GB0327462D0 - An arrangement for providing heat to a portion of a component of a gas turbine engine - Google Patents

An arrangement for providing heat to a portion of a component of a gas turbine engine

Info

Publication number
GB0327462D0
GB0327462D0 GBGB0327462.8A GB0327462A GB0327462D0 GB 0327462 D0 GB0327462 D0 GB 0327462D0 GB 0327462 A GB0327462 A GB 0327462A GB 0327462 D0 GB0327462 D0 GB 0327462D0
Authority
GB
United Kingdom
Prior art keywords
arrangement
component
gas turbine
turbine engine
providing heat
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.)
Ceased
Application number
GBGB0327462.8A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GBGB0327462.8A priority Critical patent/GB0327462D0/en
Publication of GB0327462D0 publication Critical patent/GB0327462D0/en
Priority to EP04256739A priority patent/EP1535679A1/en
Priority to US10/978,429 priority patent/US20050109480A1/en
Priority to US11/294,408 priority patent/US20060090822A1/en
Ceased 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GBGB0327462.8A 2003-11-26 2003-11-26 An arrangement for providing heat to a portion of a component of a gas turbine engine Ceased GB0327462D0 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GBGB0327462.8A GB0327462D0 (en) 2003-11-26 2003-11-26 An arrangement for providing heat to a portion of a component of a gas turbine engine
EP04256739A EP1535679A1 (en) 2003-11-26 2004-11-01 An arrangement for providing heat to a portion of a component
US10/978,429 US20050109480A1 (en) 2003-11-26 2004-11-02 Arrangement for providing heat to a portion of a component
US11/294,408 US20060090822A1 (en) 2003-11-26 2005-12-06 Arrangement for providing heat to a portion of a component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0327462.8A GB0327462D0 (en) 2003-11-26 2003-11-26 An arrangement for providing heat to a portion of a component of a gas turbine engine

Publications (1)

Publication Number Publication Date
GB0327462D0 true GB0327462D0 (en) 2003-12-31

Family

ID=29797828

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0327462.8A Ceased GB0327462D0 (en) 2003-11-26 2003-11-26 An arrangement for providing heat to a portion of a component of a gas turbine engine

Country Status (3)

Country Link
US (2) US20050109480A1 (en)
EP (1) EP1535679A1 (en)
GB (1) GB0327462D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2432133A (en) * 2005-11-15 2007-05-16 Rolls Royce Plc A feeder for a cast turbine blade

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1173732B (en) * 1960-06-08 1964-07-09 Gen Motors Corp Cast turbine blade
NL136758C (en) * 1963-10-21 1900-01-01
US3921271A (en) * 1973-01-02 1975-11-25 Gen Electric Air-cooled turbine blade and method of making same
US4804311A (en) * 1981-12-14 1989-02-14 United Technologies Corporation Transverse directional solidification of metal single crystal articles
FR2734188B1 (en) * 1982-09-28 1997-07-18 Snecma PROCESS FOR MANUFACTURING MONOCRYSTALLINE PARTS
DE8438413U1 (en) * 1984-10-27 1986-06-12 Hauni-Werke Körber & Co KG, 2050 Hamburg Device for the production of a cast-in clamping block for multi-part workpieces, in particular for turbine blades
DE4022389C2 (en) * 1990-07-13 1995-06-08 Leybold Ag Melting and pouring furnace
GB2259660A (en) * 1991-09-17 1993-03-24 Rolls Royce Plc A mould for casting components
GB9121364D0 (en) * 1991-10-09 1991-11-20 Rolls Royce Plc A mould for casting components
US5295530A (en) * 1992-02-18 1994-03-22 General Motors Corporation Single-cast, high-temperature, thin wall structures and methods of making the same
US5568833A (en) * 1995-06-07 1996-10-29 Allison Engine Company, Inc. Method and apparatus for directional solidification of integral component casting
US6217286B1 (en) * 1998-06-26 2001-04-17 General Electric Company Unidirectionally solidified cast article and method of making
US6276432B1 (en) * 1999-06-10 2001-08-21 Howmet Research Corporation Directional solidification method and apparatus
EP1076119A1 (en) * 1999-08-11 2001-02-14 ABB Alstom Power (Schweiz) AG Apparatus and method for manufacture a directionally solidified columnar grained article
US6497272B1 (en) * 1999-10-14 2002-12-24 Howmet Research Corporation Single crystal casting mold
US6619373B1 (en) * 2002-04-25 2003-09-16 General Motors Corporation Lost foam casting apparatus for reducing porosity and inclusions in metal castings

Also Published As

Publication number Publication date
EP1535679A1 (en) 2005-06-01
US20050109480A1 (en) 2005-05-26
US20060090822A1 (en) 2006-05-04

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)