DE60235863D1 - Verfahren zum Bilden eines geformten Loches - Google Patents

Verfahren zum Bilden eines geformten Loches

Info

Publication number
DE60235863D1
DE60235863D1 DE60235863T DE60235863T DE60235863D1 DE 60235863 D1 DE60235863 D1 DE 60235863D1 DE 60235863 T DE60235863 T DE 60235863T DE 60235863 T DE60235863 T DE 60235863T DE 60235863 D1 DE60235863 D1 DE 60235863D1
Authority
DE
Germany
Prior art keywords
forming
shaped hole
shaped
hole
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 - Lifetime
Application number
DE60235863T
Other languages
English (en)
Inventor
Pamela J Byrd
Neil K Hastilow
Martin J Stevens
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
Application granted granted Critical
Publication of DE60235863D1 publication Critical patent/DE60235863D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • F01D5/186—Film cooling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36—Removing material
    • B23K26/38—Removing material by boring or cutting
    • B23K26/382—Removing material by boring or cutting by boring
    • B23K26/384—Removing material by boring or cutting by boring of specially shaped holes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/36—Removing material
    • B23K26/38—Removing material by boring or cutting
    • B23K26/382—Removing material by boring or cutting by boring
    • B23K26/389—Removing material by boring or cutting by boring of fluid openings, e.g. nozzles, jets
    • 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
    • F05D2230/10—Manufacture by removing material
    • F05D2230/13—Manufacture by removing material using lasers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • Laser Beam Processing (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60235863T 2001-10-30 2002-10-28 Verfahren zum Bilden eines geformten Loches Expired - Lifetime DE60235863D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0126006A GB2381489B (en) 2001-10-30 2001-10-30 Method of forming a shaped hole

Publications (1)

Publication Number Publication Date
DE60235863D1 true DE60235863D1 (de) 2010-05-20

Family

ID=9924773

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60235863T Expired - Lifetime DE60235863D1 (de) 2001-10-30 2002-10-28 Verfahren zum Bilden eines geformten Loches

Country Status (4)

Country Link
US (2) US6781091B2 (de)
EP (1) EP1308236B1 (de)
DE (1) DE60235863D1 (de)
GB (1) GB2381489B (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2395157B (en) * 2002-11-15 2005-09-07 Rolls Royce Plc Laser driliing shaped holes
US7223072B2 (en) * 2004-01-27 2007-05-29 Honeywell International, Inc. Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
US7540083B2 (en) * 2005-09-28 2009-06-02 Honeywell International Inc. Method to modify an airfoil internal cooling circuit
US20090003987A1 (en) * 2006-12-21 2009-01-01 Jack Raul Zausner Airfoil with improved cooling slot arrangement
US8007237B2 (en) 2006-12-29 2011-08-30 Pratt & Whitney Canada Corp. Cooled airfoil component
US7812282B2 (en) * 2007-03-15 2010-10-12 Honeywell International Inc. Methods of forming fan-shaped effusion holes in combustors
US7820267B2 (en) * 2007-08-20 2010-10-26 Honeywell International Inc. Percussion drilled shaped through hole and method of forming
US20090169394A1 (en) * 2007-12-28 2009-07-02 General Electric Company Method of forming cooling holes and turbine airfoil with hybrid-formed cooling holes
US10189100B2 (en) 2008-07-29 2019-01-29 Pratt & Whitney Canada Corp. Method for wire electro-discharge machining a part
JP5839994B2 (ja) * 2009-02-27 2016-01-06 ピコドリル エスアー 基板中にホール又は凹部又はくぼみを発生させる方法、該方法を実行するためのデバイス及び該デバイスで用いる高周波高電圧源
US8319146B2 (en) * 2009-05-05 2012-11-27 General Electric Company Method and apparatus for laser cutting a trench
US8925201B2 (en) * 2009-06-29 2015-01-06 Pratt & Whitney Canada Corp. Method and apparatus for providing rotor discs
US20120205355A1 (en) * 2009-08-17 2012-08-16 Muenzer Jan Method for producing an asymmetric diffuser using different laser positions
EP2286955B1 (de) * 2009-08-17 2012-06-13 Siemens Aktiengesellschaft Verfahren zur Herstellung eines Lochs unter Verwendung verschiedener Laserstellungen
US20110097191A1 (en) * 2009-10-28 2011-04-28 General Electric Company Method and structure for cooling airfoil surfaces using asymmetric chevron film holes
US9890647B2 (en) * 2009-12-29 2018-02-13 Rolls-Royce North American Technologies Inc. Composite gas turbine engine component
US8857055B2 (en) * 2010-01-29 2014-10-14 General Electric Company Process and system for forming shaped air holes
EP2712700A1 (de) * 2010-05-04 2014-04-02 Siemens Aktiengesellschaft Laserbohren ohne Gratbildung
US8905713B2 (en) 2010-05-28 2014-12-09 General Electric Company Articles which include chevron film cooling holes, and related processes
US20120102959A1 (en) * 2010-10-29 2012-05-03 John Howard Starkweather Substrate with shaped cooling holes and methods of manufacture
US9696035B2 (en) 2010-10-29 2017-07-04 General Electric Company Method of forming a cooling hole by laser drilling
US9157328B2 (en) 2010-12-24 2015-10-13 Rolls-Royce North American Technologies, Inc. Cooled gas turbine engine component
EP2568118A1 (de) * 2011-09-12 2013-03-13 Siemens Aktiengesellschaft Gasturbinenkomponente
US9931712B2 (en) 2012-01-11 2018-04-03 Pim Snow Leopard Inc. Laser drilling and trepanning device
GB201205020D0 (en) * 2012-03-22 2012-05-09 Rolls Royce Plc A method of manufacturing a thermal barrier coated article
US10030524B2 (en) 2013-12-20 2018-07-24 Rolls-Royce Corporation Machined film holes
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US9611824B2 (en) * 2015-02-18 2017-04-04 Caterpillar Inc. Process for manufacturing an injector body
US10239157B2 (en) 2016-04-06 2019-03-26 General Electric Company Additive machine utilizing rotational build surface
US20190071977A1 (en) * 2017-09-07 2019-03-07 General Electric Company Component for a turbine engine with a cooling hole
US10760431B2 (en) 2017-09-07 2020-09-01 General Electric Company Component for a turbine engine with a cooling hole
DE102018113508A1 (de) * 2018-06-06 2019-12-12 Liebherr-Components Deggendorf Gmbh Verfahren zum Fertigen einer Düse
US11585224B2 (en) 2020-08-07 2023-02-21 General Electric Company Gas turbine engines and methods associated therewith
US20230070114A1 (en) * 2021-09-03 2023-03-09 Raytheon Technologies Corporation Multi-step method for machining blind ope1ning in ceramic component

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2227965B (en) * 1988-10-12 1993-02-10 Rolls Royce Plc Apparatus for drilling a shaped hole in a workpiece
US6744010B1 (en) * 1991-08-22 2004-06-01 United Technologies Corporation Laser drilled holes for film cooling
US5511946A (en) * 1994-12-08 1996-04-30 General Electric Company Cooled airfoil tip corner
US5747769A (en) * 1995-11-13 1998-05-05 General Electric Company Method of laser forming a slot
US5609779A (en) * 1996-05-15 1997-03-11 General Electric Company Laser drilling of non-circular apertures
US5837964A (en) * 1998-01-16 1998-11-17 Chromalloy Gas Turbine Corporation Laser drilling holes in components by combined percussion and trepan drilling
DE59802893D1 (de) * 1998-03-23 2002-03-14 Alstom Nichtkreisförmige Kühlbohrung und Verfahren zur Herstellung derselben
US6362446B1 (en) * 1999-08-02 2002-03-26 General Electric Company Method for drilling hollow components
DE19960797C1 (de) * 1999-12-16 2001-09-13 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Öffnung in einem metallischen Bauteil
US6573474B1 (en) * 2000-10-18 2003-06-03 Chromalloy Gas Turbine Corporation Process for drilling holes through a thermal barrier coating
US6420677B1 (en) * 2000-12-20 2002-07-16 Chromalloy Gas Turbine Corporation Laser machining cooling holes in gas turbine components

Also Published As

Publication number Publication date
EP1308236A1 (de) 2003-05-07
EP1308236B1 (de) 2010-04-07
GB2381489A (en) 2003-05-07
US6914214B2 (en) 2005-07-05
US6781091B2 (en) 2004-08-24
US20030091432A1 (en) 2003-05-15
GB0126006D0 (en) 2001-12-19
GB2381489A8 (en) 2003-05-22
US20040232122A1 (en) 2004-11-25
GB2381489B (en) 2004-11-17

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Legal Events

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8364 No opposition during term of opposition