DE502007003043D1 - TURBINE BLADE - Google Patents
TURBINE BLADEInfo
- Publication number
- DE502007003043D1 DE502007003043D1 DE502007003043T DE502007003043T DE502007003043D1 DE 502007003043 D1 DE502007003043 D1 DE 502007003043D1 DE 502007003043 T DE502007003043 T DE 502007003043T DE 502007003043 T DE502007003043 T DE 502007003043T DE 502007003043 D1 DE502007003043 D1 DE 502007003043D1
- Authority
- DE
- Germany
- Prior art keywords
- blade
- shield element
- turbine blade
- leading edge
- edge area
- 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.)
- Active
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
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.
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 |
---|---|
DE502007003043D1 true DE502007003043D1 (en) | 2010-04-15 |
Family
ID=37945313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE502007003043T Active DE502007003043D1 (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)
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 |
EP3105425B1 (en) * | 2014-02-13 | 2019-03-20 | 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)
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 |
WO1998025009A1 (en) * | 1996-12-02 | 1998-06-11 | Siemens Aktiengesellschaft | Turbine blade and its use in a gas turbine system |
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 |
-
2006
- 2006-10-30 EP EP06022622A patent/EP1930544A1/en not_active Withdrawn
-
2007
- 2007-09-20 RU RU2009120554/06A patent/RU2405940C1/en not_active IP Right Cessation
- 2007-09-20 CN CNA2007800407001A patent/CN101535601A/en active Pending
- 2007-09-20 PL PL07820422T patent/PL2084368T3/en unknown
- 2007-09-20 AT AT07820422T patent/ATE459784T1/en active
- 2007-09-20 US US12/447,972 patent/US20100068069A1/en not_active Abandoned
- 2007-09-20 WO PCT/EP2007/059989 patent/WO2008052846A1/en active Application Filing
- 2007-09-20 EP EP07820422A patent/EP2084368B1/en not_active Not-in-force
- 2007-09-20 DE DE502007003043T patent/DE502007003043D1/en active Active
- 2007-09-20 JP JP2009533769A patent/JP2010508461A/en active Pending
- 2007-09-20 ES ES07820422T patent/ES2341384T3/en active Active
Also Published As
Publication number | Publication date |
---|---|
ES2341384T3 (en) | 2010-06-18 |
EP2084368B1 (en) | 2010-03-03 |
EP2084368A1 (en) | 2009-08-05 |
EP1930544A1 (en) | 2008-06-11 |
ATE459784T1 (en) | 2010-03-15 |
RU2405940C1 (en) | 2010-12-10 |
JP2010508461A (en) | 2010-03-18 |
CN101535601A (en) | 2009-09-16 |
US20100068069A1 (en) | 2010-03-18 |
WO2008052846A1 (en) | 2008-05-08 |
PL2084368T3 (en) | 2010-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |