Forging hammer device for machining aero-engine blade

Abstract

The invention relates to the technical field of aero-engine blade machining equipment, and discloses an aero-engine blade machining forging hammer device which comprises a base and further comprises a main body part and a forging part, the replacement part is mounted in the base; the locking part is arranged on the front side of the base; the number of the bulletproof parts is two, and the two bulletproof parts are both installed on the base; the replacing part comprises a limiting assembly, and the limiting assembly is arranged in the base. The rotating assembly is located in the base; the limiting assembly comprises a mold arranged in the base. According to the blade machining forging hammer device, by arranging the replacing part, the problems that in the using process of an existing blade machining forging hammer device, a mold needed by a forging hammer is inconvenient to replace, workers need to spend a large amount of time for operation in the production process, the preparation time needed by work of the forging hammer is prolonged, and then the production efficiency is reduced are solved.

Description

Technical Field

[0001] This invention relates to the field of aero-engine blade processing equipment technology, specifically to a forging hammer device for aero-engine blade processing. Background Technology

[0002] Aero engines are the core power source of aviation equipment, and their performance directly determines the flight efficiency and reliability of the equipment. As a key load-bearing component of the engine, blades must withstand high temperatures, high pressures, and complex loads, requiring extremely high material strength, precision, and stability. Blade processing is one of the core challenges in aviation manufacturing. Forging technology can significantly improve the density and mechanical properties of blade materials and is a core processing step for high-quality blades. As a key piece of equipment in blade forging, the forging hammer device achieves plastic forming of metal blanks through precise and controllable impact loads, which can efficiently create blade blanks that meet design requirements, laying the foundation for subsequent precision machining. It is an important support for ensuring the mass production and quality of aero engine blades.

[0003] However, the existing blade processing forging hammer device is not convenient for changing the mold required for the forging hammer during use, which requires the staff to spend a lot of time operating it during the production process, thus prolonging the preparation time required for the forging hammer and reducing production efficiency. Summary of the Invention

[0004] The purpose of this invention is to provide a forging hammer device for aero-engine blade processing. By setting up a replacement part, it solves the problem that existing blade processing forging hammer devices are inconvenient to replace the molds required for forging hammers during use, which leads to workers having to spend a lot of time operating them during production, thus prolonging the preparation time required for forging hammer work and reducing production efficiency.

[0005] To solve the above-mentioned technical problems, the present invention is achieved through the following technical solution: This invention relates to a forging hammer device for processing aero-engine blades, comprising a base, and further comprising: a main body mounted on the base; a replacement part mounted inside the base; a locking part located on the front side of the base; and two bulletproof parts mounted on the base. The replacement part includes a limiting component located inside the base; and a rotating component located inside the base. The limiting component includes a mold located inside the base, the mold having several limiting grooves. The inner wall of the base has several sliding grooves, and the inner walls of each sliding groove are slidably connected to limiting plates. The shapes of the limiting plates are respectively adapted to the limiting grooves.

[0006] Furthermore, the main body includes a frame fixedly connected to the outer wall of the base, a hydraulic cylinder fixedly connected to the inner wall of the frame, and a punching head fixedly connected to the output end of the hydraulic cylinder.

[0007] Furthermore, the locking part includes a connecting component, which is installed on the front side of the base; and a locking component, of which there are two, both of which are located on the front side of the base and are circumferentially distributed.

[0008] Furthermore, the bulletproof part includes an adjustment component disposed outside the mold; and two extrusion components, both of which are located outside the base and are mirror images of each other.

[0009] Furthermore, the rotating assembly includes several springs fixedly connected to the bottom of several limiting plates, the bottom of several springs being fixedly connected to several sliding grooves, a rotating shaft being rotatably connected to the inner wall of the base, several gears being fixedly connected to the outer wall of the rotating shaft, and racks being fixedly connected to the inner walls of several limiting plates. Each limiting plate corresponds to two springs, and the gears mesh with the racks respectively.

[0010] Furthermore, the connecting assembly includes a connecting block fixedly connected to the outer wall of the rotating shaft, and a handle is fixedly connected to the outer wall of the connecting block.

[0011] Furthermore, the locking assembly includes a limiting block 1 fixedly connected to the front side of the base, a sliding groove 2 is provided on the rear side of the connecting block 1, a spring 2 is fixedly connected to the inner wall of the sliding groove 2, the limiting block 2 is slidably connected to the inner wall of the sliding groove 2, the front side of the limiting block 2 is fixedly connected to the spring 2, and the limiting block 2 is adapted to the limiting block 1.

[0012] Furthermore, the adjustment component includes two slide grooves three respectively opened on the left and right sides of the base, and sliders are slidably connected to the inner walls of the two slide grooves three. Limiting strips are fixedly connected to the inner walls of the two sliders, and the two sliders are mirror images of each other.

[0013] Furthermore, the extrusion assembly includes a rotating shaft two rotatably connected to the inner wall of the slider, a connecting block two fixedly connected to the outer wall of the rotating shaft two, an elastic element provided inside the connecting block two, a handle on the front side of the connecting block two, the elastic element including an extrusion block slidably connected to the inner wall of the connecting block two, two springs three fixedly connected to the inner wall of the extrusion block, the side of the two springs three away from the base being fixedly connected to the connecting block two, and the side of the extrusion block near the base having an arc-shaped head.

[0014] The present invention has the following beneficial effects: (1) By setting up a replacement part, when in use, the rotating component drives the gear to rotate, and the gear drives the limiting plate to slide in the slide groove through the rack. After the limiting plate slides out of the limiting groove, the mold is no longer restricted. After replacing the mold, the rotating component resets so that the limiting plate is locked into the limiting groove of the new mold under the action of the elastic element to complete the fixation. The mold can be replaced with simple operation. Through the cooperation of the limiting component and the rotating component, the restriction on the original mold can be quickly released. At the same time, the newly replaced mold can be stably limited and fixed, ensuring the smooth progress of subsequent forging hammer processing. This reduces the time required for device preparation and improves production efficiency.

[0015] (2) By setting a locking part, when rotating, the rotating handle drives the connecting block one and the rotating shaft one to rotate. The limiting block two rotates with the connecting block one and is squeezed into the slide groove two by the limiting block one. Then, under the action of the elastic element, it is locked on the limiting block one. When unlocking, the limiting block two is pulled to slide into the slide groove two. After the connecting block one is unrestricted, it resets. The position of the rotating component can be stably locked. During the mold replacement process, the rotating component will not rotate at will, providing a safe and stable operating environment for the mold to be taken out and installed. At the same time, the locking state can be reliably released without affecting the reset and fixation after the mold is replaced.

[0016] (3) By setting up a bulletproof part, when preparing, the limiting strip is pulled to drive the slider to slide in the slide groove three, so that the limiting strip presses against the blade blank. The connecting block two is rotated to drive the rotating shaft two to rotate. After the extrusion block extrudes the base, it slides into the connecting block two and compresses the elastic element. Under the elastic force of the elastic element, the extrusion block abuts against the base to complete the slider fixation. It can stably limit and fix the blade blank, avoid the blade blank from bouncing up during the forging hammer process, ensure the safety of the forging hammer process, and at the same time, the limiting position can be flexibly adjusted to adapt to the processing needs of blade blanks of various specifications.

[0017] Of course, any product implementing this invention does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0018] To more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a partial cross-sectional view of the present invention; Figure 2 This is a partial cross-sectional view of the rotating assembly of the present invention; Figure 3 This is a schematic diagram of the overall structure of the gear of the present invention; Figure 4 This is a partial cross-sectional view of the limiting component of the present invention; Figure 5 This is a partial cross-sectional view of the locking part of the present invention; Figure 6 This is a partial cross-sectional view of the bulletproof part of the present invention; Figure 7 For the present invention Figure 6 A magnified structural diagram of A in the diagram.

[0020] The attached diagram lists the components represented by each number as follows: In the diagram: 1. Main body; 101. Base; 102. Frame; 103. Hydraulic cylinder; 104. Punch head; 2. Replacement part; 21. Limiting assembly; 211. Mold; 212. Limiting groove; 213. Slide groove one; 214. Limiting plate; 22. Rotating assembly; 221. Spring one; 222. Rotating shaft one; 223. Gear; 224. Rack; 3. Locking part; 31. Connecting assembly; 311. Connecting block one; 312. Handle; 32. Locking assembly; 321. Limiting block one; 322. Slide groove two; 323. Spring two; 324. Limiting block two; 4. Bulletproof part; 41. Adjusting assembly; 411. Slide groove three; 412. Slider; 413. Limiting strip; 42. Extrusion assembly; 421. Rotating shaft two; 422. Connecting block two; 423. Extrusion block; 424. Spring three. Detailed Implementation

[0021] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0022] Please see Figure 1 - Figure 7 As shown, the present invention is a forging hammer device for processing aero-engine blades, including a base 101, and further including: a main body 1, which is mounted on the base 101; a replacement part 2, which is mounted inside the base 101; a locking part 3, which is located on the front side of the base 101; and two bulletproof parts 4, both of which are mounted on the base 101. The main body 1 includes a frame 102 fixedly connected to the outer wall of the base 101, and a hydraulic cylinder 103 fixedly connected to the inner wall of the frame 102. A stamping head 104 is fixedly connected to the output end of the hydraulic cylinder 103.

[0023] The replacement unit 2 includes a limiting component 21 disposed within the base 101; and a rotating component 22 located within the base 101. The limiting component 21 includes a mold 211 disposed within the base 101, with several limiting grooves 212 formed therein. The inner wall of the base 101 has several sliding grooves 213, each with a limiting plate 214 slidably connected to its inner wall. The shapes of the limiting plates 214 are respectively adapted to the limiting grooves 212. The rotating component 22 includes several springs 221 respectively fixedly connected to the bottom of the limiting plates 214, with the bottoms of the springs 221 respectively fixedly connected to the sliding grooves 213. The inner wall of 101 is rotatably connected to a rotating shaft 222. The outer wall of the rotating shaft 222 is fixedly connected to several gears 223. The inner walls of several limiting plates 214 are fixedly connected to racks 224. Each limiting plate 214 corresponds to two springs 221. The gears 223 mesh with the racks 224 respectively. By setting the replacement part 2, the mold 211 can be replaced with simple operation. Through the cooperation of the limiting component 21 and the rotating component 22, the restriction on the original mold 211 can be quickly released. At the same time, the newly replaced mold 211 can be stably limited and fixed, ensuring the smooth progress of subsequent forging hammer processing. This reduces the time required for device preparation and improves production efficiency.

[0024] The locking part 3 includes a connecting component 31, which is installed on the front side of the base 101; and two locking components 32, both located on the front side of the base 101 and arranged in a circle. The connecting component 31 includes a connecting block 311 fixedly connected to the outer wall of the pivot 222, and a handle 312 fixedly connected to the outer wall of the connecting block 311. The locking component 32 includes a limiting block 321 fixedly connected to the front side of the base 101. A sliding groove 322 is provided on the rear side of the connecting block 311. Spring 223 is fixedly connected to the inner wall of 22, and limit block 24 is slidably connected to the inner wall of slide groove 222. The front side of limit block 224 is fixedly connected to spring 223. Limit block 224 is adapted to limit block 1 321. By setting locking part 3, the position of rotating component 22 can be stably locked, ensuring that rotating component 22 will not rotate randomly during mold 211 replacement, providing a safe and stable operating environment for mold 211 removal and installation, and can reliably release the locking state without affecting the reset and fixation of mold 211 after replacement.

[0025] The bulletproof part 4 includes an adjustment component 41, which is disposed outside the mold 211; and two extrusion components 42, both located outside the base 101 and mirror images of each other. The adjustment component 41 includes two slide grooves 411 respectively opened on the left and right sides of the base 101. The inner walls of the two slide grooves 411 are slidably connected to sliders 412. The inner walls of the two sliders 412 are fixedly connected to limit strips 413. The two sliders 412 are mirror images of each other. The extrusion component 42 includes a rotating shaft 421 rotatably connected to the inner wall of the slider 412. The outer wall of the rotating shaft 421 is fixedly connected to a connecting block 2. 422, an elastic element is provided inside the connecting block 2 422. The front side of the connecting block 2 422 has a handle. The elastic element includes a pressing block 423 that is slidably connected to the inner wall of the connecting block 2 422. Two springs 3 424 are fixedly connected to the inner wall of the pressing block 423. The side of the two springs 3 424 away from the base 101 is fixedly connected to the connecting block 2 422. The side of the pressing block 423 near the base 101 has an arc-shaped head. By setting the anti-bullet part 4, the blade blank can be stably limited and fixed, preventing the blade blank from bouncing during the forging hammer processing, ensuring the safety of the forging hammer processing. At the same time, the limiting position can be flexibly adjusted to adapt to the processing needs of blade blanks of various specifications.

[0026] It should be noted that the hydraulic cylinder 103 in this application is equipped with a corresponding hydraulic pump to drive the hydraulic cylinder 103, thereby ensuring the normal operation of the forging hammer.

[0027] In use, the blade blank can be placed on top of the mold 211, and the limiting strip 413 can be pulled to make the slider 412 slide within the groove 411. At this time, the blade blank can be pressed under the limiting strip 413. Then, the connecting block 422 can be pulled to make the rotating shaft 421 rotate. At this time, the extrusion block 423 will extrude the base 101 and slide into the connecting block 422. At this time, the spring 424 will be compressed and generate elastic force. Subsequently, under the action of the elastic force of the spring 424, the extrusion block 423 will be compressed and generate elastic force. The pressure block 423 abuts against the base 101, thus fixing the slider 412. At this time, the blade blank will be restricted in position by the two limiting strips 413. Then, the hydraulic cylinder 103 can be activated, causing its output end to drive the punch head 104 to hammer downwards, thus completing the forging of the blade blank. When it is necessary to change the mold 211, the handle 312 can be turned, causing the connecting block 1 311 to rotate. At this time, the limiting block 2 324 will rotate accordingly, and finally, the limiting block 2 324 will be pressed by the limiting block 1 321 and slide into the slide groove 2 3. Within 22, spring 223 will compress and generate elastic force. Finally, under the action of the elastic force of spring 223, the limiting block 224 will be locked onto the limiting block 1 321, thus completing the limiting. When connecting block 1 311 rotates, it will drive rotating shaft 1 222 to rotate. At this time, rotating shaft 1 222 will drive gear 223 to rotate. Gear 223 will then drive limiting plate 214 to slide within slide groove 1 213 via rack 224. At this time, spring 1 221 will compress and generate elastic force, causing limiting plate 214 to slide within slide groove 1 213. 4. When sliding, it will slide out of the limiting groove 212. At this time, the mold 211 will lose its restriction. Then, the mold 211 can be pulled out of the base 101. Then, a new mold 211 can be installed. Then, the limiting block 224 can be pulled to slide in the sliding groove 222. At this time, the spring 223 will be compressed and generate elastic force. At this time, the connecting block 1 311 will lose its restriction. At this time, under the action of the elastic force of the spring 1 221, the limiting plate 214 will be driven to be inserted into the limiting groove 212, thereby completing the restriction.

[0028] The preferred embodiments of the present invention disclosed above are merely illustrative of the invention. These preferred embodiments do not exhaustively describe all details, nor do they limit the invention to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of the invention, thereby enabling those skilled in the art to better understand and utilize the invention. The invention is limited only by the claims and their full scope and equivalents.

Claims

1. A forging hammer device for processing aero-engine blades, comprising a base (101), characterized in that, Also includes: The main body (1) is mounted on the base (101); Replacement part (2), said replacement part (2) is installed inside the base (101); Locking part (3), the locking part (3) is disposed on the front side of the base (101); There are two bulletproof parts (4), and both bulletproof parts (4) are mounted on the base (101); The replacement part (2) includes a limiting component (21) disposed within the base (101); and Rotating assembly (22), which is located within base (101); The limiting component (21) includes a mold (211) disposed in the base (101), the mold (211) having a plurality of limiting grooves (212) and the inner wall of the base (101) having a plurality of sliding grooves (213), the inner walls of the plurality of sliding grooves (213) being slidably connected to limiting plates (214). Among them, the shapes of several limiting plates (214) are respectively adapted to several limiting grooves (212).

2. The forging hammer device for processing aero-engine blades according to claim 1, characterized in that, The main body (1) includes a frame (102) fixedly connected to the outer wall of the base (101), a hydraulic cylinder (103) fixedly connected to the inner wall of the frame (102), and a punch head (104) fixedly connected to the output end of the hydraulic cylinder (103).

3. The forging hammer device for processing aero-engine blades according to claim 2, characterized in that, The locking part (3) includes a connecting component (31) which is mounted on the front side of the base (101); as well as Locking components (32) are provided in two, both of which are located on the front side of the base (101); Among them, the two locking components (32) are arranged in a circular pattern.

4. The forging hammer device for processing aero-engine blades according to claim 3, characterized in that, The bulletproof part (4) includes an adjustment assembly (41) disposed outside the mold (211); and Two extrusion assemblies (42) are provided, and both extrusion assemblies (42) are located outside the base (101); The two extrusion components (42) are mirror images of each other.

5. The forging hammer device for processing aero-engine blades according to claim 4, characterized in that, The rotating assembly (22) includes several springs (221) fixedly connected to the bottom of several limiting plates (214), the bottom of several springs (221) being fixedly connected to several sliding grooves (213), the inner wall of the base (101) being rotatably connected to a rotating shaft (222), the outer wall of the rotating shaft (222) being fixedly connected to several gears (223), and the inner walls of several limiting plates (214) being fixedly connected to racks (224). Among them, one limiting plate (214) corresponds to two springs (221), and several gears (223) mesh with several racks (224) respectively.

6. The forging hammer device for processing aero-engine blades according to claim 5, characterized in that, The connecting assembly (31) includes a connecting block (311) fixedly connected to the outer wall of the rotating shaft (222), and a handle (312) is fixedly connected to the outer wall of the connecting block (311).

7. The forging hammer device for processing aero-engine blades according to claim 6, characterized in that, The locking assembly (32) includes a limiting block (321) fixedly connected to the front side of the base (101), a sliding groove (322) is provided on the rear side of the connecting block (311), a spring (323) is fixedly connected to the inner wall of the sliding groove (322), a limiting block (324) is slidably connected to the inner wall of the sliding groove (322), and the front side of the limiting block (324) is fixedly connected to the spring (323). Among them, limit block two (324) is adapted to limit block one (321).

8. The forging hammer device for processing aero-engine blades according to claim 7, characterized in that, The adjustment component (41) includes two slide grooves (411) respectively opened on the left and right sides of the base (101). The inner walls of the two slide grooves (411) are slidably connected to sliders (412), and the inner walls of the two sliders (412) are fixedly connected to limit strips (413). The two sliders (412) are mirror images of each other.

9. The forging hammer device for processing aero-engine blades according to claim 8, characterized in that, The extrusion assembly (42) includes a second rotating shaft (421) rotatably connected to the inner wall of the slider (412), a second connecting block (422) is fixedly connected to the outer wall of the second rotating shaft (421), and an elastic element is provided inside the second connecting block (422); The front side of the connecting block 2 (422) has a handle.

10. A forging hammer device for processing aero-engine blades according to claim 9, characterized in that, The elastic element includes a compression block (423) that is slidably connected to the inner wall of the connecting block two (422). The inner wall of the compression block (423) is fixedly connected to two springs three (424). The side of the two springs three (424) away from the base (101) is fixedly connected to the connecting block two (422). Among them, the side of the extrusion block (423) near the base (101) has an arc-shaped head.

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