ES432010A1 - Mould for use in the manufacture of hollow turbine blades and method of use thereof - Google Patents

Mould for use in the manufacture of hollow turbine blades and method of use thereof

Info

Publication number
ES432010A1
ES432010A1 ES432010A ES432010A ES432010A1 ES 432010 A1 ES432010 A1 ES 432010A1 ES 432010 A ES432010 A ES 432010A ES 432010 A ES432010 A ES 432010A ES 432010 A1 ES432010 A1 ES 432010A1
Authority
ES
Spain
Prior art keywords
mold
blade
turbine blades
manufacture
outer edges
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
ES432010A
Other languages
Spanish (es)
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 Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Publication of ES432010A1 publication Critical patent/ES432010A1/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • B22D27/045—Directionally solidified castings
    • C—CHEMISTRY; METALLURGY
    • C30—CRYSTAL GROWTH
    • C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
    • C30B11/002—Crucibles or containers for supporting the melt
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

Improvements in the molds to manufacture hollow turbine blades, characterized in that the mold includes: a central mold element having on each side at least part of the configuration of the hollow interior of the blade; opposing outer mold elements cooperating with the central member on opposite sides thereof, each outer mold element having an inner wall surface corresponding to a finished blade surface; said central mold element having outer edges extending beyond the blade configuration thereon and said outer elements having similar outer edges extending beyond the blade surface thereon, said outer edges of the elements cooperating of mold with each other for coupling to each other to form the finished mold and to separate opposing cooperating surfaces from the mold cavity. (Machine-translation by Google Translate, not legally binding)
ES432010A 1973-11-16 1974-11-16 Mould for use in the manufacture of hollow turbine blades and method of use thereof Expired ES432010A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US41656373A 1973-11-16 1973-11-16

Publications (1)

Publication Number Publication Date
ES432010A1 true ES432010A1 (en) 1976-10-16

Family

ID=23650446

Family Applications (1)

Application Number Title Priority Date Filing Date
ES432010A Expired ES432010A1 (en) 1973-11-16 1974-11-16 Mould for use in the manufacture of hollow turbine blades and method of use thereof

Country Status (14)

Country Link
JP (1) JPS5622624B2 (en)
BE (1) BE821315A (en)
BR (1) BR7409588A (en)
CA (1) CA1030322A (en)
CH (1) CH596917A5 (en)
DE (1) DE2453090C3 (en)
ES (1) ES432010A1 (en)
FR (1) FR2251392B1 (en)
GB (1) GB1471963A (en)
IL (1) IL45616A (en)
IT (1) IT1025729B (en)
NL (1) NL7413004A (en)
SE (1) SE408622B (en)
ZA (1) ZA745190B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2518155C2 (en) * 1975-04-24 1984-05-24 Klöckner-Humboldt-Deutz AG, 5000 Köln Casting mold in split, reusable design
GB2121115A (en) * 1982-06-03 1983-12-14 Rolls Royce Aerofoil vane assembly
FR2698126B1 (en) * 1992-11-18 1994-12-16 Snecma Hollow fan blade or turbomachine compressor.
DE19726111C1 (en) * 1997-06-20 1998-11-12 Mtu Muenchen Gmbh Process for the production of a turbomachine blade by casting
DE19926575C2 (en) * 1999-06-11 2003-04-17 Porsche Ag Wheel for a motor vehicle
US6257831B1 (en) * 1999-10-22 2001-07-10 Pratt & Whitney Canada Corp. Cast airfoil structure with openings which do not require plugging
DE10064267A1 (en) 2000-12-22 2002-07-04 Alstom Switzerland Ltd Process for quickly manufacturing hollow turbine blades for manufacturing development and component testing
DE10064268A1 (en) * 2000-12-22 2002-07-04 Alstom Switzerland Ltd Tool and method for casting a molded part for the manufacture of a turbine blade
US20050000674A1 (en) * 2003-07-01 2005-01-06 Beddard Thomas Bradley Perimeter-cooled stage 1 bucket core stabilizing device and related method

Also Published As

Publication number Publication date
GB1471963A (en) 1977-04-27
AU7422374A (en) 1976-04-15
FR2251392A1 (en) 1975-06-13
DE2453090B2 (en) 1979-07-26
FR2251392B1 (en) 1979-03-02
JPS5080918A (en) 1975-07-01
BE821315A (en) 1975-02-17
ZA745190B (en) 1975-08-27
BR7409588A (en) 1976-05-25
NL7413004A (en) 1975-05-21
DE2453090A1 (en) 1975-05-22
SE7412578L (en) 1975-05-20
CA1030322A (en) 1978-05-02
CH596917A5 (en) 1978-03-31
SE408622B (en) 1979-06-25
JPS5622624B2 (en) 1981-05-26
DE2453090C3 (en) 1980-04-03
IL45616A (en) 1979-10-31
IL45616A0 (en) 1974-11-29
IT1025729B (en) 1978-08-30

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