CN103111857B - A kind of clamp structure of milling full length of turbine rotors - Google Patents

A kind of clamp structure of milling full length of turbine rotors Download PDF

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Publication number
CN103111857B
CN103111857B CN201210453100.0A CN201210453100A CN103111857B CN 103111857 B CN103111857 B CN 103111857B CN 201210453100 A CN201210453100 A CN 201210453100A CN 103111857 B CN103111857 B CN 103111857B
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CN
China
Prior art keywords
base plate
straight line
groove
described base
turbine rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201210453100.0A
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Chinese (zh)
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CN103111857A (en
Inventor
高锡民
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.)
Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Original Assignee
Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Mingzhu Turbocharger Manufacturing Co Ltd filed Critical Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Priority to CN201210453100.0A priority Critical patent/CN103111857B/en
Publication of CN103111857A publication Critical patent/CN103111857A/en
Application granted granted Critical
Publication of CN103111857B publication Critical patent/CN103111857B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention provides a kind of clamp structure of milling full length of turbine rotors, for the turbine rotor of different size, its flexibility is better, suitability is higher.It comprises base plate, base is installed on described base plate side by side, lower straight line V-type groove is had in the upper surface of described base, turbine rotor is embedded in described lower straight line V-type groove, the straight line that the linear vertical that described lower straight line V-type groove is formed is arranged in described base, the turbine end of described turbine rotor is mounted on locating piece, described locating piece is fastenedly connected described base plate, it is characterized in that: the centre position being positioned at described base plate, perpendicular to the rectilinear direction that described lower straight line V-type groove is formed, described base plate is provided with guide rail, groove is provided with in the lower surface of described base, described guide rail correspondence is installed in described groove, and be slidably matched with described groove.

Description

A kind of clamp structure of milling full length of turbine rotors
Technical field
The present invention relates to the technical field utilizing milling machine to process turbine rotor, be specially a kind of clamp structure of milling full length of turbine rotors.
Background technology
Milling machine is utilized to process the device of full length of turbine rotors in prior art, as shown in Figure 1, two base 3 straight lines are arranged on base plate 1, the upper surface of base 3 has lower straight line V-type groove, turbine rotor 2 is embedded in lower straight line V-type groove respectively, the turbine end of turbine rotor 2 is mounted on locating piece 5, and locating piece 5 is fastenedly connected base plate 1.This structure can time processing at least two full length of turbine rotors, and working (machining) efficiency is higher, but for the turbine rotor of different size, shortage is compared in its flexibility.
Summary of the invention
For the problems referred to above, the invention provides a kind of clamp structure of milling full length of turbine rotors, for the turbine rotor of different size, its flexibility is better, suitability is higher.
Its technical scheme is such, it comprises base plate, base is installed on described base plate side by side, lower straight line V-type groove is had in the upper surface of described base, turbine rotor is embedded in described lower straight line V-type groove, the straight line that the linear vertical that described lower straight line V-type groove is formed is arranged in described base, the turbine end of described turbine rotor is mounted on locating piece, described locating piece is fastenedly connected described base plate, it is characterized in that: the centre position being positioned at described base plate, perpendicular to the rectilinear direction that described lower straight line V-type groove is formed, described base plate is provided with guide rail, groove is provided with in the lower surface of described base, described guide rail correspondence is installed in described groove, and be slidably matched with described groove.
It is further characterized in that: on the body of described locating piece, be provided with L-type step surface, and the turbine end of described turbine rotor is mounted on described L-type step surface, and slidingly contacts with described L-type step surface.
In said structure of the present invention, be positioned at the centre position of base plate, perpendicular to the rectilinear direction that lower straight line V-type groove is formed, base plate is provided with guide rail, groove is provided with in the lower surface of base, guide rail correspondence is installed in groove, and be slidably matched with groove, this structure makes base can move along guide rail, drive the turbine rotor in the lower straight line V-type groove be embedded on base to move simultaneously, position with regard to the turbine rotor achieved for different size like this, therefore flexibility is better, suitability is stronger.And on the body of locating piece, being provided with L-type step surface, the turbine end of turbine rotor is mounted on L-type step surface, and slidingly contacts with L-type step surface, and this design makes simple to operate, ensures further the reliability of turbine rotor movement to play positioning action simultaneously.
Accompanying drawing explanation
Fig. 1 is the plan structure schematic diagram of prior art;
Fig. 2 is plan structure schematic diagram of the present invention;
Fig. 3 is main TV structure schematic diagram of the present invention;
Fig. 4 is A direction view enlarged diagram in Fig. 3 (main position relationship of expressing guide rail and base plate, base);
Fig. 5 is the main TV structure enlarged diagram of locating piece in the present invention;
Fig. 6 is the side view of Fig. 5.
Detailed description of the invention
See Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, the present invention includes base plate 1, turbine rotor 2, at least two base 3 straight lines are arranged on base plate 1, the upper surface of base 3 has lower straight line V-type groove 4, the straight line that the linear vertical that base 3 is arranged is formed in lower straight line V-type groove 4, turbine rotor 2 is embedded in lower straight line V-type groove 4, turbine rotor 2 exposes to the upper surface of base 3, pressing plate 6 is pressed on turbine rotor 2, the position that pressing plate 6 press against turbine rotor 2 has straight line V-type groove 7, pressing plate 6 is fastenedly connected base plate 1 by bolt 8, be positioned at the centre position of base plate 1, perpendicular to the rectilinear direction that lower straight line V-type groove 4 is formed, base plate 1 is provided with guide rail 9, groove 10 is provided with in the lower surface of base 3, guide rail 9 correspondence is installed in groove 10, and be slidably matched with groove 10, the body of locating piece 5 is provided with L-type step surface 5-1, locating piece 5 is fastenedly connected base plate 1, the turbine end of turbine rotor 2 is mounted on L-type step surface 5-1, and slidingly contact with L-type step surface 5-1, the part to be processed of turbine rotor 2 is towards milling cutter 11.

Claims (1)

1. the clamp structure of a milling full length of turbine rotors, it comprises base plate, base is installed on described base plate side by side, lower straight line V-type groove is had in the upper surface of described base, turbine rotor is embedded in described lower straight line V-type groove, the straight line that the linear vertical that described lower straight line V-type groove is formed is arranged in described base, the turbine end of described turbine rotor is mounted on locating piece, described locating piece is fastenedly connected described base plate, it is characterized in that: the centre position being positioned at described base plate, perpendicular to the rectilinear direction that described lower straight line V-type groove is formed, described base plate is provided with guide rail, groove is provided with in the lower surface of described base, described guide rail correspondence is installed in described groove, and be slidably matched with described groove, the body of described locating piece is provided with L-type step surface, and the turbine end of described turbine rotor is mounted on described L-type step surface, and slidingly contacts with described L-type step surface, pressing plate is bolted connection described base plate, and is pressed on described turbine rotor.
CN201210453100.0A 2012-11-13 2012-11-13 A kind of clamp structure of milling full length of turbine rotors Expired - Fee Related CN103111857B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210453100.0A CN103111857B (en) 2012-11-13 2012-11-13 A kind of clamp structure of milling full length of turbine rotors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210453100.0A CN103111857B (en) 2012-11-13 2012-11-13 A kind of clamp structure of milling full length of turbine rotors

Publications (2)

Publication Number Publication Date
CN103111857A CN103111857A (en) 2013-05-22
CN103111857B true CN103111857B (en) 2015-12-16

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CN201210453100.0A Expired - Fee Related CN103111857B (en) 2012-11-13 2012-11-13 A kind of clamp structure of milling full length of turbine rotors

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106077777A (en) * 2016-08-29 2016-11-09 上海特波电机有限公司 Rotor milling attachment
CN109434579A (en) * 2018-12-31 2019-03-08 横店集团英洛华电气有限公司 Without center hole rotor outer circle grinding auxiliary device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2923154Y (en) * 2006-06-21 2007-07-18 渤海船舶重工有限责任公司 Large horizontal machine tool fitted with numerical-control boring-milling head
CN201249361Y (en) * 2008-07-11 2009-06-03 桂林机床股份有限公司 Automatic hydraulic clamp device
CN102357807A (en) * 2011-09-28 2012-02-22 无锡明珠增压器制造有限公司 Fixture for milling full length of turbine rotors
CN102371495A (en) * 2011-09-08 2012-03-14 杭州杭机数控机床有限公司 Flexible and rapid clamp device
CN202894810U (en) * 2012-11-13 2013-04-24 无锡明珠增压器制造有限公司 Fixture structure for milling turbine rotors with total lengths

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2923154Y (en) * 2006-06-21 2007-07-18 渤海船舶重工有限责任公司 Large horizontal machine tool fitted with numerical-control boring-milling head
CN201249361Y (en) * 2008-07-11 2009-06-03 桂林机床股份有限公司 Automatic hydraulic clamp device
CN102371495A (en) * 2011-09-08 2012-03-14 杭州杭机数控机床有限公司 Flexible and rapid clamp device
CN102357807A (en) * 2011-09-28 2012-02-22 无锡明珠增压器制造有限公司 Fixture for milling full length of turbine rotors
CN202894810U (en) * 2012-11-13 2013-04-24 无锡明珠增压器制造有限公司 Fixture structure for milling turbine rotors with total lengths

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CN103111857A (en) 2013-05-22

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Granted publication date: 20151216

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