CN202129628U - Numerical control hydraulic punching and drilling compound machine for angle steels - Google Patents
Numerical control hydraulic punching and drilling compound machine for angle steels Download PDFInfo
- Publication number
- CN202129628U CN202129628U CN201120193650U CN201120193650U CN202129628U CN 202129628 U CN202129628 U CN 202129628U CN 201120193650 U CN201120193650 U CN 201120193650U CN 201120193650 U CN201120193650 U CN 201120193650U CN 202129628 U CN202129628 U CN 202129628U
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- numerical control
- control hydraulic
- fuselage
- punching
- angle steel
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Abstract
The utility model discloses a numerical control hydraulic punching and drilling compound machine for angle steels. The numerical control hydraulic punching and drilling compound machine relates to angle steel punching and drilling equipment and comprises a machine body (1) with a machine body table-board (11) and a punching device (7) which is arranged on the machine body (1). The numerical control hydraulic punching and drilling compound machine is characterized in that a drilling device is also arranged on the machine body (1), wherein the drilling device is arranged in a slide rail of a vertical sliding frame (18) through a connecting plate (19) which is connected with the drilling device; the sliding frame (18) is arranged on a linear guide rail (16) in a sliding way; the linear guide rail (16) is transversely arranged on the side surface of the machine body (1); and a material pressing device (11) and a clamping device (3) are arranged on the machine body table-board (11). The punching device and the drilling device are integrated on one piece of equipment by the special structural design, so that the punching machining and the drilling machining which are originally finished on two pieces of equipment can be finished on one piece of equipment. The numerical control hydraulic punching and drilling compound machine has high machining efficiency and high machining precision and can greatly reduce the equipment investment.
Description
Technical field
The utility model relates to a kind of angle steel process equipment, and particularly a kind of angle steel eyelet work, rig belong to the Machining Technology field.
Background technology
At present electric power is processed with the punching and the two kinds of processing technologys of holing with the angle steel hole on the needed a large amount of angle steel of angle steel tower; Need on punching apparatus and rig, to process respectively; It is low that this kind processing mode exists working (machining) efficiency; Problems such as machining accuracy is low, and equipment investment is big, and workman's amount of labour is big.
The utility model content
To the above-mentioned defective that exists in the prior art, the utility model provides a kind of novel numerical control hydraulic angle steel drill compounding machine that integrates punching, holes.
The utility model is realized through following technical scheme: a kind of numerical control hydraulic angle steel drill compounding machine; Comprise the fuselage that has the fuselage table top and be arranged on the hole punched device on the said fuselage; Its special character is; Also be provided with drilling equipment on the said fuselage, said drilling equipment is slidingly arranged in through connected connecting plate in the slide rail of vertically disposed travelling carriage, and said travelling carriage is slidingly arranged on the line slideway of horizontally set of fuselage side; Also be provided with material pressing device and clamping device on the said fuselage table top.
The utility model is to be provided with in the side of fuselage to reach the drilling equipment that moves forward and backward up and down, makes this equipment possess the function of punching and boring, original like this need on an equipment, can the realization in boring of accomplishing on two equipment and punching processing.Hole punched device and drilling equipment in the utility model are prior art.Material pressing device in the utility model and clamping device are respectively applied for workpiece pressing and clamping work pieces.
The utility model also is provided with typing apparatus on said fuselage, the typewriting cushion block of said typing apparatus is connected with the punching press guide runner of said hole punched device.Like this, typewriting can be by same hydraulic oil cylinder driving with punching.Described typing apparatus is a prior art.
Material pressing device in the utility model can adopt any press material structure form of the prior art; But consider the simple and reliability of structural design; But said material pressing device comprises the strut and tie that compresses pawl, is connected with the actuating unit of translation that has the clamping arm that is dihedral; Saidly compress the front end that pawl is arranged on strut and tie rotationally, the rear end of strut and tie is connected with said actuating unit; Front bottom end at strut and tie is provided with ejector pin and spring.When material pressing device is specifically worked; Actuating unit drives strut and tie and moves forward; One of them clamping arm that compresses pawl contacts with workpiece and under the effect of spring knock pin, promotes workpiece locatees to the precalculated position, and actuating unit drives strut and tie to be continued to move forward, and promotes to compress the pawl upset; Another clamping arm that compresses pawl is pressed on the workpiece, thereby with Work-sheet pressing.
Reliable in order to guarantee to add the man-hour binder, said material pressing device is two covers that are oppositely arranged, and correspondence is arranged on the below of said hole punched device.
In order to guarantee the binder reliable in action and be convenient to the workpiece location that said strut and tie is located in the depression bar seat that is fixed on the fuselage table top.
But the actuating unit of the described translation of the utility model can be cylinder or hydraulic cylinder.
Clamping device in the utility model can adopt any clamping structure of prior art; But consider the simple and reliability of structural design; Clamping device according to the invention is two covers that are oppositely arranged; Every cover comprises the clamping seats that is fixedly connected with the fuselage table top, the clamp shaft that is connected with oil cylinder, and the other end of said clamp shaft is located in the said clamping seats.Thereby move through the hydraulic oil cylinder driving clamp shaft workpiece is clamped.
For ability reliable grip workpiece, the clamping working face of the front end of said clamp shaft is the inclined-plane.
The beneficial effect of the utility model is: the utility model combines in hole punched device and drilling equipment on the equipment through special structural design; Make and to be processed on the equipment and can to accomplish in punching of accomplishing on two equipment and boring originally; Realize that clamping can accomplish two processing tasks of punching and boring; Working (machining) efficiency is high, and machining accuracy is high, greatly reduces working strength of workers; Simultaneously, because punching and boring are combined in an equipment, can reduce equipment investment greatly; The utility model has been owing to adopted special material pressing device, the location that can realize workpiece synchronously with compress, it is simple in structure, and is safe and reliable, and cost is low; In addition, the utility model has adopted special clamping device, and clamping work pieces is convenient to workpiece processing reliably.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment;
Fig. 2 is that A-A among Fig. 1 is to sketch map;
Fig. 3 is that B-B among Fig. 1 is to sketch map;
Fig. 4 is that D among Fig. 1 is to partial schematic diagram;
Fig. 5 is the structural representation of the drilling equipment among Fig. 1;
Fig. 6 is the left view of Fig. 5;
Fig. 7 is that C-C among Fig. 6 is to enlarged diagram;
Fig. 8 is the drift mobile device sketch map of the hole punched device among Fig. 1;
Fig. 9 is that E-E among Fig. 8 is to view;
Figure 10 is the sketch map of the typing apparatus among Fig. 1;
Figure 11 is the left view of Figure 10;
Figure 12 is the cross-sectional schematic of the hole punched device among Fig. 1;
Figure 13 is that sketch map is looked on the left side of Figure 12;
Figure 14 is the sketch map of the material pressing device among Fig. 1;
Figure 15 is the sketch map of the clamping device among Fig. 1;
Among the figure, 1, fuselage, 2, the support roller assembly, 3, clamping device, 4, plunger rod, 5, drilling equipment; 6, punching press oil cylinder, 7, hole punched device, 8, the punching press guide runner, 9, the punching mould bases, 10, typing apparatus, 11, the fuselage table top; 12, material pressing device, 14, the drift mobile device, 15, boring unit head mobile device, 16, line slideway, 17, ball screw assembly, I, 18, travelling carriage; 19, connecting plate, 20, servomotor I, 21, the mould bases pull bar, 22, servomotor II, 23, ball screw assembly, II, 24, the mould bases guide rail; 25, mould, 26, the typewriting pressure head, 27, the typewriting mould bases, 28, the typewriting jumper bar, 29, the pressure head cushion block, 30, the typewriting cylinder; 31, typewriting cushion block, 32, the mould guide rail, 33, adjusting device, 34, the conversion cylinder, 35, punching cushion block supporting plate, 36, pressure head; 38, punching cushion block, 39, the binder cylinder, 40, the depression bar seat, 41, strut and tie, 42, binder pawl axle, 43, compress pawl; 44, ejector pin, 45, spring, 46, clamping cylinder, 47, clamping seats, 48, clamp shaft, 49, base plate.
The specific embodiment
Through non-limiting embodiment the utility model is further described below:
Shown in accompanying drawing, be a kind of numerical control hydraulic angle steel drill compounding machine, it comprises fuselage 1, hole punched device 7, drilling equipment 5, typing apparatus 10, clamping device 3, material pressing device 12, support roller assembly 2.Wherein, fuselage 1 has fuselage table top 11, and fuselage table top 11 is provided with base plate 49.Said hole punched device 7 is arranged on the fuselage 1; Said hole punched device 7 is a prior art; It comprises the punching press oil cylinder 6 that is fixed on the fuselage 1, the punching press guide runner 8 that is connected with the cylinder bar of punching press oil cylinder 6, the pressure head 36 that is connected with punching press guide runner 8, conversion cylinder 34, has the punch-head assembly of plunger rod 4, is arranged on the punching mould bases 9 that can move horizontally on the base plate 49, and punching mould bases 9 is driven through connected mould bases pull bar 21 by the drift mobile device that is arranged on base plate 49 belows 14 and moves.Described drift mobile device 14 comprises servomotor II 22, the ball screw assembly, II 23 that is connected with servomotor II 22, drives ball screw assembly, II 23 drive punching mould bases 9 through servomotor II 22 and moves.Conversion cylinder 34 is connected with punching cushion block 38.During punching,, promote pressure head 36 to be contacted, to carry out the punching operation with plunger rod 4 in the cushion block groove in the corresponding punching cushion block 38 entering pressure heads 36 by 34 actions of program control system control conversion cylinder.Typing apparatus 10 is arranged on the below of punching press guide runner 8; It comprises typewriting mould bases 27, typewriting jumper bar 28, typewriting pressure head 26, the pressure head cushion block 29 that is connected typewriting pressure head 26 bottoms, typewriting cushion block 31, mould 25; Wherein, Typewriting cushion block 31 is arranged on the bottom of punching press guide runner 8 and is connected with it, and typewriting mould bases 27 is slidingly arranged on the guide rail on the base plate 49, and typewriting mould bases 27 moves by being arranged on connected typewriting cylinder 30 drives in typewriting mould bases 27 rear portions; The front portion of typewriting mould bases 27 is provided with adjusting device 33, and mould 25 is arranged on the mould guide rail 32.Typing apparatus 10 and hole punched device 7 shared punching press oil cylinders 6 are through control conversion cylinder 34 and the conversion of typewriting cylinder 30 realization typewritings with punching.Drilling equipment 5 is arranged on the side of fuselage 1; It is a prior art; It is slidingly arranged in the slide rail of vertically disposed travelling carriage 18 through connected connecting plate 19; Travelling carriage 18 is slidingly arranged on the line slideway 16 of horizontally set of fuselage 1 side, and drilling equipment 5 drives it through the boring unit head mobile device 15 that is connected with travelling carriage 18 and laterally moves.Described boring unit head mobile device 15 comprises servomotor I 20 and ball screw assembly, I17, drives ball screw assembly, I17 drive drilling equipment 5 through servomotor I 20 and laterally moves.Two covers of material pressing device 12 for being oppositely arranged; Correspondence is arranged on the base plate 49 of below of said hole punched device; Every cover material pressing device 12 comprises and compresses pawl 43, depression bar seat 40, strut and tie 41, binder cylinder 39, wherein, compresses pawl 43 and has two clamping arms that are dihedral; Compress pawl 43 is arranged on strut and tie 41 rotationally through binder pawl axle 42 front end; Strut and tie 41 is located in the hole of depression bar seat 40, and the rear end of strut and tie 41 is connected with binder cylinder 39, is provided with ejector pin 44 and spring 45 in the front bottom end of strut and tie 41.Two depression bar seats 40 are separately fixed at the front side and the rear side of punching mould bases 9, and the front end of two depression bar seats 40 in the present embodiment is respectively as the positioning reference of workpiece.During binder; 39 actions of binder cylinder drive strut and tie 41 and compress pawl 43 advances; After a clamping arm that compresses pawl 43 is near workpiece; Under the effect of ejector pin 44 and spring 45, shift workpiece onto positioning reference and position, binder cylinder 39 continuation promotion strut and ties 41 will compress pawl 43 upsets is pressed on the workpiece its another clamping arm.During the hole of processing work opposite side, after the workpiece upset, the material pressing device that starts opposite side is with Work-sheet pressing.Carry out binder when action, the front end of depression bar seat 40 that does not carry out binder action side is as the positioning reference of workpiece processing.Clamping device 3 is arranged on the fuselage table top 11; It is two covers that are oppositely arranged; Every cover comprises clamping seats 47, clamp shaft 48, the clamping cylinder 46 that is fixedly connected with fuselage table top 11, and an end of clamp shaft 48 is connected with clamping cylinder 46, and its other end is located in the axis hole of clamping seats 47.In order to guarantee the reliable grip workpiece, the clamping working face of the front end of the clamp shaft 48 in the present embodiment is designed to the inclined-plane.Clamp when action, wherein clamping cylinder 46 actions of the side clamp shaft 48 that drives these sides advances, and the clamping seats of opposite side is as locating surface, thereby workpiece is clamped.Support roller assembly 2 is separately positioned on the charging aperture and the discharging opening of fuselage table top 11, is used for supporting workpiece.
The utility model can be realized the automatic operation of angle steel hole processing through using with multinomial technological synthesis such as pneumatic, hydraulic pressure, electrical equipment.
Other parts of present embodiment all adopt prior art, repeat no more at this.
The concrete course of work of the utility model is: the angle steel of being sent here by pay-off; Behind the interior precalculated position of entering angle steel drift drilling composite machine clamping device and material pressing device; By program control system control clamping device and material pressing device angle clip is tight compact; Drive drift mobile device (or boring unit head mobile device) by servo-drive system then and drift (or drill bit) is moved to the position that needs processing, beginning punching (or boring).After processing a hole, once more by servo-drive system movable punching head (or drill bit), processing is with other holes of row.After one round processed, when needing to change the position, the control system sent signal, unclamps clamping device and material pressing device, and simultaneously, pay-off is sent predetermined length to according to program, repeats above-mentioned action then, until all holes are all processed.
The typing apparatus working time generally is set at last, and its position also is by program setting, and typewriting and punching be by same hydraulic oil cylinder driving, realizes the conversion of typewriting and punching through programme-control conversion cylinder and typewriting cylinder.
The above embodiments only are used for the explanation to the utility model, are not limitation ot it, and those skilled in the art also can make change on this basis.
Claims (8)
1. numerical control hydraulic angle steel drill compounding machine; Comprise the fuselage (1) that has fuselage table top (11) and be arranged on the hole punched device (7) on the said fuselage (1); It is characterized in that: said fuselage also is provided with drilling equipment on (1); Said drilling equipment is slidingly arranged in the slide rail of vertically disposed travelling carriage (18) through connected connecting plate (19), and said travelling carriage (18) is slidingly arranged on the line slideway (16) of horizontally set of fuselage (1) side; Also be provided with material pressing device (12) and clamping device (3) on the said fuselage table top (11).
2. numerical control hydraulic angle steel drill compounding machine according to claim 1 is characterized in that: also be provided with typing apparatus (10) on the said fuselage (1), the typewriting cushion block (31) of said typing apparatus (10) is connected with the punching press guide runner (37) of said hole punched device (7).
3. numerical control hydraulic angle steel drill compounding machine according to claim 1 and 2; It is characterized in that: said material pressing device (12) comprise have the clamping arm that is dihedral compress pawl (43) but, the strut and tie (41) that is connected with the actuating unit of translation; Saidly compress the front end that pawl (43) is arranged on strut and tie (41) rotationally, the rear end of strut and tie (41) is connected with said actuating unit; Front bottom end at strut and tie (41) is provided with ejector pin (44) and spring (45).
4. numerical control hydraulic angle steel drill compounding machine according to claim 3 is characterized in that: two covers of said material pressing device (12) for being oppositely arranged, correspondence is arranged on the below of said hole punched device (7).
5. numerical control hydraulic angle steel drill compounding machine according to claim 4 is characterized in that: said strut and tie (41) is located in the depression bar seat (40) that is fixed on the fuselage table top (11).
6. numerical control hydraulic angle steel drill compounding machine according to claim 3 is characterized in that: but the actuating unit of described translation is cylinder or hydraulic cylinder.
7. numerical control hydraulic angle steel drill compounding machine according to claim 1 and 2; It is characterized in that: two covers of said clamping device (3) for being oppositely arranged; Every cover comprises the clamping seats (47) that is fixedly connected with fuselage table top (11), the clamp shaft (48) that is connected with oil cylinder, and the other end of said clamp shaft (48) is located in the said clamping seats (47).
8. numerical control hydraulic angle steel drill compounding machine according to claim 6, it is characterized in that: the clamping working face of the front end of said clamp shaft (48) is the inclined-plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201120193650U CN202129628U (en) | 2011-06-10 | 2011-06-10 | Numerical control hydraulic punching and drilling compound machine for angle steels |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201120193650U CN202129628U (en) | 2011-06-10 | 2011-06-10 | Numerical control hydraulic punching and drilling compound machine for angle steels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202129628U true CN202129628U (en) | 2012-02-01 |
Family
ID=45518415
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201120193650U Expired - Lifetime CN202129628U (en) | 2011-06-10 | 2011-06-10 | Numerical control hydraulic punching and drilling compound machine for angle steels |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202129628U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102259268A (en) * | 2011-06-10 | 2011-11-30 | 济南兴田阳光数控机械有限公司 | Numerical-control hydraulic angle iron sinker drill compound machine |
| CN115179052A (en) * | 2022-09-14 | 2022-10-14 | 北京成立科技有限公司 | Aerospace engine flame tube head machining device and method |
-
2011
- 2011-06-10 CN CN201120193650U patent/CN202129628U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102259268A (en) * | 2011-06-10 | 2011-11-30 | 济南兴田阳光数控机械有限公司 | Numerical-control hydraulic angle iron sinker drill compound machine |
| CN115179052A (en) * | 2022-09-14 | 2022-10-14 | 北京成立科技有限公司 | Aerospace engine flame tube head machining device and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20120201 Effective date of abandoning: 20140212 |
|
| RGAV | Abandon patent right to avoid regrant |