CN103273010A - Near net shape casting method of fine grain block casting turbine for lightweight gas turbine - Google Patents

Near net shape casting method of fine grain block casting turbine for lightweight gas turbine Download PDF

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Publication number
CN103273010A
CN103273010A CN2013101619885A CN201310161988A CN103273010A CN 103273010 A CN103273010 A CN 103273010A CN 2013101619885 A CN2013101619885 A CN 2013101619885A CN 201310161988 A CN201310161988 A CN 201310161988A CN 103273010 A CN103273010 A CN 103273010A
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CN
China
Prior art keywords
formwork
afterwards
turbine
casting
wax
Prior art date
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Pending
Application number
CN2013101619885A
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Chinese (zh)
Inventor
唐亚俊
陈建种
秦人骥
唐浩军
唐柱松
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.)
Wuxi Taiyuan Machinery Co., Ltd.
Original Assignee
WUXI SHANFA CASTING TECHNOLOGY 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 WUXI SHANFA CASTING TECHNOLOGY Co Ltd filed Critical WUXI SHANFA CASTING TECHNOLOGY Co Ltd
Priority to CN2013101619885A priority Critical patent/CN103273010A/en
Publication of CN103273010A publication Critical patent/CN103273010A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a near net shape casting method of a fine grain block casting turbine for a lightweight gas turbine, and particularly relates to a method used for casting a turbine of the lightweight gas turbine. The near net shape casting method is characterized by sequentially comprising the steps of: manufacturing a wax mould, installing and welding the wax mould, manufacturing a mould housing, dewaxing, roasting, casting under the condition of vibration, furnace cooling, removing the mould housing and eliminating sand grains on the surface of a casting, and cutting off a casting head. The fine grain block casting turbine for the lightweight gas turbine, cast by using the method, is capable of meeting the requirement on high temperature resistance; and the low cycle fatigue performance is improved, and the service life of the turbine is prolonged.

Description

Lightweight gas turbine is with the nearly clean shape casting method of thin brilliant block cast turbine
Technical field
The present invention relates to a kind of turbine casting method.Specifically, be to cast the method that lightweight gas turbine is used turbine.
Background technology
At present, being used for casting lightweight gas turbine mainly contains with the method for turbine and makes wax-pattern, wax-pattern assembly welding, makes formwork, dewaxes, carries out roasting, casts, cools off, sloughs formwork, cuts step such as dead head.Wherein, in casting cycle, formwork is fixed on the casting bed.Because when casting, formwork maintained static, and that the design feature of turbine is blade section is thinner, the core wheel section is thicker, like this, core wheel crystal grain after the casting is thicker, and blade crystal grain is thinner, is difficult to satisfy the heat-resisting quantity of turbine, particularly low cycle fatigue property descends, and has influenced the service life of turbine.
Summary of the invention
The problem to be solved in the present invention provides a kind of lightweight gas turbine with the nearly clean shape casting method of thin brilliant block cast turbine.Adopt the turbine of this method casting, can satisfy the resistance to elevated temperatures requirement of turbine, improve low cycle fatigue property, prolong the service life of turbine.
For addressing the above problem, take following technical scheme:
Lightweight gas turbine of the present invention is to may further comprise the steps successively with the near clean shape casting method characteristics of thin brilliant block cast turbine:
Make wax-pattern earlier
Utilize mould under the pressure of 43 ~ 48 temperature of spending, 0.03 ~ 0.05Mpa, to suppress wax impeller processed;
Carry out the wax-pattern assembly welding again
Dead head and wax impeller processed are welded together, obtain module;
Afterwards, make formwork
Be coated with the extension refractory material on the module surface, form formwork on the surface;
Afterwards, dewax
Be that the steam of 95 ~ 105 degree are heated to formwork with temperature, make the wax material in the formwork melt fully, deviate from, obtain formwork;
Afterwards, carry out roasting
Formwork is put into the roaster that temperature is 940 ~ 960 degree, kept 1.8 ~ 2.2 hours;
Afterwards, cast
Arrange in vacuum furnace in 80 ~ 120 rev/mins the whirling vibration platform, it is on the adjustable whirling vibration platform of 95 ~ 105 rev/mins rotating speed that baked formwork is fixed on rotating speed, is that 1570 ~ 1590 molten metal injects in the formwork with temperature; Afterwards, make that the whirling vibration platform is forward and reverse alternately to be rotated for 3 ~ 5 seconds;
Afterwards, the formwork that is cast with molten metal is carried out taking out during to the dead head surface skining with the stove cooling;
Afterwards, remove formwork and remove the sand grains of cast(ing) surface;
Afterwards, cut dead head, obtain lightweight gas turbine block cast turbine.
Described refractory material is to be mixed together form slurry with 325 purpose zirconium English powder and Ludox, and after module put into described slurry and make it be coated with full slurry and take out, and spills zircon sand again and forms.
Take such scheme, have the following advantages:
By such scheme as can be seen, be on 80 ~ 120 rev/mins the whirling vibration platform because formwork is fixed on rotating speed, after the molten metal that with temperature is 1570 ~ 1590 injects formwork, make that the whirling vibration platform is forward and reverse alternately to be rotated for 3 ~ 5 seconds.Like this, under the vibration operating mode, cast, branch crystal grain is ruptured because of rotation, make that core increases, grain refinement, make that the crystal grain difference of the blade water the turbine foundry goods that casts out and core wheel is less and thinner, its high-temperature behavior and low cycle fatigue property improve, and prolong service life.
The specific embodiment
Be described in further details below in conjunction with the present invention of embodiment.
Embodiment one
Make wax-pattern earlier.Utilize mould under the pressure of 43 temperature of spending, 0.04Mpa, to suppress wax impeller processed.
Carry out the wax-pattern assembly welding again.Dead head and wax impeller processed are welded together, obtain module.
Afterwards, make formwork.Be coated with the extension refractory material on the module surface that combines, form formwork on the module surface.Described refractory material is to be mixed together form slurry with 325 purpose zirconium English powder and Ludox, and after module put into described slurry and make it be coated with full slurry and take out, and spills zircon sand again and forms.
Afterwards, dewax.Be that 100 degrees centigrade steam is heated to formwork with temperature, make module fusing in the formwork, deviate from, obtain formwork.
Afterwards, carry out roasting.Formwork is put into the roaster that temperature is 960 degree, kept 1.8 hours.
Afterwards, cast.Arrange in vacuum furnace in 120 rev/mins the whirling vibration platform, it is on 120 rev/mins the whirling vibration platform that baked formwork is fixed on rotating speed, is that 1570 molten metal injects in the formwork with temperature.Afterwards, make that the whirling vibration platform is forward and reverse alternately to be rotated for 4 seconds.
Afterwards, the formwork that is cast with molten metal is carried out taking out during to the dead head surface skining with the stove cooling.
Afterwards, remove formwork and remove the sand grains of cast(ing) surface.
Afterwards, cut dead head, obtain lightweight gas turbine with thin brilliant block cast turbine.
Embodiment two
Make wax-pattern earlier.Utilize mould under the pressure of 45 temperature of spending, 0.03Mpa, to suppress wax impeller processed.
Carry out the wax-pattern assembly welding again.Dead head and wax impeller processed are welded together, obtain module.
Afterwards, make formwork.Be coated with the extension refractory material on the module surface that combines, form formwork on the module surface.Described refractory material is to be mixed together form slurry with 325 purpose zirconium English powder and Ludox, and after module put into described slurry and make it be coated with full slurry and take out, and spills zircon sand again and forms.
Afterwards, dewax.Be that 105 degrees centigrade steam is heated to formwork with temperature, make module fusing in the formwork, deviate from, obtain formwork.
Afterwards, carry out roasting.Formwork is put into the roaster that temperature is 950 degree, kept 2.0 hours.
Afterwards, cast.Arrange in vacuum furnace in 80 rev/mins the whirling vibration platform, it is on 80 rev/mins the whirling vibration platform that baked formwork is fixed on rotating speed, is that 1580 molten metal injects in the formwork with temperature.Afterwards, make that the whirling vibration platform is forward and reverse alternately to be rotated for 5 seconds.
Afterwards, the formwork that is cast with molten metal is carried out taking out during to the dead head surface skining with the stove cooling.
Afterwards, remove formwork and remove the sand grains of cast(ing) surface.
Afterwards, cut dead head, obtain lightweight gas turbine with thin brilliant block cast turbine.
Embodiment three
Make wax-pattern earlier.Utilize mould under the pressure of 48 temperature of spending, 0.05Mpa, to suppress wax impeller processed.
Carry out the wax-pattern assembly welding again.Dead head and wax impeller processed are welded together, obtain module.
Afterwards, make formwork.Be coated with the extension refractory material on the module surface that combines, form formwork on the module surface.Described refractory material is to be mixed together form slurry with 325 purpose zirconium English powder and Ludox, and after module put into described slurry and make it be coated with full slurry and take out, and spills zircon sand again and forms.
Afterwards, dewax.Be that 95 degrees centigrade steam is heated to formwork with temperature, make module fusing in the formwork, deviate from, obtain formwork.
Afterwards, carry out roasting.Formwork is put into the roaster that temperature is 950 degree, kept 2.2 hours.
Afterwards, cast.Arrange in vacuum furnace in 100 rev/mins the whirling vibration platform, it is on 100 rev/mins the whirling vibration platform that baked formwork is fixed on rotating speed, is that 1590 molten metal injects in the formwork with temperature.Afterwards, make that the whirling vibration platform is forward and reverse alternately to be rotated for 3 seconds.
Afterwards, the formwork that is cast with molten metal is carried out taking out during to the dead head surface skining with the stove cooling.
Afterwards, remove formwork and remove the sand grains of cast(ing) surface.
Afterwards, cut dead head, obtain lightweight gas turbine with thin brilliant block cast turbine.

Claims (2)

1. lightweight gas turbine is characterized in that may further comprise the steps successively with the nearly clean shape casting method of thin brilliant block cast turbine:
Make wax-pattern earlier
Utilize mould under the pressure of 43 ~ 48 temperature of spending, 0.03 ~ 0.05Mpa, to suppress wax impeller processed;
Carry out the wax-pattern assembly welding again
Dead head and wax impeller processed are welded together, obtain module;
Afterwards, make formwork
Be coated with the extension refractory material on the module surface, form formwork on the surface;
Afterwards, dewax
Be that the steam of 95 ~ 105 degree are heated to formwork with temperature, make the wax material in the formwork melt fully, deviate from, obtain formwork;
Afterwards, carry out roasting
Formwork is put into the roaster that temperature is 940 ~ 960 degree, kept 1.8 ~ 2.2 hours;
Afterwards, cast
Arrange in vacuum furnace in 80 ~ 120 rev/mins the whirling vibration platform, it is on the adjustable whirling vibration platform of 95 ~ 105 rev/mins rotating speed that baked formwork is fixed on rotating speed, is that 1570 ~ 1590 molten metal injects in the formwork with temperature; Afterwards, make that the whirling vibration platform is forward and reverse alternately to be rotated for 3 ~ 5 seconds;
Afterwards, the formwork that is cast with molten metal is carried out taking out during to the dead head surface skining with the stove cooling;
Afterwards, remove formwork and remove the sand grains of cast(ing) surface;
Afterwards, cut dead head, obtain lightweight gas turbine block cast turbine.
2. lightweight gas turbine according to claim 1 is with the nearly clean shape casting method of thin brilliant block cast turbine, it is characterized in that described refractory material is to be mixed together form slurry with 325 purpose zirconium English powder and Ludox, and after module put into described slurry and make it be coated with full slurry and take out, spill zircon sand again and form.
CN2013101619885A 2013-05-06 2013-05-06 Near net shape casting method of fine grain block casting turbine for lightweight gas turbine Pending CN103273010A (en)

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Application Number Priority Date Filing Date Title
CN2013101619885A CN103273010A (en) 2013-05-06 2013-05-06 Near net shape casting method of fine grain block casting turbine for lightweight gas turbine

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103658536A (en) * 2014-01-06 2014-03-26 山东建筑大学 Fired mold low-pressure casting process of integral type compressor impeller
CN104148583A (en) * 2014-08-20 2014-11-19 无锡柯马机械有限公司 Investment casting method
CN104399884A (en) * 2014-10-22 2015-03-11 江苏美特林科特殊合金有限公司 Casting process of turbine of turbocharger for gasoline engine
CN105710303A (en) * 2016-04-01 2016-06-29 北京昌航精铸技术有限公司 Vacuum vibration precise casting device and method of high-temperature alloy
CN106077561A (en) * 2016-08-22 2016-11-09 浙江遂金特种铸造有限公司 Low speed synchronous belt pulley casting technique
CN108500207A (en) * 2017-02-27 2018-09-07 上海中洲特种合金材料股份有限公司 investment casting method
CN108555237A (en) * 2018-04-18 2018-09-21 常州环能涡轮动力股份有限公司 The preparation method of turbine and turbine wax-pattern

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2264054Y (en) * 1996-06-05 1997-10-08 天津大学 Compound movable electroslag smelting casting
EP0924008A1 (en) * 1997-12-22 1999-06-23 Ford Global Technologies, Inc. Rapidly forming complex hollow shapes using lost wax investment casting
CN1683099A (en) * 2005-02-02 2005-10-19 哈尔滨鑫润精铸工业有限公司 Fine casting method for super long lower pressure partition guide blade of turbine in stainless steel investment mold
CN201008963Y (en) * 2007-03-23 2008-01-23 韶关市伟光液压机械有限公司 Equipment for vibration-casting metal casting
CN101181746A (en) * 2007-11-23 2008-05-21 华中科技大学 Lost foam casting vibration clotting method
CN101602090A (en) * 2009-01-20 2009-12-16 无锡益通机械科技有限公司 The manufacturing process of cylinder body of material press oil cylinder
CN102019348A (en) * 2010-12-30 2011-04-20 沈阳黎明航空发动机(集团)有限责任公司 Preparation method of low pressure guide connected hollow blade
CN102581245A (en) * 2011-01-11 2012-07-18 中国科学院金属研究所 Multifunctional vacuum centrifugal oscillating fine grain melting and casting furnace
CN102974748A (en) * 2012-11-29 2013-03-20 沈阳铸造研究所 Precise casting method of ceramic mould of turbine casing, namely critical component of heavy-duty gas turbine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2264054Y (en) * 1996-06-05 1997-10-08 天津大学 Compound movable electroslag smelting casting
EP0924008A1 (en) * 1997-12-22 1999-06-23 Ford Global Technologies, Inc. Rapidly forming complex hollow shapes using lost wax investment casting
CN1683099A (en) * 2005-02-02 2005-10-19 哈尔滨鑫润精铸工业有限公司 Fine casting method for super long lower pressure partition guide blade of turbine in stainless steel investment mold
CN201008963Y (en) * 2007-03-23 2008-01-23 韶关市伟光液压机械有限公司 Equipment for vibration-casting metal casting
CN101181746A (en) * 2007-11-23 2008-05-21 华中科技大学 Lost foam casting vibration clotting method
CN101602090A (en) * 2009-01-20 2009-12-16 无锡益通机械科技有限公司 The manufacturing process of cylinder body of material press oil cylinder
CN102019348A (en) * 2010-12-30 2011-04-20 沈阳黎明航空发动机(集团)有限责任公司 Preparation method of low pressure guide connected hollow blade
CN102581245A (en) * 2011-01-11 2012-07-18 中国科学院金属研究所 Multifunctional vacuum centrifugal oscillating fine grain melting and casting furnace
CN102974748A (en) * 2012-11-29 2013-03-20 沈阳铸造研究所 Precise casting method of ceramic mould of turbine casing, namely critical component of heavy-duty gas turbine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
中国铸造协会: "《熔模铸造手册》", 31 October 2000, article "熔模铸造手册" *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103658536A (en) * 2014-01-06 2014-03-26 山东建筑大学 Fired mold low-pressure casting process of integral type compressor impeller
CN104148583A (en) * 2014-08-20 2014-11-19 无锡柯马机械有限公司 Investment casting method
CN104399884A (en) * 2014-10-22 2015-03-11 江苏美特林科特殊合金有限公司 Casting process of turbine of turbocharger for gasoline engine
CN105710303A (en) * 2016-04-01 2016-06-29 北京昌航精铸技术有限公司 Vacuum vibration precise casting device and method of high-temperature alloy
CN106077561A (en) * 2016-08-22 2016-11-09 浙江遂金特种铸造有限公司 Low speed synchronous belt pulley casting technique
CN108500207A (en) * 2017-02-27 2018-09-07 上海中洲特种合金材料股份有限公司 investment casting method
CN108555237A (en) * 2018-04-18 2018-09-21 常州环能涡轮动力股份有限公司 The preparation method of turbine and turbine wax-pattern

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Address after: Huishan District of Jiangsu city in Wuxi Province, 214181 former State Street Yang Jia Wei Cun

Applicant after: Wuxi Taiyuan Machinery Co., Ltd.

Address before: 214174 Jiangsu province Wuxi city Huishan District Yanqiao Industrial Park Yanqiao Road No. 35

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Application publication date: 20130904