CN201997784U - Processing clamp for steam turbine guide blade with eccentric cambered surfaces as end surfaces of blade shroud and blade base - Google Patents
Processing clamp for steam turbine guide blade with eccentric cambered surfaces as end surfaces of blade shroud and blade base Download PDFInfo
- Publication number
- CN201997784U CN201997784U CN2010206422555U CN201020642255U CN201997784U CN 201997784 U CN201997784 U CN 201997784U CN 2010206422555 U CN2010206422555 U CN 2010206422555U CN 201020642255 U CN201020642255 U CN 201020642255U CN 201997784 U CN201997784 U CN 201997784U
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- blade
- blade root
- integral shroud
- connecting plate
- shroud
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Abstract
The utility model relates to a processing clamp for a steam turbine guide blade with eccentric cambered surfaces as the end surfaces of a blade shroud and a blade base. The processing clamp comprises a blade shroud thimble sleeve and a blade base clamp used in coordination with the blade shroud thimble sleeve; the guide blade is fixed through the blade shroud thimble sleeve and the blade base clamp, wherein the gyration centers of the blade shroud thimble sleeve and the blade base are coincident with the gyration centre of the guide blade and respectively coincident with the gyration centre of a thimble of a milling machine and the gyration centre of the clamp body of a driving disc, so that the gyration centre of the guide blade is enabled to be highly coincident with that of the milling machine, and the processing accuracy is improved; and by adopting the clamp, holes are not required to be drilled at the two ends of the guide blade, so that procedures are decreased, and the production efficiency is improved. Moreover, a set screw can prevent the guide blade from moving slightly during the gyration process, so that the processing accuracy is ensured.
Description
Technical field
The utility model relates to a kind of frock clamp, the steam turbine guide vane clamp for machining that particularly a kind of integral shroud blade root end face is eccentric cambered surface.
Background technology
Usually in that being carried out high accuracy, turbine blade adds man-hour, need on milling machine, to determine earlier the centre of gyration of blade, the general three thimble fixed blades of butt two thimble bizets one thimble that adopt are processed it, adopt this thimble to process centre hole at the integral shroud and the blade root end face of not moulding, again the centre hole milling is excised after the process finishing, this employing method clamps blade, the centre of gyration registration of blade and lathe is poor, machining accuracy can not get guaranteeing, increase operating procedure simultaneously, reduced production efficiency.Be the steam turbine guide vane of eccentric cambered surface producing integral shroud blade root end face particularly, because integral shroud blade root end face is eccentric cambered surface, the clamping location is trouble more, and it is particularly evident adopting this method.
The utility model content
The steam turbine guide vane clamp for machining that it is eccentric cambered surface that the technical problems to be solved in the utility model provides a kind of integral shroud blade root end face, simple in structure, convenient mounting and clamping.
For solving the problems of the technologies described above, the technical solution of the utility model is: the steam turbine guide vane clamp for machining that a kind of integral shroud blade root end face is eccentric cambered surface, comprise integral shroud tailstock barrel and blade root anchor clamps matching used with it, it is characterized in that: described integral shroud tailstock barrel is made of integral shroud framework connecting plate inwall welding integral shroud location-plate, the inner face of described integral shroud location-plate and integral shroud framework connecting plate constitute can be chimeric with integral shroud the outer arc die cavity, have the centre hole that overlaps with the guide vane centre of gyration at integral shroud location-plate center; Described blade root anchor clamps embed the blade root location-plate by blade root framework connecting plate inwall and constitute, the inner face of described blade root location-plate and blade root framework connecting plate constitute can be chimeric with blade root the inner arc die cavity, have the setting circle pin-and-hole that overlaps with the guide vane centre of gyration at blade root framework connecting plate center, blade root framework connecting plate four limit symmetries have four screw hole are installed.
Further, all be drilled with screwed hole on described integral shroud framework connecting plate and the blade root framework connecting plate, the screwed hole screw-internal thread fit has holding screw.
Advantage of the present utility model is: during installation, adopt the integral shroud tailstock barrel and the blade root anchor clamps that overlap with the guide vane centre of gyration to fix guide vane, and the centre of gyration of integral shroud tailstock barrel and blade root anchor clamps self overlaps with thimble, the driving disc spacing pressing clamp body centre of gyration of milling machine respectively, guaranteed the high contact ratio of the blade and the milling machine centre of gyration, improved the precision of processing, and adopt this anchor clamps to need not again the blade two ends and bore centre hole, reduced operation, improved production efficiency.Holding screw can prevent that micro-position from appearring in guide vane in turning course, guarantees the precision of processing.
Description of drawings
Fig. 1 is that the steam turbine guide vane of eccentric cambered surface adds for the utility model integral shroud blade root end face
Integral shroud tailstock barrel structural representation in the clamping apparatus;
Fig. 2 is a cutaway view of the present utility model shown in Figure 1;
Fig. 3 is that the steam turbine guide vane of eccentric cambered surface adds for the utility model integral shroud blade root end face
Blade root clamp structure schematic diagram in the clamping apparatus;
Fig. 4 is a cutaway view of the present utility model shown in Figure 3;
Fig. 5 is the steam turbine guide vane clamp for machining use schematic diagram of eccentric cambered surface for the utility model integral shroud blade root end face.
The specific embodiment
Shown in Fig. 1 to 4, the steam turbine guide vane clamp for machining that it is eccentric cambered surface that the utility model relates to a kind of integral shroud blade root end face, it comprises integral shroud tailstock barrel 1 and blade root anchor clamps 2 matching used with it.
Above-mentioned integral shroud tailstock barrel 1 is made of integral shroud framework connecting plate 11 inwalls welding integral shroud location-plate 12, the inwall of integral shroud framework connecting plate 11 can be identical with steam turbine guide vane integral shroud outer mold surface, the inner face of integral shroud location-plate 12 is the outer arcuate that cooperates with the eccentric intrados of integral shroud, inner face and integral shroud framework connecting plate 11 inwalls by integral shroud location-plate 12 constitute and the chimeric outer arc die cavity of guide vane integral shroud, have the centre hole 13 that overlaps with the guide vane centre of gyration at integral shroud location-plate 12 centers.
Blade root anchor clamps 2 embed blade root location-plate 22 by blade root framework connecting plate 21 inwalls and constitute, the inwall of blade root framework connecting plate 21 can be identical with steam turbine guide vane blade root outer mold surface, the inner face of blade root location-plate 22 is the arc that cooperates with the eccentric extrados of blade root, inner face and blade root framework connecting plate 21 inwalls by blade root location-plate 22 constitute and the chimeric inner arc die cavity of guide vane integral shroud, have the setting circle pin-and-hole 23 that overlaps with the blade centre of gyration at blade root location-plate 22 centers, blade root framework connecting plate 21 4 limit symmetries have four screw hole 24 are installed.
During installation, as shown in Figure 5, the centre hole 13 of integral shroud tailstock barrel 1 and 4 coaxial connections of the thimble of milling machine, the pin hole 23 of blade root anchor clamps 2 is by driving disc spacing pressing clamp body 6 coaxial are connected of round pin 5 with milling machine, and be connected and fixed by four limits and the driving disc spacing pressing clamp body 6 of bolt with blade root anchor clamps 2, obtain the milling machine centre of gyration and overlap, realize that promptly the milling machine centre of gyration overlaps with the height of the steam turbine guide vane centre of gyration with integral shroud tailstock barrel 1, blade root anchor clamps 2 centres of gyration.
For preventing that micro-position from appearring in guide vane in turning course, guarantee the precision of processing.All be drilled with screwed hole on integral shroud framework connecting plate 11 and the blade root framework connecting plate 21, be combined with holding screw 3 in the screwed hole.
Claims (2)
1. steam turbine guide vane clamp for machining that integral shroud blade root end face is eccentric cambered surface, comprise integral shroud tailstock barrel and blade root anchor clamps matching used with it, it is characterized in that: described integral shroud tailstock barrel is made of integral shroud framework connecting plate inwall welding integral shroud location-plate, the inner face of described integral shroud location-plate and integral shroud framework connecting plate constitute can be chimeric with integral shroud the outer arc die cavity, have the centre hole that overlaps with the guide vane centre of gyration at integral shroud location-plate center; Described blade root anchor clamps embed the blade root location-plate by blade root framework connecting plate inwall and constitute, the inner face of described blade root location-plate and blade root framework connecting plate constitute can be chimeric with blade root the inner arc die cavity, have the setting circle pin-and-hole that overlaps with the guide vane centre of gyration at blade root framework connecting plate center, blade root framework connecting plate four limit symmetries have four screw hole are installed.
2. the steam turbine guide vane clamp for machining that integral shroud blade root end face according to claim 1 is eccentric cambered surface is characterized in that: all be drilled with screwed hole on described integral shroud framework connecting plate and the blade root framework connecting plate, be combined with holding screw in the screwed hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010206422555U CN201997784U (en) | 2010-12-06 | 2010-12-06 | Processing clamp for steam turbine guide blade with eccentric cambered surfaces as end surfaces of blade shroud and blade base |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010206422555U CN201997784U (en) | 2010-12-06 | 2010-12-06 | Processing clamp for steam turbine guide blade with eccentric cambered surfaces as end surfaces of blade shroud and blade base |
Publications (1)
Publication Number | Publication Date |
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CN201997784U true CN201997784U (en) | 2011-10-05 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2010206422555U Expired - Fee Related CN201997784U (en) | 2010-12-06 | 2010-12-06 | Processing clamp for steam turbine guide blade with eccentric cambered surfaces as end surfaces of blade shroud and blade base |
Country Status (1)
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CN (1) | CN201997784U (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103586709A (en) * | 2013-11-01 | 2014-02-19 | 哈尔滨汽轮机厂有限责任公司 | Auxiliary clamping method and auxiliary clamp for five-axis NC machine tool steam passage workpieces |
CN105352385A (en) * | 2015-08-05 | 2016-02-24 | 南通中能机械制造有限公司 | Multifunctional integration measuring tool of blade on the basis of two ejector pins |
CN112097260A (en) * | 2020-07-08 | 2020-12-18 | 成都航利航空科技有限责任公司 | Novel high-precision air swirler and manufacturing method thereof |
CN114888610A (en) * | 2022-05-31 | 2022-08-12 | 哈尔滨汽轮机厂有限责任公司 | Tooth-shaped positioning block for positioning blade and clamping and aligning method for machining blade steam passage |
-
2010
- 2010-12-06 CN CN2010206422555U patent/CN201997784U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103586709A (en) * | 2013-11-01 | 2014-02-19 | 哈尔滨汽轮机厂有限责任公司 | Auxiliary clamping method and auxiliary clamp for five-axis NC machine tool steam passage workpieces |
CN105352385A (en) * | 2015-08-05 | 2016-02-24 | 南通中能机械制造有限公司 | Multifunctional integration measuring tool of blade on the basis of two ejector pins |
CN105352385B (en) * | 2015-08-05 | 2018-01-16 | 南通中能机械制造有限公司 | A kind of blade multifunctional comprehensive measurer on the basis of two thimble |
CN112097260A (en) * | 2020-07-08 | 2020-12-18 | 成都航利航空科技有限责任公司 | Novel high-precision air swirler and manufacturing method thereof |
CN112097260B (en) * | 2020-07-08 | 2022-09-09 | 成都航利航空科技有限责任公司 | High-precision air swirler and manufacturing method thereof |
CN114888610A (en) * | 2022-05-31 | 2022-08-12 | 哈尔滨汽轮机厂有限责任公司 | Tooth-shaped positioning block for positioning blade and clamping and aligning method for machining blade steam passage |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111005 Termination date: 20131206 |