EP1548235A3 - Cooled vane cluster - Google Patents

Cooled vane cluster Download PDF

Info

Publication number
EP1548235A3
EP1548235A3 EP04257975A EP04257975A EP1548235A3 EP 1548235 A3 EP1548235 A3 EP 1548235A3 EP 04257975 A EP04257975 A EP 04257975A EP 04257975 A EP04257975 A EP 04257975A EP 1548235 A3 EP1548235 A3 EP 1548235A3
Authority
EP
European Patent Office
Prior art keywords
duct
cooling
cooling holes
visible
vane cluster
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.)
Withdrawn
Application number
EP04257975A
Other languages
German (de)
French (fr)
Other versions
EP1548235A2 (en
Inventor
Todd Coons
Edward Pietraszkiewicz
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 Technologies Corp filed Critical United Technologies Corp
Publication of EP1548235A2 publication Critical patent/EP1548235A2/en
Publication of EP1548235A3 publication Critical patent/EP1548235A3/en
Withdrawn legal-status Critical Current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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using 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
    • 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
    • F05D2230/12—Manufacture by removing material by spark erosion methods
    • 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
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A cast vane cluster (32) with enhanced cooling contains an inner and an outer platform (34, 36) and at least two airfoils (38) for directing a primary fluid stream axially rearward . A duct (56) is bounded by inner and outer endwall surfaces (40, 44), and adjacent airfoil fluid directing surfaces. One or more cooling holes (62) in the duct are drilled using an electrodischarge machine (EDM) method without a line of sight from the drilling equipment to the cooling hole location. One or more cooling holes (62), located in portions of the duct, may not be visible when viewed from an external location. Additionally, one or more cooling holes (62) may only have an outlet cross sectional ar ea (66) visible when viewed along a longitudinal axis from an external location.
EP04257975A 2003-12-22 2004-12-20 Cooled vane cluster Withdrawn EP1548235A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US743516 2003-12-22
US10/743,516 US20050135923A1 (en) 2003-12-22 2003-12-22 Cooled vane cluster

Publications (2)

Publication Number Publication Date
EP1548235A2 EP1548235A2 (en) 2005-06-29
EP1548235A3 true EP1548235A3 (en) 2008-11-19

Family

ID=34552829

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04257975A Withdrawn EP1548235A3 (en) 2003-12-22 2004-12-20 Cooled vane cluster

Country Status (9)

Country Link
US (1) US20050135923A1 (en)
EP (1) EP1548235A3 (en)
JP (1) JP2005180447A (en)
KR (1) KR20050063678A (en)
CN (1) CN1637235A (en)
AU (1) AU2004240240A1 (en)
CA (1) CA2489964A1 (en)
NO (1) NO20045594L (en)
RU (1) RU2004136896A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2350847T3 (en) * 2005-09-06 2011-01-27 Volvo Aero Corporation PROCEDURE FOR THE MANUFACTURE OF A WALL STRUCTURE OF A MOTOR.
US7625172B2 (en) 2006-04-26 2009-12-01 United Technologies Corporation Vane platform cooling
US8197184B2 (en) * 2006-10-18 2012-06-12 United Technologies Corporation Vane with enhanced heat transfer
US8191504B2 (en) * 2006-11-27 2012-06-05 United Technologies Corporation Coating apparatus and methods
US7862291B2 (en) * 2007-02-08 2011-01-04 United Technologies Corporation Gas turbine engine component cooling scheme
EP2436884A1 (en) * 2010-09-29 2012-04-04 Siemens Aktiengesellschaft Turbine arrangement and gas turbine engine
FR2978197B1 (en) * 2011-07-22 2015-12-25 Snecma TURBINE AND TURBINE TURBINE TURBINE DISPENSER HAVING SUCH A DISPENSER
WO2016133987A2 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Forming cooling passages in combustion turbine superalloy castings
CN105171158B (en) * 2015-10-10 2017-11-14 贵阳中航动力精密铸造有限公司 A kind of turborotor taper air film hole processing technology
US10436042B2 (en) 2015-12-01 2019-10-08 United Technologies Corporation Thermal barrier coatings and methods
US10641102B2 (en) * 2017-09-01 2020-05-05 United Technologies Corporation Turbine vane cluster including enhanced vane cooling
US11125164B2 (en) * 2019-07-31 2021-09-21 Raytheon Technologies Corporation Baffle with two datum features
CN112091336B (en) * 2020-09-21 2022-02-25 中国航发沈阳黎明航空发动机有限责任公司 Method for accurately positioning interference gas film hole of integrally cast blade by electric spark machining

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3529903A (en) * 1968-11-29 1970-09-22 Westinghouse Electric Corp Nozzle blade structure
JPS59180006A (en) * 1983-03-30 1984-10-12 Hitachi Ltd Gas turbine stator blade segment
US4693667A (en) * 1980-04-29 1987-09-15 Teledyne Industries, Inc. Turbine inlet nozzle with cooling means
US5813832A (en) * 1996-12-05 1998-09-29 General Electric Company Turbine engine vane segment
WO2001012382A1 (en) * 1999-08-12 2001-02-22 Chromalloy Gas Turbine Corporation Method for replacing a turbine vane airfoil
EP1176284A2 (en) * 2000-07-27 2002-01-30 General Electric Company Brazeless fillet turbine nozzle
EP1262634A2 (en) * 2001-05-29 2002-12-04 General Electric Company Integral nozzle and shroud
US20030002979A1 (en) * 2001-06-28 2003-01-02 Koschier Angelo Von Hybrid turbine nozzle

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5637239A (en) * 1995-03-31 1997-06-10 United Technologies Corporation Curved electrode and method for electrical discharge machining curved cooling holes
GB2313414B (en) * 1996-05-24 2000-05-17 Rolls Royce Plc Gas turbine engine blade tip clearance control
US6416278B1 (en) * 2000-11-16 2002-07-09 General Electric Company Turbine nozzle segment and method of repairing same
DE10059997B4 (en) * 2000-12-02 2014-09-11 Alstom Technology Ltd. Coolable blade for a gas turbine component
US6382908B1 (en) * 2001-01-18 2002-05-07 General Electric Company Nozzle fillet backside cooling

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3529903A (en) * 1968-11-29 1970-09-22 Westinghouse Electric Corp Nozzle blade structure
US4693667A (en) * 1980-04-29 1987-09-15 Teledyne Industries, Inc. Turbine inlet nozzle with cooling means
JPS59180006A (en) * 1983-03-30 1984-10-12 Hitachi Ltd Gas turbine stator blade segment
US5813832A (en) * 1996-12-05 1998-09-29 General Electric Company Turbine engine vane segment
WO2001012382A1 (en) * 1999-08-12 2001-02-22 Chromalloy Gas Turbine Corporation Method for replacing a turbine vane airfoil
EP1176284A2 (en) * 2000-07-27 2002-01-30 General Electric Company Brazeless fillet turbine nozzle
EP1262634A2 (en) * 2001-05-29 2002-12-04 General Electric Company Integral nozzle and shroud
US20030002979A1 (en) * 2001-06-28 2003-01-02 Koschier Angelo Von Hybrid turbine nozzle

Also Published As

Publication number Publication date
CA2489964A1 (en) 2005-06-22
RU2004136896A (en) 2006-05-27
EP1548235A2 (en) 2005-06-29
US20050135923A1 (en) 2005-06-23
KR20050063678A (en) 2005-06-28
CN1637235A (en) 2005-07-13
JP2005180447A (en) 2005-07-07
AU2004240240A1 (en) 2005-07-07
NO20045594L (en) 2005-06-23

Similar Documents

Publication Publication Date Title
EP1548235A3 (en) Cooled vane cluster
EP1443178A3 (en) Turbine blade
DE10355449B4 (en) turbine blade
EP1505255A3 (en) Cooling hole configuration for a perimeter-cooled turbine bucket airfoil
CN101025091B (en) Bucket platform cooling circuit and method
EP2230383A1 (en) Blade for a gas turbine with cooled tip cap
CN101008323B (en) Gas turbine bucket with cooled platform edge and method of cooling platform leading edge
EP1267037A3 (en) Cooled hollow tip shroud of a turbine blade
US7641444B1 (en) Serpentine flow circuit with tip section cooling channels
EP1101563A3 (en) Modification and repair of film cooling holes in gas turbine engine components
EP1798374A3 (en) Cooled turbine blade
EP1205634A3 (en) Cooling of a gas turbine blade
EP1363078A3 (en) Bulkhead panel for use in a combustion chamber of a gas turbine engine
EP1881156A3 (en) Turbine vane with removable platform inserts
EP0971095A3 (en) A coolable airfoil for a gas turbine engine
DE60110483D1 (en) Tool for clamping machining
EP1074696A3 (en) Stator vane for a rotary machine
EP2942487A1 (en) Reducing variation in cooling hole meter length
CN106609682A (en) Turbine bucket and corresponding turbine
EP1041247A3 (en) Cooling circuit for a gas turbine bucket and tip shroud
EP1085171A3 (en) Thermal barrier coated squealer tip cavity
EP1512835A3 (en) Rotor blade and gas turbine engine comprising a corresponding rotor assembly
DE102008037391A1 (en) Turbine blade for gas turbine engine, has set of cooling channels extending between foot section and tip section of blade leaf, where channels are positioned in curve line pattern and each channel passes to tip section
EP1052372A3 (en) Trailing edge cooling passages for gas turbine nozzles with turbulators
WO2001088354A3 (en) Device for controlling the cooling flows of gas turbines

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR LV MK YU

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR LV MK YU

17P Request for examination filed

Effective date: 20081223

17Q First examination report despatched

Effective date: 20090305

AKX Designation fees paid

Designated state(s): DE GB

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20090716