CN215147022U - But quick assembly disassembly's aviation spare part adds clamping apparatus - Google Patents
But quick assembly disassembly's aviation spare part adds clamping apparatus Download PDFInfo
- Publication number
- CN215147022U CN215147022U CN202121569967.3U CN202121569967U CN215147022U CN 215147022 U CN215147022 U CN 215147022U CN 202121569967 U CN202121569967 U CN 202121569967U CN 215147022 U CN215147022 U CN 215147022U
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- rod
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- clamping
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- 230000002457 bidirectional effect Effects 0.000 claims abstract description 12
- 238000003754 machining Methods 0.000 claims description 11
- 125000003003 spiro group Chemical group 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 7
- 238000000034 method Methods 0.000 description 6
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000001737 promoting effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 230000008093 supporting effect Effects 0.000 description 2
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 1
- 235000017491 Bambusa tulda Nutrition 0.000 description 1
- 241001330002 Bambuseae Species 0.000 description 1
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 1
- 239000011425 bamboo Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 210000005056 cell body Anatomy 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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- Jigs For Machine Tools (AREA)
Abstract
The utility model discloses a clamp for processing aviation parts capable of being quickly disassembled and assembled, which belongs to the technical field of clamps and comprises a base, wherein the four corners of the top wall of the base are all fixedly provided with a mounting seat, and the middle top walls of the front side and the rear side of the base are all fixedly provided with a mounting cylinder, the utility model discloses a large-scale cylindrical aviation parts are placed on a clamping table, under the condition of the self weight of the aviation parts to be processed, the clamping table is displaced downwards, four groups of first articulated rods do downward arc motion, and the parts on the clamping table are in an initial clamping state, thereby effectively avoiding the condition that the parts are in an unstable state and need to be manually righted by a worker after being placed, reducing the work burden of the worker, and enabling two groups of screwed second clamping blocks to form a clamping effect on the parts through a motor and a bidirectional threaded rod, the phenomenon that the staff passes through manual regulation anchor clamps has been replaced, promotes the centre gripping effect and has further alleviateed staff's work burden.
Description
Technical Field
The utility model relates to an anchor clamps technical field specifically is an but quick assembly disassembly's anchor clamps for aviation spare part processing.
Background
The jig is a device for fixing a processing object to a correct position for receiving construction or inspection in a machine manufacturing process, and may be called a jig in a broad sense, and a device for quickly, conveniently and safely mounting a workpiece in any process. The aviation parts are core parts in an aviation system, generally have a function of quick disassembly and assembly, the performance of the aviation parts directly relates to aviation safety, clamps are required to be used in the process of machining the aviation parts, and particularly, cylindrical aviation parts with large mass are machined.
The current anchor clamps to this type of aviation spare part processing most all adopt the staff manually to adjust anchor clamps, and place this type of spare part and carry out the in-process that manually adjusts the anchor clamps on pressing from both sides the bench, spare part self is unstable, rolls easily, still needs the staff to manually right, and this kind of anchor clamps are comparatively wasted time and energy, very big increase staff's work burden.
Based on this, the utility model designs a but quick assembly disassembly's anchor clamps are used in aviation spare part processing to solve above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a but quick assembly disassembly's anchor clamps for aviation parts machining to solve the current anchor clamps to this type of aviation parts machining that proposes in the above-mentioned background art most all adopt the staff manually to adjust anchor clamps, and place this type of parts and carry out the in-process of manual regulation to the anchor clamps on pressing from both sides the bench, parts self is unstable, roll easily, still need the manual righting of staff, this kind of anchor clamps comparatively waste time and energy, very big increase the problem of staff's work burden.
In order to achieve the above object, the utility model provides a following technical scheme: a clamp capable of being quickly disassembled and assembled for machining aviation parts comprises a base, wherein mounting seats are fixedly mounted at four corners of the top wall of the base, mounting barrels are fixedly mounted at the top walls of the middle parts of the front side and the rear side of the base, springs are fixedly mounted at the bottom wall of the inner cavity of the mounting barrels, piston rods are mounted in the inner cavities of the mounting barrels, the bottom walls of the piston rods are fixedly connected with elastic bodies at the top ends of the springs, clamping tables are fixedly mounted at the top walls of the piston rods, groove bodies are formed in the middle seat bodies of the base, hydraulic push rods are fixedly mounted in the inner cavities of the groove bodies, mounting plates are fixedly mounted between the mounting seats in the front and rear directions, bidirectional threaded rods and guide rods are mounted at the upper parts of the seat bodies of the base, the bidirectional threaded rods are located above the guide rods, and the left ends and the right ends of rod bodies of the bidirectional threaded rods respectively penetrate through the plate bodies of the mounting plates located at the left side and the right side, fixed connection is in the left and right sides respectively at both ends about the two-way threaded rod body the inside wall of mounting panel, the inside wall fixed mounting of mount pad has the hinge, it has first hinge bar and second hinge bar to articulate on the hinge, just the inner body of rod of second hinge bar with the diapire looks fixed connection of centre gripping platform, first hinge bar with the second hinge bar is certain angle just first hinge bar is located the top of second hinge bar, the inner body of rod fixed mounting of first hinge bar has first chuck, the equal spiro union of the body of rod at both ends has the second chuck about the two-way threaded rod, just the body of rod of guide bar runs through the plate body of second chuck.
Preferably, the left wall of the base is fixedly provided with a connecting seat, the top wall of the connecting seat is fixedly provided with a motor, and the output end of the motor is connected with the left end rod body of the bidirectional threaded rod.
Preferably, the two groups of the groove bodies are symmetrically arranged along the front-back direction.
Preferably, the two groups of the mounting cylinders are symmetrically mounted in the left-right direction.
Preferably, the top walls of the left end and the right end of the clamping table are fixedly provided with second clamping blocks.
Preferably, the inner side wall of the second chuck and the inner side wall of the first chuck are both fixedly provided with a first clamping block.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a place large-scale cylinder class aviation spare part on the grip slipper, under the condition of the self weight of this type of aviation spare part of processing, make the grip slipper displacement downwards, make the first articulated arm of four groups do decurrent arc motion, and form initial clamping state to the spare part above the grip slipper, it is in unstable state and needs the manual condition of rightting of staff after effectively having avoided placing spare part, staff's work burden has been alleviateed, and the second grip block that makes two sets of spiro couplings through motor and two-way threaded rod forms the clamping effect to spare part, the phenomenon that the staff passes through manual regulation anchor clamps has been replaced, further lightened staff's work burden when promoting the clamping effect.
Of course, it is not necessary for any particular product to achieve all of the above-described advantages at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;
FIG. 2 is a schematic top view of the present invention;
fig. 3 is a schematic side sectional view of the clamping table portion of the present invention.
In the drawings, the components represented by the respective reference numerals are listed below:
1-mounting seat, 2-hinge joint, 3-first hinge rod, 4-first chuck, 5-first clamping block, 6-second clamping block, 7-clamping table, 8-piston rod, 9-second hinge rod, 10-groove body, 11-hydraulic push rod, 12-spring, 13-mounting cylinder, 14-guide rod, 15-connecting seat, 16-motor, 17-bidirectional threaded rod, 18-base, 19-second chuck and 20-mounting plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a clamp capable of being quickly disassembled and assembled for machining aviation parts comprises a base 18, mounting seats 1 are fixedly mounted at four corners of the top wall of the base 18, mounting cylinders 13 are fixedly mounted at the top walls of the middle parts of the front side and the rear side of the base 18, springs 12 are fixedly mounted at the bottom walls of the inner cavities of the mounting cylinders 13, piston rods 8 are mounted in the inner cavities of the mounting cylinders 13, the bottom walls of the piston rods 8 are fixedly connected with top springs of the springs 12, clamping tables 7 are fixedly mounted at the top walls of the piston rods 8, one side close to the middle plate of the clamping tables 7 is an inner side, otherwise, the side is an outer side, the clamping tables 7 can move downwards under the elastic action of the springs 12, groove bodies 10 are formed in the middle seat body of the base 18, hydraulic push rods 11 are fixedly mounted in the inner cavities of the groove bodies 10, and after the parts are machined, the clamping tables 7 can be pushed upwards through the hydraulic push rods 11, so that clamping of first clamping heads 4 is loosened, a mounting plate 20 is fixedly mounted between the mounting seats 1 in the front-back direction, a bidirectional threaded rod 17 and a guide rod 14 are mounted on the upper portion of the seat body of the base 18, the bidirectional threaded rod 17 is positioned above the guide rod 14, the left end and the right end of the rod body of the bidirectional threaded rod 17 respectively penetrate through the plate bodies of the mounting plates 20 positioned on the left side and the right side through mounting bearings, the left end and the right end of the rod body of the bidirectional threaded rod 17 are respectively fixedly connected with the inner side walls of the mounting plates 20 positioned on the left side and the right side, a hinge joint 2 is fixedly mounted on the inner side walls of the mounting seats 1, a first hinge rod 3 and a second hinge rod 9 are hinged on the hinge joint 2, the inner end of the second hinge rod 9 is fixedly connected with the bottom wall of the clamping table 7, the first hinge rod 3 and the second hinge rod 9 form a certain angle, the first hinge rod 3 is positioned above the second hinge rod 9, and a first clamping head 4 is fixedly mounted on the inner end of the first hinge rod 3, the equal spiro union of the body of rod at both ends has second chuck 19 about two-way threaded rod 17, and the body of rod of guide bar 14 runs through the plate body of second chuck 19, second chuck 19 can slide on guide bar 14, the left wall fixed mounting of base 18 has connecting seat 15, the roof fixed mounting of connecting seat 15 has motor 16, and the shaft coupling of motor 16's output is connected with the left end pole body of two-way threaded rod 17, the cell body 10 has seted up two sets ofly along the symmetry on the fore-and-aft direction, the purpose is in order to set up two sets of hydraulic push rod 11, it is better to make the supporting effect, the installation section of thick bamboo 13 is installed two sets ofly along the symmetry on the left and right directions, promote the supporting effect, the equal fixed mounting of roof at both ends has second grip block 6 about grip block 7, the purpose is for promoting the centre gripping effect, the equal fixed mounting of inside wall of second chuck 19 and the inside wall of first chuck 4 has first grip block 5.
One specific application of this embodiment is: by placing large cylindrical aviation parts on the top wall of the clamping table 7, under the condition of the self weight of the processed aviation parts, the clamping table 7 is displaced downwards, the clamping table 7 descends in the displacement process, the piston rod 8 is driven to displace downwards, the spring 12 generates elastic deformation, meanwhile, in the descending process of the clamping table 7, the four groups of second hinged rods 9 connected with the clamping table 7 also move, under the hinging action of the hinged joint 2, the four groups of first hinged rods 3 do downward arc motion, and when the clamping table 7 stops descending, the parts placed on the clamping table 7 are in an initial clamping state, the clamping structure utilizing the self weight of the parts effectively avoids the situation that the parts are in an unstable state and need to be manually righted by a worker, the work burden of the worker is reduced, and by starting the motor 16, the shaft coupling of motor 16's output drives two-way threaded rod 17 and rotates, makes the second grip block 19 of two sets of spiro couplings make opposite directions motion to finally form the centre gripping effect to spare part, replaced the phenomenon that the staff passes through manual regulation anchor clamps, further lightened staff's work burden when promoting the centre gripping effect.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrally connected; may be mechanically coupled, may be directly coupled, or may be indirectly coupled through an intermediary. To those of ordinary skill in the art, the specific meaning of the above terms in the present invention is understood according to the specific situation. In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (6)
1. The utility model provides a but quick assembly disassembly's anchor clamps for aviation parts machining, includes base (18), its characterized in that: the mounting device is characterized in that mounting seats (1) are fixedly mounted at four corners of the top wall of the base (18), mounting cylinders (13) are fixedly mounted at the top walls of the middle parts of the front side and the rear side of the base (18), springs (12) are fixedly mounted at the bottom wall of the inner cavity of the mounting cylinders (13), piston rods (8) are mounted in the inner cavities of the mounting cylinders (13), the bottom walls of the piston rods (8) are fixedly connected with top springs of the springs (12), clamping tables (7) are fixedly mounted at the top walls of the piston rods (8), groove bodies (10) are formed in a seat body in the middle part of the base (18), hydraulic push rods (11) are fixedly mounted in the inner cavities of the groove bodies (10), mounting plates (20) are fixedly mounted between the mounting seats (1) in the front-back direction, and two-way threaded rods (17) and guide rods (14) are mounted at the upper parts of the seat body of the base (18), the bidirectional threaded rod (17) is positioned above the guide rod (14), the left end and the right end of the rod body of the bidirectional threaded rod (17) are respectively penetrated through the plate bodies of the mounting plates (20) positioned on the left side and the right side, the left end and the right end of the rod body of the bidirectional threaded rod (17) are respectively fixedly connected with the inner side walls of the mounting plates (20) positioned on the left side and the right side, the inner side wall of the mounting seat (1) is fixedly provided with a hinge joint (2), the hinge joint (2) is hinged with a first hinge rod (3) and a second hinge rod (9), the inner end of the second hinge rod (9) is fixedly connected with the bottom wall of the clamping table (7), the first hinge rod (3) and the second hinge rod (9) are at a certain angle, the first hinge rod (3) is positioned above the second hinge rod (9), the inner end of the first hinge rod (3) is fixedly provided with a first clamping head (4), the body of rod at both ends all the spiro union about two-way threaded rod (17) has second chuck (19), just the body of rod of guide bar (14) runs through the plate body of second chuck (19).
2. The quickly detachable clamp for machining aviation components and parts as claimed in claim 1, wherein: the left wall of base (18) fixed mounting has connecting seat (15), the roof fixed mounting of connecting seat (15) has motor (16), just the output of motor (16) with the left end rod body of two-way threaded rod (17) is connected.
3. The quickly detachable clamp for machining aviation components and parts as claimed in claim 1, wherein: two groups of groove bodies (10) are symmetrically arranged along the front and back direction.
4. The quickly detachable clamp for machining aviation components and parts as claimed in claim 1, wherein: two groups of the mounting cylinders (13) are symmetrically mounted in the left-right direction.
5. The quickly detachable clamp for machining aviation components and parts as claimed in claim 1, wherein: and the top walls of the left end and the right end of the clamping table (7) are fixedly provided with second clamping blocks (6).
6. The quickly detachable clamp for machining aviation components and parts as claimed in claim 1, wherein: and a first clamping block (5) is fixedly arranged on the inner side wall of the second chuck (19) and the inner side wall of the first chuck (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121569967.3U CN215147022U (en) | 2021-07-12 | 2021-07-12 | But quick assembly disassembly's aviation spare part adds clamping apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121569967.3U CN215147022U (en) | 2021-07-12 | 2021-07-12 | But quick assembly disassembly's aviation spare part adds clamping apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215147022U true CN215147022U (en) | 2021-12-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121569967.3U Expired - Fee Related CN215147022U (en) | 2021-07-12 | 2021-07-12 | But quick assembly disassembly's aviation spare part adds clamping apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215147022U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115156933A (en) * | 2022-06-20 | 2022-10-11 | 唐山合源钢管有限公司 | Steel pipe chamfering machine with positioning function |
| CN115302248A (en) * | 2022-07-27 | 2022-11-08 | 江南数控机床有限公司 | Gantry type turning and milling compound machine |
| CN115430859A (en) * | 2022-11-10 | 2022-12-06 | 安徽明腾永磁机电设备有限公司 | Motor shaft key groove milling machine tool for permanent magnet motor production |
| CN116619109A (en) * | 2023-07-19 | 2023-08-22 | 山东莱锻机械股份有限公司 | Shaft forging processing manipulator |
-
2021
- 2021-07-12 CN CN202121569967.3U patent/CN215147022U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115156933A (en) * | 2022-06-20 | 2022-10-11 | 唐山合源钢管有限公司 | Steel pipe chamfering machine with positioning function |
| CN115302248A (en) * | 2022-07-27 | 2022-11-08 | 江南数控机床有限公司 | Gantry type turning and milling compound machine |
| CN115302248B (en) * | 2022-07-27 | 2023-12-29 | 江南数控机床有限公司 | Planer-type turning and milling compounding machine |
| CN115430859A (en) * | 2022-11-10 | 2022-12-06 | 安徽明腾永磁机电设备有限公司 | Motor shaft key groove milling machine tool for permanent magnet motor production |
| CN115430859B (en) * | 2022-11-10 | 2023-01-13 | 安徽明腾永磁机电设备有限公司 | Motor shaft key groove milling machine tool for permanent magnet motor production |
| CN116619109A (en) * | 2023-07-19 | 2023-08-22 | 山东莱锻机械股份有限公司 | Shaft forging processing manipulator |
| CN116619109B (en) * | 2023-07-19 | 2023-09-12 | 山东莱锻机械股份有限公司 | Shaft forging processing manipulator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211214 |