CN209598733U - Clamping tooling for high-temperature alloy blades wire cutting - Google Patents

Clamping tooling for high-temperature alloy blades wire cutting Download PDF

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Publication number
CN209598733U
CN209598733U CN201920157700.XU CN201920157700U CN209598733U CN 209598733 U CN209598733 U CN 209598733U CN 201920157700 U CN201920157700 U CN 201920157700U CN 209598733 U CN209598733 U CN 209598733U
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China
Prior art keywords
temperature alloy
root
blade
tip
alloy blades
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Active
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CN201920157700.XU
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Chinese (zh)
Inventor
刘光文
王勇
宋扬
罗学均
肖锡铭
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Chengdu Aerospace Superalloy Technology Co Ltd
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Chengdu Aerospace Superalloy Technology Co Ltd
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Abstract

The utility model discloses a kind of clamping toolings for high-temperature alloy blades wire cutting, belong to engine alloy blade processing technique equipment Design manufacturing technology field.There is provided a kind of clamped one time effectively can carry out the clamping tooling for high-temperature alloy blades wire cutting of accurate machining in each position to alloy sheet.The clamping tooling includes the pedestal containing bottom plate and support, the clamping tooling further includes compressing device assembly, root positioning component and tip positioning component, the compression device assembly is movable to be mounted on the support, on bottom plate described in the arrangement that the root positioning block assembly and the tip locating piece module position are mutually adapted;It needs to carry out the high-temperature alloy blades of linear cutter by the root positioning component and the tip positioning component, edge horizontal direction, tenon and blade tip and horizontal direction is vented under the cooperation for compressing device assembly on the clamping tooling described in being packed in of 45 degree angles.

Description

Clamping tooling for high-temperature alloy blades wire cutting
Technical field
The utility model relates to a kind of clamping toolings, more particularly, to a kind of clamping for high-temperature alloy blades wire cutting Tooling belongs to engine alloy blade processing technique equipment Design manufacturing technology field.
Background technique
High-temperature alloy blades are the critical components of aero-engine.The blade of aero-engine is mainly cast by fusible pattern at present Method is made to manufacture.After blade casting and forming, the positions such as tenon, blade tip and exhaust side on blade can generally use linear cutter Mode carry out roughing.For the linear cutter of blade, it is ensured that the machining accuracy of wire cutting need to make clamping work Dress carries out firm clamping and accurately positioning to blade.But most of blade wire cutting clamping tooling is only applicable at present In the position of the cutting easy cutting such as tenon and blade tip, for there are exhaust sides of special relationship etc. to be not easy to cut with tenon, blade tip The position cut is difficult to accomplish effective clamping, not can guarantee the machining accuracy at the positions such as exhaust side, increases adding for subsequent handling Work difficulty and process time.
Utility model content
The technical problem to be solved by the utility model is to provide a kind of clamped one times can be effectively to alloy sheet Each position carries out the clamping tooling for high-temperature alloy blades wire cutting of accurate machining.
Used technical solution is to solve above-mentioned technical problem: a kind of clamping for high-temperature alloy blades wire cutting Tooling, including the pedestal containing bottom plate and support, the clamping tooling further includes compressing device assembly, root positioning component and point Portion's positioning component, the compression device assembly is movable to be mounted on the support, the root positioning component and described The arrangement that is mutually adapted of tip positioning component position described on bottom plate;Need to carry out the high-temperature alloy blades of linear cutter By the root positioning component and the tip positioning component, edge water is vented under the cooperation for compressing device assembly Square to, tenon and blade tip and horizontal direction on the clamping tooling described in being packed in of 45 degree angles.
Further, the clamping tooling further includes C1 locating piece, rim is arranged on the C1 locating piece Positioning pin, the listrium side of the high-temperature alloy blades are bonded with the rim positioning pin;In line cutting processing, high temperature Alloy vane is limited along the movement of Z-direction by the rim positioning pin.
The preferred mode of the above solution is that the root positioning component includes at least the root positioning containing inclined surface Block, the tip positioning component include at least the tip locating piece containing inclined surface, the inclined surface of the root locating piece and Horizontal by 45 degree of angles, the tenon and blade tip of the high-temperature alloy blades lead to respectively for the inclined surface of the tip locating piece It crosses the inclined surface to arrange horizontal by 45 degree of angles, exhaust side the matching in the inclined surface of the high-temperature alloy blades It is arranged in the horizontal direction under conjunction.
Further, being additionally provided on the root locating piece, blade stretches root positioning pin and blade leading edge is fixed Position pin, is additionally provided with blade leading edge straight pin on the tip locating piece, and the blade of high-temperature alloy blades stretches root position Root is stretched by the blade and positions finger setting, and the leading edge of high-temperature alloy blades passes through the blade leading edge positioning pin With the blade leading edge straight pin alignment by union.
The preferred mode of the above solution is that it is two pieces that the blade being arranged on the root locating piece, which stretches root positioning pin, Blade described in two pieces is stretched root positioning pin and is arranged along the inclined surface sequence.
Further, the compression device assembly includes compactor, hold-down head and installing mechanism, the hold-down head is logical It crosses the installing mechanism to be arranged on the compactor, the compactor is packed on the support.
The preferred mode of the above solution is that the installing mechanism includes mounting plate and connection bolt, the hold-down head It is packed on the mounting plate, the mounting plate is arranged on the compactor by the connection bolt.
Further, being additionally provided with base point for checking cutting tool block on the bottom plate.
The beneficial effects of the utility model are: according to the investigation to the high-temperature alloy blades structure for needing to add, it is existing combining There are the problem of big processed position of difficulty of processing can not being fixed to suitable Working position existing for clamping tooling, the application On the basis of existing clamping tooling by adjusting with the shape that changes root positioning component and tip positioning component, make to need into The high-temperature alloy blades of line cutting processing are by the root positioning component and the tip positioning component, in the pressure It is vented edge horizontal direction, tenon and blade tip under the cooperation of tight device assembly and horizontal direction is in that being packed in for 45 degree of angles is described On clamping tooling.In this way, the big exhaust side of difficulty of processing is arranged into horizontal position by above-mentioned technical proposal provided by the present application It sets, the low tenon in difficult processing bottom and blade tip is arranged into the position with horizontal direction in 45 degree of angles, can effectively be realized Clamped one time successively completes high-temperature alloy blades tenon, blade tip and the processing for being vented side, due to the reduction of clamping times, so as to To greatly improve the quality and machining accuracy of processing.
Detailed description of the invention
Fig. 1 is three dimensional structure diagram of the utility model for the clamping tooling of high-temperature alloy blades wire cutting.
In the figure, it is marked as bottom plate 1, support 2, pedestal 3, compress device assembly 4, root positioning component 5, tip positioning component 6, High-temperature alloy blades 7, C1 locating piece 8, rim positioning pin 9, root locating piece 10, tip locating piece 11, blade stretch root positioning Pin 12, blade leading edge positioning pin 13, blade leading edge straight pin 14, compactor 15, hold-down head 16, installing mechanism 17, installation Plate 18, connection bolt 19, base point for checking cutting tool block 20.
Specific embodiment
It is that a kind of clamped one time provided by the utility model can be effectively to each position of alloy sheet as shown in Figure 1 Carry out the clamping tooling for high-temperature alloy blades wire cutting of accurate machining.The clamping tooling includes containing 1 He of bottom plate The pedestal 3 of support 2, the clamping tooling further include compressing device assembly 4, root positioning component 5 and tip positioning component 6, institute The compression device assembly 4 stated is movable to be mounted on the support 2, and the root positioning block assembly 5 and the tip are fixed On bottom plate 2 described in the arrangement that position 6 position of block assembly is mutually adapted;The high-temperature alloy blades 7 for needing to carry out linear cutter are logical The root positioning component 5 and the tip positioning component 6 are crossed, is vented edge under the cooperation for compressing device assembly 4 Horizontal direction, tenon and blade tip and horizontal direction are on the clamping tooling described in being packed in of 45 degree angles.Add according to needs High-temperature alloy blades structure investigation, combine can not be big by difficulty of processing existing for existing clamping tooling processed position The problem of fixed to suitable Working position, the application position on the basis of existing clamping tooling by adjusting with change root The shape of component and tip positioning component makes that the high-temperature alloy blades for carrying out linear cutter is needed to position by the root Component and the tip positioning component are vented edge horizontal direction, tenon and blade tip under the cooperation for compressing device assembly With horizontal direction on the clamping tooling described in being packed in of 45 degree angles.In this way, passing through above-mentioned technical side provided by the present application The big exhaust side of difficulty of processing is arranged into horizontal position, the low tenon in difficult processing bottom and blade tip is arranged into and level side by case To the position for being in 45 degree of angles, it can effectively realize that clamped one time successively completes high-temperature alloy blades tenon, blade tip and row The processing on gas side, due to the reduction of clamping times, so as to greatly improve the quality and machining accuracy of processing.
It is described herein meanwhile in order to control the movement for the Z-direction that high-temperature alloy blades 7 define in processing technology Clamping tooling further includes C1 locating piece 8, and rim positioning pin 9, the high-temperature alloy blades are arranged on the C1 locating piece 8 7 listrium side is bonded with the rim positioning pin 9;In line cutting processing, shifting of the high-temperature alloy blades 7 along Z-direction It is dynamic to be limited by the rim positioning pin 9.
In above embodiment, in order to borrow the prior art as far as possible, under the conditions of improvement amount as few as possible Realize the above-mentioned function of the application, at the same to the greatest extent can with make root positioning component 5 and tip positioning component 6 described herein Structure is relatively easy, and root positioning component 5 described herein includes at least the root locating piece 10 containing inclined surface, described Tip positioning component 6 includes at least the tip locating piece 11 containing inclined surface, the inclined surface of the root locating piece 10 and described Horizontal by 45 degree of angles, the tenon and blade tip of the high-temperature alloy blades 7 lead to respectively for the inclined surface of tip locating piece 11 It crosses the inclined surface and arranges that the exhaust side of the high-temperature alloy blades 7 is in the inclined surface horizontal by 45 degree of angles It is arranged in the horizontal direction under cooperation.At this point, the positioning in order to realize point contact, improves location efficiency and positioning accuracy, described Root locating piece 10 on be additionally provided with blade and stretch root positioning pin 12 and blade leading edge positioning pin 13, it is fixed in the tip Blade leading edge straight pin 14 is additionally provided on the block 11 of position, the blade of high-temperature alloy blades 7 stretches root position and passes through the blade Stretch the positioning of root positioning pin 12, the leading edges of high-temperature alloy blades 7 passes through the blade leading edge positioning pin 13 and described 14 alignment by union of blade leading edge straight pin.Correspondingly, the blade being arranged on the root locating piece 10 stretches root positioning pin For 12 two pieces, blade described in two pieces is stretched root positioning pin 12 and is arranged along the inclined surface sequence.
Further, in order to realize the substrate hold-down function of high-temperature alloy blades 7, while facilitating its dress on clamping tooling again Folder and disassembly, compression device assembly 4 described herein include compactor 15, hold-down head 16 and installing mechanism 17, the compression First 16 are arranged on the compactor 15 by the installing mechanism 17, and the compactor 15 is packed in the support On 2.At this point, the installing mechanism 17 includes mounting plate 18 and connection bolt 19, the hold-down head 16 is packed in described On mounting plate 18, the mounting plate 18 is arranged on the compactor 15 by the connection bolt 19.
It is convenient for being additionally provided with base point for checking cutting tool block 20 on the bottom plate 1 to knife when certainly, in order to process.In this way, in height After the completion of 7 clamping of temperature alloy blade, starting cutting position can be determined by base point for checking cutting tool block 20, respectively to blade tip, exhaust Side and tenon are cut.

Claims (8)

1. a kind of clamping tooling for high-temperature alloy blades wire cutting, the pedestal (3) including containing bottom plate (1) and support (2), It is characterized by: the clamping tooling further includes compressing device assembly (4), root positioning component (5) and tip positioning component (6), the compression device assembly (4) is movable is mounted on the support (2), the root positioning component (5) and institute On bottom plate (1) described in the arrangement that tip positioning component (6) position stated is mutually adapted;Need to carry out the high temperature of linear cutter Alloy vane (7) is by the root positioning component (5) and the tip positioning component (6), in the compression device assembly (4) edge horizontal direction, tenon and blade tip and horizontal direction are vented under cooperation in the clamping described in being packed in of 45 degree angles In tooling.
2. the clamping tooling according to claim 1 for high-temperature alloy blades wire cutting, it is characterised in that: the folder Holding tooling further includes C1 locating piece (8), is arranged in rim positioning pin (9), the high temperature alloy on the C1 locating piece (8) The listrium side of blade (7) is bonded with the rim positioning pin (9);In line cutting processing, high-temperature alloy blades (7) edge The movement of Z-direction is limited by the rim positioning pin (9).
3. the clamping tooling according to claim 1 or 2 for high-temperature alloy blades wire cutting, it is characterised in that: described Root positioning component (5) include at least the root locating piece (10) containing inclined surface, the tip positioning component (6) is at least Including the tip locating piece (11) containing inclined surface, the inclined surface of the root locating piece (10) and the tip locating piece (11) Inclined surface horizontal by 45 degree of angles, the tenon and blade tip of the high-temperature alloy blades (7) pass through respectively described to incline Inclined-plane arranges that the high-temperature alloy blades (7) are vented side in the cooperation lower edge of the inclined surface horizontal by 45 degree of angles Horizontal direction arrangement.
4. the clamping tooling according to claim 3 for high-temperature alloy blades wire cutting, it is characterised in that: described It is additionally provided with blade on root locating piece (10) and stretches root positioning pin (12) and blade leading edge positioning pin (13), in the point Blade leading edge straight pin (14) is additionally provided on portion's locating piece (11), the blade of high-temperature alloy blades (7) is stretched root position and passed through The blade stretches root positioning pin (12) positioning, and the leading edge of high-temperature alloy blades (7) is fixed by the blade leading edge Position pin (13) and described blade leading edge straight pin (14) alignment by union.
5. the clamping tooling according to claim 4 for high-temperature alloy blades wire cutting, it is characterised in that: be arranged in institute Stating the blade on root locating piece (10) to stretch root positioning pin (12) is two pieces, and blade described in two pieces stretches root positioning pin (12) it is arranged along the inclined surface sequence.
6. the clamping tooling according to claim 1 or 2 for high-temperature alloy blades wire cutting, it is characterised in that: described Compression device assembly (4) include compactor (15), hold-down head (16) and installing mechanism (17), the hold-down head (16) passes through institute The installing mechanism (17) stated is arranged on the compactor (15), and the compactor (15) is packed in the support (2) On.
7. the clamping tooling according to claim 6 for high-temperature alloy blades wire cutting, it is characterised in that: the peace Mounting mechanism (17) includes mounting plate (18) and connection bolt (19), and the hold-down head (16) is packed in the mounting plate (18) On, the mounting plate (18) is arranged on the compactor (15) by the connection bolt (19).
8. the clamping tooling according to claim 1 or 2 for high-temperature alloy blades wire cutting, it is characterised in that: in institute Base point for checking cutting tool block (20) are additionally provided on the bottom plate (1) stated.
CN201920157700.XU 2019-01-29 2019-01-29 Clamping tooling for high-temperature alloy blades wire cutting Active CN209598733U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920157700.XU CN209598733U (en) 2019-01-29 2019-01-29 Clamping tooling for high-temperature alloy blades wire cutting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920157700.XU CN209598733U (en) 2019-01-29 2019-01-29 Clamping tooling for high-temperature alloy blades wire cutting

Publications (1)

Publication Number Publication Date
CN209598733U true CN209598733U (en) 2019-11-08

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Application Number Title Priority Date Filing Date
CN201920157700.XU Active CN209598733U (en) 2019-01-29 2019-01-29 Clamping tooling for high-temperature alloy blades wire cutting

Country Status (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114043022A (en) * 2021-10-18 2022-02-15 马鞍山经纬回转支承有限公司 Technological method for enveloping worm cutter
CN114714119A (en) * 2022-05-05 2022-07-08 中国航发航空科技股份有限公司 Clamping device of intermediary cartridge receiver extension board

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114043022A (en) * 2021-10-18 2022-02-15 马鞍山经纬回转支承有限公司 Technological method for enveloping worm cutter
CN114714119A (en) * 2022-05-05 2022-07-08 中国航发航空科技股份有限公司 Clamping device of intermediary cartridge receiver extension board

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