BR7409588A - Molde para producao de pas de turbina ocas e processo para fabricacao das mesmas - Google Patents

Molde para producao de pas de turbina ocas e processo para fabricacao das mesmas

Info

Publication number
BR7409588A
BR7409588A BR9588/74A BR958874A BR7409588A BR 7409588 A BR7409588 A BR 7409588A BR 9588/74 A BR9588/74 A BR 9588/74A BR 958874 A BR958874 A BR 958874A BR 7409588 A BR7409588 A BR 7409588A
Authority
BR
Brazil
Prior art keywords
template
manufacture
production
turbine blades
hollow turbine
Prior art date
Application number
BR9588/74A
Other languages
English (en)
Portuguese (pt)
Inventor
C Phipps
D Hayes
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 BR7409588A publication Critical patent/BR7409588A/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • B22D27/045Directionally solidified castings
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-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
    • C30B11/00Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
    • C30B11/002Crucibles or containers for supporting the melt
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (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)
BR9588/74A 1973-11-16 1974-11-14 Molde para producao de pas de turbina ocas e processo para fabricacao das mesmas BR7409588A (pt)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BR7409588A true BR7409588A (pt) 1976-05-25

Family

ID=23650446

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9588/74A BR7409588A (pt) 1973-11-16 1974-11-14 Molde para producao de pas de turbina ocas e processo para fabricacao das mesmas

Country Status (14)

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

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2518155C2 (de) * 1975-04-24 1984-05-24 Klöckner-Humboldt-Deutz AG, 5000 Köln Gießform in geteilter, wiederverwendbarer Ausführung
GB2121115A (en) * 1982-06-03 1983-12-14 Rolls Royce Aerofoil vane assembly
FR2698126B1 (fr) * 1992-11-18 1994-12-16 Snecma Aube creuse de soufflante ou compresseur de turbomachine.
DE19726111C1 (de) * 1997-06-20 1998-11-12 Mtu Muenchen Gmbh Verfahren zur gießtechnischen Herstellung einer Turbomaschinenschaufel
DE19926575C2 (de) * 1999-06-11 2003-04-17 Porsche Ag Rad für ein Kraftfahrzeug
US6257831B1 (en) 1999-10-22 2001-07-10 Pratt & Whitney Canada Corp. Cast airfoil structure with openings which do not require plugging
DE10064268A1 (de) * 2000-12-22 2002-07-04 Alstom Switzerland Ltd Werkzeug und Verfahren zum Giessen eines Formteils für die Herstellung einer Turbinenschaufel
DE10064267A1 (de) 2000-12-22 2002-07-04 Alstom Switzerland Ltd Verfahren zum schnellen Herstellen von hohlen Turbinenschaufeln für die Fertigungsentwicklung und Bauteiltests
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
IL45616A (en) 1979-10-31
DE2453090C3 (de) 1980-04-03
FR2251392B1 (it) 1979-03-02
SE408622B (sv) 1979-06-25
BE821315A (fr) 1975-02-17
GB1471963A (en) 1977-04-27
AU7422374A (en) 1976-04-15
JPS5080918A (it) 1975-07-01
FR2251392A1 (it) 1975-06-13
ZA745190B (en) 1975-08-27
SE7412578L (it) 1975-05-20
CA1030322A (en) 1978-05-02
NL7413004A (nl) 1975-05-21
JPS5622624B2 (it) 1981-05-26
DE2453090A1 (de) 1975-05-22
DE2453090B2 (de) 1979-07-26
IL45616A0 (en) 1974-11-29
ES432010A1 (es) 1976-10-16
IT1025729B (it) 1978-08-30
CH596917A5 (it) 1978-03-31

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