PL2912274T3 - Układ chłodzenia do podzespołu turbiny gazowej - Google Patents

Układ chłodzenia do podzespołu turbiny gazowej

Info

Publication number
PL2912274T3
PL2912274T3 PL13786117T PL13786117T PL2912274T3 PL 2912274 T3 PL2912274 T3 PL 2912274T3 PL 13786117 T PL13786117 T PL 13786117T PL 13786117 T PL13786117 T PL 13786117T PL 2912274 T3 PL2912274 T3 PL 2912274T3
Authority
PL
Poland
Prior art keywords
gas turbine
turbine component
cooling arrangement
cooling
arrangement
Prior art date
Application number
PL13786117T
Other languages
English (en)
Inventor
Ching-Pang Lee
Benjamin E. Heneveld
Original Assignee
Siemens Aktiengesellschaft
Mikro Systems, 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 Aktiengesellschaft, Mikro Systems, Inc. filed Critical Siemens Aktiengesellschaft
Publication of PL2912274T3 publication Critical patent/PL2912274T3/pl

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
    • F01D5/187—Convection cooling
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/185—Two-dimensional patterned serpentine-like
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
PL13786117T 2012-10-23 2013-10-23 Układ chłodzenia do podzespołu turbiny gazowej PL2912274T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/657,923 US8951004B2 (en) 2012-10-23 2012-10-23 Cooling arrangement for a gas turbine component
PCT/US2013/066369 WO2014066495A1 (en) 2012-10-23 2013-10-23 Cooling arrangement for a gas turbine component
EP13786117.5A EP2912274B1 (en) 2012-10-23 2013-10-23 Cooling arrangement for a gas turbine component

Publications (1)

Publication Number Publication Date
PL2912274T3 true PL2912274T3 (pl) 2019-09-30

Family

ID=49517768

Family Applications (1)

Application Number Title Priority Date Filing Date
PL13786117T PL2912274T3 (pl) 2012-10-23 2013-10-23 Układ chłodzenia do podzespołu turbiny gazowej

Country Status (4)

Country Link
US (1) US8951004B2 (pl)
EP (1) EP2912274B1 (pl)
PL (1) PL2912274T3 (pl)
WO (1) WO2014066495A1 (pl)

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WO2016036366A1 (en) * 2014-09-04 2016-03-10 Siemens Aktiengesellschaft Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of a gas turbine airfoil
US9840930B2 (en) 2014-09-04 2017-12-12 Siemens Aktiengesellschaft Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoil
EP3037727A1 (en) * 2014-12-22 2016-06-29 Frank J. Cunha Gas turbine engine components and cooling cavities
US10094287B2 (en) * 2015-02-10 2018-10-09 United Technologies Corporation Gas turbine engine component with vascular cooling scheme
US10156157B2 (en) * 2015-02-13 2018-12-18 United Technologies Corporation S-shaped trip strips in internally cooled components
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US10208671B2 (en) * 2015-11-19 2019-02-19 United Technologies Corporation Turbine component including mixed cooling nub feature
US10428659B2 (en) 2015-12-21 2019-10-01 United Technologies Corporation Crossover hole configuration for a flowpath component in a gas turbine engine
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US10823511B2 (en) 2017-06-26 2020-11-03 Raytheon Technologies Corporation Manufacturing a heat exchanger using a material buildup process
US10753210B2 (en) * 2018-05-02 2020-08-25 Raytheon Technologies Corporation Airfoil having improved cooling scheme
US11168570B1 (en) * 2020-08-27 2021-11-09 Raytheon Technologies Corporation Cooling arrangement for gas turbine engine components
GB202105026D0 (en) * 2021-04-08 2021-05-26 Siemens Energy Global Gmbh & Co Kg Aerofoil and method
US12031724B2 (en) * 2022-05-05 2024-07-09 General Electric Company Turbine engine combustor having a combustion chamber heat shield
JP2023165485A (ja) * 2022-05-06 2023-11-16 三菱重工業株式会社 タービン翼及びガスタービン

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Also Published As

Publication number Publication date
US8951004B2 (en) 2015-02-10
EP2912274A1 (en) 2015-09-02
EP2912274B1 (en) 2019-03-13
US20140112799A1 (en) 2014-04-24
WO2014066495A1 (en) 2014-05-01

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