CN215509059U - Numerical control drilling machine for machining aviation electrical socket structure - Google Patents

Numerical control drilling machine for machining aviation electrical socket structure Download PDF

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Publication number
CN215509059U
CN215509059U CN202120823663.9U CN202120823663U CN215509059U CN 215509059 U CN215509059 U CN 215509059U CN 202120823663 U CN202120823663 U CN 202120823663U CN 215509059 U CN215509059 U CN 215509059U
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CN
China
Prior art keywords
workbench
drilling machine
wall
dust suction
stand column
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Expired - Fee Related
Application number
CN202120823663.9U
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Chinese (zh)
Inventor
徐丽娅
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Suzhou Xiangyijie Precision Machinery Co ltd
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Suzhou Xiangyijie Precision Machinery Co ltd
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Filing date
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Priority to CN202120823663.9U priority Critical patent/CN215509059U/en
Application granted granted Critical
Publication of CN215509059U publication Critical patent/CN215509059U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a numerical control drilling machine for processing an aviation electrical socket structure in the technical field of aviation electrical, which comprises a workbench, wherein the top of the workbench is provided with a clamping component, the left side of the workbench is provided with a driving component, the right side of the top of the workbench is fixedly provided with a stand column, the right side of the stand column is provided with an exhaust fan, the middle part of the stand column is provided with a dust suction pipe through a bracket, the end part of the dust suction pipe is provided with a dust suction hood, the top of the stand column is fixedly provided with a fixed seat, the left side of the fixed seat is respectively and fixedly connected with an electric push rod and a guide rod, the outer wall of the guide rod is movably sleeved with a movable block, the bottom of the movable block is fixedly provided with a hydraulic cylinder, the output end of the hydraulic cylinder is provided with a drilling mechanism, the numerical control drilling machine is simple in operation, can realize clamping of workpieces with different sizes, and simultaneously can avoid the appearance of the workpieces from being damaged, the adaptability is better, can handle the piece that produces simultaneously when the work piece is processed.

Description

Numerical control drilling machine for machining aviation electrical socket structure
Technical Field
The utility model relates to the technical field of aviation and electrical, in particular to a numerical control drilling machine for machining an aviation electrical socket structure.
Background
Aviation, a complex and strategic human activity. The aircraft is flying (sailing) in the earth atmosphere (air space), and related fields such as scientific research and education, industrial manufacturing, public transportation, professional operation, aviation movement, national defense and military, government management and the like. By the use of air space and aircraft (aeronautical vehicles), aviation activities can be subdivided into a number of independent industries and fields, typically aeronautical manufacturing, civil aviation, and the like. People can often see that the word is used from respective fields, and the content of the word is extremely rich and varied. An avionic socket, also known as an avionic plug and socket, is widely used in various electrical circuits to function as a connection or disconnection circuit. In order to guarantee the quality of aviation electric socket, generally need numerically-controlled drilling machine to process the structure of socket, traditional numerically-controlled drilling machine is comparatively troublesome to operate when carrying out the centre gripping to the work piece, and cause the damage to the outward appearance of work piece easily, adaptability is relatively poor, traditional numerically-controlled drilling machine can produce a large amount of pieces when adding man-hour to the work piece simultaneously, the efficiency of work piece processing can be reduced if these pieces are not handled in time, for this reason, we propose the numerically-controlled drilling machine of aviation electric socket structure processing.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a numerical control drilling machine for machining an aviation electrical socket structure, and aims to solve the problems that the traditional numerical control drilling machine provided in the background art is troublesome to operate when clamping a workpiece and generates a large amount of scraps when drilling the workpiece.
In order to achieve the purpose, the utility model provides the following technical scheme: the numerically controlled drilling machine for machining the aviation electrical socket structure comprises a workbench, wherein supporting legs are fixedly arranged on the periphery of the bottom of the workbench, a clamping assembly is arranged at the top of the workbench, a driving assembly matched with the clamping assembly is arranged on the left side of the workbench, a stand column is fixedly arranged on the right side of the top of the workbench, an exhaust fan fixedly arranged at the top of the workbench is arranged on the right side of the stand column, a dust suction pipe is arranged in the middle of the stand column through a support, a dust suction cover is arranged at the end of the dust suction pipe and corresponds to the clamping assembly in position, the dust suction pipe is connected with the exhaust fan through a connecting pipe, a fixed seat is fixedly arranged at the top of the stand column, an electric push rod and a guide rod are fixedly connected to the left side of the fixed seat from top to bottom respectively, a movable block is movably sleeved on the outer wall of the guide rod, and the output end of the electric push rod is fixedly connected with the movable block, the bottom fixed mounting of movable block has the pneumatic cylinder, the output installation of pneumatic cylinder is provided with drilling mechanism.
Preferably, the clamping component comprises two groups of fixed blocks fixedly arranged at the top of the workbench, a movable rod is movably inserted into the fixed blocks on the left side, a clamping block is fixedly connected to the right end of the movable rod, and an elastic anti-slip layer is arranged on the right side of the fixed block and the opposite side of the clamping block in a laminating mode.
Preferably, the driving assembly comprises a driving motor, the driving motor is fixedly arranged on the left side of the workbench, a groove is formed in the top of the workbench and located between the two groups of fixed blocks, the left side and the right side of the groove are rotatably connected with a lead screw through a bearing, a supporting block is sleeved on the outer wall of the lead screw, the top of the supporting block is fixedly connected with the bottom of the clamping block, and the left end of the lead screw penetrates through the outer wall of the left side of the workbench and is connected with the output end of the driving motor.
Preferably, a nut is fixedly arranged on the inner wall of the supporting block, the nut is sleeved on the outer wall of the lead screw in a threaded manner, and a thread groove matched with the thread of the outer wall of the lead screw is formed in the inner wall of the nut.
Preferably, a limiting plate is fixedly arranged at the left end of the guide rod.
Preferably, the number of the supporting legs is four, and the bottom of each supporting leg is fixedly connected with a damping base.
Compared with the prior art, the utility model has the beneficial effects that:
1. the clamping device is provided with the clamping component and the driving component, a workpiece to be processed is placed between the clamping block and the right side fixing block, the driving motor is started to drive the screw rod to rotate, the supporting block and the clamping plate are driven to move left and right through the matching of the screw rod and the nut, the elastic anti-slip layers arranged on the opposite sides of the clamping block and the right side fixing block flexibly clamp the workpiece, the operation is simple, the clamping of workpieces with different sizes can be realized, meanwhile, the appearance of the workpiece can be prevented from being damaged, and the adaptability is good.
2. The utility model is provided with the dust absorption pipe and the exhaust fan, the exhaust fan is started, and under the action of the connecting pipe, a large amount of scraps generated during workpiece processing are absorbed and discharged in time through the matching use of the dust absorption pipe and the dust absorption cover, so that the workpiece processing efficiency is ensured.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural diagram of a driving assembly;
FIG. 3 is a schematic view of the connection structure of the lead screw and the support block.
In the figure: 1. a work table; 2. supporting legs; 3. a damping mount; 4. a clamping assembly; 41. a fixed block; 42. a movable rod; 43. a clamping block; 5. a drive assembly; 51. a drive motor; 52. a groove; 53. a lead screw; 54. a support block; 55. a nut; 6. a column; 7. a dust collection pipe; 8. an exhaust fan; 9. a fixed seat; 10. a guide bar; 11. a movable block; 12. a limiting plate; 13. an electric push rod; 14. a hydraulic cylinder; 15. a drilling mechanism.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1:
referring to fig. 1-3, the present invention provides a technical solution: a numerical control drilling machine for machining an aviation electrical socket structure comprises a workbench 1, wherein supporting legs 2 are fixedly arranged on the periphery of the bottom of the workbench 1, the workbench 1 is supported, the number of the supporting legs 2 is four, the bottom of each supporting leg 2 is fixedly connected with a damping base 3, vibration generated during workpiece machining can be reduced through the damping bases 3, a clamping assembly 4 is arranged at the top of the workbench 1, a workpiece is clamped through the clamping assembly 4, subsequent machining is facilitated, the clamping assembly 4 comprises two groups of fixed blocks 41 fixedly arranged at the top of the workbench 1, a movable rod 42 is movably inserted into the fixed block 41 on the left side, a clamping block 43 is fixedly connected to the right end of the movable rod 42, elastic anti-slip layers are arranged on the opposite sides of the fixed block 41 on the right side and the clamping block 43 in a laminating mode, the phenomenon that a workpiece slides when clamped is avoided, and meanwhile a good protection effect can be provided for the workpiece, the left side of the workbench 1 is provided with a driving component 5 matched with the clamping component 4, the clamping component 4 is provided with power through the driving component 5, the driving component 5 comprises a driving motor 51, the driving motor 51 is fixedly arranged on the left side of the workbench 1, the top of the workbench 1 is provided with a groove 52, the groove 52 is positioned between the two groups of fixed blocks 41, the left side and the right side of the groove 52 are rotatably connected with a lead screw 53 through a bearing, the outer wall of the lead screw 53 is sleeved with a supporting block 54, the top of the supporting block 54 is fixedly connected with the bottom of the clamping block 43, the left end of the lead screw 53 penetrates through the outer wall of the left side of the workbench 1 and is connected with the output end of the driving motor 51, the inner wall of the supporting block 54 is fixedly provided with a nut 55, the nut 55 is sleeved on the outer wall of the lead screw 53 in a threaded manner, the inner wall of the nut 55 is provided with a thread groove matched with the thread of the outer wall of the lead screw 53, a workpiece to be processed is placed between the clamping block 43 and the right fixed block 41, drive lead screw 53 through start-up driving motor 51 and rotate, drive supporting shoe and splint through the cooperation of lead screw 53 and nut 55 and remove for the elasticity skid resistant course that clamp splice 43 and right side fixed block 41 opposite side set up carries out flexible centre gripping to the work piece, and easy operation can realize carrying out the centre gripping to not unidimensional work piece, can avoid the outward appearance of work piece to receive the damage simultaneously, and adaptability is better.
Please refer to fig. 1, a vertical column 6 is fixedly mounted on the right side of the top of the workbench 1, an exhaust fan 8 fixedly mounted on the top of the workbench 1 is arranged on the right side of the vertical column 6, a dust suction pipe 7 is mounted in the middle of the vertical column 6 through a support, a dust suction cover is mounted at the end of the dust suction pipe 7 and used for increasing the dust suction area, the position of the dust suction cover corresponds to the position of the clamping assembly 4, the dust suction pipe 7 is connected with the exhaust fan 8 through a connecting pipe, the exhaust fan 8 is started, under the action of the connecting pipe, a large amount of chips generated during workpiece machining are timely absorbed and discharged through the matching of the dust suction pipe 7 and the dust suction cover, and further the workpiece machining efficiency is ensured.
Example 2:
referring to fig. 1, different from embodiment 1, a fixed seat 9 is fixedly disposed at the top of an upright 6, an electric push rod 13 and a guide rod 10 are respectively and fixedly connected to the left side of the fixed seat 9 from top to bottom, a movable block 11 is movably sleeved on the outer wall of the guide rod 10, the guide rod 10 guides the movement of the movable block 11 and supports the movable block 11, a limit plate 12 is fixedly disposed at the left end of the guide rod 10 to prevent the movable block 11 from falling off from the guide rod 10, the output end of the electric push rod 13 is fixedly connected with the movable block 11, a hydraulic cylinder 14 is fixedly disposed at the bottom of the movable block 11, a drilling mechanism 15 is disposed at the output end of the hydraulic cylinder 14, after clamping of a workpiece is completed, the electric push rod 13 is started to enable the movable block 11 to slide left and right along the guide rod 10, and after the drilling mechanism 15 moves to a proper position, and closing the electric push rod 13, driving the drilling mechanism 15 to move downwards by starting the hydraulic cylinder 14, and processing the workpiece by starting the drilling mechanism 15.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. Numerical control drilling machine of aviation electrical socket structure processing, including workstation (1), its characterized in that: supporting legs (2) are fixedly arranged on the periphery of the bottom of a workbench (1), a clamping assembly (4) is arranged at the top of the workbench (1), a driving assembly (5) matched with the clamping assembly (4) is arranged on the left side of the workbench (1), a stand column (6) is fixedly arranged on the right side of the top of the workbench (1), an exhaust fan (8) fixedly arranged at the top of the workbench (1) is arranged on the right side of the stand column (6), a dust suction pipe (7) is arranged in the middle of the stand column (6) through a support, a dust suction cover is arranged at the end part of the dust suction pipe (7) and corresponds to the clamping assembly (4), the dust suction pipe (7) is connected with the exhaust fan (8) through a connecting pipe, a fixed seat (9) is fixedly arranged at the top of the stand column (6), an electric push rod (13) and a guide rod (10) are fixedly connected to the left side of the fixed seat (9) from top to bottom respectively, the outer wall activity of guide bar (10) has cup jointed movable block (11), and electric putter's (13) output and movable block (11) fixed connection, the bottom fixed mounting of movable block (11) has pneumatic cylinder (14), and the output installation of pneumatic cylinder (14) is provided with drilling mechanism (15).
2. The numerically controlled drilling machine for structural machining of an avionics socket according to claim 1, characterized in that: the clamping assembly (4) comprises two groups of fixed blocks (41) fixedly arranged at the top of the workbench (1), a movable rod (42) is movably inserted into the left fixed block (41), a clamping block (43) is fixedly connected to the right end of the movable rod (42), and an elastic anti-slip layer is attached to the opposite sides of the right fixed block (41) and the clamping block (43).
3. The numerically controlled drilling machine for structural machining of an avionics socket according to claim 2, characterized in that: drive assembly (5) include driving motor (51), driving motor (51) are fixed to be set up in the left side of workstation (1), recess (52) are seted up at the top of workstation (1), and recess (52) are located between two sets of fixed blocks (41), the left and right sides of recess (52) is rotated through the bearing and is connected with lead screw (53), the outer wall cup joint of lead screw (53) is provided with supporting shoe (54), the top of supporting shoe (54) and the bottom fixed connection of clamp splice (43), the left end of lead screw (53) runs through the left side outer wall of workstation (1) and is connected with driving motor (51) output.
4. The numerically controlled drilling machine for structural machining of an avionics socket according to claim 3, characterized in that: the inner wall of supporting shoe (54) is fixed and is provided with nut (55), and nut (55) screw thread cup joints the outer wall at lead screw (53), and the inner wall of nut (55) is seted up with lead screw (53) outer wall screw thread assorted thread groove.
5. The numerically controlled drilling machine for structural machining of an avionics socket according to claim 1, characterized in that: a limiting plate (12) is fixedly arranged at the left end of the guide rod (10).
6. The numerically controlled drilling machine for structural machining of an avionics socket according to claim 1, characterized in that: the number of the supporting legs (2) is four, and the bottom of each supporting leg (2) is fixedly connected with a damping base (3).
CN202120823663.9U 2021-04-21 2021-04-21 Numerical control drilling machine for machining aviation electrical socket structure Expired - Fee Related CN215509059U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120823663.9U CN215509059U (en) 2021-04-21 2021-04-21 Numerical control drilling machine for machining aviation electrical socket structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120823663.9U CN215509059U (en) 2021-04-21 2021-04-21 Numerical control drilling machine for machining aviation electrical socket structure

Publications (1)

Publication Number Publication Date
CN215509059U true CN215509059U (en) 2022-01-14

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ID=79802466

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120823663.9U Expired - Fee Related CN215509059U (en) 2021-04-21 2021-04-21 Numerical control drilling machine for machining aviation electrical socket structure

Country Status (1)

Country Link
CN (1) CN215509059U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115415834A (en) * 2022-09-16 2022-12-02 郑远芝 Numerically-controlled machine tool with vibration damping device for part machining

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115415834A (en) * 2022-09-16 2022-12-02 郑远芝 Numerically-controlled machine tool with vibration damping device for part machining
CN115415834B (en) * 2022-09-16 2023-07-28 深圳市台钲精密机械有限公司 Numerical control machine tool with vibration damping device for part machining

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Granted publication date: 20220114