IN2015DN03335A - - Google Patents

Info

Publication number
IN2015DN03335A
IN2015DN03335A IN3335DEN2015A IN2015DN03335A IN 2015DN03335 A IN2015DN03335 A IN 2015DN03335A IN 3335DEN2015 A IN3335DEN2015 A IN 3335DEN2015A IN 2015DN03335 A IN2015DN03335 A IN 2015DN03335A
Authority
IN
India
Prior art keywords
casting
wall
airfoil
main wall
tip
Prior art date
Application number
Other languages
English (en)
Inventor
Christian X Campbell
Dimitrios Thomaidis
Original Assignee
Siemens Energy Inc
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 Siemens Energy Inc filed Critical Siemens Energy Inc
Publication of IN2015DN03335A publication Critical patent/IN2015DN03335A/en

Links

Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D46/00Controlling, supervising, not restricted to casting covered by a single main group, e.g. for safety reasons
    • 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
    • F05D2230/10Manufacture by removing material
    • 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
    • F05D2230/21Manufacture essentially without removing material by casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
IN3335DEN2015 2012-11-13 2013-11-12 IN2015DN03335A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/675,345 US8720526B1 (en) 2012-11-13 2012-11-13 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip
PCT/US2013/069671 WO2014078305A1 (en) 2012-11-13 2013-11-12 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip

Publications (1)

Publication Number Publication Date
IN2015DN03335A true IN2015DN03335A (ru) 2015-10-23

Family

ID=49759538

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3335DEN2015 IN2015DN03335A (ru) 2012-11-13 2013-11-12

Country Status (8)

Country Link
US (1) US8720526B1 (ru)
EP (1) EP2920425B1 (ru)
JP (1) JP5973081B2 (ru)
CN (1) CN104812994B (ru)
IN (1) IN2015DN03335A (ru)
RU (1) RU2015117767A (ru)
SA (1) SA515360421B1 (ru)
WO (1) WO2014078305A1 (ru)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10260352B2 (en) 2013-08-01 2019-04-16 Siemens Energy, Inc. Gas turbine blade with corrugated tip wall
JP2018508685A (ja) 2015-01-13 2018-03-29 ゼネラル・エレクトリック・カンパニイ ヒューズ構造を有する複合材エーロフォイル
US10101577B2 (en) * 2015-04-13 2018-10-16 Siemens Energy, Inc. System to prognose gas turbine remaining useful life
CN108698128B (zh) 2016-04-27 2021-01-29 西门子能源美国公司 制造燃气涡轮发动机叶片的方法及燃气涡轮发动机叶片
EP3551852B1 (en) 2017-01-13 2021-10-27 Siemens Energy Global GmbH & Co. KG Adaptive machining of cooled turbine airfoil
EP3511522A1 (en) * 2018-01-11 2019-07-17 Siemens Aktiengesellschaft Gas turbine blade and method for producing such blade
FR3103126B1 (fr) * 2019-11-20 2022-03-25 Safran Aircraft Engines Dispositif et procédé améliorés d’usinage de pièce aéronautique
FR3143685A1 (fr) * 2022-12-16 2024-06-21 Safran Aircraft Engines Systeme propulsif aeronautique

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB627295A (en) * 1946-04-10 1949-08-05 Adrian Albert Lombard Improvements in or relating to the manufacture of guide vanes for axial-flow turbines and compressors
US3935766A (en) 1973-10-09 1976-02-03 Masters Christopher F Method and apparatus for machining cylindrical tubes
GB8508391D0 (en) * 1985-03-30 1985-05-09 Ae Plc Measurement of engineering components
US4959523A (en) 1988-11-18 1990-09-25 Hydro-Quebec Method and apparatus for automatically sensing the configuration of a surface area and effecting a work function thereon
US5446673A (en) 1993-03-30 1995-08-29 General Electric Company System and method for finish machining an in-process part having an inaccessible interior cavity
EP0894558A1 (de) * 1997-07-29 1999-02-03 Siemens Aktiengesellschaft Turbinenschaufel sowie Verfahren zur Herstellung einer Turbinenschaufel
US6850874B1 (en) 1998-04-17 2005-02-01 United Technologies Corporation Method and apparatus for predicting a characteristic of a product attribute formed by a machining process using a model of the process
DE60026934T2 (de) * 1999-06-02 2006-12-14 General Electric Co. Verfahren zur Verminderung der Wandstärke nach dem Giessen einen Turbinenschaufels mittels Funkenerosionsbearbeitung
DE10001516B4 (de) 2000-01-15 2014-05-08 Alstom Technology Ltd. Zerstörungsfreies Verfahren zur Bestimmung der Schichtdicke einer metallischen Schutzschicht auf einem metallischen Grundmaterial
US6376801B1 (en) 2000-10-12 2002-04-23 General Electric Company Gas turbine component refurbishment apparatus and repair method
US6968290B2 (en) 2001-03-27 2005-11-22 General Electric Company Electrochemical machining tool assembly and method of monitoring electrochemical machining
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
US7204019B2 (en) 2001-08-23 2007-04-17 United Technologies Corporation Method for repairing an apertured gas turbine component
US6701615B2 (en) 2002-03-08 2004-03-09 General Electric Company Inspection and sorting system and method for part repair
JP2003344026A (ja) * 2002-05-27 2003-12-03 Mitsubishi Heavy Ind Ltd 中空翼検査方法、及び中空翼検査用コンピュータプログラム
DE10255346A1 (de) * 2002-11-28 2004-06-09 Alstom Technology Ltd Verfahren zum Herstellen einer Turbinenschaufel
US6969821B2 (en) * 2003-06-30 2005-11-29 General Electric Company Airfoil qualification system and method
US20050091848A1 (en) * 2003-11-03 2005-05-05 Nenov Krassimir P. Turbine blade and a method of manufacturing and repairing a turbine blade
US7010982B2 (en) 2004-04-30 2006-03-14 General Electric Company Method of ultrasonically inspecting airfoils
EP1593445B1 (de) * 2004-05-03 2007-07-18 Siemens Aktiengesellschaft Verfahren zum Herstellen eines hohlgegossenen Bauteils mit Innenbeschichtung
DE102005025338B4 (de) 2005-05-31 2019-03-14 Siemens Aktiengesellschaft 08.Verfahren zur Bearbeitung eines Werkstückes
US7272529B2 (en) 2005-07-08 2007-09-18 Honeywell International, Inc. Dual wall turbine blade ultrasonic wall thickness measurement technique
US7306026B2 (en) 2005-09-01 2007-12-11 United Technologies Corporation Cooled turbine airfoils and methods of manufacture
GB0518153D0 (en) 2005-09-07 2005-10-12 Rolls Royce Plc Apparatus for measuring wall thicknesses of objects
US8244025B2 (en) 2006-03-20 2012-08-14 Siemens Energy, Inc. Method of coalescing information about inspected objects
US8477154B2 (en) 2006-03-20 2013-07-02 Siemens Energy, Inc. Method and system for interactive virtual inspection of modeled objects
DE102006043339B4 (de) 2006-09-15 2010-11-11 Siemens Ag Verfahren und Vorrichtung zur Bestimmung von Bauteilwandstärken mittels Thermographie
DE102006050440A1 (de) * 2006-10-26 2008-04-30 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Leichtbau-Turbinenschaufel
US8087447B2 (en) 2006-10-30 2012-01-03 United Technologies Corporation Method for checking wall thickness of hollow core airfoil
CN102016234B (zh) * 2008-03-28 2015-05-20 阿尔斯通技术有限公司 燃气轮机的导向叶片
US9177371B2 (en) 2008-06-09 2015-11-03 Siemens Energy, Inc. Non-destructive examination data visualization and analysis
US8500411B2 (en) 2010-06-07 2013-08-06 Siemens Energy, Inc. Turbine airfoil with outer wall thickness indicators
EP2469099B1 (de) * 2010-12-23 2017-08-02 Grundfos Management A/S Laufrad für eine Pump- sowie Kernanordnung und Verfahren zum Gießen eines Laufrades einer Pumpe

Also Published As

Publication number Publication date
US8720526B1 (en) 2014-05-13
US20140130999A1 (en) 2014-05-15
CN104812994B (zh) 2018-01-26
JP5973081B2 (ja) 2016-08-23
JP2015536404A (ja) 2015-12-21
RU2015117767A (ru) 2017-01-10
EP2920425A1 (en) 2015-09-23
SA515360421B1 (ar) 2016-12-18
WO2014078305A1 (en) 2014-05-22
EP2920425B1 (en) 2016-11-02
CN104812994A (zh) 2015-07-29

Similar Documents

Publication Publication Date Title
IN2015DN03335A (ru)
WO2014147048A3 (de) Vorrichtung und verfahren zum ausschneiden von konturen aus flächigen substraten mittels laser
GB2490606A (en) Spalling for a semiconductor substrate
EP3064711B8 (en) Component for a gas turbine engine, corresponding gas turbine engine and method of forming an airfoil
SG10201609716UA (en) System and method for locating a probe within a gas turbine engine
EP4306233A3 (en) Method of forming a component of a gas turbine engine
WO2015057310A3 (en) Platform cooling core for a gas turbine engine rotor blade
MX2016014298A (es) Metodo para la construccion en capas de cuerpos que comprenden material de base para molde refractario y resoles, y moldes o nucleos fabricados de acuerdo con dicho metodo.
EP3044427B8 (en) Gas turbine engine and corresponding method for regulating blade tip clearance
EP2841703A4 (en) GAS TURBINE ENGINE AERODYNAMIC PROFILE GEOMETRIES FOR PROCESS OF MANUFACTURING
EP3030751B8 (en) Gas turbine engine component and corresponding method of forming a gas turbine engine component
EP3088688B8 (en) Lubrication system for gas turbine engines
GB2500466B (en) Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle
GB201614070D0 (en) A component for a gas turbine engine and method of manufacture
WO2014163694A3 (en) Trenched cooling hole arrangement for a ceramic matrix composite vane
EP2730395B8 (de) Verfahren zur Herstellung einer Welle eines Gasturbinentriebwerks
GB201311460D0 (en) An abradable liner for a gas turbine engine
WO2015020711A3 (en) Gas turbine blade configuration
EP2952685B8 (en) Airfoil for a gas turbine engine, a gas turbine engine and a method for reducing frictional heating between airfoils and a case of a gas turbine engine
GB2562150B (en) Gas turbine, guide blade ring of a gas turbine and method for producing the same
EA201491538A1 (ru) Штампы для формирования емкостей и способы их изготовления
WO2015057309A3 (en) Insert and standoff design for a gas turbine engine vane
WO2014175940A3 (en) Gas turbine engine component manufacturing method and core for making same
WO2015049084A3 (de) Verfahren und vorrichtung zur qualitätskontrolle der geometrie eines bauteils
MX340931B (es) Un proceso para la fabricacion de un envase y un envase.