CN219967178U - Aviation position processing jig for positioning double-hole column - Google Patents
Aviation position processing jig for positioning double-hole column Download PDFInfo
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- CN219967178U CN219967178U CN202321269449.9U CN202321269449U CN219967178U CN 219967178 U CN219967178 U CN 219967178U CN 202321269449 U CN202321269449 U CN 202321269449U CN 219967178 U CN219967178 U CN 219967178U
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- 238000012545 processing Methods 0.000 title claims abstract description 33
- 238000009434 installation Methods 0.000 claims abstract description 15
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 7
- 230000000149 penetrating effect Effects 0.000 claims description 9
- 230000008859 change Effects 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 5
- 239000000741 silica gel Substances 0.000 claims description 5
- 229910002027 silica gel Inorganic materials 0.000 claims description 5
- 210000001503 joint Anatomy 0.000 claims description 4
- 238000005728 strengthening Methods 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims 4
- 230000009977 dual effect Effects 0.000 claims 2
- 229910000831 Steel Inorganic materials 0.000 claims 1
- 239000010959 steel Substances 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 14
- 230000000694 effects Effects 0.000 abstract description 3
- 238000003723 Smelting Methods 0.000 abstract 1
- 230000008569 process Effects 0.000 description 9
- 230000009471 action Effects 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000011161 development Methods 0.000 description 3
- 230000001788 irregular Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012938 design process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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- Jigs For Machine Tools (AREA)
Abstract
The utility model provides an aviation part processing jig for positioning a double-hole column, which relates to the technical field of double-hole column positioning and comprises a rigid frame, wherein a reinforcing support rib frame is welded at the top of the side edge of the rigid frame; through adjusting under the effect of balladeur train subassembly, be convenient for make when fixing in the location to aviation position part through diplopore post locating bolt, can make the installation locating bottom plate move slider, spout piece and spout end's cooperation under, and then make restriction hole groove and constant head tank corresponding, and then ensure diplopore post locating bolt and fix in the steadiness when fixing in the location to aviation position part, reduce aviation position part in the course of working, receive the impact of force and make diplopore post locating bolt produce the skew, and then make aviation position part cause the damage, simultaneously effectively reduce each aviation position part variation for in location centre gripping in-process, need multiunit processing smelting tool to operate, make holistic industrial cost increase's problem.
Description
Technical Field
The utility model relates to the technical field of positioning and processing of double-hole columns, in particular to an aviation part processing jig for positioning double-hole columns.
Background
Aviation products often take a lot of time during the design process, and some production processes are also affected by many factors during the lengthy design cycle. The method not only relates to complex software, but also has direct association with various hardware, is representative of advanced production technology, and in the production process of aviation products, because general aviation products are mostly composed of subsystems and a plurality of subsystems, no matter components or internal aviation components are required to be subjected to extremely complex precision processing in terms of structure and port mounting design, the method is an integrated mode of production and development in terms of overall aviation product production, can effectively realize linkage of production and development, ensures development quality to be satisfied in the production process, and therefore, needs to cooperate with aviation parts to carry out positioning processing operation through a jig.
But in the aviation position processing tool use of specific diplopore post location, each aviation position part is different for in location centre gripping in-process, need multiunit processing tool to operate, make holistic industrial cost increase, diplopore post location produces the skew at the impact of power to make diplopore post location at processing operation in-process simultaneously, and then makes aviation position part cause the damage, consequently, need propose the aviation position processing tool of a novel diplopore post location.
Disclosure of Invention
The utility model aims to solve the problems that in the prior art, in the use process of a specific double-hole column positioning aviation part processing jig, all aviation part parts are different, so that in the positioning and clamping process, a plurality of groups of processing jigs are required to operate, the whole industrial cost is increased, and meanwhile, in the processing operation process, the double-hole column positioning is offset due to force impact, so that the aviation part parts are damaged, and the double-hole column positioning aviation part processing jig is provided.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the aviation part processing jig comprises a rigid frame, wherein a reinforcing support rib frame is welded at the top of the side edge of the rigid frame, an adjusting carriage assembly is welded at the bottom of the rigid frame, and a positioning hole plate frame is fixedly arranged on the bottom surface of the rigid frame;
the adjusting sliding frame assembly comprises a side edge rigid frame, a sliding groove end is formed in the inner side surface of the side edge rigid frame, a sliding groove block is welded on the top end of the inner side surface of the side edge rigid frame, a movable sliding block is connected to the inner side of the sliding groove end in a sliding mode, a fixing pin is fixedly arranged on the top end surface of the movable sliding block through a butt joint hole end which is formed, an installation positioning bottom plate is fixedly arranged on the side of the movable sliding block, and a limiting hole groove is uniformly formed in the surface of the installation positioning bottom plate in a penetrating mode.
Preferably, the top welding of strengthening support rib frame has the mounting bracket, both ends all are provided with and install adjusting screw about the mounting bracket, adjusting screw's side is provided with the rocking wheel.
Preferably, the front end fastening of adjusting screw installs and connects the fixed block, the front end of connecting the fixed block is provided with and adjusts the change groove, the inside rotation of adjusting the change groove is provided with the column, the avris fastening of column installs the grip block, the avris setting of grip block installs soft silica gel cushion, adjust the change groove with the outer wall surface fastening of column installs the fastening adjustment bolt.
Preferably, a positioning plate is embedded in the positioning hole plate frame, and positioning grooves are uniformly formed in the surface of the positioning plate in a penetrating manner.
Preferably, the bottom of side rigid frame welds there is the supporting seat, the bottom welding of supporting seat has rigid H type to support the ladder frame.
Preferably, the positioning groove and the limiting hole groove are internally provided with a double-hole column positioning bolt in a penetrating way.
Preferably, lifting lugs are oppositely welded on the surfaces of the left side and the right side of the rigid H-shaped supporting ladder frame, and rubber stand feet are arranged at the bottom ends of the left side and the right side of the rigid H-shaped supporting ladder frame.
Compared with the prior art, the utility model has the advantages and positive effects that,
1. according to the utility model, under the action of the adjusting carriage assembly, when the aviation part is positioned and fixed through the double-hole column positioning bolt, the installation positioning bottom plate can be extended under the matching action of the moving sliding block, the sliding groove block and the sliding groove end, so that the limiting hole groove is corresponding to the positioning groove, the stability of the double-hole column positioning bolt when the aviation part is positioned and fixed is further ensured, the problem that the double-hole column positioning bolt is offset due to the impact of force in the processing process of the aviation part is reduced, the aviation part is damaged, meanwhile, the different types of aviation part parts are effectively reduced, and a plurality of groups of processing tools are required to operate in the positioning and clamping process, so that the whole industrial cost is increased is solved.
2. According to the utility model, under the cooperation of the adjusting rotating groove, the rotating column and the fastening adjusting bolt, the clamping block drives the soft silica gel cushion block to conduct angle adjustment, and then clamps the aviation part, so that the industrial cost of operation of a plurality of groups of processing tools is effectively reduced when the irregular part is clamped and fixed.
Drawings
Fig. 1 is a schematic perspective view of an aviation part processing fixture with double-hole column positioning according to the present utility model;
fig. 2 is a schematic diagram showing the separation of the three-dimensional structure of the tooling fixture for the aviation part positioned by the double-hole column;
FIG. 3 is a schematic diagram of a part of a tooling fixture for positioning an aviation part with double-hole columns according to the present utility model;
fig. 4 is an enlarged schematic view of the structure of the aviation part processing fixture in fig. 1 in a double-hole column positioning mode according to the present utility model.
Legend description: 1. a rigid frame; 2. reinforcing the support rib frame; 3. a mounting frame; 4. adjusting a screw; 41. connecting a fixed block; 42. adjusting the rotating groove; 43. a rotating column; 44. fastening the adjusting bolt; 5. shaking wheel; 6. positioning the hole plate frame; 7. adjusting the carriage assembly; 71. a side rigid frame; 72. a chute end; 73. a chute block; 74. moving the slide block; 75. installing a positioning bottom plate; 76. limiting the hole slot; 8. a rigid H-shaped supporting ladder frame; 9. lifting lugs; 10. rubber stand legs; 11. a double-hole column positioning bolt; 12. a positioning plate; 13. and a positioning groove.
Detailed Description
In order that the above objects, features and advantages of the utility model will be more clearly understood, a further description of the utility model will be rendered by reference to the appended drawings and examples. It should be noted that, without conflict, the embodiments of the present utility model and features in the embodiments may be combined with each other.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present utility model, however, the present utility model may be practiced otherwise than as described herein, and therefore the present utility model is not limited to the specific embodiments of the disclosure that follow.
Example 1
As shown in fig. 1 to 4, the present utility model provides a technical solution: the aviation part processing jig comprises a rigid frame 1, wherein a reinforcing support rib frame 2 is welded at the top of the side edge of the rigid frame 1, an adjusting carriage assembly 7 is welded at the bottom of the rigid frame 1, and a positioning hole plate frame 6 is fastened and installed on the bottom surface of the rigid frame 1; the adjusting carriage assembly 7 comprises a side edge rigid frame 71, a chute end 72 is formed in the inner side surface of the side edge rigid frame 71, a chute block 73 is welded on the top end of the inner side surface of the side edge rigid frame 71, a movable sliding block 74 is connected to the inner side of the chute end 72 in a sliding manner, a fixing pin is fixedly arranged on the top end surface of the movable sliding block 74 through a butt joint hole end formed, a mounting positioning bottom plate 75 is fixedly arranged on the side of the movable sliding block 74, a limiting hole groove 76 is uniformly formed in the surface of the mounting positioning bottom plate 75 in a penetrating manner, an installing frame 3 is welded on the top of the reinforcing supporting rib frame 2, adjusting screws 4 are respectively arranged at the left end and the right end of the installing frame 3, rocking wheels 5 are arranged at the side ends of the adjusting screws 4, a connecting fixing block 41 is fixedly arranged at the front end of the connecting fixing block 41, an adjusting rotary groove 42 is rotatably arranged in the adjusting rotary groove 42, a clamping block is fixedly arranged on the side of the rotary column 43, a soft silica gel cushion block is arranged on the side of the clamping block, and a fastening bolt 44 is fixedly arranged on the outer wall surface of the adjusting rotary groove 42.
In the embodiment, the reinforcing support rib frame 2 is welded at the top of the side edge of the rigid frame 1, so that the rigidity of the whole device is ensured, then the bottom of the rigid frame 1 is welded with the adjusting carriage component 7, and the bottom surface of the rigid frame 1 is fastened and provided with the positioning hole plate frame 6 through a fastening bolt; when the aviation part processing operation of double-hole column positioning is performed, the installation positioning bottom plate 75 is extended under the matching action of the sliding groove block 73 welded at the top end of the inner side surface of the side rigid frame 71 and the moving sliding block 74 in sliding connection with the sliding groove end 72, so that the surface of the installation positioning bottom plate 75 is uniformly penetrated and provided with the corresponding limiting hole groove 76 and the positioning groove 13, the stability of the double-hole column positioning bolt 11 when positioning and fixing the aviation part is ensured, the stability of the double-hole column positioning bolt 11 is reduced when the aviation part is subjected to force impact in the processing process, the double-hole column positioning bolt 11 is offset, the aviation part is damaged, meanwhile, the difference of the aviation part parts is effectively reduced, a plurality of groups of processing tools are required to perform the operation in the positioning and clamping process, the problem of increasing the whole industrial cost is solved, then the installation and disassembly operation of the installation positioning bottom plate 75 are convenient under the action of the fixing pins which are fastened and installed on the top surface of the top end of the movable sliding block 74 through the opened butt joint hole ends, the later maintenance operation efficiency is improved, then the installation frame 3 is installed at the top of the reinforced supporting rib frame 2 in a relative vertical welding way, then under the action of the rocking wheel 5 which is arranged at the side end of the adjusting screw 4, the connecting and fixing blocks 41 which are fastened and installed at the front end of the adjusting screw 4 are driven by the adjusting screw 4 which are arranged at the left end and the right end of the installation frame 3 to carry out the fixed clamping operation, meanwhile, the rocking wheel 5 and the adjusting screw 4 are respectively arranged into two groups in a relative vertical way, so that the clamping and fixing of aviation parts with different widths and heights are convenient, and then under the action of the adjusting rotating grooves 42 which are arranged at the front end of the connecting and fixing blocks 41, the clamping blocks which are arranged on the side of the rotating column 43 and are fastened and installed on the side of the rotating column 43 are driven by the rotating column 43 which is arranged in the rotating groove 42 to adjust and clamp irregular aviation parts, and then the rotating column 43 can be limited and fixed in the rotating groove 42 after angle adjustment by the fastening adjusting bolt 44 which is arranged on the outer wall surface of the rotating column 43 and fastened and installed on the outer wall surface of the rotating groove 42.
Example 2
As shown in fig. 1-4, a positioning plate 12 is embedded in the positioning hole plate frame 6, positioning grooves 13 are uniformly formed in the surface of the positioning plate 12 in a penetrating manner, supporting seats are welded at the bottom ends of the side edge rigid frames 71, rigid H-shaped supporting trapezoid frames 8 are welded at the bottom ends of the supporting seats, double-hole column positioning bolts 11 are arranged in the positioning grooves 13 and the limiting hole grooves 76 in a penetrating manner, lifting lugs 9 are oppositely welded on the left side surface and the right side surface of the rigid H-shaped supporting trapezoid frames 8, and rubber stand feet 10 are arranged at the bottom ends of the left side and the right side of the rigid H-shaped supporting trapezoid frames 8.
In this embodiment, install locating plate 12 at the inside gomphosis of locating hole grillage 6, evenly run through at locating plate 12 surface and offered constant head tank 13, afterwards make the supporting seat welding in the bottom of side rigidity frame 71, the operation of whole device is firm through the rigid H type supporting ladder frame 8 of supporting seat bottom welded, ensure the firm supportability of whole operation, afterwards when carrying out aviation position processing operation, can be under manual operation, make constant head tank 13 and limiting hole groove 76 inside run through the diplopore post locating bolt 11 that sets up to fix a position the restriction fastening to aviation position, afterwards under the effect through rigid H type supporting ladder frame 8 left and right sides face homophase opposition welded lug 9, be convenient for carry out steady installation with whole device and place, under the rubber standing foot 10 effect that all installs in rigid H type supporting ladder frame 8 left and right sides bottom, effectively cushion the processing operation of whole device.
The working principle of the embodiment is as follows: when the device is used, firstly, the whole device can be installed and placed through the lifting lug 9, afterwards, the aviation part is placed above the positioning plate 12, afterwards, the adjusting screw 4 is driven by the adjusting screw 5 to be connected with the fixed block 41, the adjusting rotary groove 42, the rotary column 43, the fastening adjusting bolt 44, the clamping block and the soft silica gel cushion block for fixing and clamping, meanwhile, the clamping can be conveniently adjusted and clamped on the irregular aviation part under the adjusting action of the fastening adjusting bolt 44, the industrial cost of the configuration operation of a plurality of groups of processing industry tools is reduced, afterwards, the installation positioning bottom plate 75 can be extended under the matching action of the sliding groove block 73, the sliding groove end 72 and the movable sliding block 74, further, the surface of the installation positioning bottom plate 75 is uniformly penetrated and is corresponding to the positioning groove 13, the stability of the aviation part is guaranteed when the double-hole column positioning bolt 11 is used for fixing the aviation part, the double-hole column positioning bolt is offset in the processing process, the aviation part is further caused by the fact that the aviation part is damaged, and the parts of each part are effectively reduced, the whole processing cost is required to be different in the positioning and clamping process, and the whole processing cost is increased.
The present utility model is not limited to the above-mentioned embodiments, and any equivalent embodiments which can be changed or modified by the technical content disclosed above can be applied to other fields, but any simple modification, equivalent changes and modification made to the above-mentioned embodiments according to the technical substance of the present utility model without departing from the technical content of the present utility model still belong to the protection scope of the technical solution of the present utility model.
Claims (7)
1. The utility model provides an aviation position processing tool of diplopore post location which characterized in that: the steel support comprises a rigid frame (1), wherein a reinforcing support rib frame (2) is welded at the top of the side edge of the rigid frame (1), an adjusting carriage assembly (7) is welded at the bottom of the rigid frame (1), and a positioning hole plate frame (6) is fixedly arranged on the bottom surface of the rigid frame (1);
the adjusting sliding frame assembly (7) comprises a side edge rigid frame (71), a sliding groove end (72) is formed in the inner side surface of the side edge rigid frame (71), a sliding groove block (73) is welded at the top end of the inner side surface of the side edge rigid frame (71), a movable sliding block (74) is connected to the inner side of the sliding groove end (72) in a sliding mode, a fixing pin is fixedly arranged on the top end surface of the movable sliding block (74) through a butt joint hole end which is formed in the surface of the movable sliding block, an installation positioning bottom plate (75) is fixedly arranged on the side of the movable sliding block (74), and a limiting hole groove (76) is uniformly formed in the surface of the installation positioning bottom plate (75) in a penetrating mode.
2. The dual-hole post positioned aerospace part machining jig of claim 1, wherein: the top welding of strengthening support rib frame (2) has mounting bracket (3), both ends all are provided with adjusting screw (4) about mounting bracket (3), the side of adjusting screw (4) is provided with shakes wheel (5).
3. The dual-hole post positioned aerospace part machining jig of claim 2, wherein: the front end fastening of adjusting screw (4) is installed and is connected fixed block (41), the front end of connecting fixed block (41) is provided with and adjusts change groove (42), the inside rotation of adjusting change groove (42) is provided with swivel post (43), the block is installed in the avris fastening of swivel post (43), soft silica gel cushion is installed in the avris setting of block, adjust change groove (42) with the outer wall surface fastening of swivel post (43) installs fastening adjustment bolt (44).
4. The dual-hole post positioned aerospace part machining jig of claim 1, wherein: the locating plate (12) is embedded in the locating hole plate frame (6), and locating grooves (13) are uniformly formed in the surface of the locating plate (12) in a penetrating mode.
5. The dual-hole post positioned aerospace part machining jig of claim 1, wherein: the bottom of side rigid frame (71) is welded with the supporting seat, the bottom welding of supporting seat has rigid H type to support ladder frame (8).
6. The dual post positioned aerospace part tooling fixture of claim 4, wherein: the positioning groove (13) and the limiting hole groove (76) are internally provided with a double-hole column positioning bolt (11) in a penetrating mode.
7. The dual post positioned aerospace part tooling fixture of claim 5, wherein: lifting lugs (9) are oppositely welded on the surfaces of the left side and the right side of the rigid H-shaped supporting ladder frame (8), and rubber stand feet (10) are arranged at the bottoms of the left side and the right side of the rigid H-shaped supporting ladder frame (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321269449.9U CN219967178U (en) | 2023-05-24 | 2023-05-24 | Aviation position processing jig for positioning double-hole column |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321269449.9U CN219967178U (en) | 2023-05-24 | 2023-05-24 | Aviation position processing jig for positioning double-hole column |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219967178U true CN219967178U (en) | 2023-11-07 |
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ID=88581137
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321269449.9U Active CN219967178U (en) | 2023-05-24 | 2023-05-24 | Aviation position processing jig for positioning double-hole column |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219967178U (en) |
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2023
- 2023-05-24 CN CN202321269449.9U patent/CN219967178U/en active Active
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