ATE459784T1 - TURBINE BLADE - Google Patents

TURBINE BLADE

Info

Publication number
ATE459784T1
ATE459784T1 AT07820422T AT07820422T ATE459784T1 AT E459784 T1 ATE459784 T1 AT E459784T1 AT 07820422 T AT07820422 T AT 07820422T AT 07820422 T AT07820422 T AT 07820422T AT E459784 T1 ATE459784 T1 AT E459784T1
Authority
AT
Austria
Prior art keywords
blade
shield element
turbine blade
leading edge
edge area
Prior art date
Application number
AT07820422T
Other languages
German (de)
Inventor
Fathi Ahmad
Original Assignee
Siemens Ag
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 Ag filed Critical Siemens Ag
Application granted granted Critical
Publication of ATE459784T1 publication Critical patent/ATE459784T1/en

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The turbine blade has a blade basic body (30), whose external surface (32,36) is provided in the leading edge area with heat shield element (22) arranged at a distance from blade basic body. The multiple auxiliary cooling channels (24) branch off from a main cooling channel (26), which is formed in blade body, in which auxiliary cooling channels open into outlet openings in leading edge area of blade body. The shield element has multiple outlet channels (28) arranged behind one another in longitudinal direction and extend from main cooling channel to the outer wall face of the shield element.
AT07820422T 2006-10-30 2007-09-20 TURBINE BLADE ATE459784T1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP06022622A EP1930544A1 (en) 2006-10-30 2006-10-30 Turbine blade
PCT/EP2007/059989 WO2008052846A1 (en) 2006-10-30 2007-09-20 Turbine blade

Publications (1)

Publication Number Publication Date
ATE459784T1 true ATE459784T1 (en) 2010-03-15

Family

ID=37945313

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07820422T ATE459784T1 (en) 2006-10-30 2007-09-20 TURBINE BLADE

Country Status (10)

Country Link
US (1) US20100068069A1 (en)
EP (2) EP1930544A1 (en)
JP (1) JP2010508461A (en)
CN (1) CN101535601A (en)
AT (1) ATE459784T1 (en)
DE (1) DE502007003043D1 (en)
ES (1) ES2341384T3 (en)
PL (1) PL2084368T3 (en)
RU (1) RU2405940C1 (en)
WO (1) WO2008052846A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH700687A1 (en) * 2009-03-30 2010-09-30 Alstom Technology Ltd Chilled component for a gas turbine.
US9399271B2 (en) * 2010-12-28 2016-07-26 Rolls-Royce Corporation Heat treating and brazing of an object
WO2015123006A1 (en) 2014-02-13 2015-08-20 United Technologies Corporation Gas turbine engine component cooling circuit with respirating pedestal
US10301945B2 (en) * 2015-12-18 2019-05-28 General Electric Company Interior cooling configurations in turbine rotor blades
CN105422188A (en) * 2016-01-13 2016-03-23 北京航空航天大学 Turbine blade with heat shield type composite cooling structure
US10577942B2 (en) * 2016-11-17 2020-03-03 General Electric Company Double impingement slot cap assembly
US20190024513A1 (en) * 2017-07-19 2019-01-24 General Electric Company Shield for a turbine engine airfoil
KR102028803B1 (en) * 2017-09-29 2019-10-04 두산중공업 주식회사 Gas Turbine
US11286783B2 (en) * 2020-04-27 2022-03-29 Raytheon Technologies Corporation Airfoil with CMC liner and multi-piece monolithic ceramic shell

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB841117A (en) * 1957-08-02 1960-07-13 Rolls Royce Improvements in or relating to stator blades of fluid machines
GB995182A (en) * 1963-06-20 1965-06-16 Rolls Royce Improvements in or relating to gas turbine engine combustion equipment
US3269700A (en) * 1964-12-07 1966-08-30 United Aircraft Corp Heat shield for turbine strut
US3423069A (en) * 1967-09-29 1969-01-21 Trw Inc Airfoil
JPS527482B2 (en) * 1972-05-08 1977-03-02
US4026659A (en) * 1975-10-16 1977-05-31 Avco Corporation Cooled composite vanes for turbine nozzles
JPS5390509A (en) * 1977-01-20 1978-08-09 Koukuu Uchiyuu Gijiyutsu Kenki Structure of air cooled turbine blade
JP4027430B2 (en) * 1996-12-02 2007-12-26 シーメンス アクチエンゲゼルシヤフト Turbine blades and their use in gas turbine equipment
DE19848104A1 (en) * 1998-10-19 2000-04-20 Asea Brown Boveri Turbine blade
US6709230B2 (en) * 2002-05-31 2004-03-23 Siemens Westinghouse Power Corporation Ceramic matrix composite gas turbine vane
US7011502B2 (en) * 2004-04-15 2006-03-14 General Electric Company Thermal shield turbine airfoil
US7871246B2 (en) * 2007-02-15 2011-01-18 Siemens Energy, Inc. Airfoil for a gas turbine

Also Published As

Publication number Publication date
EP2084368B1 (en) 2010-03-03
RU2405940C1 (en) 2010-12-10
WO2008052846A1 (en) 2008-05-08
PL2084368T3 (en) 2010-07-30
EP2084368A1 (en) 2009-08-05
DE502007003043D1 (en) 2010-04-15
US20100068069A1 (en) 2010-03-18
EP1930544A1 (en) 2008-06-11
CN101535601A (en) 2009-09-16
ES2341384T3 (en) 2010-06-18
JP2010508461A (en) 2010-03-18

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