CN104400521B - A kind of angular precision positioning centering and clamping mechanism - Google Patents

A kind of angular precision positioning centering and clamping mechanism Download PDF

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Publication number
CN104400521B
CN104400521B CN201410632137.9A CN201410632137A CN104400521B CN 104400521 B CN104400521 B CN 104400521B CN 201410632137 A CN201410632137 A CN 201410632137A CN 104400521 B CN104400521 B CN 104400521B
Authority
CN
China
Prior art keywords
chuck
blade
tapered sleeve
cone
taper shank
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
CN201410632137.9A
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Chinese (zh)
Other versions
CN104400521A (en
Inventor
彭会文
张娟
赵西松
金秀杰
申玉萍
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.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201410632137.9A priority Critical patent/CN104400521B/en
Publication of CN104400521A publication Critical patent/CN104400521A/en
Application granted granted Critical
Publication of CN104400521B publication Critical patent/CN104400521B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/12Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for securing to a spindle in general

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Jigs For Machine Tools (AREA)

Abstract

A kind of angular precision positioning centering and clamping mechanism, belongs to technical field of aircraft engine part manufacture.The voussoir of the present invention is positioned at taper shank groove and is driven by fishbolt, and cone contacts cooperation with voussoir, and tapered sleeve is inner to be connected with cone dorsal part, and coat suit is in tapered sleeve outer end, and overcoat is connected with taper shank by pedestal;Chuck is connected with deck, and tapered sleeve coordinates with chuck, and chuck entirety uses and uses elastic caoutchouc to connect between multi-clove type structure, and two lobes;Chuck inner surface is provided with flexibly positioned piece, and flexibly positioned piece flat with blade side coordinates, and chuck inner surface diameter is ± 0.2mm with the dimensional fits scope of the big axle journal of blade.The flexibly positioned piece of compression flat realization in blade side of the present invention angularly positions, hold blade axle journal tightly by chuck and realize Non-clearance Alignment location, angular location flat to blade side will not be held blade axle journal tightly with chuck and be interfered, and achieve axle journal and side the most flat while position, location centering precision is high, it is possible to meet the requirement on machining accuracy of blade.

Description

A kind of angular precision positioning centering and clamping mechanism
Technical field
The invention belongs to technical field of aircraft engine part manufacture, particularly relate to a kind of angular precision positioning centering clamping machine Structure.
Background technology
Blade is as the core building block of aero-engine, and its requirement on machining accuracy is high, but is affected by the limit of blade self structure System, its locating and machining difficulty is big, as a example by a kind of angle adjustable blade, when processing this kind of blade, it is desirable to the angle of blade profile Degree is flat with the side of big journal end higher relative accuracy, determines angle so that side is flat, center with axle journal during processing blade.
Using traditional blade centering location clamping mode at present, by the center of circle set position assurance axle journal, side is flat is positioned at circle set The inside, above circle set, a square opening is opened in flat position, and puts into angular locating piece, then realizes angular by compressing locating piece Location.
But traditional blade centering location clamping mode also exists some problem following:
1. using circle set location, the machining tolerance overlapped by blade and circle is affected, and exists between certain location when both reassemble Gap, when angular locating piece compresses, can cause the deflection of locating shaft.
2. when angular locating piece slides in circle set square opening, can there is certain glade plane space, owing to locating surface is less, this is right Angular positioning effects is relatively big, and angular positioning precision also can be impacted by the mismachining tolerance of angular locating piece.
3. after blade axle journal is held tightly, just cannot carry out angularly have adjusted of blade again, and after the most angularly reserving, enter Can make again when row axle journal is held tightly to reserve angular changes again, therefore it is difficult to ensure that the angular positioning requirements of blade.
Therefore, use said method can only meet the blade that required precision is the highest, and for the high blade of required precision, this biography The location mode of system cannot meet the required precision of blade.
Summary of the invention
The problem existed for prior art, the present invention provides a kind of angular precision positioning centering and clamping mechanism, at angle adjustable leaf In the process of sheet, it is possible to ensure the blade profile center position consistency to journal centre, it is ensured that the angle of blade profile and side Flat have higher relative accuracy, without gap, location when axle journal is held tightly, it is achieved axle journal is flat with side to be positioned simultaneously, and positioning precision is high.
To achieve these goals, the present invention adopts the following technical scheme that a kind of angular precision positioning centering and clamping mechanism, including Taper shank, voussoir, cone, pedestal, deck, tapered sleeve, overcoat and chuck, radially have a groove on described taper shank, Taper shank is centrally along axially having a circular hole, and described voussoir is positioned at the groove of taper shank, and voussoir quantity is two, and two voussoirs are relative Arrange, and two voussoirs are linked together by fishbolt;Described cone is positioned at the circular hole of taper shank, and the taper seat of cone is same Time contact with two voussoirs;
Described tapered sleeve the inner is fixedly connected with cone dorsal part, and cone is slidably matched with the circular hole of taper shank, and described coat suit is outside tapered sleeve Holding, and tapered sleeve is slidably matched with overcoat, overcoat is fixed on pedestal, and pedestal is fixedly connected with taper shank;
Described deck is positioned at inside overcoat and is fixed on pedestal, and chuck is connected with deck by draw-in groove, and chuck matches with tapered sleeve Close.
Described tapered sleeve outer inner uses inner conical surface structure, and chuck outer surface uses male cone (strobilus masculinus) structure, and chuck entirety uses many lobes Elastic caoutchouc is used to connect between formula structure, and two lobes;Described chuck inner surface is the face of cylinder, and axle journal big with blade matches.
Described chuck inner surface diameter is ± 0.2mm with the dimensional fits scope of the big axle journal of blade.
Being provided with flexibly positioned piece at described chuck inner surface, flexibly positioned piece flat with blade side matches.
The clamping face of described flexibly positioned piece is not more than 0.005mm with the depth of parallelism of the positioning reference plane of chuck.
Between described tapered sleeve and cone, back-moving spring is installed.
Beneficial effects of the present invention:
The present invention compared with prior art, can be compressed the flat realization in blade side by flexibly positioned piece and angularly position, be held tightly by chuck Blade axle journal realizes Non-clearance Alignment location, and the flexibly positioned piece of angular location flat to blade side, will not hold tightly with chuck completely Blade axle journal interferes, be successfully realized axle journal and side flat while position, and location centering precision is high, in blade processing mistake Cheng Zhong, it is possible to ensure the blade profile center position consistency to journal centre, thus meet the requirement on machining accuracy of blade.
Accompanying drawing explanation
Fig. 1 is a kind of angular precision positioning centering and clamping mechanism structural representation of the present invention;
Fig. 2 is the collet segment structural representation of the present invention;
Fig. 3 is the side view of Fig. 2;
Fig. 4 is a kind of angle adjustable blade schematic diagram;
In figure, 1 taper shank, 2 voussoirs, 3 cones, 4 pedestals, 5 decks, 6 tapered sleeves, 7 overcoats, 8 chucks, 9 flexibly positioned pieces, 10 fishbolts, 11 back-moving springs, 12 blade sides are flat, the 13 big axle journals of blade, 14 blades Pilot pin, 15 flexibly positioned pieces of clamping faces, 16 chuck positioning reference planes.
Detailed description of the invention
The present invention is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1, 2, 3, a kind of angular precision positioning centering and clamping mechanism, including taper shank 1, voussoir 2, cone 3, base Seat 4, deck 5, tapered sleeve 6, overcoat 7 and chuck 8, radially have a groove, at taper shank 1 center on described taper shank 1 Having a circular hole vertically, described voussoir 2 is positioned at the groove of taper shank 1, and voussoir 2 quantity is two, and two voussoirs 2 are relative Arrange, and two voussoirs 2 are linked together by fishbolt 10;Described cone 3 is positioned at the circular hole of taper shank 1, cone 3 Taper seat contact with two voussoirs 2 simultaneously;
Described tapered sleeve 6 the inner is fixedly connected with cone 3 dorsal part, and cone 3 is slidably matched with the circular hole of taper shank 1, and described overcoat 7 overlaps Being contained in tapered sleeve 6 outer end, and tapered sleeve 6 is slidably matched with overcoat 7, overcoat 7 is fixed on pedestal 4, pedestal 4 and taper shank 1 phase It is connected;
Described deck 5 is positioned at inside overcoat 7 and is fixed on pedestal 4, and chuck 8 is connected with deck 5 by draw-in groove, and chuck 8 match with tapered sleeve 6.
Described tapered sleeve 6 outer inner uses inner conical surface structure, and chuck 8 outer surface uses male cone (strobilus masculinus) structure, and chuck 8 entirety is adopted Use and between three-clove style structure, and two lobes, use elastic caoutchouc to connect;Described chuck 8 inner surface is the face of cylinder, and axle big with blade Neck 13 matches.
Described chuck 8 inner surface diameter is ± 0.2mm with the dimensional fits scope of the big axle journal of blade 13.
Being provided with flexibly positioned piece 9 at described chuck 8 inner surface, flexibly positioned piece 9 flat with blade side 12 is matched.
Described flexibly positioned piece of 9 clamping faces 15 are not more than 0.005mm with the depth of parallelism of chuck 8 positioning reference plane 16.
Between described tapered sleeve 6 and cone 3, back-moving spring 11 is installed.
The first use process of the present invention is described below in conjunction with the accompanying drawings:
In the present embodiment, by Five Axis numerical control blade milling machine, a kind of angle adjustable blade shown in Fig. 4 is carried out blade type facing cut Processing, needs axle journal 13 big to blade and blade pilot pin 14 to hold tightly before processing, and by the leaf of blade big axle journal 14 end Sheet side flat 12 controls blade angle.
First, by taper shank 1, the present invention is connected on the main shaft of milling machine, chooses an inspection plug, wherein check plug The diameter of diameter axle journal big with blade 13 is consistent, is inserted in chuck 8 by inspection plug, utilizes spanner to screw fishbolt 10, Make two voussoirs 2 close to each other along groove, promote cone 3 to move in taper shank 1 circular hole by voussoir 2, and then band mantle Set 6 moves in overcoat 7, and makes chuck 8 inwardly tighten up by the movement of tapered sleeve 6, thus realizes chuck 8 and hold inspection core tightly Rod.
Then, working origin and coordinate system are set up by inspection plug and chuck 8 positioning reference plane 16.Spanner is utilized to unclamp clamping Bolt 10, makes two voussoirs 2 be located remotely from each other along groove, and under back-moving spring 11 acts on, cone 3 is return, and then drives Tapered sleeve 6 is return, and is return by tapered sleeve 6 and makes chuck 8 return to free state from the state of tightening up, and now chuck 8 unclamps, will inspection Test plug to unload.
Finally, inserting in chuck 8 by the big axle journal of blade 13 of angle adjustable blade to be processed, blade side flat 12 is at contact bullet Property locating piece 9 can experience in a flash certain resistance, then firmly inwardly push away and make the clamping face 15 of flexibly positioned piece 9 complete Fitting in blade side flat 12, thus realize the angular location of blade, refer again to inspection plug holds mode tightly, axle big to blade Neck 13 is held tightly, finally utilizes modular toolholder to hold blade pilot pin 14 tightly, the most just can start blade type facing cut and add Work.
In order to adapt to different leaves and journal size thereof, chuck 8 quantity is some, and the inner surface diameter of some chucks 8 is the most each Differ, according to the journal size of respective vanes, the chuck 8 of optional correspondingly-sized, and in the present invention, carry out quick-replaceable, It is achieved thereby that the location centering clamping to different leaves, meet the processing request of different leaves.
The taper shank 1 of the present invention also can use the versions such as flange-type, with the connection request of satisfied different machining tools.
Scheme in embodiment is also not used to limit the scope of patent protection of the present invention, all equivalence enforcement done without departing from the present invention Or change, it is both contained in the scope of the claims of this case.

Claims (5)

1. an angular precision positioning centering and clamping mechanism, it is characterised in that: include taper shank, voussoir, cone, pedestal, deck, Tapered sleeve, overcoat and chuck, radially have a groove on described taper shank, at taper shank centrally along axially having a circular hole, described Voussoir is positioned at the groove of taper shank, and voussoir quantity is two, and two voussoirs are oppositely arranged, and two voussoirs are by fishbolt even It is connected together;Described cone is positioned at the circular hole of taper shank, and the taper seat of cone contacts with two voussoirs simultaneously;
Described tapered sleeve the inner is fixedly connected with cone dorsal part, and cone is slidably matched with the circular hole of taper shank, and described coat suit is outside tapered sleeve Holding, and tapered sleeve is slidably matched with overcoat, overcoat is fixed on pedestal, and pedestal is fixedly connected with taper shank;
Described deck is positioned at inside overcoat and is fixed on pedestal, and chuck is connected with deck by draw-in groove, and chuck matches with tapered sleeve Close;
Described tapered sleeve outer inner uses inner conical surface structure, and chuck outer surface uses male cone (strobilus masculinus) structure, and chuck entirety uses many lobes Elastic caoutchouc is used to connect between formula structure, and two lobes;Described chuck inner surface is the face of cylinder, and axle journal big with blade matches.
One the most according to claim 1 angular precision positioning centering and clamping mechanism, it is characterised in that: table in described chuck Face diameter is ± 0.2mm with the dimensional fits scope of the big axle journal of blade.
One the most according to claim 1 angular precision positioning centering and clamping mechanism, it is characterised in that: in described chuck Surface is provided with flexibly positioned piece, and flexibly positioned piece flat with blade side matches.
One the most according to claim 3 angular precision positioning centering and clamping mechanism, it is characterised in that: described flexibly positioned The clamping face of block is not more than 0.005mm with the depth of parallelism of the positioning reference plane of chuck.
One the most according to claim 1 angular precision positioning centering and clamping mechanism, it is characterised in that: described tapered sleeve with Back-moving spring is installed between cone.
CN201410632137.9A 2014-11-10 2014-11-10 A kind of angular precision positioning centering and clamping mechanism Expired - Fee Related CN104400521B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410632137.9A CN104400521B (en) 2014-11-10 2014-11-10 A kind of angular precision positioning centering and clamping mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410632137.9A CN104400521B (en) 2014-11-10 2014-11-10 A kind of angular precision positioning centering and clamping mechanism

Publications (2)

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CN104400521A CN104400521A (en) 2015-03-11
CN104400521B true CN104400521B (en) 2016-09-07

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Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105300216B (en) * 2015-11-19 2018-04-20 中国南方航空工业(集团)有限公司 Blade profile measuring device
CN106965339B (en) * 2017-04-07 2019-06-14 苏州赫瑞特电子专用设备科技有限公司 A kind of centering location structure of multi-line cutting machine
CN110052855A (en) * 2019-04-01 2019-07-26 杭州泽正机械有限公司 A kind of high-accuracy spring perch

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2641996A2 (en) * 1988-11-15 1990-07-27 Pfalzgraf Emile Epb Sa CONICAL TAIL MOUNTING DEVICE, ESPECIALLY 7 / 24E CONE, WITH CONE AND SIDE APPLICATION FOR ATTACHMENTS, TOOL HOLDERS AND TOOLS
DE29502137U1 (en) * 1995-02-09 1996-06-05 Siemens AG, 80333 München Clamping device for a workpiece to be held in a hollow shaft
CN201211621Y (en) * 2008-07-14 2009-03-25 南京数控机床有限公司 Elastic gripping device
CN201295851Y (en) * 2008-11-05 2009-08-26 环一军 Clamping device for turning rotor
CN203900968U (en) * 2014-04-22 2014-10-29 兰溪市海德机床制造有限公司 Centrifugal chuck of spindle

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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City

CP01 Change in the name or title of a patent holder
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160907

Termination date: 20201110

CF01 Termination of patent right due to non-payment of annual fee