Apparatus for aircraft profile sink forming
Patent Information
- Application Number
- CN202522450885.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-11-19
- Publication Date
- 2026-10-13
- Estimated Expiration
- 2035-11-19
AI Technical Summary
[0003]本实用新型的目的在于提供用于飞机型材下陷成型装置,解决了现有技术中不同航空零件加工需要频繁更换模具导致生产效率低下的问题
[0012]本实用新型的有益效果是:用于飞机型材下陷成型装置,通用性强,一套模具可满足多种下陷尺寸要求,模具数量减少60%以上;成本效益显著,模具制造和维护成本降低40-50%;生产效率提升,减少换模时间,提高生产节奏;调节精度高,严格控制零件下陷深度公差和长度公差。
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Figure CN224846517U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the technical field of aerospace sheet metal manufacturing equipment, specifically relating to a device for forming aircraft profiles by sinking. Background Technology
[0002] In the field of aircraft sheet metal manufacturing, profile recessing is a common processing technique. Currently, the industry generally uses specialized forming dies that perfectly match the recessed dimensions of the parts. These dies typically consist of a set of upper and lower molds. However, existing dies have the following significant drawbacks: High specialization: each set of dies is only suitable for parts with specific recess depths and lengths; High cost: each part requires a separately designed and manufactured dies; Long manufacturing cycle: the design and manufacturing cycle of dies significantly impacts production schedules; Frequent die changes: processing different parts requires frequent die changes, reducing production efficiency. A single aircraft model requires hundreds of different specifications of recessing dies, resulting in large dies inventory, complex management, and high overall costs. Utility Model Content
[0003] The purpose of this invention is to provide a device for forming aircraft profiles by sinking, which solves the problem of low production efficiency caused by the need for frequent mold changes in the processing of different aerospace parts in the prior art.
[0004] The technical solution adopted by this utility model is: an aircraft profile sinking forming device, including an upper template, an upper top plate connected to the upper template, and a left upper pressure block and a right upper pressure block connected to the side of the upper top plate away from the upper template through a first connecting component and a second connecting component, respectively. The bottom surfaces of the left upper pressure block and the right upper pressure block are not on the same plane, and an upper elastic rubber block is provided between the left upper pressure block and the upper top plate. It also includes a lower mold, in which a replacement mold assembly is sandwiched, and the replacement mold assembly is positioned opposite to the upper left pressure block and the upper right pressure block.
[0005] The feature of this utility model is that, The first connecting component includes a connecting block, a connecting rod that runs through the connecting block along its length, and grooves that are formed on both sides of the bottom surface of the connecting block along its length. The upper left pressure block is set in the groove, the upper top plate has a groove, the upper elastic rubber block is set in the groove, a round hole is formed in the inner wall of the groove, one end of the connecting rod matches the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod passes.
[0006] The length of the groove is not less than the length of the connecting block, and there is a height difference between the two sides of the groove.
[0007] The second connecting component includes an "L"-shaped connecting plate. One side of the connecting plate is bolted to the side wall of the top plate. The bottom surface of the other side of the connecting plate has sliding grooves along its length on both sides. The upper right pressure block is set in the sliding groove.
[0008] The lower mold includes a lower template, and a lower top plate is connected to the surface of the lower template. A slot is opened on the surface of the lower top plate, and a movable pressure plate is matched and arranged in the slot. One side of the slot is connected to a rear top plate arranged parallel to the movable pressure plate, and the other side of the slot is connected to a movable component. The movable component is arranged close to the movable pressure plate. The replacement mold assembly is arranged between the movable pressure plate and the rear top plate.
[0009] The movable component includes a rotating shaft connected to one side of the slot, and an eccentric pressure handle connected to the shaft body, which contacts the movable pressure plate.
[0010] The slot is provided with a lower elastic rubber block, which is located between the movable pressure plate and the rear top plate. The lower elastic rubber block is positioned opposite to the upper right pressure block.
[0011] The replacement mold assembly includes two side-by-side front molds and two side-by-side rear molds. The front and rear molds are positioned between the movable pressure plate and the rear top plate. There is a height difference between the front and rear molds. The front and rear molds are positioned opposite the upper left and upper right pressure blocks.
[0012] The beneficial effects of this utility model are: it is used in aircraft profile sinking forming device, has strong versatility, one set of mold can meet a variety of sinking size requirements, and the number of molds is reduced by more than 60%; it has significant cost benefits, reducing mold manufacturing and maintenance costs by 40-50%; it improves production efficiency, reduces mold change time, and increases production pace; it has high adjustment precision, and strictly controls the sinking depth tolerance and length tolerance of parts. Attached Figure Description
[0013] Figure 1 This is a schematic diagram of the structure of the device for forming aircraft profiles using this utility model. Figure 2 This is a front view of the device for forming aircraft profiles using this utility model; Figure 3 This is a cross-sectional view of the upper mold in the aircraft profile sinking forming device of this utility model; Figure 4 This is a schematic diagram of the lower mold in the aircraft profile sinking forming device of this utility model; Figure 5 This is a top view of the lower mold in the aircraft profile sinking forming device of this utility model; Figure 6 This is a diagram showing the working state of the mold replacement assembly in the aircraft profile sinking forming device of this utility model.
[0014] In the diagram, 100. Upper mold, 101. Upper template, 102. Upper top plate, 103. Upper elastic block, 104. Upper pressure block, 105. Upper right pressure block, 106. Connecting block, 107. Connecting rod, 108. Connecting plate, 109. Limiting rod, 110. Limiting connecting rod, 200. Lower mold, 201. Lower template, 202. Lower top plate, 203. Movable pressure plate, 204. Rear top plate, 205. Eccentric pressure handle, 206. Lower elastic block, 207. Rotating shaft, 301. Recessed front mold, 302. Recessed rear mold, 303. Profile. Detailed Implementation
[0015] The present invention will now be described in detail with reference to the accompanying drawings and specific embodiments.
[0016] This utility model provides a device for forming the sinking of aircraft profiles, such as... Figure 1-3 As shown, it includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 through a first connecting component and a second connecting component, respectively. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. It also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is arranged opposite to the left upper pressure block 104 and the right upper pressure block 105. The upper mold 100 is composed of components such as the upper template 101, upper top plate 102, upper elastic rubber block 103, upper left pressure block 104, and upper right pressure block 105. The upper mold 100 is positioned opposite to the replacement mold assembly in the lower mold 200. The profile 303 is placed on the replacement mold assembly, and the replacement mold assembly is clamped by the lower mold. The lower mold 200 is fixed on the machine tool worktable, and the upper mold 100 is fixed to the machine tool slider. The machine tool stroke is set, the upper mold 100 descends, pressing the profile 303 down to the set depth to form a depression, and the upper mold 100 returns to remove the formed workpiece. The mold assembly can be replaced according to the shape of the profile 303, without the need to replace the upper mold 100 and the lower mold 200, which saves costs, shortens the replacement time, and greatly increases production efficiency.
[0017] Example 1 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0018] The first connecting component includes a connecting block 106, with a connecting rod 107 extending through the connecting block 106 along its length. The bottom surface of the connecting block 106 has grooves on both opposite sides along its length. A left upper pressure block 104 is disposed within the groove. A groove is formed in the upper top plate 102, and an upper elastic rubber block 103 is disposed within the groove. A circular hole is formed in the inner wall of the groove, and one end of the connecting rod 107 matches the circular hole. A through hole is formed on the side wall opposite the circular hole in the groove, through which the connecting rod 107 passes. There is a 9mm height difference between the left upper pressure block 104 and the right upper pressure block 105. During the downward movement of the upper mold 100, the left upper pressure block 104 first contacts the profile 303 for positioning. As the upper mold 100 continues to move downward, the right upper pressure block 105 contacts the profile 303 and presses down to determine the depth of the profile 303's depression. During this process, the left upper pressure block 104 compresses the upper elastic rubber block 103 through the connecting block 106. The dimensions of the round hole and the through hole are larger than the dimensions of the connecting rod 107, ensuring that the upper left pressure block 104 can drive the connecting block 106 to move smoothly upward during the downward movement of the upper mold 100. The upper left pressure block 104 is installed on the bottom surface of the connecting block 106 through a slide groove for easy replacement. During operation, the end of the connecting rod 107 is connected to the limiting rod 109. The limiting rod 109 clamps one side of the upper left pressure block 104, and the other side of the upper left pressure block 104 abuts against the upper right pressure block 105 to limit its movement and prevent it from falling out of the slide groove.
[0019] Example 2 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0020] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0021] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove. The length of the groove is greater than the length of the connecting block 106, ensuring that when the upper right pressure block 105 is in operation, the upper left pressure block 104 can drive the connecting block 106 to move upward. The right side of the groove is higher than the left side, which makes it easier for the connecting rod 107 to be inserted into the round hole.
[0022] Example 3 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0023] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0024] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove.
[0025] The second connecting assembly includes an "L"-shaped connecting plate 108. One side of the connecting plate 108 is bolted to the side wall of the upper top plate 102. The bottom surface of the other side of the connecting plate 108 has sliding grooves along its length on both opposite sides. The upper right pressure block 105 is disposed in the sliding groove. One side of the connecting plate 108 is connected to one side of the upper top plate 102, and the other side of the connecting plate 108 is disposed on the bottom surface of the upper top plate 102 and fits against the bottom surface of the upper top plate 102. The upper right pressure block 105 is disposed in the sliding groove for easy replacement. An arc-shaped limiting plate is provided on the right side of the upper right pressure block 105. One side of the connecting bolt of the connecting plate 108 is also bolted to a limiting connecting rod 110. When the upper right pressure block 105 is placed in the sliding groove, one side of it abuts against the upper left pressure block 104, and the limiting plate and the limiting connecting rod 110 are locked together to prevent it from falling off.
[0026] Example 4 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0027] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0028] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove.
[0029] The second connecting component includes an "L"-shaped connecting plate 108. One side of the connecting plate 108 is bolted to the side wall of the upper top plate 102. The bottom surface of the other side of the connecting plate 108 has sliding grooves along its length on both sides. The upper right pressure block 105 is disposed in the sliding groove.
[0030] like Figure 4 As shown, the lower mold 200 includes a lower template 201, with a lower top plate 202 connected to its surface. The lower top plate 202 has a slot on its surface, within which a movable pressure plate 203 is fitted. One side of the slot is connected to a rear top plate 204, parallel to the movable pressure plate 203, and the other side is connected to a movable component. The movable component is positioned close to the movable pressure plate 203. A replacement mold assembly is positioned between the movable pressure plate 203 and the rear top plate 204. The lower template 201 is fixed to the machine tool's worktable. The profile 303 is clamped between the movable pressure plate 203 and the rear top plate 204 via the replacement mold assembly. The movable component pushes the movable pressure plate 203 closer to the rear top plate 204, thereby clamping the replacement mold assembly.
[0031] Example 5 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0032] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0033] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove.
[0034] The second connecting component includes an "L"-shaped connecting plate 108. One side of the connecting plate 108 is bolted to the side wall of the upper top plate 102. The bottom surface of the other side of the connecting plate 108 has sliding grooves along its length on both sides. The upper right pressure block 105 is disposed in the sliding groove.
[0035] The lower mold 200 includes a lower template 201. A lower top plate 202 is connected to the surface of the lower template 201. A slot is provided on the surface of the lower top plate 202. A movable pressure plate 203 is matched and arranged in the slot. A rear top plate 204 is connected to one side of the slot and arranged parallel to the movable pressure plate 203. A movable component is connected to the other side of the slot. The movable component is arranged close to the movable pressure plate 203. A replacement mold assembly is arranged between the movable pressure plate 203 and the rear top plate 204.
[0036] The movable component includes a rotating shaft 207, which is connected to one side of the slot. An eccentric pressure handle 205 is connected to the shaft of the rotating shaft 207, and the eccentric pressure handle 205 contacts the movable pressure plate 203. The rotating shaft 207 is rotatably connected to the lower template 201 and is located near the edge of the lower template 201. When the eccentric pressure handle 205 rotates, it pushes the movable pressure plate 203 closer to the rear top plate 204.
[0037] Example 6 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0038] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0039] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove.
[0040] The second connecting component includes an "L"-shaped connecting plate 108. One side of the connecting plate 108 is bolted to the side wall of the upper top plate 102. The bottom surface of the other side of the connecting plate 108 has sliding grooves along its length on both sides. The upper right pressure block 105 is disposed in the sliding groove.
[0041] The lower mold 200 includes a lower template 201. A lower top plate 202 is connected to the surface of the lower template 201. A slot is provided on the surface of the lower top plate 202. A movable pressure plate 203 is matched and arranged in the slot. A rear top plate 204 is connected to one side of the slot and arranged parallel to the movable pressure plate 203. A movable component is connected to the other side of the slot. The movable component is arranged close to the movable pressure plate 203. A replacement mold assembly is arranged between the movable pressure plate 203 and the rear top plate 204.
[0042] The movable component includes a rotating shaft 207, which is connected to one side of the slot. The shaft of the rotating shaft 207 is connected to an eccentric pressure handle 205, which contacts the movable pressure plate 203.
[0043] like Figure 5 As shown, a lower elastic rubber block 206 is provided in the slot. The lower elastic rubber block 206 is located between the movable pressure plate 203 and the rear top plate 204, and is positioned opposite to the upper right pressure block 105. The lower elastic rubber block 206 and the upper elastic rubber block 103 are staggered to ensure that the upper right pressure block 105 presses down on the profile 303 to form a depression during the downward movement of the upper mold 100.
[0044] Example 7 The device for forming aircraft profiles includes an upper template 101, which is connected to an upper top plate 102. The upper top plate 102 is connected to a left upper pressure block 104 and a right upper pressure block 105 on the side away from the upper template 101 via a first connecting component and a second connecting component. The bottom surfaces of the left upper pressure block 104 and the right upper pressure block 105 are not on the same plane. An upper elastic rubber block 103 is provided between the left upper pressure block 104 and the upper top plate 102. The device also includes a lower mold 200, in which a replacement mold assembly is sandwiched. The replacement mold assembly is positioned opposite to the left upper pressure block 104 and the right upper pressure block 105.
[0045] The first connecting component includes a connecting block 106, a connecting rod 107 that runs through the connecting block 106 along its length, and grooves that are formed on both sides of the bottom surface of the connecting block 106 along its length. The upper left pressure block 104 is disposed in the groove, the upper top plate 102 has a groove, the upper elastic rubber block 103 is disposed in the groove, a round hole is formed on the inner wall of the groove, one end of the connecting rod 107 is matched with the round hole, and a through hole is formed on the side wall of the groove opposite to the round hole, through which the connecting rod 107 passes.
[0046] The length of the groove is not less than the length of the connecting block 106, and there is a height difference between the two sides of the groove.
[0047] The second connecting component includes an "L"-shaped connecting plate 108. One side of the connecting plate 108 is bolted to the side wall of the upper top plate 102. The bottom surface of the other side of the connecting plate 108 has sliding grooves along its length on both sides. The upper right pressure block 105 is disposed in the sliding groove.
[0048] The lower mold 200 includes a lower template 201. A lower top plate 202 is connected to the surface of the lower template 201. A slot is provided on the surface of the lower top plate 202. A movable pressure plate 203 is matched and arranged in the slot. A rear top plate 204 is connected to one side of the slot and arranged parallel to the movable pressure plate 203. A movable component is connected to the other side of the slot. The movable component is arranged close to the movable pressure plate 203. A replacement mold assembly is arranged between the movable pressure plate 203 and the rear top plate 204.
[0049] The movable component includes a rotating shaft 207, which is connected to one side of the slot. The shaft of the rotating shaft 207 is connected to an eccentric pressure handle 205, which contacts the movable pressure plate 203.
[0050] The slot is provided with a lower elastic rubber block 206, which is located between the movable pressure plate 203 and the rear top plate 204. The lower elastic rubber block 206 is positioned opposite to the upper right pressure block 105.
[0051] like Figure 6As shown, the replaceable mold assembly includes two side-by-side recessed front molds 301, and two side-by-side recessed rear molds 302 on one side of the two recessed front molds 301. The recessed front molds 301 and recessed rear molds 302 are positioned between the movable pressure plate 203 and the rear top plate 204. There is a height difference between the recessed front molds 301 and recessed rear molds 302. The recessed front molds 301 and recessed rear molds 302 are positioned opposite to the upper left pressure block 104 and the upper right pressure block 105. The two recessed front molds 301 and recessed rear molds 302 are spliced together to form the platform of the profile 303. Matching recessed front molds 301 and recessed rear molds 302 are selected according to the specifications of the profile 303. The recessed front molds 301 and recessed rear molds 302 have low manufacturing costs and are easy to replace.
[0052] The working principle of this utility model for aircraft profile sinking forming device is as follows: Fix the upper template 101 to the machine tool slider, and fix the lower template 201 to the machine tool worktable. Select the matching front mold 301 and rear mold 302 according to the specifications of the profile 303. Place the profile on the front mold 301 and rear mold 302, and place the front mold 301 and rear mold 302 between the movable pressure plate 203 and the rear top plate 204. Rotate the eccentric pressure handle 205 to push the movable pressure plate 203 closer to the rear top plate 204. Adjust the distance between the front mold 301 and rear mold 302 to the required depression length. Set the machine tool stroke and start the machine tool. The upper mold 100 moves downward. The upper left pressure block 104 first contacts the profile 303 to achieve positioning. The upper mold 100 continues to move downward. The upper right pressure block 105 presses the profile 301 down to the set depth to form a depression. The upper mold 100 returns and the formed workpiece is taken out.
[0053] This utility model is used for aircraft profile sinking forming device, applicable to profile thickness of 1.0-4.0mm, sinking depth adjustment range of 0.5-3.0mm, sinking depth adjustment range of 10-100mm, with strong versatility, significant cost-effectiveness and high production efficiency.
Claims
1. An apparatus for forming aircraft profiles by sinking, characterized in that, Includes an upper template (101), the upper template (101) is connected to an upper top plate (102), the upper top plate (102) is connected to a left upper pressure block (104) and a right upper pressure block (105) on the side away from the upper template (101) through a first connecting component and a second connecting component respectively, the bottom surfaces of the left upper pressure block (104) and the right upper pressure block (105) are not on the same plane, and an upper elastic rubber block (103) is provided between the left upper pressure block (104) and the upper top plate (102); It also includes a lower mold (200), in which a replacement mold assembly is sandwiched, and the replacement mold assembly is arranged opposite to the upper left pressure block (104) and the upper right pressure block (105).
2. The device for forming aircraft profiles by sinking as described in claim 1, characterized in that, The first connecting component includes a connecting block (106), a connecting rod (107) is connected through the connecting block (106) along its length direction, the bottom surface of the connecting block (106) has grooves on both sides along its length direction, the upper left pressure block (104) is disposed in the groove, the upper top plate (102) has a groove, the upper elastic rubber block (103) is disposed in the groove, a round hole is provided on one inner wall of the groove, one end of the connecting rod (107) matches the round hole, a through hole is provided on the side wall of the groove opposite to the round hole, and the connecting rod (107) passes through the through hole.
3. The device for forming aircraft profile sinking as described in claim 2, characterized in that, The length of the groove is not less than the length of the connecting block (106), and there is a height difference between the two sides of the groove.
4. The device for forming aircraft profiles by sinking as described in claim 1, characterized in that, The second connecting component includes an "L"-shaped connecting plate (108). One side of the connecting plate (108) is bolted to the side wall of the top plate (102). The bottom surface of the other side of the connecting plate (108) is provided with sliding grooves along its length on both sides. The upper right pressure block (105) is disposed in the sliding groove.
5. The device for forming aircraft profile sinking as described in claim 1, characterized in that, The lower mold (200) includes a lower template (201), and a lower top plate (202) is connected to the surface of the lower template (201). A slot is provided on the surface of the lower top plate (202), and a movable pressure plate (203) is matched and arranged in the slot. A rear top plate (204) is connected to one side of the slot and arranged parallel to the movable pressure plate (203). A movable component is connected to the other side of the slot. The movable component is arranged close to the movable pressure plate (203). The mold replacement component is arranged between the movable pressure plate (203) and the rear top plate (204).
6. The device for forming aircraft profile sinking as described in claim 5, characterized in that, The movable component includes a rotating shaft (207) connected to one side of the slot, and an eccentric pressure handle (205) connected to the shaft of the rotating shaft (207), which contacts the movable pressure plate (203).
7. The device for forming aircraft profiles by sinking as described in claim 5, characterized in that, The slot is provided with a lower elastic rubber block (206), which is located between the movable pressure plate (203) and the rear top plate (204). The lower elastic rubber block (206) is arranged opposite to the upper right pressure block (105).
8. The device for forming aircraft profiles by sinking as described in claim 5, characterized in that, The replacement mold assembly includes two side-by-side recessed front molds (301), and two side-by-side recessed rear molds (302) on one side of the two recessed front molds (301). The recessed front molds (301) and the recessed rear molds (302) are located between the movable pressure plate (203) and the rear top plate (204). There is a height difference between the recessed front molds (301) and the recessed rear molds (302). The recessed front molds (301) and the recessed rear molds (302) are arranged opposite to the upper left pressure block (104) and the upper right pressure block (105).