AU2005201224B2 - Arrangement for sealing off a transition between cooling passages of two components of a turbomachine - Google Patents
Arrangement for sealing off a transition between cooling passages of two components of a turbomachine Download PDFInfo
- Publication number
- AU2005201224B2 AU2005201224B2 AU2005201224A AU2005201224A AU2005201224B2 AU 2005201224 B2 AU2005201224 B2 AU 2005201224B2 AU 2005201224 A AU2005201224 A AU 2005201224A AU 2005201224 A AU2005201224 A AU 2005201224A AU 2005201224 B2 AU2005201224 B2 AU 2005201224B2
- Authority
- AU
- Australia
- Prior art keywords
- components
- component
- arrangement
- transition
- cooling
- 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.)
- Ceased
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
- F01D9/06—Fluid supply conduits to nozzles or the like
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5021—Expansivity
- F05D2300/50212—Expansivity dissimilar
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102004014118.5 | 2004-03-23 | ||
| DE200410014118 DE102004014118A1 (de) | 2004-03-23 | 2004-03-23 | Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU2005201224A1 AU2005201224A1 (en) | 2005-10-13 |
| AU2005201224B2 true AU2005201224B2 (en) | 2012-02-09 |
Family
ID=34854002
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2005201224A Ceased AU2005201224B2 (en) | 2004-03-23 | 2005-03-22 | Arrangement for sealing off a transition between cooling passages of two components of a turbomachine |
Country Status (4)
| Country | Link |
|---|---|
| EP (1) | EP1580401B1 (fr) |
| CN (1) | CN100491712C (fr) |
| AU (1) | AU2005201224B2 (fr) |
| DE (1) | DE102004014118A1 (fr) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8186933B2 (en) | 2009-03-24 | 2012-05-29 | General Electric Company | Systems, methods, and apparatus for passive purge flow control in a turbine |
| JP5723659B2 (ja) * | 2011-04-12 | 2015-05-27 | 本田技研工業株式会社 | 鋳抜きピン装置 |
| CN114483322B (zh) * | 2021-12-29 | 2023-09-19 | 中国航发长春控制科技有限公司 | 一种具有温度补偿功能的航空发动机起动引气装置 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3021110A (en) * | 1960-03-01 | 1962-02-13 | Gen Electric | High temperature turbine nozzle retaining means |
| US3966354A (en) * | 1974-12-19 | 1976-06-29 | General Electric Company | Thermal actuated valve for clearance control |
| JPH10238301A (ja) * | 1997-02-21 | 1998-09-08 | Mitsubishi Heavy Ind Ltd | ガスタービン翼の冷却通路 |
| US6067791A (en) * | 1997-12-11 | 2000-05-30 | Pratt & Whitney Canada Inc. | Turbine engine with a thermal valve |
| DE19963371A1 (de) * | 1999-12-28 | 2001-07-12 | Alstom Power Schweiz Ag Baden | Gekühltes Hitzeschild |
| EP1118806A1 (fr) * | 2000-01-20 | 2001-07-25 | Siemens Aktiengesellschaft | Structure de paroi sous charge thermique et méthode pour fermer des fentes dans une tel structure |
-
2004
- 2004-03-23 DE DE200410014118 patent/DE102004014118A1/de not_active Withdrawn
-
2005
- 2005-03-15 EP EP20050102044 patent/EP1580401B1/fr not_active Expired - Lifetime
- 2005-03-22 AU AU2005201224A patent/AU2005201224B2/en not_active Ceased
- 2005-03-23 CN CN 200510083795 patent/CN100491712C/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1580401B1 (fr) | 2012-10-31 |
| CN1769652A (zh) | 2006-05-10 |
| DE102004014118A1 (de) | 2005-10-13 |
| CN100491712C (zh) | 2009-05-27 |
| EP1580401A3 (fr) | 2010-07-07 |
| EP1580401A2 (fr) | 2005-09-28 |
| AU2005201224A1 (en) | 2005-10-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FGA | Letters patent sealed or granted (standard patent) | ||
| MK14 | Patent ceased section 143(a) (annual fees not paid) or expired |