CN101961835A - Numerical control turning-milling compound machine - Google Patents

Numerical control turning-milling compound machine Download PDF

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Publication number
CN101961835A
CN101961835A CN 201010255910 CN201010255910A CN101961835A CN 101961835 A CN101961835 A CN 101961835A CN 201010255910 CN201010255910 CN 201010255910 CN 201010255910 A CN201010255910 A CN 201010255910A CN 101961835 A CN101961835 A CN 101961835A
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China
Prior art keywords
axis
fuselage
screw
block
tailstock
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Granted
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CN 201010255910
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Chinese (zh)
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CN101961835B (en
Inventor
周沃强
萧耀荣
罗锦伟
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Guangdong new NC Equipment Co. Ltd.
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FOSHAN SHENGTESI UNMERICAL CONTROL Co Ltd
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Priority to CN2010102559106A priority Critical patent/CN101961835B/en
Publication of CN101961835A publication Critical patent/CN101961835A/en
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Publication of CN101961835B publication Critical patent/CN101961835B/en
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Abstract

The invention relates to a numerical control turning-milling compound machine. A machine tool is provided with a lifting Y shaft power knife rest device, a main shaft transmission device with main shaft clamp and an ejector pin hydraulic tail holder device respectively. The compound machine has a rational and compact structure, high rigidity and high machining accuracy, and the structure of each shaft device is improved, so that normal standard members can be machined, and the compound machine can be applied to machining of special shapes, such as turning, milling, drilling, tapping and the like, of various complex axial end faces and radial end faces.

Description

A kind of numerically-controlled milking composite machine
Technical field
The present invention relates to numerically controlled lathe and CNC milling machine field, but the dual-purpose multifunctional numerical control complex milling machine of especially a kind of turnning and milling.
Background technology
Existing numerically-controlled milking composite machine, its diverse in function, but complex structure, machining accuracy is difficult to guarantee that each shaft device of fuselage still has the following disadvantages: (1) conventional knives rack device structure is single, can not install multiple difform cutter simultaneously, and the upper and lower lifting of Y-axis is adopted manually or common electric machine is regulated, degree of regulation is low, can not satisfy the processing request of specific workpiece, has also restricted cutter to a certain extent to the special shape processing request; (2) traditional main shaft device structure is single, can not carry out positioned at arbitrary angles to workpiece, and after the stall of main shaft, depends merely on spindle motor and brake, and rigidity descends when making main shaft stressed, influences machining accuracy; (3) traditional tailstock device is made up of thimble and hydraulic cylinder haply, both operated by rotary motion are in becoming same axis inner and outer sleeves, the inner sleeve that hydraulic cylinder will be equipped with thimble during use ejects, the tailstock device of this movable pins structure, complex structure works long hours, damage easily, the shake cutter appears easily, poor rigidity, and it is low to bear pressure.
Summary of the invention
The objective of the invention is to overcome above-mentioned the deficiencies in the prior art part, and provide a kind of rational in infrastructure, tight, good rigidly, machining accuracy height, each shaft device has been carried out the improvement of structure and perfect, not only can process the common standard part, more can be applicable to the processing of the given shapes such as turning, milling, boring and tapping of the axial end of various complexity and radial end face.
The object of the present invention is achieved like this:
A kind of numerically-controlled milking composite machine is characterized in that, is respectively arranged with liftable Y-axis power knife rest device, band main shaft pincers spindle gearing and thimble hydraulic pressure tailstock device on the lathe;
Liftable Y-axis power knife rest device, comprise that fuselage is provided with support, the support both sides are provided with the knife rest frame guide rail, the fuselage bottom of corresponding knife rest frame guide rail is equipped with slide block, fuselage is seated on the support two side tool post frame guide rails by slide block, a side is installed with the screw axis of vertical setting on the described fuselage, being arranged with on the screw axis can be along on the screw axis, the nut seat of lower slider, nut seat is provided with connecting plate, be separately installed with unit head and carriage saddle on the connecting plate, described fuselage opposite side is equipped with the counterweight casing, the fuselage top is fixed with pulley bracket by two supporting plates, before the pulley bracket, the rear end is equiped with pulley, the connecting plate top is provided with hook, the counterweight casing successively overlaps two pulleys by chain and is connected with hook, also is fixed with the Y-axis lifting motor on the fuselage between described screw axis and the counterweight casing, and the output shaft of Y-axis lifting motor drives by belt and screw axis top and connects;
Band main shaft pincers spindle gearing, comprise the spindle drum that is fixed on the lathe, axle sleeve is installed on the spindle drum, spindle set is in axle sleeve and preceding, the rear end is extended the axle sleeve outside respectively, described rear-end of spindle is provided with by the main axle servo motor on belt and the lathe and drives the belt pulley that connects, belt pulley one side is provided with circular brake block, be mounted with braking clamp on the spindle drum of corresponding brake block, described braking clamp is by framework, the back taper pushing block, two fixture blocks and cylinder are formed, the brake block both sides of two fixture blocks upper end are provided with the chuck that can clamp brake block, two fixture blocks are relative shape and place interior its two chuck of framework to extend the framework outside, formation one is suitable for the back taper cavity wide at the top and narrow at the bottom of ccontaining back taper pushing block between two fixture blocks of two chuck lower ends, and back taper pushing block lower end is connected with cylinder piston rod;
Thimble hydraulic pressure tailstock device, comprise tailstock guide is installed on the lathe, tailstock guide be provided with can forward and backward slip thimble hydraulic pressure tailstock device, thimble hydraulic pressure tailstock device comprises fixedly corner bracket of tailstock, oil cylinder and cylinder putter, tailstock is made up of pedestal and the thimble cylindrical shell that is arranged on pedestal one side, pedestal is provided with oil cylinder and is seated on the tailstock guide, cylinder putter fixedly corner bracket is connected in pedestal bottom between two tailstock guides, cylinder putter on the pedestal terminal with cylinder putter fixedly corner bracket be connected, cylinder putter fixedly corner bracket is fixedly installed on the lathe.
Described connecting plate both sides are slide rail vertically are installed, and are fixed with slide on the fuselage of corresponding slide rail.
Described screw axis near the top is provided with screw mandrel shaft block, be connected with the bearing gland that is connected with screw axis on the screw mandrel shaft block, be set with high-precision screw mandrel bearing on the screw axis in the screw mandrel shaft block of bearing gland below, bearing gland is passed on the screw axis top, and to extend fuselage outer and the screw axis belt pulley is housed, the Y-axis lifting motor is connected with fuselage by installing plate, and its output shaft connects by the screw axis belt wheel driving on belt and screw axis top.
Described support one side is equipped with Y-axis feeding motor, drive on the Y-axis feeding motor output shaft and be connected to Y-axis feed screw one end, on the Y-axis feed screw slip blade is installed, slip blade is connected with fuselage bottom, be fixed with bearing block on the support of the Y-axis feed screw other end, bearing is installed on the bearing block and compresses by bearing gland, the Y-axis feed screw other end is connected with bearing gland.
Be separately installed with at least two unit heads and carriage saddle on the described connecting plate.
Described framework is installed with spindle drum by contiguous block and is connected.
One side of described brake block also is extended with the installation portion that angling cylinder can be installed.
Described main axle servo motor rear end is equipped with encoder.
Described pedestal is the setting of casing shape, is provided with the reinforcement gusset that improves the pedestal rigidity in the pedestal, and oil cylinder crouches and is located in the casing of strengthening the gusset below and fixing, its cylinder putter end extend the casing outside and cylinder putter fixedly corner bracket be connected.
Described thimble cylindrical shell is provided with thimble.
The invention has the beneficial effects as follows:
(1), numerically-controlled milking composite machine of the present invention, in Y-axis power knife rest device, the connecting plate of drive head and carriage saddle is installed on vertical screw axis of fuselage, by the Y-axis lifting motor screw mandrel is driven, thereby make unit head and carriage saddle carry out upper and lower descending operation according to reality processing needs, vertically screw axis also cooperates the counterweight casing to carry out counterweight stabilization under the inactive state, makes whole Y-axis power knife rest device have characteristics stable, that noise is little, machining accuracy is high;
(2), numerically-controlled milking composite machine of the present invention, in Y-axis power knife rest device, connecting plate along the upper and lower slip of slide, makes the unit head of Y-axis and the upper and lower lifting of carriage saddle more steady, more linear by slide rail;
(3), numerically-controlled milking composite machine of the present invention, in Y-axis power knife rest device, a plurality of unit heads and carriage saddle are installed on the connecting plate, the difform cutter of processing can be installed simultaneously, save tool change time.
(4), numerically-controlled milking composite machine of the present invention, spindle gearing is regulated the function that realizes infinitely variable speeds rotation or positioned at arbitrary angles by band encoder main axle servo motor-driven main shaft, the milling and any hole drill of workpiece of realization slender piece lateral surface helical oil groove are cut, rear-end of spindle also cooperates the braking clamp function, braking clamp utilizes cylinder that the brake block of two fixture blocks to rear-end of spindle vised firmly, play the brake positioning action, prevent to rotate, also effectively improve main shaft rigidity when stressed, effectively improve the workpiece machining accuracy;
(5), numerically-controlled milking composite machine of the present invention, thimble hydraulic pressure tailstock device separates setting by the thimble cylindrical shell with oil cylinder, make the thimble cylindrical shell can use the bearing revolution of big gauge size, it is bigger to make thimble bear pressure, effectively improves the rigidity of whole tailstock device, the machining accuracy height, along the forward and backward slip of guide rail, structure is more stable, reasonable, practical by hydraulic oil cylinder driving for tailstock, and the thimble hydraulic pressure tailstock device of this separate type, the thimble tube structure is simple, and thimble is changed convenient;
(6), numerically-controlled milking composite machine of the present invention, not only can process the common standard part, more can be applicable to the processing of the given shapes such as turning, milling, boring and tapping of the axial end of various complexity and radial end face.
Description of drawings
Fig. 1 is a structural representation of the present invention;
Fig. 2 is the structural representation of liftable Y-axis power knife rest device among the present invention;
Fig. 3 is the structural representation of another state of liftable Y-axis power knife rest device among the present invention;
Fig. 4 is the structural representation of another state of liftable Y-axis power knife rest device among the present invention;
Fig. 5 is the structural representation of another state of the present invention;
Fig. 6 is the structural representation of another state of the present invention;
Fig. 7 is the structural representation of braking clamp in the band main shaft pincers spindle gearing of the present invention;
Fig. 8 is the structural representation of another state of the present invention;
Fig. 9 is the structural representation of thimble hydraulic pressure tailstock device of the present invention;
Figure 10 is the structural representation of another angle of thimble hydraulic pressure tailstock device of the present invention.
The specific embodiment
The present invention is further described below in conjunction with drawings and Examples.
Shown in Fig. 1 to 10, a kind of numerically-controlled milking composite machine is characterized in that, is respectively arranged with liftable Y-axis power knife rest device 1, band main shaft pincers spindle gearing 2 and thimble hydraulic pressure tailstock device 3 on the lathe 4;
Liftable Y-axis power knife rest device 1, comprise that fuselage 101 is provided with support 102, support 102 both sides are provided with knife rest frame guide rail 103, slide block 104 is equipped with in fuselage 101 bottoms of corresponding knife rest frame guide rail 103, fuselage 101 is seated on 102 liang of side tool post frame guide rails 103 of support by slide block 104, a side is installed with the screw axis 105 of vertical setting on the described fuselage 101, being arranged with on the screw axis 105 can be along on the screw axis 105, the nut seat 106 of lower slider, 106 are provided with connecting plate 107 on the nut seat, be separately installed with unit head 108 and carriage saddle 109 on the connecting plate 107, described fuselage 101 opposite sides are equipped with counterweight casing 110, fuselage 101 tops are fixed with pulley bracket 112 by two supporting plates 111, before the pulley bracket 112, the rear end is equiped with pulley 113, connecting plate 111 tops are provided with hook 114, counterweight casing 110 successively overlaps two pulleys 113 by chain 115 and is connected with hook 114, also be fixed with Y-axis lifting motor 116 on the fuselage 101 between described screw axis 105 and the counterweight casing 110, the output shaft 117 of Y-axis lifting motor 116 drives with screw axis 105 tops by belt (not indicating among the figure) and connects;
Band main shaft pincers spindle gearing 2, comprise the spindle drum 201 that is fixed on the lathe 4, axle sleeve 202 is installed on the spindle drum 201, it is interior and preceding that main shaft 203 is sleeved on axle sleeve 202, rear end 204,205 extend axle sleeve 202 outsides respectively, described main shaft 203 rear ends 205 are provided with by the main axle servo motor 207 on belt 206 and the lathe and drive the belt pulley 208 that connects, belt pulley 208 1 sides are provided with circular brake block 209, be mounted with braking clamp 210 on the spindle drum 201 of corresponding brake block 209, described braking clamp is by framework 211, back taper pushing block 212, two fixture blocks 213,214 and cylinder 215 form, two fixture blocks 213, brake block 209 both sides of 214 upper ends are provided with the chuck 213a that can clamp brake block 209,214a, two fixture blocks 213,214 are relative shape places its two chuck 213a in the framework 211,214a extends framework 211 outsides, two chuck 213a, two fixture blocks 213 of 214a lower end, formation one is suitable for the back taper cavity 216 wide at the top and narrow at the bottom of ccontaining back taper pushing block 212 between 214, and back taper pushing block 216 lower ends are connected with cylinder 217 piston rods 218;
Thimble hydraulic pressure tailstock device 3, comprise tailstock guide 301 is installed on the lathe 4, tailstock guide 301 be provided with can before, the thimble hydraulic pressure tailstock device 302 that slides in the back, thimble hydraulic pressure tailstock device 302 comprises tailstock 303, oil cylinder 304 and cylinder putter be corner bracket 305 fixedly, tailstock 303 is made up of pedestal 306 and the thimble cylindrical shell 307 that is arranged on pedestal 306 1 sides, pedestal 306 is provided with oil cylinder 304 and is seated on the tailstock guide 301, cylinder putter fixedly corner bracket 305 is connected in pedestal 306 bottoms between two tailstock guides 301, cylinder putter 308 on the pedestal 306 terminal with cylinder putter fixedly corner bracket 305 be connected, cylinder putter fixedly corner bracket 305 is fixedly installed on the lathe 4.
Described connecting plate 107 both sides are slide rail 118 vertically are installed, and are fixed with slide 119 on the fuselage 101 of corresponding slide rail 118.
Described screw axis 105 near the top is provided with screw mandrel shaft block 120, be connected with the bearing gland 121 that is connected with screw axis 105 on the screw mandrel shaft block 120, be set with high-precision screw mandrel bearing on the screw axis 105 in the screw mandrel shaft block 120 of bearing gland 121 belows, bearing gland 121 is passed on screw axis 105 tops, and to extend fuselage 101 outer and screw axis belt pulley 122 is housed, Y-axis lifting motor 116 is connected with fuselage 101 by installing plate 123, and the screw axis belt pulley 122 of its output shaft 117 by belt (among the figure sign) and screw axis 105 tops drives and connect.
Described support 102 1 sides are equipped with Y-axis feeding motor 124, drive on Y-axis feeding motor 124 output shafts and be connected to Y-axis feed screw 125 1 ends, slip blade 126 is installed on the Y-axis feed screw 125, slip blade 126 is connected with fuselage 101 bottoms, be fixed with bearing block 127 on the support 102 of Y-axis feed screw 125 other ends, bearing is installed on the bearing block 127 and compresses by bearing gland 128, Y-axis feed screw 125 other ends are connected with bearing gland 128.
Be separately installed with at least two unit heads 108 and carriage saddle 109 on the described connecting plate 107.
Described framework 211 is installed with spindle drum 201 by contiguous block 219 and is connected.
One side of described brake block 209 also is extended with the installation portion 220 that angling cylinder (not indicating among the figure) can be installed.
Described main axle servo motor 207 rear ends are equipped with encoder 221.
Described pedestal 306 is the setting of casing shape, be provided with the reinforcement gusset 309 that improves pedestal 306 rigidity in the pedestal 306, oil cylinder 304 crouches and is located in the casing of strengthening gusset 309 belows and fixing, its cylinder putter 308 ends extend the casing outside and cylinder putter fixedly corner bracket 305 be connected.
Described thimble cylindrical shell 307 is provided with thimble 310.

Claims (10)

1. a numerically-controlled milking composite machine is characterized in that, is respectively arranged with liftable Y-axis power knife rest device (1), band main shaft pincers spindle gearing (2) and thimble hydraulic pressure tailstock device (3) on the lathe (4);
Liftable Y-axis power knife rest device (1), comprise that fuselage (101) is provided with support (102), support (102) both sides are provided with knife rest frame guide rail (103), slide block (104) is equipped with in fuselage (101) bottom of corresponding knife rest frame guide rail (103), fuselage (101) is seated on support (102) the two side tool post frame guide rails (103) by slide block (104), the last side of described fuselage (101) is installed with the screw axis (105) of vertical setting, being arranged with on the screw axis (105) can be along on the screw axis (105), the nut seat of lower slider (106), (106) are provided with connecting plate (107) on the nut seat, be separately installed with unit head (108) and carriage saddle (109) on the connecting plate (107), described fuselage (101) opposite side is equipped with counterweight casing (110), fuselage (101) top is fixed with pulley bracket (112) by two supporting plates (111), pulley bracket (112) is preceding, the rear end is equiped with pulley (113), connecting plate (111) top is provided with hook (114), counterweight casing (110) successively overlaps two pulleys (113) by chain (115) and is connected with hook (114), also be fixed with Y-axis lifting motor (116) on the fuselage (101) between described screw axis (105) and the counterweight casing (110), the output shaft (117) of Y-axis lifting motor (116) drives by belt and screw axis (105) top and connects;
Band main shaft pincers spindle gearing (2), comprise the spindle drum (201) that is fixed on the lathe (4), axle sleeve (202) is installed on the spindle drum (201), it is interior and preceding that main shaft (203) is sleeved on axle sleeve (202), rear end (204,205) extend axle sleeve (202) outside respectively, described main shaft (203) rear end (205) is provided with by the main axle servo motor (207) on belt (206) and the lathe and drives the belt pulley (208) that connects, belt pulley (208) one sides are provided with circular brake block (209), be mounted with braking clamp (210) on the spindle drum (201) of corresponding brake block (209), described braking clamp is by framework (211), back taper pushing block (212), two fixture blocks (213,214) and cylinder (215) form, two fixture blocks (213,214) Shang Duan brake block (209) both sides are provided with the chuck (213a that can clamp brake block (209), 214a), two fixture blocks (213,214) be relative shape and place its two chuck (213a in the framework (211), 214a) extend framework (211) outside, two chuck (213a, 214a) two fixture blocks (213 of lower end, 214) formation one is suitable for the back taper cavity (216) wide at the top and narrow at the bottom of ccontaining back taper pushing block (212) between, and back taper pushing block (216) lower end is connected with cylinder (217) piston rod (218);
Thimble hydraulic pressure tailstock device (3), comprise tailstock guide (301) is installed on the lathe (4), tailstock guide (301) be provided with can before, the thimble hydraulic pressure tailstock device (302) that slides in the back, thimble hydraulic pressure tailstock device (302) comprises tailstock (303), oil cylinder (304) and cylinder putter be corner bracket (305) fixedly, tailstock (303) is made up of pedestal (306) and the thimble cylindrical shell (307) that is arranged on pedestal (306) one sides, pedestal (306) is provided with oil cylinder (304) and is seated on the tailstock guide (301), cylinder putter fixedly corner bracket (305) is connected in pedestal (306) bottom between two tailstock guides (301), cylinder putter (308) on the pedestal (306) terminal with cylinder putter fixedly corner bracket (305) be connected, cylinder putter fixedly corner bracket (305) is fixedly installed on the lathe (4).
2. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that described connecting plate (107) both sides are slide rail (118) vertically is installed, and are fixed with slide (119) on the fuselage (101) of corresponding slide rail (118).
3. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that, described screw axis (105) near the top is provided with screw mandrel shaft block (120), be connected with the bearing gland (121) that is connected with screw axis (105) on the screw mandrel shaft block (120), be set with high-precision screw mandrel bearing on the screw axis (105) in the screw mandrel shaft block (120) of bearing gland (121) below, bearing gland (121) is passed on screw axis (105) top, and to extend fuselage (101) outer and screw axis belt pulley (122) is housed, Y-axis lifting motor (116) is connected with fuselage (101) by installing plate (123), and the screw axis belt pulley (122) of its output shaft (117) by belt and screw axis (105) top drives and connect.
4. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that, described support (102) one sides are equipped with Y-axis feeding motor (124), drive on Y-axis feeding motor (124) output shaft and be connected to Y-axis feed screw (125) one ends, slip blade (126) is installed on the Y-axis feed screw (125), slip blade (126) is connected with fuselage (101) bottom, be fixed with bearing block (127) on the support (102) of Y-axis feed screw (125) other end, bearing is installed on the bearing block (127) also compresses by bearing gland (128), Y-axis feed screw (125) other end is connected with bearing gland (128).
5. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that, be separately installed with at least two unit heads (108) and carriage saddle (109) on the described connecting plate (107).
6. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that described framework (211) is installed with spindle drum (201) by contiguous block (219) and is connected.。
7. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that a side of described brake block (209) also is extended with the installation portion (220) that angling cylinder can be installed.
8. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that described main axle servo motor (207) rear end is equipped with encoder (221).
9. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that, described pedestal (306) is the setting of casing shape, be provided with the reinforcement gusset (309) that improves pedestal (306) rigidity in the pedestal (306), oil cylinder (304) crouches and to be located in the casing of strengthening gusset (309) below and fixing, its cylinder putter (308) end extend the casing outside and cylinder putter fixedly corner bracket (305) be connected.
10. according to the described numerically-controlled milking composite machine of claim 1, it is characterized in that described thimble cylindrical shell (307) is provided with thimble (310).
CN2010102559106A 2010-08-17 2010-08-17 Numerical control turning-milling compound machine Active CN101961835B (en)

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Application Number Priority Date Filing Date Title
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103692220A (en) * 2013-12-18 2014-04-02 江苏建一机床有限公司 Seven-axis turn-milling machining center
CN104858666A (en) * 2015-06-12 2015-08-26 舟山市智海技术开发有限公司 Machining assembly robot
CN106181525A (en) * 2016-07-28 2016-12-07 江门市弘程精密制造有限公司 A kind of separately machined unit head of lathe
CN107297634A (en) * 2017-05-25 2017-10-27 中山市捷上同程数控机床有限公司 A kind of hydraulic clip compact form walks scheming
CN108971992A (en) * 2018-08-03 2018-12-11 重庆工业职业技术学院 It is a kind of for processing the numerically controlled processing equipment of axle sleeve
CN112108692A (en) * 2020-09-08 2020-12-22 宁波中策动力机电集团有限公司 Horizontal numerical control crankshaft machining equipment
CN112475944A (en) * 2020-11-25 2021-03-12 山东普利森集团有限公司 Y-axis mechanism of turning and milling composite machine tool

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Publication number Priority date Publication date Assignee Title
JPS62105209A (en) * 1985-10-31 1987-05-15 Mitsui Seiki Kogyo Kk Moving balance device for heavy body by motor
CN2559449Y (en) * 2002-05-09 2003-07-09 唐兴联 Multifunction machine tool
CN2574823Y (en) * 2002-11-04 2003-09-24 常熟市中恒数控设备制造有限公司 Pedestal structure of airborne channelling machine
WO2008003891A1 (en) * 2006-07-03 2008-01-10 Aro Welding Technologies Sheet metal clamp used in combination with a manipulator arm, and having an electromechanical balancing module

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62105209A (en) * 1985-10-31 1987-05-15 Mitsui Seiki Kogyo Kk Moving balance device for heavy body by motor
CN2559449Y (en) * 2002-05-09 2003-07-09 唐兴联 Multifunction machine tool
CN2574823Y (en) * 2002-11-04 2003-09-24 常熟市中恒数控设备制造有限公司 Pedestal structure of airborne channelling machine
WO2008003891A1 (en) * 2006-07-03 2008-01-10 Aro Welding Technologies Sheet metal clamp used in combination with a manipulator arm, and having an electromechanical balancing module

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103692220A (en) * 2013-12-18 2014-04-02 江苏建一机床有限公司 Seven-axis turn-milling machining center
CN104858666A (en) * 2015-06-12 2015-08-26 舟山市智海技术开发有限公司 Machining assembly robot
CN106181525A (en) * 2016-07-28 2016-12-07 江门市弘程精密制造有限公司 A kind of separately machined unit head of lathe
CN107297634A (en) * 2017-05-25 2017-10-27 中山市捷上同程数控机床有限公司 A kind of hydraulic clip compact form walks scheming
CN108971992A (en) * 2018-08-03 2018-12-11 重庆工业职业技术学院 It is a kind of for processing the numerically controlled processing equipment of axle sleeve
CN108971992B (en) * 2018-08-03 2020-09-29 重庆工业职业技术学院 Numerical control machining equipment for machining shaft sleeve
CN112108692A (en) * 2020-09-08 2020-12-22 宁波中策动力机电集团有限公司 Horizontal numerical control crankshaft machining equipment
CN112475944A (en) * 2020-11-25 2021-03-12 山东普利森集团有限公司 Y-axis mechanism of turning and milling composite machine tool

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