DE2536751C3 - Verfahren zum Gießen von Hohlgußkörpern aus Hochtemperaturlegierungen, insbesondere Turbinenschaufeln - Google Patents

Verfahren zum Gießen von Hohlgußkörpern aus Hochtemperaturlegierungen, insbesondere Turbinenschaufeln

Info

Publication number
DE2536751C3
DE2536751C3 DE2536751A DE2536751A DE2536751C3 DE 2536751 C3 DE2536751 C3 DE 2536751C3 DE 2536751 A DE2536751 A DE 2536751A DE 2536751 A DE2536751 A DE 2536751A DE 2536751 C3 DE2536751 C3 DE 2536751C3
Authority
DE
Germany
Prior art keywords
core
model
turbine blades
marks
temperature alloys
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
Application number
DE2536751A
Other languages
German (de)
English (en)
Other versions
DE2536751B2 (de
DE2536751A1 (de
Inventor
Charles Merrick Ridgewood N.J. Phipps
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE2536751A1 publication Critical patent/DE2536751A1/de
Publication of DE2536751B2 publication Critical patent/DE2536751B2/de
Application granted granted Critical
Publication of DE2536751C3 publication Critical patent/DE2536751C3/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/02—Sand moulds or like moulds for shaped castings
    • B22C9/04—Use of lost patterns
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Turning (AREA)
  • Hinges (AREA)
  • Chairs Characterized By Structure (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
DE2536751A 1974-08-21 1975-08-18 Verfahren zum Gießen von Hohlgußkörpern aus Hochtemperaturlegierungen, insbesondere Turbinenschaufeln Expired DE2536751C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/499,227 US3981344A (en) 1974-08-21 1974-08-21 Investment casting mold and process

Publications (3)

Publication Number Publication Date
DE2536751A1 DE2536751A1 (de) 1976-03-04
DE2536751B2 DE2536751B2 (de) 1981-02-05
DE2536751C3 true DE2536751C3 (de) 1981-10-08

Family

ID=23984372

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2536751A Expired DE2536751C3 (de) 1974-08-21 1975-08-18 Verfahren zum Gießen von Hohlgußkörpern aus Hochtemperaturlegierungen, insbesondere Turbinenschaufeln

Country Status (17)

Country Link
US (1) US3981344A (enExample)
JP (1) JPS5726853B2 (enExample)
AR (1) AR207872A1 (enExample)
BE (1) BE832534A (enExample)
BR (1) BR7505255A (enExample)
CA (1) CA1064220A (enExample)
CH (1) CH604966A5 (enExample)
DE (1) DE2536751C3 (enExample)
ES (1) ES440339A1 (enExample)
FR (1) FR2282311A1 (enExample)
GB (1) GB1508888A (enExample)
IL (1) IL47904A (enExample)
IT (1) IT1041960B (enExample)
NL (1) NL171780C (enExample)
NO (2) NO142990C (enExample)
SE (2) SE421180B (enExample)
ZA (1) ZA755051B (enExample)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4148352A (en) 1975-08-15 1979-04-10 Nissan Motor Company, Limited Method of preparing an exhaust port arrangement of a cylinder head
IT1096996B (it) * 1977-07-22 1985-08-26 Rolls Royce Metodo per la fabbricazione di una pala o lama per motori a turbina a gas
US4195396A (en) * 1977-12-15 1980-04-01 Trw Inc. Method of forming an airfoil with inner and outer shroud sections
US4276922A (en) * 1978-05-24 1981-07-07 Trw Inc. Plug mold assembly
GB2028928B (en) * 1978-08-17 1982-08-25 Ross Royce Ltd Aerofoil blade for a gas turbine engine
US4549599A (en) * 1978-10-19 1985-10-29 United Technologies Corporation Preventing mold and casting cracking in high rate directional solidification processes
GB2050918B (en) * 1979-06-06 1982-12-15 Rolls Royce Manufacture and inspection of an article
US4289191A (en) * 1980-04-02 1981-09-15 United Technologies Corporation Injection molding thermoplastic patterns having ceramic cores
US4283835A (en) * 1980-04-02 1981-08-18 United Technologies Corporation Cambered core positioning for injection molding
US4375282A (en) * 1980-06-30 1983-03-01 United Technologies Corporation Core configuration for casting hollow parts in mating halves
GB2096525B (en) * 1981-04-14 1984-09-12 Rolls Royce Manufacturing gas turbine engine blades
GB2108879A (en) * 1981-08-12 1983-05-25 Rolls Royce Foundry machinery
JPS5884143A (ja) * 1981-11-10 1983-05-20 Natl Inst For Res In Inorg Mater 低膨張ガラス組成物
EP0084234A1 (en) * 1981-12-16 1983-07-27 Vickers Plc Investment casting process and mould
JPH0639338B2 (ja) * 1986-06-20 1994-05-25 日本電気硝子株式会社 繊維用ガラス組成物
JPS6349343A (ja) * 1986-08-14 1988-03-02 Nobuyoshi Sasaki 中子、その製造方法およびインベストメント鋳造用鋳型の製造方法
JPH0193437A (ja) * 1987-10-05 1989-04-12 Nippon Sheet Glass Co Ltd 低膨脹ガラス
GB8800686D0 (en) * 1988-01-13 1988-02-10 Rolls Royce Plc Method of supporting core in mould
ES2046078B1 (es) * 1991-07-08 1995-10-01 Metalogenia Sa Perfeccionamientos en la fabricacion de piezas moldeadas de acero, dotadas de cavidades interiores.
US5291654A (en) * 1993-03-29 1994-03-08 United Technologies Corporation Method for producing hollow investment castings
US5607007A (en) * 1994-10-19 1997-03-04 Hitchiner Manufacturing Co., Inc. Directional solidification apparatus and method
US5662160A (en) * 1995-10-12 1997-09-02 General Electric Co. Turbine nozzle and related casting method for optimal fillet wall thickness control
US6325871B1 (en) 1997-10-27 2001-12-04 Siemens Westinghouse Power Corporation Method of bonding cast superalloys
JP4240808B2 (ja) 1997-10-27 2009-03-18 シーメンス パワー ジェネレイション インコーポレイテッド タービン翼の製造方法
US20050000674A1 (en) * 2003-07-01 2005-01-06 Beddard Thomas Bradley Perimeter-cooled stage 1 bucket core stabilizing device and related method
DE102004062174A1 (de) * 2004-12-17 2006-06-22 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung von hoch belastbaren Bauteilen durch Präzisionsschmieden
US20070074839A1 (en) * 2005-10-03 2007-04-05 United Technologies Corporation Method for manufacturing a pattern for a hollow component
US7918265B2 (en) * 2008-02-14 2011-04-05 United Technologies Corporation Method and apparatus for as-cast seal on turbine blades
US20100238967A1 (en) * 2009-03-18 2010-09-23 Bullied Steven J Method of producing a fine grain casting
US8240355B2 (en) * 2010-01-29 2012-08-14 United Technologies Corporation Forming a cast component with agitation
FR2957545B1 (fr) * 2010-03-19 2012-07-27 Snecma Procede de realisation d'un insert metallique pour la protection d'un bord d'attaque en materiau composite
FR3035604B1 (fr) * 2015-04-30 2023-01-13 Snecma Procede de fabrication de modele pour fonderie a modele perdu
CN106001513B (zh) * 2016-04-19 2018-04-13 中国航空工业集团公司北京航空材料研究院 一种熔模精密铸造单晶高温合金薄壁试样的制备方法
CN107008857B (zh) * 2017-04-17 2020-11-10 东方电气集团东方汽轮机有限公司 可消除变截面零件铸造热裂缺陷的陶瓷模壳及其成型方法
FR3068271B1 (fr) 2017-06-29 2021-12-10 Safran Aircraft Engines Procede de fonderie avec coulee en moule chaud
CN107584084A (zh) * 2017-09-12 2018-01-16 东方电气集团东方汽轮机有限公司 空心叶片精铸用陶瓷模壳成型方法
CN114425598B (zh) * 2021-12-31 2023-10-27 北京航空材料研究院股份有限公司 一种含异型缝隙孔的钛及钛合金铸件制备方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB678035A (en) * 1950-03-17 1952-08-27 Rolls Royce Improvements in processes for precision castings
US2782476A (en) * 1952-10-16 1957-02-26 Joseph B Brennan Apparatus for casting air foils and the like
US2912729A (en) * 1956-07-24 1959-11-17 John M Webb Refractory molds
US3669177A (en) * 1969-09-08 1972-06-13 Howmet Corp Shell manufacturing method for precision casting
US3627015A (en) * 1970-06-01 1971-12-14 Hughes Aircraft Co Cocoon casting of directionally solidified articles
DE2301105C2 (de) * 1973-01-10 1984-07-05 Sherwood Refractories Inc., Cleveland, Ohio Präzisionsgußform und Verfahren zu deren Herstellung

Also Published As

Publication number Publication date
ZA755051B (en) 1976-07-28
NL171780B (nl) 1982-12-16
NO752857L (enExample) 1976-02-24
AU8366675A (en) 1977-02-10
BR7505255A (pt) 1976-08-03
GB1508888A (en) 1978-04-26
DE2536751B2 (de) 1981-02-05
US3981344A (en) 1976-09-21
ES440339A1 (es) 1977-03-01
DE2536751A1 (de) 1976-03-04
NO142990C (no) 1980-11-26
SE421180B (sv) 1981-12-07
SE7902076L (sv) 1979-03-08
IT1041960B (it) 1980-01-10
AR207872A1 (es) 1976-11-08
CH604966A5 (enExample) 1978-09-15
FR2282311B1 (enExample) 1982-01-22
SE432546B (sv) 1984-04-09
IL47904A (en) 1980-01-31
NL171780C (nl) 1983-05-16
NO791336L (no) 1976-02-24
IL47904A0 (en) 1975-11-25
NO143610C (no) 1981-03-18
FR2282311A1 (fr) 1976-03-19
NO142990B (no) 1980-08-18
NL7509246A (nl) 1976-02-24
CA1064220A (en) 1979-10-16
USB499227I5 (enExample) 1976-01-27
JPS5726853B2 (enExample) 1982-06-07
JPS5146523A (enExample) 1976-04-21
SE7509056L (sv) 1976-02-23
BE832534A (fr) 1975-12-16
NO143610B (no) 1980-12-08

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Legal Events

Date Code Title Description
OD Request for examination
C3 Grant after two publication steps (3rd publication)