CN213887692U - Processing tool for airplane slide rail rib parts - Google Patents
Processing tool for airplane slide rail rib parts Download PDFInfo
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- CN213887692U CN213887692U CN202022535519.3U CN202022535519U CN213887692U CN 213887692 U CN213887692 U CN 213887692U CN 202022535519 U CN202022535519 U CN 202022535519U CN 213887692 U CN213887692 U CN 213887692U
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- groove
- workbench
- feed chute
- slide rail
- side plates
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Abstract
The utility model discloses an aircraft slide rail rib part processing tool, which relates to the slide rail roll-in molding field and comprises a workbench, a side plate, a feed chute, a stop block, a roller, a rotating shaft, a butt joint groove, a chute seat, a sponge plate and a fluid pipeline; aluminum plate moves along the inside recess of butt joint inslot portion forward, and aluminum plate becomes "Contraband" template by the straight board simultaneously, and in order to avoid the in-process aluminum plate's of processing temperature higher, begin to extract oil with oil pipeline bottom opening up, spout oil through the nozzle that also has the pipeline top, cool down aluminum plate, and after the processing was accomplished, the one end of the aluminum plate that the processing was accomplished feed chute was carried out in the institute to make the track that needs use.
Description
Technical Field
The utility model relates to a slide rail roll-in shaping technical field specifically is an aircraft slide rail rib parts machining frock.
Background
The rolling deformation is line contact, continuously and gradually carried out, the required deformation force is small, one or more workpieces can be produced in one stroke, compared with the cutting and grinding process, the rolling forming process has the advantages of high production efficiency, material saving, high product strength and stable quality, the process is particularly suitable for processing the workpieces which are extremely long and short and difficult to cut, and is most beneficial to large-batch products produced in millions per year, and the economic benefit is also the most considerable.
Present authorized utility model patent, patent application number is 201821743002.X, and the patent name is a slide rail roll-in device of integration processing, including the roll-in make-up machine body, two slide rails of top fixedly connected with of roll-in make-up machine body, it is left the top sliding connection of slide rail has evenly distributed's first supporting block, the left side fixedly connected with conversion equipment of first supporting block, conversion equipment's left end runs through and extends to the inside of first supporting block. The utility model discloses a, possess advantages such as being convenient for change roll-in wheel, it is generally one-to-one to have solved slide rail roll-in device on the market, can only process single kind shape, when processing the slide rail of another kind of shape, just need use another kind of roll-in device to process sometimes to improved manufacturing cost, also made operating personnel's burden become heavy, the roll-in device's of general removable roll-in wheel change step is loaded down with trivial details, be unfavorable for user's operation, and strengthened the problem of cost of labor.
However, the above scheme has some problems, firstly, the mode of circular film pressing is adopted from top to bottom, the deviation of the die is easily caused, so that the accuracy of the finally formed slide rail is not high, secondly, no cooling liquid is arranged, and accidents easily occur due to overhigh alloy temperature in the bending process.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an aircraft slide rail rib part processing tool, which is used for solving the technical problems existing in the prior art; firstly, all adopt the mode of circular press mold from top to bottom, cause the deviation of mould easily to lead to final fashioned slide rail precision not high, secondly, do not set up the coolant liquid, the too high accident that takes place easily of in-process alloy temperature of bending.
The utility model aims to overcome the not enough of prior art, provide an aircraft slide rail rib parts machining frock: comprises a workbench, a side plate, a feed chute, a stop block, a roller, a rotating shaft, a butt-joint chute, a chute seat, a sponge plate and an oil pipeline;
wherein the bottom of the groove seat is fixedly connected with the middle part of the top end of the workbench, the side plates are fixedly arranged at two sides of the groove seat, a gap is arranged between the side plates and the groove seat, the bottom of the side plates is fixedly connected with the top of the workbench, the bottom of the butt joint groove is fixedly connected with the top of the groove seat,
the side walls of the side plates are provided with a plurality of through holes in a penetrating way, the rotating shaft is rotatably connected with the through holes corresponding to the two side plates, the middle part of the rotating shaft is fixedly provided with a roller, the bottom of the roller is matched with the groove at the top of the butting groove, one end of the oil pipeline is fixedly connected in the annular groove of the workbench, the other end of the oil pipeline is fixedly arranged at the top of the side plates, the opening at the top end of the oil pipeline faces the roller,
the feed chute is fixedly connected with the same end of the two side plates, the top end of the feed chute is provided with a groove, the groove at the top end of the feed chute is matched with the groove at the top of the abutting chute, the stop block adopts a square strip structure, the length of the stop block is longer than that of the feed chute groove, the bottom of the stop block is fixedly connected with the top of the feed chute groove, the part of the feed chute connected with the stop block forms a square through hole,
a sponge plate is fixedly arranged at the bottom of the workbench.
Further, a bearing is arranged at a part of the side plate, which is in contact with the rotating shaft.
Furthermore, an annular groove is formed in the outer ring of the connecting part of the top of the workbench and the side plate.
Furthermore, a nozzle is arranged at the opening at the top end of the oil pipeline.
Furthermore, a motor is arranged on the side surface of the rotating shaft.
Furthermore, the opening of the feeding of the abutting groove adopts an inclined design.
Further, oil is placed in an annular groove of a connecting portion of the top of the workbench and the side plate.
Furthermore, the sponge plate is made of sponge materials.
The utility model has the advantages that: (1) the aluminum plate moves along the groove inside the abutting groove, and the aluminum plate is changed from a straight plate into an Contraband-shaped plate.
(2) In order to avoid the high temperature of the aluminum plate in the machining process, the oil liquid at the bottom opening of the oil liquid pipeline is extracted upwards, and the oil liquid is sprayed out through the nozzle with the top end of the pipeline, so that the aluminum plate is cooled.
(3) And after the processing is finished, conveying the processed aluminum plate out of one end of the yard feeding groove so as to manufacture the rail to be used.
Drawings
Fig. 1 is the utility model relates to an aircraft slide rail rib parts machining frock sketch map.
Figure 2 is the utility model relates to an aircraft slide rail rib parts machining frock cross-sectional view.
Figure 3 is the utility model relates to an aircraft slide rail rib parts machining frock butt groove view.
Figure 4 is the utility model relates to an aircraft slide rail rib parts machining frock workstation view.
In the figure, 1-workbench, 2-side plate, 3-feeding groove, 4-baffle block, 5-roller, 6-rotating shaft, 7-butt groove, 8-groove seat, 9-sponge plate and 10-oil pipeline.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to fig. 1-4 of the present invention, and it should be apparent that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
An aircraft slide rail rib part machining tool comprises a workbench 1, a side plate 2, a feed chute 3, a stop block 4, a roller 5, a rotating shaft 6, a butt groove 7, a groove seat 8, a sponge plate 9 and an oil pipeline 10
Wherein the bottom of the groove seat 8 is fixedly connected with the middle part of the top end of the workbench 1, the side plates 2 are fixedly arranged at two sides of the groove seat 8, a gap is arranged between the side plates 2 and the groove seat 8, the bottom of the side plates 2 is fixedly connected with the top of the workbench 1, the bottom of the abutting groove 7 is fixedly connected with the top of the groove seat 8,
the side walls of the side plates 2 are provided with a plurality of through holes in a penetrating way, the rotating shaft 6 is rotatably connected with the corresponding through holes of the two side plates 2, the middle part of the rotating shaft 6 is fixedly provided with a roller 5, the bottom of the roller 5 is matched with the groove at the top of the butt groove 7, one end of an oil pipeline 10 is fixedly connected in the annular groove of the workbench 1, the other end of the oil pipeline 10 is fixedly arranged at the top of the side plates 2, and the opening at the top end of the oil pipeline 10 faces the roller 5,
the feed chute 3 is fixedly connected with the same end of the two side plates 2, the top end of the feed chute 3 is provided with a groove, the groove at the top end of the feed chute 3 is matched with the groove at the top of the butt groove 7, the stop block 4 adopts a square strip structure, the length of the stop block 4 is longer than that of the groove of the feed chute 3, the bottom of the stop block 4 is fixedly connected with the top of the groove of the feed chute 3, the connecting part of the feed chute 3 and the stop block 4 forms a square through hole,
a sponge plate 9 is fixedly arranged at the bottom of the workbench 1.
Referring to fig. 1-4, the present invention provides a technical solution; the bottom of the groove seat 8 is connected with the middle part of the top end of the workbench 1, the side plates 2 are arranged at two sides of the groove seat 8, the bottom of the side plates 2 is connected with the top of the workbench 1, the bottom of the butt groove 7 is connected with the top of the groove seat 8, the rotating shaft 6 is rotatably connected with the through hole of the side plates 2, one end of the oil pipeline 10 is connected with the annular groove of the workbench 1, the other end is arranged at the top of the side plates 2, the opening of the top end of the oil pipeline 10 faces the roller 5, the side surface of the feed chute 3 is connected with one end of the two side plates 2, the length of the stop block 4 is longer than that of the groove of the feed chute 3, the bottom of the stop block 4 is connected with the top of the stop block 4, the bottom of the workbench 1 is provided with a sponge plate 9, when the utility model is used, unprocessed aluminum plates are placed in the square through holes formed by the feed chute 3 and the stop block 4 and move forwards, when the aluminum plates move to the gap between the roller 5 and the butt groove 7, carry out the butt, need not artificially control aluminum plate this moment, start the starter motor, aluminum plate moves along the recess of butt slot 7 inside forward, aluminum plate becomes "Contraband" template by the straight board simultaneously, to avoid the in-process aluminum plate's of processing temperature higher, begin to extract oil with oil pipeline 10 bottom opening up, spout oil through the nozzle that also has pipeline 10 top, cool down aluminum plate, after processing is accomplished, the aluminum plate that processing was accomplished is carried out in the one end of feed chute 3 in the institute to make the track that needs use.
Further, the part of the side plate 2 contacting with the rotating shaft 6 is provided with a bearing, so that the stability of the rotating shaft is enhanced.
Furthermore, an annular groove is formed in the outer ring of the connecting part of the top of the workbench 1 and the side plate 2, so that oil can be collected and discharged conveniently.
Furthermore, a nozzle is arranged at the opening at the top end of the oil pipeline 10, so that oil can be conveniently aligned to an object to be cooled.
Furthermore, a motor is arranged on the side surface of the rotating shaft 6, so that the machine can be started conveniently.
Furthermore, the opening part for feeding the abutting groove 7 adopts an inclined design, so that the articles can be conveniently processed.
Furthermore, oil is placed in the annular groove of the connecting part of the top of the workbench 1 and the side plate 2, so that the oil can be collected and used conveniently.
Furthermore, the sponge plate 9 is made of sponge materials, and the damping effect is enhanced.
In the description of the present invention, it should be understood that the terms "counterclockwise", "clockwise", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description of the present invention, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Claims (8)
1. The machining tool for the rib part of the airplane sliding rail is characterized by comprising a workbench (1), side plates (2), a feeding groove (3), a stop block (4), a roller (5), a rotating shaft (6), a butting groove (7), a groove seat (8), a sponge plate (9) and an oil pipeline (10);
wherein the bottom of the groove seat (8) is fixedly connected with the middle part of the top end of the workbench (1), the side plates (2) are fixedly arranged at two sides of the groove seat (8), a gap is arranged between the side plates (2) and the groove seat (8), the bottom of the side plates (2) is fixedly connected with the top of the workbench (1), the bottom of the butt joint groove (7) is fixedly connected with the top of the groove seat (8),
a plurality of through holes are arranged on the side wall of each side plate (2) in a penetrating way, a rotating shaft (6) is rotatably connected at the corresponding through holes of the two side plates (2), a roller (5) is fixedly arranged in the middle of the rotating shaft (6), the bottom of the roller (5) is matched with a groove at the top of a butt joint groove (7), one end of an oil pipeline (10) is fixedly connected in an annular groove of a workbench (1), the other end of the oil pipeline (10) is fixedly arranged at the top of each side plate (2), and an opening at the top end of the oil pipeline (10) faces towards the roller (5),
the feed chute (3) is fixedly connected with the same end of the two side plates (2), the top end of the feed chute (3) is provided with a groove, the groove at the top end of the feed chute (3) is matched with the groove at the top of the butt joint groove (7), the stop block (4) adopts a square strip structure, the length of the stop block (4) is longer than that of the groove of the feed chute (3), the bottom of the stop block (4) is fixedly connected with the top of the groove of the feed chute (3), and the connecting part of the feed chute (3) and the stop block (4) forms a square through hole,
a sponge plate (9) is fixedly arranged at the bottom of the workbench (1).
2. The tooling for machining the rib part of the airplane slide rail according to claim 1, wherein a bearing is arranged at the contact part of the side plate (2) and the rotating shaft (6).
3. The processing tool for the rib part of the aircraft sliding rail according to claim 1, wherein an annular groove is formed in an outer ring of a connecting part of the top of the workbench (1) and the side plate (2).
4. The processing tool for the rib part of the aircraft sliding rail according to claim 1, wherein a spray nozzle is arranged at an opening at the top end of the oil pipeline (10).
5. The processing tool for the rib part of the airplane slide rail according to claim 1, wherein a motor is arranged on the side surface of the rotating shaft (6).
6. The tooling for machining the rib parts of the aircraft slide rails as claimed in claim 1, wherein the opening for feeding the abutting groove (7) is of an inclined design.
7. The processing tool for the rib part of the aircraft sliding rail according to claim 1, wherein oil is placed in an annular groove at the connecting part of the top of the workbench (1) and the side plate (2).
8. The processing tool for the rib part of the aircraft slide rail as claimed in claim 1, wherein the sponge plate (9) is made of sponge material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022535519.3U CN213887692U (en) | 2020-11-05 | 2020-11-05 | Processing tool for airplane slide rail rib parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022535519.3U CN213887692U (en) | 2020-11-05 | 2020-11-05 | Processing tool for airplane slide rail rib parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213887692U true CN213887692U (en) | 2021-08-06 |
Family
ID=77117241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022535519.3U Active CN213887692U (en) | 2020-11-05 | 2020-11-05 | Processing tool for airplane slide rail rib parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213887692U (en) |
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2020
- 2020-11-05 CN CN202022535519.3U patent/CN213887692U/en active Active
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