IT1048452B - Disposizione di tenuta per anelli di chiusura fissi di turbine a gas - Google Patents
Disposizione di tenuta per anelli di chiusura fissi di turbine a gasInfo
- Publication number
- IT1048452B IT1048452B IT28032/75A IT2803275A IT1048452B IT 1048452 B IT1048452 B IT 1048452B IT 28032/75 A IT28032/75 A IT 28032/75A IT 2803275 A IT2803275 A IT 2803275A IT 1048452 B IT1048452 B IT 1048452B
- Authority
- IT
- Italy
- Prior art keywords
- sealing arrangement
- gas turbines
- fixed closing
- closing rings
- rings
- Prior art date
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/513,001 US3947145A (en) | 1974-10-07 | 1974-10-07 | Gas turbine stationary shroud seals |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1048452B true IT1048452B (it) | 1980-11-20 |
Family
ID=24041511
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT28032/75A IT1048452B (it) | 1974-10-07 | 1975-10-07 | Disposizione di tenuta per anelli di chiusura fissi di turbine a gas |
Country Status (4)
Country | Link |
---|---|
US (1) | US3947145A (it) |
JP (1) | JPS5164113A (it) |
CA (1) | CA1013258A (it) |
IT (1) | IT1048452B (it) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1483532A (en) * | 1974-09-13 | 1977-08-24 | Rolls Royce | Stator structure for a gas turbine engine |
US4470754A (en) * | 1980-05-19 | 1984-09-11 | Avco Corporation | Partially segmented supporting and sealing structure for a guide vane array of a gas turbine engine |
US4398866A (en) * | 1981-06-24 | 1983-08-16 | Avco Corporation | Composite ceramic/metal cylinder for gas turbine engine |
US4439107A (en) * | 1982-09-16 | 1984-03-27 | United Technologies Corporation | Rotor blade cooling air chamber |
US4902198A (en) * | 1988-08-31 | 1990-02-20 | Westinghouse Electric Corp. | Apparatus for film cooling of turbine van shrouds |
JPH03213602A (ja) * | 1990-01-08 | 1991-09-19 | General Electric Co <Ge> | ガスタービンエンジンの当接セグメントを連結する自己冷却式ジョイント連結構造 |
US5188507A (en) * | 1991-11-27 | 1993-02-23 | General Electric Company | Low-pressure turbine shroud |
US5846050A (en) * | 1997-07-14 | 1998-12-08 | General Electric Company | Vane sector spring |
US7575415B2 (en) * | 2005-11-10 | 2009-08-18 | General Electric Company | Methods and apparatus for assembling turbine engines |
US9915153B2 (en) * | 2015-05-11 | 2018-03-13 | General Electric Company | Turbine shroud segment assembly with expansion joints |
US11047248B2 (en) * | 2018-06-19 | 2021-06-29 | General Electric Company | Curved seal for adjacent gas turbine components |
US11248705B2 (en) * | 2018-06-19 | 2022-02-15 | General Electric Company | Curved seal with relief cuts for adjacent gas turbine components |
CN109882255B (zh) * | 2019-03-01 | 2021-10-19 | 西安航天动力研究所 | 带叶片型线槽的涡轮静子顶部封严限位结构 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1057827B (de) * | 1955-08-18 | 1959-05-21 | Stroemungsmasch Anst | Feststehender Laufradkranz fuer Gasturbinen |
GB1081458A (en) * | 1965-12-28 | 1967-08-31 | Rolls Royce | Blade assembly for a fluid flow machine such as a gas turbine engine |
GB1185189A (en) * | 1967-09-25 | 1970-03-25 | Prvni Brnenska Strojirna Zd Y | Improvements in or relating to turbines, particularly gas turbines |
US3519366A (en) * | 1968-05-22 | 1970-07-07 | Westinghouse Electric Corp | Turbine diaphragm seal structure |
US3542483A (en) * | 1968-07-17 | 1970-11-24 | Westinghouse Electric Corp | Turbine stator structure |
US3728041A (en) * | 1971-10-04 | 1973-04-17 | Gen Electric | Fluidic seal for segmented nozzle diaphragm |
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
-
1974
- 1974-10-07 US US05/513,001 patent/US3947145A/en not_active Expired - Lifetime
-
1975
- 1975-09-25 CA CA236,410A patent/CA1013258A/en not_active Expired
- 1975-10-06 JP JP50119857A patent/JPS5164113A/ja active Granted
- 1975-10-07 IT IT28032/75A patent/IT1048452B/it active
Also Published As
Publication number | Publication date |
---|---|
US3947145A (en) | 1976-03-30 |
JPS5164113A (en) | 1976-06-03 |
JPS5514883B2 (it) | 1980-04-19 |
CA1013258A (en) | 1977-07-05 |
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