CN221160045U - Clamping device for machining aero-engine blades - Google Patents
Clamping device for machining aero-engine blades Download PDFInfo
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- CN221160045U CN221160045U CN202323077572.3U CN202323077572U CN221160045U CN 221160045 U CN221160045 U CN 221160045U CN 202323077572 U CN202323077572 U CN 202323077572U CN 221160045 U CN221160045 U CN 221160045U
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- 238000003754 machining Methods 0.000 title claims description 13
- 230000005540 biological transmission Effects 0.000 claims description 27
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 9
- 238000009434 installation Methods 0.000 abstract description 8
- 230000000694 effects Effects 0.000 abstract description 7
- 244000309464 bull Species 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a clamping device for processing aero-engine blades, which comprises a bottom plate, wherein an installation seat is arranged at the center of the outer wall of the top of the bottom plate through a bolt, a double-shaft motor is arranged in the installation seat through a bolt, a screw rod is arranged at the output end of the double-shaft motor through a coupler, a movable block is connected to the outer wall of the screw rod in a threaded manner, a lifting plate is connected to the inside of the installation seat in a sliding manner, a bent rod which is movably connected with the lifting plate is movably arranged on the outer wall of the top of the movable block through a rotating shaft, and the lifting seat is arranged on the outer wall of the top of the lifting plate through a bolt. Through the biax motor that sets up, when starting biax motor, biax motor can drive the screw rod and rotate, can utilize the threaded connection motion with the movable block at screw rod pivoted in-process, the movable block utilizes the effect of bent lever to drive lifter plate and lifting seat and moves to when carrying out the centre gripping to the material, can support the processing to the material.
Description
Technical Field
The utility model relates to the technical field of aero-engine blades, in particular to a clamping device for machining aero-engine blades.
Background
Aero-blades are used in aero-engines, which provide power to the aircraft and are therefore called the "heart" of the aircraft, in which the number of blade parts is the greatest, and which rely on these numerous blades to accomplish the compression and expansion of the gas and to generate powerful power with the highest efficiency to propel the aircraft.
The device that is comparatively common in the market is generally fixed the material directly, but in the in-process that uses of such device, because of the device can not effectually support the material to can reduce the practicality and the popularization nature of device, consequently, need to design a clamping device for aeroengine blade processing to solve above-mentioned problem.
Disclosure of utility model
The utility model aims to solve the defects in the prior art, and provides a clamping device for machining an aero-engine blade.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
The utility model provides a clamping device is used in aeroengine blade processing, includes the bottom plate, the top outer wall center department of bottom plate has the mount pad through the bolt mounting, and the inside of mount pad has the biax motor through the bolt mounting, the screw rod is installed through the shaft coupling to the output of biax motor, and threaded connection has the movable block on the outer wall of screw rod, the inside sliding connection of mount pad has the lifter plate, and is swing joint's curved bar through pivot movable mounting and lifter plate on the top outer wall of movable block, install the lifter plate through the bolt on the top outer wall of lifter plate.
The key conception of the technical scheme is as follows: through the biax motor that sets up, when starting biax motor, biax motor can drive the screw rod and rotate, can utilize the threaded connection motion with the movable block at screw rod pivoted in-process, the movable block utilizes the effect of bent lever to drive lifter plate and lifting seat and moves to when carrying out the centre gripping to the material, can support the processing to the material.
Further, the assembly seats are arranged on two sides of the outer wall of the top of the bottom plate through bolts, and the assembly seats are arranged between the assembly seats.
Furthermore, a plurality of rotating grooves are formed in the assembly seat, and the rotating grooves are distributed in an up-down structure.
Furthermore, the inside of the rotary groove is movably provided with a rotary rod and a threaded rod through bearings respectively, the outer walls of the threaded rod and the rotary rod are provided with driving wheels through bolts, and the outer walls of the driving wheels are sleeved with driving belts.
Further, the inner walls of two sides of the adjacent top of the assembly seat are provided with moving grooves, and a transmission groove is formed between the moving grooves and the inner parts of the rotating grooves of the assembly seat.
Further, the inside of transmission groove is through bearing movable mounting to extend to the inside screw drive pole of removal groove, and screw drive pole and threaded rod are located the inside outer wall of transmission groove and install intermeshing's gear through the bolt, threaded connection has the grip block on the outer wall of threaded rod and screw drive pole.
The beneficial effects of the utility model are as follows:
1. Through the biax motor that sets up, when starting biax motor, biax motor can drive the screw rod and rotate, can utilize the threaded connection motion with the movable block at screw rod pivoted in-process, the movable block utilizes the effect of bent lever to drive lifter plate and lifting seat and moves to when carrying out the centre gripping to the material, can support the processing to the material.
2. Through the bull stick that sets up, when rotating the bull stick, the bull stick can utilize the effect of drive wheel and drive belt to drive the threaded rod and rotate to utilize the effect of gear and screw drive pole to drive the movable block motion, make there be the movable block to carry out the centre gripping to the material fixedly, perfect the centre gripping function of material.
Drawings
Fig. 1 is a schematic structural view of a clamping device for machining an aero-engine blade;
Fig. 2 is a schematic structural view of a mounting seat and a lifting seat of a clamping device for machining an aero-engine blade;
FIG. 3 is a schematic plan view of a mounting seat of a clamping device for machining an aero-engine blade;
fig. 4 is a schematic plan view of an assembling seat of a clamping device for machining an aero-engine blade.
In the figure: 1 a bottom plate, 2 a mounting seat, 3 a double-shaft motor, 4 screws, 5 moving blocks, 6 lifting plates, 7 curved bars, 8 lifting seats, 9 assembling seats, 10 rotating grooves, 11 rotating bars, 12 moving grooves, 13 threaded rods, 14 driving wheels, 15 driving grooves, 16 threaded driving rods, 17 gears and 18 clamping blocks.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
It will be understood that when an element is referred to as being "fixed to" another element, it can be directly on the other element or intervening elements may also be present. When a component is considered to be "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When an element is referred to as being "disposed on" another element, it can be directly on the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this utility model belongs. The terminology used herein in the description of the utility model is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
Please see simultaneously fig. 1 to 4, a clamping device for aeroengine blade processing, comprising a base plate 1, install mount pad 2 through the bolt in the top outer wall center department of bottom plate 1, and the inside of mount pad 2 is through the bolt-mounting to have biax motor 3, the screw rod 4 is installed through the shaft coupling to the output of biax motor 3, and threaded connection has movable block 5 on the outer wall of screw rod 4, the inside sliding connection of mount pad 2 has lifter plate 6, and be swing joint's curved bar 7 with lifter plate 6 through pivot movable mounting on the top outer wall of movable block 5, install lifter plate 8 through the bolt on the top outer wall of lifter plate 6, when biax motor 3 drives screw rod 4 and rotates, screw rod 4 can utilize the effect of movable block 5 and curved bar 7 to drive lifter plate 6 motion, can drive lifter plate 8 motion at the in-process of lifter plate 6 motion.
Further, the assembly seats 9 are mounted on two sides of the top outer wall of the bottom plate 1 through bolts, the mounting seats 2 are located between the assembly seats 9, and the assembly seats 9 can be mounted on two sides of the top outer wall of the bottom plate 1.
Further, a plurality of rotating grooves 10 are formed in the assembling seat 9, the rotating grooves 10 are distributed in an up-down structure, and the rotating grooves 10 can be used for limiting the installation positions of the rotating rod 11 and the threaded rod 13.
Further, the rotating rod 11 and the threaded rod 13 are movably installed in the rotating groove 10 through bearings respectively, the driving wheel 14 is installed on the outer walls of the threaded rod 13 and the rotating rod 11 through bolts, a driving belt is sleeved on the outer wall of the driving wheel 14, and when the driving wheel 14 rotates, the driving wheel 14 can drive the other driving wheel 14 to rotate under the action of the driving belt.
Further, the inner walls of two adjacent sides of the top of the assembly seat 9 are provided with the movable groove 12, and a transmission groove 15 is arranged between the movable groove 12 and the inside of the rotary groove 10 of the assembly seat 9, and the arrangement of the transmission groove 15 can limit the installation position of the gear 17.
Further, the inside of the transmission groove 15 is movably provided with a threaded transmission rod 16 extending to the inside of the movable groove 12 through a bearing, the threaded transmission rod 16 and the threaded rod 13 are positioned on the outer wall of the inside of the transmission groove 15 and are provided with gears 17 meshed with each other through bolts, the threaded rod 13 and the outer wall of the threaded transmission rod 16 are in threaded connection with a clamping block 18, and in the process of rotating the threaded rod 13 and the threaded transmission rod 16, the threaded transmission rod 16 and the threaded rod 13 can be in threaded connection with the clamping block 18, so that the clamping block 18 can fix materials.
By adopting the structure, when the rotating rod is rotated, the rotating rod can drive the threaded rod to rotate by utilizing the action of the driving wheel and the driving belt, and the moving block is driven to move by utilizing the action of the gear and the threaded driving rod, so that the moving block can clamp and fix materials, and the clamping function of the materials is perfected.
The following are further enumerated as preferred embodiments or application examples to assist those skilled in the art in better understanding the technical content of the present utility model and the technical contribution of the present utility model with respect to the prior art:
example 1
The utility model provides a clamping device is used in aeroengine blade processing, including bottom plate 1, the top outer wall center department of bottom plate 1 has mount pad 2 through the bolt, and the inside of mount pad 2 has biax motor 3 through the bolt mounting, screw rod 4 is installed through the shaft coupling to the output of biax motor 3, and threaded connection has movable block 5 on the outer wall of screw rod 4, the inside sliding connection of mount pad 2 has lifter plate 6, and be movable connection's curved bar 7 with lifter plate 6 through pivot movable mounting on the top outer wall of movable block 5, install lifter plate 8 through the bolt on the top outer wall of lifter plate 6, when biax motor 3 drives screw rod 4 and rotates, screw rod 4 can utilize the effect of movable block 5 and curved bar 7 to drive lifter plate 6 motion, can drive lifter plate 8 motion at the in-process of lifter plate 6 motion.
Wherein, the two sides of the top outer wall of the bottom plate 1 are provided with the assembly seats 9 through bolts, the installation seats 2 are positioned between the assembly seats 9, and the assembly seats 9 can be arranged on the two sides of the top outer wall of the bottom plate 1; a plurality of rotating grooves 10 are formed in the assembly seat 9, the rotating grooves 10 are distributed in an up-down structure, and the rotating grooves 10 can limit the installation positions of the rotating rod 11 and the threaded rod 13; the inside of the rotary groove 10 is movably provided with a rotary rod 11 and a threaded rod 13 through bearings respectively, the threaded rod 13 and the outer wall of the rotary rod 11 are provided with a driving wheel 14 through bolts, the outer wall of the driving wheel 14 is sleeved with a driving belt, and when the driving wheel 14 rotates, the driving wheel 14 can drive the other driving wheel 14 to rotate under the action of the driving belt; the inner walls of two adjacent sides of the top of the assembly seat 9 are provided with a movable groove 12, a transmission groove 15 is arranged between the movable groove 12 and the inside of the rotary groove 10 of the assembly seat 9, and the arrangement of the transmission groove 15 can limit the installation position of the gear 17; the inside of the transmission groove 15 is movably provided with a threaded transmission rod 16 extending to the inside of the movable groove 12 through a bearing, the threaded transmission rod 16 and the threaded rod 13 are positioned on the outer wall of the inside of the transmission groove 15 and are provided with gears 17 meshed with each other through bolts, the threaded rod 13 and the outer wall of the threaded transmission rod 16 are in threaded connection with a clamping block 18, and in the rotating process of the threaded rod 13 and the threaded transmission rod 16, the threaded transmission rod 16 and the threaded rod 13 can be in threaded connection with the clamping block 18, so that the clamping block 18 can fix materials.
Working principle: when the device is used, firstly, the device is placed at a designated position, then the rotating rod 11 is rotated, the rotating rod 11 can drive the driving wheel 14 to rotate, the driving wheel 14 can drive the threaded rod 13 to rotate by utilizing the action of a driving belt, the threaded rod 16 can be driven to rotate by utilizing the action of the gear 17 in the process of rotating the threaded rod 13, the threaded rod 13 and the threaded rod 16 can be connected with the clamping block 18 through threads, the clamping block 18 can fix materials, finally, the double-shaft motor 3 is started, the double-shaft motor 3 can drive the screw 4 to rotate, the screw 4 can be connected with the threads of the moving block 5, the moving block 5 can drive the curved rod 7 to move, the curved rod 7 can be connected with the threads of the lifting plate 6, the lifting plate 6 can drive the lifting seat 8 to move upwards, and then the materials are supported.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (6)
1. The utility model provides a clamping device is used in aeroengine blade processing, includes bottom plate (1), its characterized in that, install mount pad (2) through the bolt in top outer wall center department of bottom plate (1), and the inside of mount pad (2) is through bolt mounting has biax motor (3), screw rod (4) are installed through the shaft coupling to the output of biax motor (3), and threaded connection has movable block (5) on the outer wall of screw rod (4), the inside sliding connection of mount pad (2) has lifter plate (6), and is movable connection's bent lever (7) with lifter plate (6) through pivot movable mounting on the top outer wall of movable block (5), through bolt mounting lifter plate (8) on the top outer wall of lifter plate (6).
2. Clamping device for machining an aeroengine blade according to claim 1, characterized in that the mounting seats (9) are mounted on both sides of the top outer wall of the base plate (1) by bolts, and the mounting seats (2) are located between the mounting seats (9).
3. The clamping device for machining the aero-engine blade according to claim 2, wherein a plurality of rotating grooves (10) are formed in the assembly seat (9), and the rotating grooves (10) are distributed in an up-down structure.
4. A clamping device for machining an aeroengine blade according to claim 3, wherein a rotating rod (11) and a threaded rod (13) are movably mounted in the rotating groove (10) through bearings respectively, a driving wheel (14) is mounted on the outer walls of the threaded rod (13) and the rotating rod (11) through bolts, and a driving belt is sleeved on the outer wall of the driving wheel (14).
5. The clamping device for machining the aeroengine blade according to claim 2, wherein the inner walls of two adjacent top sides of the assembly seat (9) are provided with a moving groove (12), and a transmission groove (15) is formed between the moving groove (12) and the inner part of the rotating groove (10) of the assembly seat (9).
6. The clamping device for machining the aeroengine blade according to claim 5, wherein a threaded transmission rod (16) extending to the inside of the movable groove (12) is movably arranged in the transmission groove (15) through a bearing, a gear (17) meshed with each other is arranged on the outer wall of the threaded transmission rod (16) and the threaded rod (13) positioned in the transmission groove (15) through bolts, and a clamping block (18) is connected to the outer walls of the threaded rod (13) and the threaded transmission rod (16) through threads.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323077572.3U CN221160045U (en) | 2023-11-15 | 2023-11-15 | Clamping device for machining aero-engine blades |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323077572.3U CN221160045U (en) | 2023-11-15 | 2023-11-15 | Clamping device for machining aero-engine blades |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221160045U true CN221160045U (en) | 2024-06-18 |
Family
ID=91436600
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323077572.3U Active CN221160045U (en) | 2023-11-15 | 2023-11-15 | Clamping device for machining aero-engine blades |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221160045U (en) |
-
2023
- 2023-11-15 CN CN202323077572.3U patent/CN221160045U/en active Active
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