-bench (301), and the first bevel gear (307) is fixedly sleeved on the surface of the bidirectional screw rod (303).
3. The cutting limit device for aircraft parts according to claim 2, characterized in that: A second helical gear (308) is rotatably mounted inside the I-beam (301), and the second helical gear (308) is meshedly connected with the first helical gear (307).
4. The aircraft component cutting and limiting device according to claim 3, characterized in that: A spline shaft (309) is rotatably mounted inside the work table (1), and a spline sleeve (310) is fixedly mounted inside the second helical gear (308), wherein the spline sleeve (310) is slidably mounted on the surface of the spline shaft (309).
5. The aircraft component cutting and limiting device according to claim 4, characterized in that: A first motor (311) is fixedly installed on the right side of the work table (1), and an output end of the first motor (311) is fixedly connected to the right side of the spline shaft (309).
6. The aircraft component cutting and limiting device according to claim 5, characterized in that: A moving mechanism is provided inside the work table (1), and the moving mechanism includes a slide groove (401). The slide groove (401) is opened on the top of the work table (1), and the I-bench (301) is slidably sleeved inside the slide groove (401).
7. The aircraft component cutting and limiting device according to claim 6, characterized in that: The spline shaft (309) is rotatably sleeved inside the slide groove (401), a driving screw rod (402) is rotatably installed inside the slide groove (401), a limiting rod (403) is fixedly installed inside the slide groove (401), the driving screw rod (402) and the limiting rod (403) are both sleeved inside the I-beam (301), and the driving screw rod (402) and the I-beam (301) are threadedly connected.
8. The aircraft component cutting and limiting device according to claim 7, characterized in that: A second motor (404) is fixedly mounted on the right side of the work table (1), and an output end of the second motor (404) is fixedly connected to the right side of the driving screw rod (402).