Positioning and punching device for aircraft parts

Abstract

The utility model provides a positioning and punching device for aircraft parts, which relates to the technical field of punching and comprises a device body. The device body is provided with a fixed bearing plate in the front-back direction, vertically-through fixing holes are formed in the four corners of the fixed bearing plate, a left-right-through weight reduction groove is formed in the bottom end face of the fixed bearing plate, and a vertical plate with a front-back-through threaded hole is arranged at the front end of the top end face of the fixed bearing plate. A strip-shaped groove in the front-back direction is formed in the middle of the end face of the top of the fixed bearing plate, three threaded blind holes arranged in the front-back direction are formed in the rear portion of the interior of the strip-shaped groove of the fixed bearing plate, the adjustable jaw plate can be conveniently installed on the fixed bearing plate through the jaw plate locking rod, and the adjustable jaw plate can be conveniently adjusted front and back according to the sizes of aircraft parts.

Description

Technical Field

[0001] This utility model belongs to the field of drilling technology, and in particular relates to a positioning drilling device for aircraft parts. Background Technology

[0002] The positioning and drilling device for aircraft parts is a specialized piece of equipment used for the processing of aircraft parts. It is mainly used for positioning and drilling operations on aircraft parts. The device typically includes main components such as the fuselage, support, processing table assembly, drilling assembly, water tank, and drain pipe. The positioning and drilling device for aircraft parts is widely used in the aerospace manufacturing field, especially in the processing of aircraft parts.

[0003] Based on the above, the inventors have discovered the following shortcomings in existing positioning and drilling devices:

[0004] 1. The maximum spacing between the clamping jaws is fixed, and the spacing cannot be adjusted according to the size of the aircraft parts. It is inconvenient to add adjustment measures to the device so that the jaw spacing can be adjusted according to the parts.

[0005] 2. During the batch drilling process of aircraft parts, a repositioning operation is required for each clamping process. It is inconvenient to install positioning measures on the device to position the aircraft parts. Utility Model Content

[0006] In order to at least partially solve the above-mentioned technical problems, this utility model provides a positioning and drilling device for aircraft parts.

[0007] The purpose and effect of this utility model's positioning and drilling device for aircraft parts are achieved through the following specific technical means:

[0008] A positioning and drilling device for aircraft parts includes a device body; the device body is provided with a fixed support plate in the front-rear direction, and each of the four corners of the fixed support plate has a vertical through-hole; the bottom end face of the fixed support plate has a horizontal through-hole weight reduction groove; the front end of the top end face of the fixed support plate is provided with a vertical plate with a front-rear through-hole threaded hole; the middle of the top end face of the fixed support plate has a front-rear direction strip groove; three threaded blind holes arranged front-rear are provided at the rear of the strip groove of the fixed support plate; and the middle of the right end face of the fixed support plate has a... The blind insertion hole of the fixed bearing plate has a through hole on the top wall, and an adjustable jaw plate in the left and right direction is inserted behind the strip groove of the fixed bearing plate. An insertion block is set in the middle of the bottom end face of the adjustable jaw plate. A threaded hole in the middle of the adjustable jaw plate is opened, and a jaw plate locking rod in the up and down direction is installed inside the threaded hole of the adjustable jaw plate. The lower end of the jaw plate locking rod is screwed into the threaded blind hole of the fixed bearing plate. The outer circumference of the jaw plate locking rod is threaded, and the top end face of the jaw plate locking rod is provided with a regular hexagonal groove.

[0009] Furthermore, a fixed anti-rotation post in the vertical direction is installed inside the threaded hole of the adjustable positioning plate. A threaded post is provided on the upper part of the fixed anti-rotation post. A limit ring plate is provided on the outer circumference of the bottom of the threaded post of the fixed anti-rotation post. A regular hexagonal prism is provided on the bottom end face of the threaded post of the fixed anti-rotation post.

[0010] Furthermore, an adjustable positioning plate in the vertical direction is installed on the bearing ring groove of the positioning adjustment cylinder via a bearing. A bearing circular groove is opened at the bottom of the right end face of the adjustable positioning plate. A through hole is opened inside the bearing circular groove of the adjustable positioning plate, and a threaded hole is opened on the bottom wall of the through hole of the adjustable positioning plate.

[0011] Furthermore, the positioning support rod has a left-right positioning adjustment cylinder installed on its outer circumference via threads. The positioning adjustment cylinder has threads on its inner circumference, a bearing ring groove on its left outer circumference, and a regular hexagonal structure on its right outer circumference.

[0012] Furthermore, a vertically oriented limiting anti-detachment post is installed inside the threaded hole of the positioning bearing rod. The outer circumference of the limiting anti-detachment post is threaded, and the top end face of the limiting anti-detachment post is provided with a regular hexagonal groove.

[0013] Furthermore, a positioning support rod in the left-right direction is installed inside the insertion blind hole of the fixed support plate. The outer circumference of the positioning support rod is threaded, the left end of the positioning support rod is threaded through a threaded hole, and the bottom of the outer circumference of the positioning support rod is strip-shaped groove in the left-right direction.

[0014] Furthermore, the upright plate of the fixed bearing plate is threaded with a clamping and tensioning rod in the front-to-back direction. The clamping and tensioning rod has threads on its outer circumference. The front end of the clamping and tensioning rod has a through hole in the left and right directions. A fixing post is provided on the rear end face of the clamping and tensioning rod. A rotating gripping rod in the left and right direction is inserted into the through hole of the clamping and tensioning rod. Both ends of the rotating gripping rod are provided with anti-disengagement balls. A movable jaw plate in the left and right direction is installed on the fixing post of the clamping and tensioning rod through a bearing. An insertion block is provided in the middle of the bottom end face of the movable jaw plate. A bearing groove is provided in the middle of the front end face of the movable jaw plate.

[0015] Compared with the prior art, the present invention has the following beneficial effects:

[0016] The adjustable jaw plate is mounted on the fixed support plate via a jaw plate locking rod. This allows the adjustable jaw plate to be adjusted forward and backward according to the size of the aircraft parts. This solves the problem of having a fixed maximum distance between the jaws, making it impossible to adjust the distance according to the size of the aircraft parts, and making it inconvenient to add adjustment measures to the device so that the jaw distance can be adjusted according to the parts.

[0017] The convenient positioning support rod is installed on the fixed support plate through the limit anti-detachment column to support the adjustable positioning plate. It is convenient to position the end of the aircraft parts through the adjustable positioning plate. This solves the problem that in the process of mass drilling of aircraft parts, the positioning operation needs to be re-performed every time the clamping process is carried out, and it is inconvenient to add positioning measures to the device to position the clamping position of the aircraft parts. Attached Figure Description

[0018] Figure 1 This is a top view of the structure of this utility model.

[0019] Figure 2 This is a bottom view of the structure of this utility model.

[0020] Figure 3 This is a disassembled structural diagram of the present invention.

[0021] Figure 4 This is a cross-sectional view of the assembly of the adjustable positioning plate and the fixed anti-rotation column of this utility model.

[0022] Figure 5 This is a cross-sectional view of the assembly of the clamping tension rod and the movable jaw plate of this utility model.

[0023] Figure 6 This is a cross-sectional view of the assembly of the fixed bearing plate and the adjustable jaw plate of this utility model.

[0024] In the diagram: 1. Device body; 2. Fixed bearing plate; 3. Adjustable jaw plate; 4. Jaw plate locking rod; 5. Clamping tension rod; 6. Rotating gripping rod; 7. Moving jaw plate; 8. Positioning bearing rod; 9. Limiting anti-detachment column; 10. Positioning adjustment cylinder; 11. Adjustable positioning plate; 12. Fixed anti-rotation column. Detailed Implementation

[0025] The embodiments of the present invention will be described in further detail below with reference to the accompanying drawings and examples.

[0026] Example 1:

[0027] As attached Figure 1 To be continued Figure 6 As shown:

[0028] This utility model provides a positioning and drilling device for aircraft parts, including a device body 1. The device body 1 is provided with a fixed support plate 2 in the front-rear direction for easy support of various parts. The fixed support plate 2 has a through-hole at each of its four corners for easy fixing to the drilling workbench with bolts. The bottom end face of the fixed support plate 2 has a weight-reducing groove that runs from left to right to reduce weight. The front end of the top end face of the fixed support plate 2 is provided with a vertical plate with a through-hole threaded hole for easy clamping and tightening rod 5 by threaded installation. The middle of the top end face of the fixed support plate 2 has a strip groove in the front-rear direction for easy placement of the adjustable jaw plate 3 and the movable jaw plate 7 into the guide. There are three openings at the rear of the strip groove inside the fixed support plate 2. The front and rear arranged threaded blind holes facilitate the screwing of the jaw plate locking rod 4 into the interior to fix the adjustable jaw plate 3. An insertion blind hole is provided in the middle of the right end face of the fixed bearing plate 2 to facilitate the insertion of the positioning bearing rod 8. A through hole is provided on the top wall of the insertion blind hole of the fixed bearing plate 2 to facilitate the passage of the limiting anti-detachment column 9. An adjustable jaw plate 3 in the left-right direction is inserted behind the strip groove of the fixed bearing plate 2 to facilitate its cooperation with the movable jaw plate 7 to clamp aircraft parts. An insertion block is provided in the middle of the bottom end face of the adjustable jaw plate 3 to facilitate insertion into the strip groove of the fixed bearing plate 2 for guidance. A threaded hole is provided in the middle of the adjustable jaw plate 3 to facilitate the threaded installation of the jaw plate locking rod 4. The adjustable jaw 3 is secured by a vertical jaw locking rod 4. The lower end of the locking rod 4 screws into a threaded blind hole in the fixed bearing plate 2 to prevent the adjustable jaw 3 from slipping out. The locking rod 4 has threads on its outer circumference for easy installation. A regular hexagonal groove is provided on the top face of the locking rod 4 for easy rotation and disassembly using tools. A front-to-back clamping tension rod 5 is threaded inside the upright plate of the fixed bearing plate 2, allowing for easy movement through threaded engagement. The clamping tension rod 5 also has threads on its outer circumference for easy installation. A through-hole is provided at the front end of the clamping tension rod 5 for easy insertion and installation of a rotating gripping rod 6. A fixed post is provided on the rear end face of the tensioning rod 5, which facilitates the installation of the movable jaw plate 7 via bearings. A left-right rotating gripping rod 6 is inserted into the through hole of the tensioning rod 5, which is convenient for the hand to hold and rotate the tensioning rod 5. Both ends of the rotating gripping rod 6 are provided with anti-disengagement balls for easy anti-disengagement. The left-right movable jaw plate 7 is installed on the fixed post of the tensioning rod 5 via bearings, which facilitates the movement of the movable jaw plate 7 back and forth by the bearings. An insertion block is provided in the middle of the bottom end face of the movable jaw plate 7, which is convenient for insertion into the strip groove of the fixed bearing plate 2 for guidance. A bearing groove is opened in the middle of the front end face of the movable jaw plate 7, which is convenient for the installation of the tensioning rod 5 via bearings.

[0029] The positioning support rod 8, located inside the blind insertion hole of the fixed support plate 2, is positioned in the left-right direction to facilitate the support of various components. The outer circumference of the positioning support rod 8 is threaded to facilitate the installation of the positioning adjustment cylinder 10. The left end of the positioning support rod 8 has a through-hole threaded hole to facilitate the installation of the limiting anti-detachment column 9. The bottom of the outer circumference of the positioning support rod 8 has a left-right groove to facilitate the insertion of the fixing anti-rotation column 12 to prevent the adjustable positioning plate 11 from rotating. The threaded hole of the positioning support rod 8 contains a vertically oriented... The limiting anti-detachment post 9 facilitates the prevention of detachment of the positioning support rod 8. The outer circumference of the limiting anti-detachment post 9 is threaded for easy threaded installation. A regular hexagonal groove is formed on the top end face of the limiting anti-detachment post 9 for easy rotation and disassembly using tools. A left-right positioning adjustment cylinder 10 is threadedly installed on the outer circumference of the positioning support rod 8, allowing for left and right movement via threaded engagement. The inner circumference of the positioning adjustment cylinder 10 is threaded for easy threaded installation. A bearing ring groove is formed on the outer circumference of the left end of the positioning adjustment cylinder 10 for easy adjustment. Positioning plate 11 is mounted via bearings. A regular hexagonal structure is provided on the outer right circumference of the positioning adjustment cylinder 10 for easy rotation using tools. An adjustable positioning plate 11 in the vertical direction is mounted on the bearing ring groove of the positioning adjustment cylinder 10 via bearings, allowing the positioning adjustment cylinder 10 to move the adjustable positioning plate 11 left and right via the bearings. A bearing groove is provided at the bottom of the right end face of the adjustable positioning plate 11 for easy mounting of the positioning adjustment cylinder 10 via bearings. A through hole is provided inside the bearing groove of the adjustable positioning plate 11 for easy passage of the positioning support rod 8. The bottom wall of the positioning plate 11 has a through-hole with a threaded hole, which facilitates the installation of the anti-rotation post 12 by thread. The adjustable positioning plate 11 has an anti-rotation post 12 installed inside the threaded hole, which is located in the vertical direction, to prevent the adjustable positioning plate 11 from rotating. The upper part of the anti-rotation post 12 has a threaded post, which is convenient for installation by thread. The outer circumference of the bottom of the threaded post of the anti-rotation post 12 has a limit ring plate, which is convenient for installation limit. The bottom end face of the threaded post of the anti-rotation post 12 has a regular hexagonal prism, which is convenient for rotation and disassembly by tools.

[0030] The specific usage and function of this embodiment are as follows:

[0031] In this utility model, such as Figure 1As shown, the adjustable jaw plate 3 and the movable jaw plate 7 hold the aircraft parts to be drilled. Shims are placed on the inner end faces of the adjustable jaw plate 3 and the movable jaw plate 7, thus supporting the aircraft parts. The right end face of the aircraft parts contacts the left end face of the adjustable positioning plate 11, thereby positioning the right end of the aircraft parts using the adjustable positioning plate 11. This ensures the right end of the aircraft parts is always in the same position, facilitating batch drilling operations without requiring positioning each time. When the position of the adjustable jaw plate 3 is adjusted, the jaw plate locking rod 4 is rotated using a tool to engage with the threads of the fixed support plate 2 and the adjustable jaw plate 3. This causes the jaw plate locking rod 4 to rise through the thread engagement, disengaging its lower end from the threaded blind hole of the fixed support plate 2, thereby allowing the aircraft parts to be drilled. The jaw locking rod 4 releases the adjustable jaw plate 3 from its fixation, allowing the adjustable jaw plate 3 to move forward or backward. Then, by rotating the jaw locking rod 4 with a tool, it engages with the threaded engagement of the adjustable jaw plate 3, causing the jaw locking rod 4 to descend through the threaded engagement. The lower end of the jaw locking rod 4 is then screwed into the threaded blind hole of the fixed bearing plate 2, thus achieving the rearward fixation of the adjustable jaw plate 3. When the position of the adjustable positioning plate 11 is being adjusted, the positioning adjusting cylinder 10 is rotated with a tool to engage with the threaded engagement of the positioning bearing rod 8, causing the positioning adjusting cylinder 10 to move left or right through the threaded engagement. This causes the positioning adjusting cylinder 10 to drive the adjustable positioning plate 11 to move left or right synchronously through the bearing, thus achieving the position adjustment of the adjustable positioning plate 11. At the same time, the self-locking property of the threads of the positioning bearing rod 8 and the positioning adjusting cylinder 10 achieves self-locking and stopping.

[0032] Example 2:

[0033] The difference from Embodiment 1 is that the regular hexagonal groove of the limiting anti-detachment column 9 can also be set as a regular heptagonal groove, so that the limiting anti-detachment column 9 can only be rotated by a special tool that cooperates with the regular heptagonal groove, thus preventing non-workers from rotating and disassembling the limiting anti-detachment column 9.

[0034] Example 3:

[0035] The difference from Embodiment 1 is that the regular hexagonal prism of the fixed anti-rotation post 12 can also be set as a regular heptagonal prism, so that the fixed anti-rotation post 12 can only be rotated by a special tool that cooperates with the regular heptagonal prism, thus preventing non-workers from rotating and disassembling the fixed anti-rotation post 12.

Claims

1. A positioning and drilling device for aircraft parts, characterized in that: The device includes a main body (1); the main body (1) is provided with a fixed bearing plate (2), the fixed bearing plate (2) has a through-hole at each of its four corners, a weight-reducing groove through the left and right sides on the bottom end face of the fixed bearing plate (2), a vertical plate with through-holes in the front and back on the front end of the top end face of the fixed bearing plate (2), a strip groove in the front and back direction in the middle of the top end face of the fixed bearing plate (2), three threaded blind holes arranged in the front and back are provided in the rear of the strip groove of the fixed bearing plate (2), and an insertion blind hole is provided in the middle of the right end face of the fixed bearing plate (2). The top wall of the blind insertion hole of the carrier plate (2) is provided with a through hole that runs vertically through the top and bottom. An adjustable jaw plate (3) is inserted behind the strip groove of the fixed carrier plate (2). An insertion block is provided in the middle of the bottom end face of the adjustable jaw plate (3). A threaded hole that runs vertically through the top and bottom is provided in the middle of the adjustable jaw plate (3). A jaw plate locking rod (4) is installed inside the threaded hole of the adjustable jaw plate (3). The lower end of the jaw plate locking rod (4) is screwed into the threaded blind hole of the fixed carrier plate (2). A thread is provided on the outer circumference of the jaw plate locking rod (4). A regular hexagonal groove is provided on the top end face of the jaw plate locking rod (4).

2. The positioning and drilling device for aircraft parts as described in claim 1, characterized in that: The fixed bearing plate (2) has a clamping tension rod (5) installed inside the upright plate by threads. The clamping tension rod (5) has threads on its outer circumference. The clamping tension rod (5) has a through hole at the front end and a fixed post at the rear end. A rotating gripping rod (6) is inserted into the through hole of the clamping tension rod (5). Anti-disengagement balls are provided at both ends of the rotating gripping rod (6). A movable jaw plate (7) is installed on the fixed post of the clamping tension rod (5) by bearings. An insertion block is provided in the middle of the bottom end face of the movable jaw plate (7). A bearing groove is provided in the middle of the front end face of the movable jaw plate (7).

3. The positioning and drilling device for aircraft parts as described in claim 1 or 2, characterized in that: The fixed bearing plate (2) has a positioning bearing rod (8) installed inside the insertion blind hole. The positioning bearing rod (8) has a thread on its outer circumference, a threaded hole that runs through the top and bottom on its left end, and a strip groove in the left and right directions on the bottom of its outer circumference.

4. The positioning and drilling device for aircraft parts as described in claim 3, characterized in that: The positioning support rod (8) has a limit anti-detachment column (9) installed inside the threaded hole. The limit anti-detachment column (9) has a thread on its outer circumference and a regular hexagonal groove on its top end face.

5. The positioning and drilling device for aircraft parts as described in claim 3, characterized in that: The positioning support rod (8) has a positioning adjustment cylinder (10) installed on its outer circumference by a thread. The positioning adjustment cylinder (10) has a thread on its inner circumference. The positioning adjustment cylinder (10) has a bearing ring groove on its left outer circumference and a regular hexagonal structure on its right outer circumference.

6. The positioning and drilling device for aircraft parts as described in claim 5, characterized in that: An adjustable positioning plate (11) is installed on the bearing ring groove of the positioning adjustment cylinder (10) via a bearing. A bearing circular groove is provided at the bottom of the right end face of the adjustable positioning plate (11). A through hole is provided inside the bearing circular groove of the adjustable positioning plate (11) and a threaded hole is provided on the bottom wall of the through hole of the adjustable positioning plate (11).

7. The positioning and drilling device for aircraft parts as described in claim 6, characterized in that: The adjustable positioning plate (11) has a fixed anti-rotation column (12) installed inside the threaded hole. The fixed anti-rotation column (12) has a threaded column on its upper part. The outer circumference of the bottom of the threaded column of the fixed anti-rotation column (12) is provided with a limit ring plate. The bottom end face of the threaded column of the fixed anti-rotation column (12) is provided with a regular hexagonal prism.

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