CN213708423U - Tool clamp for shot blasting strengthening of perforated airplane parts - Google Patents
Tool clamp for shot blasting strengthening of perforated airplane parts Download PDFInfo
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- CN213708423U CN213708423U CN202022215285.4U CN202022215285U CN213708423U CN 213708423 U CN213708423 U CN 213708423U CN 202022215285 U CN202022215285 U CN 202022215285U CN 213708423 U CN213708423 U CN 213708423U
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- mounting
- clamping
- tool clamp
- slider
- shot peening
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Abstract
The utility model discloses a frock clamp is reinforceed to foraminiferous type aircraft part peening, comprises a workbench, the upper surface of workstation is provided with the mounting bracket, be provided with the mounting panel on the mounting bracket, transversely be provided with the spout along on the mounting panel, sliding connection has a plurality of slider on the spout, detachably is provided with the clamping mechanism who is used for the clamping work piece on the slider. The utility model is suitable for a peening of foraminiferous type aircraft part is reinforceed, and operating personnel can select and adjust quantity, the diameter of installation stand that clamping machine constructs according to the shape of foraminiferous type aircraft part and the diameter in hole quantity, hole to it is fixed to accomplish the clamping of work piece fast, has effectively improved efficiency, the utility model discloses simple structure, convenient operation have very big spreading value.
Description
Technical Field
The utility model belongs to the technical field of the peening is reinforceed, more specifically say, relate to a reinforce frock clamp with foraminiferous type aircraft part peening.
Background
Shot peening has been widely used as a strengthening technique for surface modification in the manufacture of parts, particularly aircraft parts. In the production practice of airplane parts, there are many parts with hole structures, such as inner holes and cavities, which are widely existed in key parts of airplane landing gear, rotor system and transmission system. Compared with shot peening processing on the surface of a conventional part, although the shot peening strengthening processing technology of the porous part has no essential difference with a common workpiece, due to the fact that the number and the aperture of holes of the porous airplane part are different, various clamping tools need to be prepared during actual shot peening strengthening processing, shot peening processing can only be carried out on a single surface mostly, time and labor are wasted, and therefore the shot peening strengthening tool clamp which can be rapidly clamped and can be suitable for the porous airplane parts with different apertures is urgently needed.
Disclosure of Invention
Not enough to prior art exists, the utility model aims to provide a frock clamp is reinforceed to the peening that can quick clamping and can be applicable to the foraminiferous type aircraft part in different apertures to improve the peening strengthening efficiency of foraminiferous type aircraft part, reduce the processing cost.
In order to solve the technical problem, the utility model discloses a following technical scheme realizes:
the utility model provides a frock clamp is reinforceed to foraminiferous type aircraft part peening, includes the workstation, the upper surface of workstation is provided with the mounting bracket, be provided with the mounting panel on the mounting bracket, transversely be provided with the spout along on the mounting panel, sliding connection has a plurality of slider on the spout, detachably is provided with the clamping machine structure that is used for the clamping work piece on the slider, the slider is used for driving clamping machine structure and removes along the spout.
The utility model discloses still have following technical characteristic:
optionally, the clamping mechanism comprises a mounting upright column which is vertically arranged on the sliding block and has adjustable height, and the mounting upright column is detachably connected with a fastener.
Optionally, the number of the sliding grooves is two and the sliding grooves are arranged in parallel.
Optionally, a plurality of fastening bolt mounting holes are formed in the workbench along the circumferential direction, fastening bolts are arranged in the fastening bolt mounting holes, and the fastening bolts penetrate through the fastening bolt mounting holes to fix the mounting frame on the workbench.
Optionally, a position of the sliding block, which is opposite to the sliding groove, is provided with a limiting hole, a limiting pin is arranged in the limiting hole, and the limiting pin penetrates through the limiting hole and the sliding groove to fix the sliding block on the mounting plate.
Optionally, the mounting upright column comprises a supporting section, a connecting section and a clamping section which are sequentially arranged from bottom to top, and the diameter of the clamping section is adjustable.
Compared with the prior art, the utility model, following technological effect has:
the utility model is suitable for a peening of foraminiferous type aircraft part is reinforceed, and operating personnel can select and adjust quantity, the diameter of installation stand that clamping machine constructs according to the shape of foraminiferous type aircraft part and the diameter in hole quantity, hole to it is fixed to accomplish the clamping of work piece fast, has effectively improved efficiency, the utility model discloses simple structure, convenient operation have very big spreading value.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic view of the structure of the components of the present invention.
The meaning of the individual reference symbols in the figures is: 1-a workbench, 2-a mounting rack, 3-a mounting plate, 4-a chute, 5-a sliding block, 6-a clamping mechanism, 7-a fastening bolt mounting hole and 8-a fastening bolt;
51-limiting hole, 52-limiting pin;
61-mounting upright, 62-fastener, 611-supporting section, 612-connecting section, 613-fixing section.
The following examples are provided to explain the present invention in further detail.
Detailed Description
It is to be noted that all the components of the present invention, unless otherwise specified, are all the components known in the art.
The terms "upper", "lower", "front", "rear", and the like as used herein are used merely to facilitate the description of the invention and to simplify the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, "inner", "outer" refers to the inner and outer of the corresponding component profile, and the above terms should not be construed as limiting the invention.
Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or imply that the number of technical features indicated is significant. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature.
In the present invention, the terms "mounting", "connecting", "fixing", etc. should be understood in a broad sense without being stated to the contrary, and may be, for example, fixedly connected, or detachably connected or integrated; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Example 1:
obey above-mentioned technical scheme, as shown in fig. 1 to 2, this embodiment provides a foraminiferous type aircraft part peening strengthening frock clamp, including workstation 1, the upper surface of workstation 1 is provided with mounting bracket 2, is provided with mounting panel 3 on the mounting bracket 2, along transversely being provided with spout 4 on the mounting panel 3, and sliding connection has a plurality of slider 5 on spout 4, and detachably is provided with the clamping mechanism 6 that is used for the clamping work piece on the slider 5, and slider 5 drives clamping mechanism 6 and removes along spout 4.
In this embodiment, workstation 1 is circular, and the parallel workstation 1 fixed mounting of mounting panel 3 is on workstation 1, sliding connection 3 sliders 5 on spout 4, installs 1 clamping machine structure 6 on every slider 5, and clamping machine structure 6 is used for waiting the work piece of processing through the through-hole clamping of seting up on the work piece, and the slider is used for setting up clamping machine structure 6 and drives clamping machine structure 6 and remove along spout 4.
As a preferable scheme of this embodiment, the clamping mechanism 6 includes a height-adjustable mounting column 61 vertically disposed on the sliding block 5, and the mounting column 61 is detachably connected with a fastener 62. The mounting post 61 and the fastener 62 are cooperatively arranged for clamping a workpiece to be machined.
As a preferable solution of this embodiment, the number of the sliding grooves 4 is two and the sliding grooves are arranged in parallel.
As a preferred scheme of this embodiment, 6 fastening bolt mounting holes 7 have been seted up along circumference on workstation 1, and fastening bolt mounting hole 7 is two liang of mirror symmetry settings, is provided with fastening bolt 8 in the fastening bolt mounting hole 7, and fastening bolt 8 passes fastening bolt mounting hole 7 and fixes mounting bracket 2 to workstation 1.
As a preferable scheme of this embodiment, a position of the slider 5 opposite to the sliding groove 4 is provided with a limiting hole 51, a limiting pin 52 is disposed in the limiting hole 51, and the limiting pin 52 passes through the limiting hole 51 and the sliding groove 4 to fix the slider 5 on the mounting plate 3.
As a preferable scheme of this embodiment, the mounting column 61 includes a supporting section 611, a connecting section 612, and a fixing section 613 sequentially arranged from bottom to top, the fixing section 613 is configured to clamp a workpiece through a through hole formed in the workpiece to be processed, a diameter of the fixing section 613 is adjustable, the diameter of the fixing section 613 can be selected according to a size of an opening of the workpiece, and the fixing section 613 and the supporting section 621 are detachably connected through the connecting section 612.
The utility model discloses a use as follows:
the mounting frame 2 is fixed on the workbench 1, then the mounting plate 3 is fixed, the clamping mechanism 6 is selected according to the number of holes and the aperture of a workpiece to be processed, the selected clamping mechanism 6 is fixed on the sliding block 5, then the sliding block 5 is fixed on the mounting plate, shot peening strengthening treatment is carried out on the clamped workpiece, after shot peening strengthening treatment is completed on the upper surface of the workpiece, turning is not needed, shot peening strengthening treatment on the lower surface of the workpiece is directly completed below, and after treatment is completed, the workpiece is taken down from the device.
The utility model discloses a measuring device has accomplished the clamping experiment, and the in-service use is respond well, and the clamping is convenient quick, satisfies the requirement.
The preferred embodiments of the present invention have been described in detail with reference to the accompanying drawings, however, the present invention is not limited to the details of the above embodiments, and the technical concept of the present invention can be within the scope of the present invention to perform various simple modifications to the technical solution of the present invention, and these simple modifications all belong to the protection scope of the present invention.
In addition, various embodiments of the present invention can be combined arbitrarily, and the disclosed content should be regarded as the present invention as long as it does not violate the idea of the present invention.
Claims (6)
1. The utility model provides a foraminiferous type aircraft part peening strengthening frock clamp, includes workstation (1), its characterized in that, the upper surface of workstation (1) is provided with mounting bracket (2), be provided with mounting panel (3) on mounting bracket (2), transversely be provided with spout (4) along on mounting panel (3), sliding connection has a plurality of slider (5) on spout (4), detachably is provided with clamping machine structure (6) that are used for the clamping work piece on slider (5), slider (5) are used for driving clamping machine structure (6) and remove along spout (4).
2. A tool clamp for shot peening strengthening of airplane parts with holes as claimed in claim 1, wherein the clamping mechanism (6) comprises a height-adjustable mounting column (61) vertically arranged on the slide block (5), and the mounting column (61) is detachably connected with a fastener (62).
3. A tool clamp for shot peening strengthening of a holed aircraft part as claimed in claim 1, wherein the number of the chutes (4) is two and arranged in parallel.
4. A tool clamp for shot peening strengthening of an airplane part with holes according to claim 1, wherein a plurality of fastening bolt mounting holes (7) are formed in the circumferential direction of the workbench (1), fastening bolts (8) are arranged in the fastening bolt mounting holes (7), and the fastening bolts (8) penetrate through the fastening bolt mounting holes (7) to fix the mounting frame (2) on the workbench (1).
5. A tool clamp for shot peening strengthening of airplane parts with holes according to claim 1, characterized in that a limiting hole (51) is formed in the position of the slide block (5) opposite to the sliding groove, a limiting pin (52) is arranged in the limiting hole (51), and the limiting pin (52) penetrates through the limiting hole (51) and the sliding groove (4) to fix the slide block (5) on the mounting plate (3).
6. A tool clamp for shot peening strengthening of a perforated airplane part according to claim 2, wherein the mounting upright (61) comprises a supporting section (611), a connecting section (612) and a fixing section (613) which are arranged in sequence from bottom to top, and the diameter of the fixing section (613) is adjustable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022215285.4U CN213708423U (en) | 2020-09-30 | 2020-09-30 | Tool clamp for shot blasting strengthening of perforated airplane parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022215285.4U CN213708423U (en) | 2020-09-30 | 2020-09-30 | Tool clamp for shot blasting strengthening of perforated airplane parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213708423U true CN213708423U (en) | 2021-07-16 |
Family
ID=76796390
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022215285.4U Active CN213708423U (en) | 2020-09-30 | 2020-09-30 | Tool clamp for shot blasting strengthening of perforated airplane parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213708423U (en) |
-
2020
- 2020-09-30 CN CN202022215285.4U patent/CN213708423U/en active Active
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