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CN107931544A - A kind of conjuncted hollow guide vane investment casting process - Google Patents

A kind of conjuncted hollow guide vane investment casting process Download PDF

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Publication number
CN107931544A
CN107931544A CN201711447635.6A CN201711447635A CN107931544A CN 107931544 A CN107931544 A CN 107931544A CN 201711447635 A CN201711447635 A CN 201711447635A CN 107931544 A CN107931544 A CN 107931544A
Authority
CN
China
Prior art keywords
guide vane
wax
pattern
conjuncted
thermal insulation
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
CN201711447635.6A
Other languages
Chinese (zh)
Inventor
杜应流
林新刚
冯文刚
陶元亮
罗庆
郝大伟
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.)
Anhui Yingliu Air Source Power Technology Co
Original Assignee
Anhui Yingliu Air Source Power Technology Co
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 Anhui Yingliu Air Source Power Technology Co filed Critical Anhui Yingliu Air Source Power Technology Co
Priority to CN201711447635.6A priority Critical patent/CN107931544A/en
Publication of CN107931544A publication Critical patent/CN107931544A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/22Moulds for peculiarly-shaped castings
    • B22C9/24Moulds for peculiarly-shaped castings for hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

The invention discloses a kind of conjuncted hollow guide vane investment casting process, it is related to precision casting technology field.Cooperation shell processing, cast parameter, solve the problems, such as that common process scheme yield rate is low, complicated, easily generation is loose at blade position, improve casting qualified rate.

Description

A kind of conjuncted hollow guide vane investment casting process
Technical field
The present invention relates to hot investment casting field, is specially a kind of conjuncted hollow guide vane investment casting process.
Background technology
Casting is one of fundamental technology of modern mechanical manufacturing industry.Casting is used as a kind of metal working process, in China Development is gradually ripe.
Conjuncted hollow guide vane, generally comprises thicker big listrium installation side and the thick big boss in part at least 2, conventional Model casting scheme can set each heat energy-saving position respectively riser to carry out feeding, and assembled scheme is complicated, and product yield is low, and And it be easy to cause part key job position --- blade position thermal radiation is more, and cooling effect is poor, easily occurs loose.
The content of the invention
(1) technical problem solved
It is contemplated that a kind of simple assembled scheme of design, coordinates shell processing, cast parameter, solves common process side Case yield rate is low, it is complicated, easily produce the problem of loose at blade position, improve casting qualified rate.
(2) technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs:A kind of conjuncted hollow guide vane melts Die cast process, comprises the following steps:
(1) compacting of running gate system wax-pattern, guide vane wax-pattern and multiple riser wax-patterns is carried out, then by each wax-pattern portion Part is combined, and obtains wax pattern assemblies, and the riser wax-pattern is arranged on each heat energy-saving position of guide vane;
(2) wax pattern assemblies obtained by step (1) are subjected to shell manufacture, obtain shell model;
(3) gained shell model is subjected to bag cotton processing, be specifically done the guide vane listrium lower part, guide vane Attached thermal insulation material is not wrapped at blade and the thick big boss position of guide vane;The guide vane listrium top subpackage has 6-8mm Thick thermal insulation material, the riser position is wrapped with the thermal insulation material of 13-15mm thickness;
(4) shell coated is preheated, and carries out smelting and pouring;
(5) the casting progress heat treatment being poured in will be poured, then by cutting, polishing, heat treatment and correction step, obtained smart One-piece casting;
(6) finishing casting obtained by step (5) is subjected to size detection, fluorescent inspection, x-ray examination successively, to obtain the final product.
The thermal insulation material can be insulation quilt or insulation asbestos.
The present invention is applied in the conjuncted guide vane of certain combustion engine, casting process yield more than 60%, and casting closes Lattice rate more than 90%, one-piece parts are without loose.
(3) beneficial effect
The present invention provides a kind of conjuncted hollow guide vane investment casting process.Possesses following beneficial effect:This Invention is applied in the conjuncted guide vane of certain combustion engine, casting process yield more than 60%, casting qualified rate 90% with On, one-piece parts are without loose.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention;
In figure:1st, running gate system;2nd, guide vane;3rd, riser;4th, boss position;5th, thermal insulation material;
Embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work Embodiment, belongs to the scope of protection of the invention.
Referring to Fig. 1, the present invention provides a kind of technical solution:A kind of conjuncted hollow guide vane investment casting technique side Method, comprises the following steps:
(1) compacting of running gate system wax-pattern, guide vane wax-pattern and multiple riser wax-patterns is carried out, then by each wax-pattern portion Part is combined, and obtains wax pattern assemblies, and the riser wax-pattern is arranged on each heat energy-saving position of guide vane;
(2) wax pattern assemblies obtained by step (1) are subjected to shell manufacture, obtain shell model;
(3) gained shell model is subjected to bag cotton processing, be specifically done the 2 listrium lower part of guide vane, directing vane Attached thermal insulation material 5 is not wrapped at 2 blade of piece and the thick big boss position 4 of guide vane 2;The 2 listrium top subpackage of guide vane is attached There is the thermal insulation material 5 of 6-8mm thickness, the riser position is wrapped with the thermal insulation material 5 of 13-15mm thickness;
(4) shell coated is preheated, and carries out smelting and pouring;
(5) the casting progress heat treatment being poured in will be poured, then by cutting, polishing, heat treatment and correction step, obtained smart One-piece casting;
(6) finishing casting obtained by step (5) is subjected to size detection, fluorescent inspection, x-ray examination successively, to obtain the final product.
The thermal insulation material 5 can be insulation quilt or insulation asbestos.
The present invention uses shell mould ladder bag cotton mode, ensures that 2 position of guide vane solidifies at first, reduces micro- dredge The exceeded risk of pine;Coordinate and select appropriate shell temperature and pouring temperature, ensure that the Feeding channel of casting in itself is unimpeded, riser 3 pairs of casting have the feeding capacity of abundance, realize consecutive solidification of the casting from top to bottom, from casting to riser.
The thermal insulation material 5 can be insulation quilt or insulation asbestos.
The present invention is applied in the conjuncted guide vane of certain combustion engine, casting process yield more than 60%, and casting closes Lattice rate more than 90%, one-piece parts are without loose.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation In any this actual relation or order.Moreover, term " comprising ", "comprising" or its any other variant are intended to Non-exclusive inclusion, so that process, method, article or equipment including a series of elements not only will including those Element, but also including other elements that are not explicitly listed, or further include as this process, method, article or equipment Intrinsic key element.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of changes, modification, replace And modification, the scope of the present invention is defined by the appended.

Claims (2)

  1. A kind of 1. conjuncted hollow guide vane investment casting process, it is characterised in that:Comprise the following steps:
    (1) carry out the compacting of running gate system wax-pattern, guide vane wax-pattern and multiple riser wax-patterns, then by each wax-pattern component into Row combination, obtains wax pattern assemblies, the riser wax-pattern is arranged on each heat energy-saving position of guide vane;
    (2) wax pattern assemblies obtained by step (1) are subjected to shell manufacture, obtain shell model;
    (3) gained shell model is subjected to bag cotton processing, be specifically done the guide vane listrium lower part, guide vane blade And attached thermal insulation material is not wrapped at the thick big boss position of guide vane;The guide vane listrium top subpackage is with 6-8mm thickness Thermal insulation material, the riser position are wrapped with the thermal insulation material of 13-15mm thickness;
    (4) shell coated is preheated, and carries out smelting and pouring;
    (5) the casting progress heat treatment being poured in will be poured, then by cutting, polishing, heat treatment and correction step, obtains finishing and cast Part;
    (6) finishing casting obtained by step (5) is subjected to size detection, fluorescent inspection, x-ray examination successively, to obtain the final product.
  2. 2. the conjuncted hollow guide vane investment casting process of one kind according to claim 1, it is characterised in that:It is described Thermal insulation material can be insulation quilt or insulation asbestos.
CN201711447635.6A 2017-12-27 2017-12-27 A kind of conjuncted hollow guide vane investment casting process Pending CN107931544A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711447635.6A CN107931544A (en) 2017-12-27 2017-12-27 A kind of conjuncted hollow guide vane investment casting process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711447635.6A CN107931544A (en) 2017-12-27 2017-12-27 A kind of conjuncted hollow guide vane investment casting process

Publications (1)

Publication Number Publication Date
CN107931544A true CN107931544A (en) 2018-04-20

Family

ID=61939461

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711447635.6A Pending CN107931544A (en) 2017-12-27 2017-12-27 A kind of conjuncted hollow guide vane investment casting process

Country Status (1)

Country Link
CN (1) CN107931544A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108515146A (en) * 2018-05-22 2018-09-11 株洲中航动力精密铸造有限公司 The running gate system of whole essence casting guider
CN109622888A (en) * 2018-12-20 2019-04-16 航天海鹰(哈尔滨)钛业有限公司 A kind of cast shaping process of the multi-joint guide vane casting of complexity high temperature alloy
CN110052583A (en) * 2019-03-15 2019-07-26 启东市聚旺铸造有限公司 Precise casting process of hollow guide blade
CN110640084A (en) * 2019-10-29 2020-01-03 贵州安吉航空精密铸造有限责任公司 Preparation method of investment casting shell

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100193150A1 (en) * 2009-02-04 2010-08-05 Rolls-Royce Plc Casting method
CN204247910U (en) * 2014-10-31 2015-04-08 沈阳黎明航空发动机(集团)有限责任公司 A kind of triplet that prevents is hollow without the running gate system that cracks of surplus essence casting blade
CN105290337A (en) * 2015-11-16 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Multiple-connection-blade precision casting method
CN105364006A (en) * 2015-12-09 2016-03-02 沈阳黎明航空发动机(集团)有限责任公司 Wax mold of large-size hollow shrouded blade casting pouring system and manufacturing method of wax mold
CN107598097A (en) * 2017-11-10 2018-01-19 东方电气集团东方汽轮机有限公司 A kind of wax-pattern combination of turborotor and its fine casting method

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100193150A1 (en) * 2009-02-04 2010-08-05 Rolls-Royce Plc Casting method
CN204247910U (en) * 2014-10-31 2015-04-08 沈阳黎明航空发动机(集团)有限责任公司 A kind of triplet that prevents is hollow without the running gate system that cracks of surplus essence casting blade
CN105290337A (en) * 2015-11-16 2016-02-03 沈阳黎明航空发动机(集团)有限责任公司 Multiple-connection-blade precision casting method
CN105364006A (en) * 2015-12-09 2016-03-02 沈阳黎明航空发动机(集团)有限责任公司 Wax mold of large-size hollow shrouded blade casting pouring system and manufacturing method of wax mold
CN107598097A (en) * 2017-11-10 2018-01-19 东方电气集团东方汽轮机有限公司 A kind of wax-pattern combination of turborotor and its fine casting method

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* Cited by examiner, † Cited by third party
Title
孙长波等: "《基于ProCAST 的大型复杂空心叶片精铸的数值模拟》", 《铸造》 *
韩宏等: "《六联体导向叶片无余量精铸技术研究》", 《铸造》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108515146A (en) * 2018-05-22 2018-09-11 株洲中航动力精密铸造有限公司 The running gate system of whole essence casting guider
CN109622888A (en) * 2018-12-20 2019-04-16 航天海鹰(哈尔滨)钛业有限公司 A kind of cast shaping process of the multi-joint guide vane casting of complexity high temperature alloy
CN110052583A (en) * 2019-03-15 2019-07-26 启东市聚旺铸造有限公司 Precise casting process of hollow guide blade
CN110640084A (en) * 2019-10-29 2020-01-03 贵州安吉航空精密铸造有限责任公司 Preparation method of investment casting shell

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Application publication date: 20180420