CN106736718A - A kind of fixture for high temperature alloy precision castings blade processing - Google Patents

A kind of fixture for high temperature alloy precision castings blade processing Download PDF

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Publication number
CN106736718A
CN106736718A CN201710181195.8A CN201710181195A CN106736718A CN 106736718 A CN106736718 A CN 106736718A CN 201710181195 A CN201710181195 A CN 201710181195A CN 106736718 A CN106736718 A CN 106736718A
Authority
CN
China
Prior art keywords
seat
blade
blade tip
high temperature
temperature alloy
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.)
Pending
Application number
CN201710181195.8A
Other languages
Chinese (zh)
Inventor
徐正茂
黄爱军
刘飞扬
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.)
Falcon Aerotech Ltd
Original Assignee
Falcon Aerotech 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 Falcon Aerotech Ltd filed Critical Falcon Aerotech Ltd
Priority to CN201710181195.8A priority Critical patent/CN106736718A/en
Publication of CN106736718A publication Critical patent/CN106736718A/en
Pending legal-status Critical Current

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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
    • B23Q3/02Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06Work-clamping means
    • B23Q3/062Work-clamping means adapted for holding workpieces having a special form or being made from a special material
    • B23Q3/063Work-clamping means adapted for holding workpieces having a special form or being made from a special material for holding turbine blades

Abstract

The invention discloses a kind of fixture for high temperature alloy precision castings blade processing of blade processing technical field,Including mounting seat,Blade root clamp assemblies are provided with the top of the mounting seat,And blade root clamp assemblies include blade root Holding seat and the seat of the clamping stress on the right side of blade root Holding seat,Supporting rod is connected with by bearing pin on the blade root Holding seat,The left side of the clamping stress seat is provided with blade tip adjustment seat,The side wall of the blade tip adjustment seat is bolted with regulating bolt,And blade tip Holding seat is provided with the left of blade tip adjustment seat,The top of the blade tip Holding seat is connected with blade tip clamping part by nut,Regulating tank is provided with the blade tip clamping part,The nut is located at the inner chamber of regulating tank,Simple structure of the present invention,It is reasonable in design,Universal strong,The processing that can be widely applied for all kinds of high temperature alloy precision castings blades is fixed,Improve production efficiency simultaneously saves production cost.

Description

A kind of fixture for high temperature alloy precision castings blade processing
Technical field
The present invention relates to blade processing technical field, specially a kind of folder for high temperature alloy precision castings blade processing Tool.
Background technology
High temperature alloy is to manufacture Aeronautics and Astronautics engine and the irreplaceable material of the contour warm end pieces of combustion gas wheel, It is widely used in petrochemical industry, nuclear industry, automobile and other industries.High temperature alloy is with aviation, the development of aero engine technology And continue to develop, high temperature alloy precision casting blade machinability is poor, and blade machining is generally using cast low melting point Alloy square chest is positioned, and its processing mode has the following disadvantages:One is to process that the less efficient, process-cycle is long, circulation difficulty, The serious batch production for constraining precision castings blade;Two is that low-melting alloy is not only using square chest cast low-melting alloy positioning With blade surface directly contact, the molten low-melting alloy for moving back and removing on blade surface is needed after the completion of blade machining, and it is thorough Bottom removal is more difficult, and larger on equipment, frock influence;Therefore, adding for high temperature alloy precision castings blade we have proposed one kind The fixture of work comes into operation, to solve the above problems.
The content of the invention
It is an object of the invention to provide a kind of fixture for high temperature alloy precision castings blade processing, to solve the above-mentioned back of the body The problem proposed in scape technology.
To achieve the above object, the present invention provides following technical scheme:One kind is used for high temperature alloy precision castings blade processing Fixture, including mounting seat is provided with blade root clamp assemblies at the top of the mounting seat, and blade root clamp assemblies include blade root clamping Base and the seat of the clamping stress on the right side of blade root Holding seat, folder is connected with the blade root Holding seat by bearing pin Bar is held, the left side of the clamping stress seat is provided with blade tip adjustment seat, and the side wall of the blade tip adjustment seat is bolted with regulating bolt, And blade tip Holding seat is provided with the left of blade tip adjustment seat, the top of the blade tip Holding seat is connected with blade tip and presss from both sides by nut Portion is held, regulating tank is provided with the blade tip clamping part, the nut is located at the inner chamber of regulating tank.
Preferably, be provided with fastening bolt in the middle part of the supporting rod, and fastening bolt and blade root Holding seat top It is spirally connected, the right-hand member of the supporting rod is rotated with bare terminal end by rotating shaft and is connected.
Preferably, the bare terminal end includes being provided with the through hole being adapted with rotating shaft, the centre on middleware, and middleware Arc clamping part and flat board clamping part are separately installed with the top and bottom of part.
Preferably, being provided with the top of the bottom of the flat board clamping part and arc clamping part prevents the slow of blade root surface damage Punching pad.
Preferably, the blade tip adjustment seat is provided with hang plate, and the angle of inclination of hang plate and inclining for clamping stress seat Rake angle is identical.
Preferably, the blade tip adjustment seat and blade tip Holding seat are bolted on the top of mounting seat.
Compared with prior art, the beneficial effects of the invention are as follows:The present invention utilizes grip block and blade tip clamping part by blade Blade root and blade tip at grip respectively, and make blade it is fixed when in certain inclination angle, be easy to follow-up to blade surface Working process, simple structure of the present invention, reasonable in design, universal strong can be widely applied for all kinds of high temperature alloy precision castings leaves The processing of piece is fixed, and improve production efficiency simultaneously saves production cost.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention;
Fig. 2 is supporting rod structural representation of the present invention;
Fig. 3 is bare terminal end structural representation of the present invention.
In figure:1 mounting seat, 2 blade root Holding seats, 3 bearing pins, 4 supporting rods, 41 fastening bolts, 42 rotating shafts, 43 bare terminal ends, 431 middlewares, 432 flat board clamping parts, 433 arc clamping parts, 5 clamping stress seats, 6 blade tip adjustment seats, 7 regulating bolts, 8 blade tips Holding seat, 9 blade tip clamping parts, 10 regulating tanks, 11 nuts.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made Embodiment, belongs to the scope of protection of the invention.
Fig. 1-3 are referred to, the present invention provides a kind of technical scheme:A kind of folder for high temperature alloy precision castings blade processing Tool, including mounting seat 1, the top of the mounting seat 1 are provided with blade root clamp assemblies, and blade root clamp assemblies include that blade root clamps bottom Seat 2 and the clamping stress seat 5 positioned at the right side of blade root Holding seat 2, are flexibly connected on the blade root Holding seat 2 by bearing pin 3 The left side for having supporting rod 4, the clamping stress seat 5 is provided with blade tip adjustment seat 6, and the side wall of the blade tip adjustment seat 6 is bolted with Regulating bolt 7, and the left side of blade tip adjustment seat 6 is provided with blade tip Holding seat 8, the top of the blade tip Holding seat 8 passes through spiral shell Female 11 are connected with blade tip clamping part 9, and regulating tank 10 is provided with the blade tip clamping part 9, and the nut 11 is located at regulating tank 10 Inner chamber.
Wherein, the middle part of the supporting rod 4 is provided with fastening bolt 41, and fastening bolt 41 and blade root Holding seat 2 Top is spirally connected, and the right-hand member of the supporting rod 4 is rotated with bare terminal end 43 by rotating shaft 42 and is connected, and the bare terminal end 43 includes middleware The through hole being adapted with rotating shaft 42 is provided with 431, and middleware 431, the top and bottom of the middleware 431 are separately installed with Arc clamping part 433 and flat board clamping part 432, the bottom of the flat board clamping part 432 and the top of arc clamping part 433 are provided with Prevent the cushion pad of blade root surface damage, the blade tip adjustment seat 6 is provided with hang plate, and hang plate angle of inclination and clamping The angle of inclination of stress seat 5 is identical, and the blade tip adjustment seat 6 and blade tip Holding seat 8 are bolted on mounting seat 1 Top.
Operation principle:The lower section of supporting rod 4 will be placed at the blade root of high-temperature alloy blades, by rotational fastener bolt 41 Bare terminal end 43 and blade root surface is formed clamping force, wherein bare terminal end 43 is designed to reversible type structure, be in surface needing Using plate clamping part 432, it is necessary to when being clamped in the blade root of arc-shaped to surface, will press from both sides when flat blade root is clamped Hold bar 43 to rotate to the one side of arc clamping part 433, clamped, will be placed at blade tip in the inclination version of blade tip adjustment seat 6, By rotating regulating bolt 7, make elongate screw or the shortening of regulating bolt 7, so as to the angular adjustment of blade tip, while blade tip Another side is contacted with blade tip clamping part 9, and forms clamping force, by the effect of regulating tank 10, can adjust the position of blade tip clamping part 9 Put, realize the clamping to blade tip diverse location, the fixed processing that the present invention is adapted to various high-temperature alloy blades is practical, improves production Processing efficiency.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with Understanding can carry out various changes, modification, replacement to these embodiments without departing from the principles and spirit of the present invention And modification, the scope of the present invention be defined by the appended.

Claims (6)

1. a kind of fixture for high temperature alloy precision castings blade processing, including mounting seat(1), it is characterised in that:The installation Seat(1)Top be provided with blade root clamp assemblies, and blade root clamp assemblies include blade root Holding seat(2)Bottom is clamped with positioned at blade root Seat(2)The clamping stress seat on right side(5), the blade root Holding seat(2)It is upper to pass through bearing pin(3)It is connected with supporting rod(4), The clamping stress seat(5)Left side blade tip adjustment seat is installed(6), the blade tip adjustment seat(6)Side wall be bolted with regulation Bolt(7), and blade tip adjustment seat(6)Left side be provided with blade tip Holding seat(8), the blade tip Holding seat(8)Top lead to Cross nut(11)It is connected with blade tip clamping part(9), the blade tip clamping part(9)On be provided with regulating tank(10), the nut(11) Positioned at regulating tank(10)Inner chamber.
2. a kind of fixture for high temperature alloy precision castings blade processing according to claim 1, it is characterised in that:It is described Supporting rod(4)Middle part be provided with fastening bolt(41), and fastening bolt(41)With blade root Holding seat(2)Top be spirally connected, The supporting rod(4)Right-hand member pass through rotating shaft(42)With bare terminal end(43)Rotate connection.
3. a kind of fixture for high temperature alloy precision castings blade processing according to claim 2, it is characterised in that:It is described Bare terminal end(43)Including middleware(431), and middleware(431)On be provided with and rotating shaft(42)The through hole being adapted, the centre Part(431)Top and bottom be separately installed with arc clamping part(433)With flat board clamping part(432).
4. a kind of fixture for high temperature alloy precision castings blade processing according to claim 3, it is characterised in that:It is described Flat board clamping part(432)Bottom and arc clamping part(433)Top be provided with the cushion pad for preventing blade root surface damage.
5. a kind of fixture for high temperature alloy precision castings blade processing according to claim 1, it is characterised in that:It is described Blade tip adjustment seat(6)Be provided with hang plate, and hang plate angle of inclination and clamping stress seat(5)Angle of inclination it is identical.
6. a kind of fixture for high temperature alloy precision castings blade processing according to claim 1, it is characterised in that:It is described Blade tip adjustment seat(6)With blade tip Holding seat(8)It is bolted on mounting seat(1)Top.
CN201710181195.8A 2017-03-24 2017-03-24 A kind of fixture for high temperature alloy precision castings blade processing Pending CN106736718A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710181195.8A CN106736718A (en) 2017-03-24 2017-03-24 A kind of fixture for high temperature alloy precision castings blade processing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710181195.8A CN106736718A (en) 2017-03-24 2017-03-24 A kind of fixture for high temperature alloy precision castings blade processing

Publications (1)

Publication Number Publication Date
CN106736718A true CN106736718A (en) 2017-05-31

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Family Applications (1)

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CN201710181195.8A Pending CN106736718A (en) 2017-03-24 2017-03-24 A kind of fixture for high temperature alloy precision castings blade processing

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107322334A (en) * 2017-07-14 2017-11-07 哈尔滨汽轮机厂有限责任公司 A kind of milling integral shroud molded line special fixture
CN108326589A (en) * 2018-03-22 2018-07-27 宣化钢铁集团有限责任公司 A kind of milling train catheter fabrication special fixture and its processing method
CN108687726A (en) * 2018-07-23 2018-10-23 黄德旺 A kind of fan leaf fork angle regulating equipment
CN108747520A (en) * 2018-05-29 2018-11-06 江苏大学 A kind of adjustable fixture based on blade root contour localization
CN109531198A (en) * 2018-11-27 2019-03-29 中国航发沈阳黎明航空发动机有限责任公司 Improve the method and process area refine fixture of large and complex structure blade processing precision
EP3542951A1 (en) * 2018-03-22 2019-09-25 United Technologies Corporation Fan blade repair fixture and method of repair

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0808354D0 (en) * 2008-05-09 2008-06-18 Rolls Royce Plc Clamping system
CN201744716U (en) * 2010-08-12 2011-02-16 四川省自贡市海川实业有限公司 Clamp dedicated for fine milling of radial inclined planes of blade basin
CN103659329A (en) * 2013-11-29 2014-03-26 成都斯锐特钨钢刀具有限公司 Compression device
CN204075747U (en) * 2014-07-18 2015-01-07 常州市三维技术成套设备有限公司 A kind of steam turbine is without hat stator blade end face Machining of Curved Surface frock
CN204843399U (en) * 2015-08-31 2015-12-09 哈尔滨汽轮机厂有限责任公司 Novel si taili high temperature alloy welding position anchor clamps
CN205032978U (en) * 2015-10-21 2016-02-17 成都弘佛科技有限公司 Stator vane tenon milling fixture
CN106514356A (en) * 2016-12-28 2017-03-22 无锡透平叶片有限公司 Universal clamp device for total-length finish milling of turbine blades
CN206578578U (en) * 2017-03-24 2017-10-24 无锡飞而康精铸工程有限公司 A kind of fixture for high temperature alloy precision castings blade processing

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0808354D0 (en) * 2008-05-09 2008-06-18 Rolls Royce Plc Clamping system
CN201744716U (en) * 2010-08-12 2011-02-16 四川省自贡市海川实业有限公司 Clamp dedicated for fine milling of radial inclined planes of blade basin
CN103659329A (en) * 2013-11-29 2014-03-26 成都斯锐特钨钢刀具有限公司 Compression device
CN204075747U (en) * 2014-07-18 2015-01-07 常州市三维技术成套设备有限公司 A kind of steam turbine is without hat stator blade end face Machining of Curved Surface frock
CN204843399U (en) * 2015-08-31 2015-12-09 哈尔滨汽轮机厂有限责任公司 Novel si taili high temperature alloy welding position anchor clamps
CN205032978U (en) * 2015-10-21 2016-02-17 成都弘佛科技有限公司 Stator vane tenon milling fixture
CN106514356A (en) * 2016-12-28 2017-03-22 无锡透平叶片有限公司 Universal clamp device for total-length finish milling of turbine blades
CN206578578U (en) * 2017-03-24 2017-10-24 无锡飞而康精铸工程有限公司 A kind of fixture for high temperature alloy precision castings blade processing

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107322334A (en) * 2017-07-14 2017-11-07 哈尔滨汽轮机厂有限责任公司 A kind of milling integral shroud molded line special fixture
CN108326589A (en) * 2018-03-22 2018-07-27 宣化钢铁集团有限责任公司 A kind of milling train catheter fabrication special fixture and its processing method
EP3542951A1 (en) * 2018-03-22 2019-09-25 United Technologies Corporation Fan blade repair fixture and method of repair
US10711611B2 (en) 2018-03-22 2020-07-14 Raytheon Technologies Corporation Fan blade repair fixture and method of repair
CN108747520A (en) * 2018-05-29 2018-11-06 江苏大学 A kind of adjustable fixture based on blade root contour localization
CN108747520B (en) * 2018-05-29 2020-03-31 江苏大学 Adjustable clamp based on blade root inclined plane positioning
CN108687726A (en) * 2018-07-23 2018-10-23 黄德旺 A kind of fan leaf fork angle regulating equipment
CN109531198A (en) * 2018-11-27 2019-03-29 中国航发沈阳黎明航空发动机有限责任公司 Improve the method and process area refine fixture of large and complex structure blade processing precision
CN109531198B (en) * 2018-11-27 2020-09-18 中国航发沈阳黎明航空发动机有限责任公司 Method for improving machining precision of large-scale complex-structure blade and fine trimming clamp of process table

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Application publication date: 20170531