CN216441766U - Cutting machine is used in processing of aviation plug connector shell - Google Patents
Cutting machine is used in processing of aviation plug connector shell Download PDFInfo
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- CN216441766U CN216441766U CN202122702840.0U CN202122702840U CN216441766U CN 216441766 U CN216441766 U CN 216441766U CN 202122702840 U CN202122702840 U CN 202122702840U CN 216441766 U CN216441766 U CN 216441766U
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Abstract
The utility model discloses a cutting machine for machining an aviation connector clip shell, which comprises a rack and comprises: the cutting tools are symmetrically arranged on two sides of the middle part of the rack; the feeding runway is arranged in the middle of the rack and comprises a sliding platform, a runway shell, a ball screw and a driving motor; the jig comprises a jig main board and a jig module; the pressing device is arranged on the rack above the cutting tool and comprises a mounting frame, a driving cylinder, a push plate and a hydraulic rod. The utility model has the beneficial effects that: 1. the aviation connector clip shell on the casting can be cut and separated from the excess material at one time through the cutting tools symmetrically arranged on the two sides of the cutting table, so that the production efficiency is improved; 2. the jig module can be attached to the inner side face of the part, which is located on the outer side of the aviation connector clip, of the housing, the jig module is fixed and stable, the cutting of the blade is more stable, and the cutting precision is high.
Description
Technical Field
The utility model belongs to the technical field of aviation industry processing, and particularly relates to a cutting machine for processing an aviation connector clip shell.
Background
Aviation plug connector shell is the aluminum product foundry goods, be a mould two-chamber casting when pouring, one shot forming goes out four aviation plug connector shell work pieces, but there is the clout that produces when filling the type circulation between every aviation plug connector shell, need the excision and with four aviation plug connector shell separations, among the prior art, mostly adopt the saw blade to open the work piece and the clout rough machining and the fine-machining substep operation of instrument lathe cutting, and one-by-one cutting operation, every foundry goods needs the repetitive operation, and is low in efficiency, and the cost of labor is higher.
In summary, in order to solve the technical problems in the prior art, the utility model designs the cutting machine for machining the aviation connector shell, which is simple in structure and capable of cutting and separating the excess materials and the workpiece at one time.
Disclosure of Invention
The utility model aims to solve the technical problems in the prior art and designs the cutting machine for machining the aviation connector shell, which has a simple structure and can cut and separate excess materials and workpieces at one time.
The purpose of the utility model can be realized by the following technical scheme:
the utility model provides a cutting machine is used in processing of aviation plug connector shell, includes the frame:
the cutting tools are symmetrically arranged on two sides of the middle part of the rack, each cutting tool comprises a movable base, a cutting motor and a blade, the cutting motor is adjustably connected with the rack through the movable base, and the blades are arranged on the output end of the cutting motor;
the feeding runway is arranged in the middle of the rack and comprises a sliding table, a runway shell, a ball screw and a driving motor, the ball screw is arranged in the runway shell, the sliding table is arranged above the runway shell, the middle part below the sliding table is in transmission connection with the ball screw, the end part of the ball screw is connected with the driving motor, and one end of the feeding runway is arranged between the cutting tools;
the jig comprises a jig main board and jig modules, wherein the jig modules are uniformly distributed above the jig main board in a square array, the jig modules are semi-conical, the narrow ends of the jig modules are mutually far away, a transverse avoiding groove is formed in the end part of each jig module on the jig main board, and the jig is arranged on the sliding table;
the press device, press device sets up in the frame of cutting tool top, press device includes the mounting bracket, drives actuating cylinder, push pedal, hydraulic stem, it is vertical to drive actuating cylinder to set up in the mounting bracket, the output that drives actuating cylinder stretches out the mounting bracket downwards, the push pedal is connected on driving actuating cylinder output, the vertical setting of hydraulic stem is in the push pedal below.
Furthermore, the movable base comprises a screw rod mechanism, a first sliding rail and a sliding table, the screw rod mechanism is arranged in parallel with the first sliding rail, the sliding table is arranged above the screw rod mechanism and the first sliding rail, and the upper portion of the sliding table is connected with the lower portion of the cutting motor.
Furthermore, an adjusting indexing table is connected below the movable base.
Furthermore, two sliding rails II are symmetrically arranged on two sides of the ball screw, and two sides below the sliding table are connected with the sliding rails II in a sliding mode.
Furthermore, the jig main board is provided with a positioning hole in the middle of the outer side edge of the jig module.
Furthermore, the surfaces of the two ends of the jig module are circumferentially provided with vent grooves.
Furthermore, an anti-skid end socket is arranged at the output end of the hydraulic rod.
Compared with the prior art, the utility model has reasonable structure and arrangement: 1. the aviation connector clip shell on the casting can be cut and separated from the excess material at one time through the cutting tools symmetrically arranged on the two sides of the cutting table, so that the production efficiency is improved; 2. the jig module can be attached to the inner side surface of the housing part of the aviation plug connector and is fixed stably, so that the blade is cut more stably, and the cutting precision is high; 3. the thermal deformation of the aviation connector housing casting can be detected; 4. the aviation connector shell casting can be tightly attached to the jig module through the pressing device; 5. can improve the security through between feeding runway with aviation plug connector shell foundry goods automatic feed to the blade.
Drawings
FIG. 1 is a schematic view of the cutting machine;
FIG. 2 is a schematic view of a cutting tool and a feed runway;
FIG. 3 is a schematic view of the interior of a feed runway;
FIG. 4 is a schematic view of the movable base and the index table;
FIG. 5 is a schematic view of the interior of the mobile base and the feed runway;
FIG. 6 is a schematic view of a jig;
FIG. 7 is a schematic view of a pressing device;
see fig. 1-7, wherein: 1. a frame; 2. a cutting tool; 21. a movable base; 211. a screw mechanism; 212. a first slide rail; 213. a sliding table; 22. cutting the motor; 23. a blade; 24. adjusting the indexing table; 3. a feed runway; 31. a sliding table; 32. a runway skin; 33. a ball screw; 34. a drive motor; 35. a second slide rail; 4. a jig; 41. a jig main board; 411. an avoidance groove; 412. positioning holes; 42. a jig module; 421. a vent channel; 5. a pressing device; 51. a mounting frame; 52. a driving cylinder; 53. pushing the plate; 54. a hydraulic lever; 55. an anti-slip end.
Detailed Description
The technical solution of the present invention is further illustrated by the following examples. In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but 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, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The first embodiment is as follows:
the utility model provides a cutting machine is used in processing of aviation plug connector shell, includes frame 1, includes:
the cutting tool 2 is symmetrically arranged on two sides of the middle part of the rack 1, the cutting tool 2 comprises a movable base 21, a cutting motor 22 and a blade 23, the cutting motor 22 is adjustably connected with the rack 1 through the movable base 21, and the blade 23 is arranged at the output end of the cutting motor 22;
the feeding runway 3 is arranged in the middle of the rack 1, the feeding runway 3 comprises a sliding platform 31, a runway shell 32, a ball screw 33 and a driving motor 34, the ball screw 33 is arranged in the runway shell 32, the sliding platform 31 is arranged above the runway shell 32, the middle part below the sliding platform 31 is in transmission connection with the ball screw 33, the end part of the ball screw 33 is connected with the driving motor 34, and one end of the feeding runway 32 is arranged between the cutting tools 3;
the jig 4 comprises a jig main board 41 and jig modules 42, wherein the jig modules 42 are uniformly distributed above the jig main board 41 in a square array, the jig modules 42 are semi-conical, the narrow ends of the jig modules 42 are far away from each other, a transverse avoiding groove 411 is arranged at the end part of each jig module 42 on the jig main board 41, and the jig 4 is arranged on the sliding table 31;
the pressing device 5, the pressing device 5 sets up on the frame 1 of cutting tool 2 top, the pressing device 5 includes mounting bracket 51, drives actuating cylinder 52, push pedal 53, hydraulic stem 54, it is vertical in mounting bracket 51 to drive actuating cylinder 52, the output that drives actuating cylinder 52 stretches out mounting bracket 51 downwards, push pedal 53 is connected on driving actuating cylinder 52 output, the vertical setting of hydraulic stem 54 is in push pedal 53 below.
Specifically, the cutting tools 2 on the two sides are firstly in an open state, the sliding table 31 is firstly positioned at one end, away from the cutting tools 2, of the feeding runway 3, when the aviation connector housing casting is used, the jig main board 41 is placed on the aviation connector housing casting, the aviation connector housing part corresponds to the jig module 42, the shape of the jig module 42 is matched with the shape of the inner wall of the aviation connector housing, the aviation connector housing can be stably placed on the jig module 42, and the thermal deformation degree of the casting can be judged according to the placing stability degree; the driving motor 24 works to rotate the ball screw 33 and drive the sliding table 31 to move towards the direction of the cutting tool 2 until the jig 4 bears the aviation connector shell casting and reaches between the cutting tools 2; the pressing device 5 descends, the driving cylinder 52 works to drive the push plate 53 to move downwards, the hydraulic rod 54 is in contact with the upper surface of the casting, and the hydraulic rod 54 extends out, so that the casting is tightly attached to the jig module 42, and the phenomenon of jumping during cutting can be avoided; after the fixing, the position that needs the cutting on the foundry goods aligns with dodging the groove 411, and cutting motor 32 work drives blade 33 and rotates, and the work of movable base 31 drives the cutting motor 32 of both sides and draws close to 2 middle parts of cutting table, and at the in-process of drawing close, blade 33 cuts in from the edge of foundry goods gradually to get into gradually and dodge groove 411, finally cut off the separation with aviation plug connector shell part and clout.
Example two:
the difference between the second embodiment and the first embodiment is that the movable base 21 includes a screw rod mechanism 211, a first slide rail 212, and a sliding table 213, the screw rod mechanism 211 is parallel to the first slide rail 212, the sliding table 213 is disposed above the screw rod mechanism 211 and the first slide rail 212, and the upper side of the sliding table 213 is connected to the lower side of the cutting motor 22.
Specifically, when the movable base 21 works, the screw rod mechanism 211 works to provide power for the sliding table 213 to move transversely, and the first sliding rail 212 supports the sliding table 213, the cutting motor 22 and the blade 23, so that the weight borne by the screw rod mechanism 211 is reduced.
Example three:
the difference between the third embodiment and the first embodiment is that an adjusting index table 24 is connected below the movable base 21.
Specifically, when carrying out the aviation plug connector shell foundry goods of different batches and processing, detect the torsion degree of aviation plug connector shell foundry goods through measuring the utensil of examining, then adjust the height of adjusting indexing table 24, adjust the rising or the decline of indexing table 24 and can drive the slope of cutting tool 2 to the torsion degree of the current processing batch foundry goods of adaptation improves the machining precision.
Example four:
the difference between the fourth embodiment and the first embodiment is that two sliding rails two 35 are symmetrically arranged on two sides of the ball screw 33, and two sides below the sliding table 31 are slidably connected with the sliding rails two 35.
Specifically, the second slide rail 35 can replace the ball screw 34 to bear the weight of the sliding table 31 and the jig 4, so that the sliding table 31 cannot slide on the ball screw 34 due to the load bearing and bending of the ball screw 34 is avoided.
Example five:
the difference between the fifth embodiment and the first embodiment is that the jig main board 41 is provided with a positioning hole 412 at the middle of the outer side of the jig module 42.
Specifically, the positioning hole 412 can be matched with a connection protrusion for avoiding the side edge of the aviation connector shell, so that the aviation connector shell casting can be placed on the jig main board 41 more stably.
Example six:
the sixth embodiment is different from the first embodiment in that the jig module 42 is provided with vent grooves 421 on both end surfaces thereof in the circumferential direction.
Specifically, air channel 421 can make to exist the air between aviation plug connector shell inner wall and the tool module 42, prevents that the gas from exhausting between aviation plug connector shell and the tool module 42, and makes aviation plug connector shell adsorb and be difficult to take off on the tool module 42.
Example seven:
the seventh embodiment is different from the first embodiment in that the output end of the hydraulic rod 54 is provided with an anti-slip head 55.
Specifically, the anti-slip end 55 can prevent the hydraulic rod 54 from sliding relative to the surface of the casting when the casting is fixed, prevent the casting from sliding out from between the hydraulic rod 54 and the jig module 42, and avoid scratches on the surface of the casting when the casting is compressed.
What has been described herein is merely a preferred embodiment of the utility model, and the scope of the utility model is not limited thereto. Modifications and additions to, or substitutions in, the described embodiments by those skilled in the art are intended to be included within the scope of the utility model.
Claims (7)
1. The utility model provides a cutting machine is used in processing of aviation plug connector shell, includes the frame, its characterized in that includes:
the cutting tools are symmetrically arranged on two sides of the middle part of the rack, each cutting tool comprises a movable base, a cutting motor and a blade, the cutting motor is adjustably connected with the rack through the movable base, and the blades are arranged on the output end of the cutting motor;
the feeding runway is arranged in the middle of the rack and comprises a sliding table, a runway shell, a ball screw and a driving motor, the ball screw is arranged in the runway shell, the sliding table is arranged above the runway shell, the middle part below the sliding table is in transmission connection with the ball screw, the end part of the ball screw is connected with the driving motor, and one end of the feeding runway is arranged between the cutting tools;
the jig comprises a jig main board and jig modules, wherein the jig modules are uniformly distributed above the jig main board in a square array, the jig modules are semi-conical, the narrow ends of the jig modules are mutually far away, a transverse avoiding groove is formed in the end part of each jig module on the jig main board, and the jig is arranged on the sliding table;
the press device, press device sets up in the frame of cutting tool top, press device includes the mounting bracket, drives actuating cylinder, push pedal, hydraulic stem, it is vertical to drive actuating cylinder to set up in the mounting bracket, the output that drives actuating cylinder stretches out the mounting bracket downwards, the push pedal is connected on driving actuating cylinder output, the vertical setting of hydraulic stem is in the push pedal below.
2. The cutting machine for machining the aviation connector shell according to claim 1, wherein the movable base comprises a screw rod mechanism, a first sliding rail and a sliding table, the screw rod mechanism is arranged in parallel with the first sliding rail, the sliding table is arranged above the screw rod mechanism and the first sliding rail, and the upper portion of the sliding table is connected with the lower portion of the cutting motor.
3. The aircraft connector housing machining cutter of claim 1, wherein an adjusting indexing table is connected below the movable base.
4. The cutting machine for machining the aviation plug connector shell according to claim 1, wherein two sides of the ball screw are symmetrically provided with a second sliding rail, and two sides below the sliding table are slidably connected with the second sliding rail.
5. The cutting machine for machining the aviation connector housing according to claim 1, wherein the jig main board is provided with a positioning hole at a middle portion of an outer side edge of the jig module.
6. The cutting machine for machining the aviation connector shell according to claim 1, wherein ventilation grooves are formed in the surfaces of two ends of the jig module along the circumferential direction.
7. The cutting machine for machining the aviation plug connector shell according to claim 1, wherein an anti-slip end socket is arranged on the output end of the hydraulic rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122702840.0U CN216441766U (en) | 2021-11-01 | 2021-11-01 | Cutting machine is used in processing of aviation plug connector shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122702840.0U CN216441766U (en) | 2021-11-01 | 2021-11-01 | Cutting machine is used in processing of aviation plug connector shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216441766U true CN216441766U (en) | 2022-05-06 |
Family
ID=81351099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122702840.0U Active CN216441766U (en) | 2021-11-01 | 2021-11-01 | Cutting machine is used in processing of aviation plug connector shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216441766U (en) |
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2021
- 2021-11-01 CN CN202122702840.0U patent/CN216441766U/en active Active
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