DE69116137D1 - Abdichtung für das diaphragma einer turbine - Google Patents
Abdichtung für das diaphragma einer turbineInfo
- Publication number
- DE69116137D1 DE69116137D1 DE69116137T DE69116137T DE69116137D1 DE 69116137 D1 DE69116137 D1 DE 69116137D1 DE 69116137 T DE69116137 T DE 69116137T DE 69116137 T DE69116137 T DE 69116137T DE 69116137 D1 DE69116137 D1 DE 69116137D1
- Authority
- DE
- Germany
- Prior art keywords
- diaphragma
- turbine
- seal
- 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.)
- Expired - Fee Related
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
-
- 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
- F01D25/14—Casings modified therefor
- F01D25/145—Thermally insulated casings
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 |
---|---|---|---|
US07/627,019 US5125228A (en) | 1990-12-13 | 1990-12-13 | Diaphragm seal plate |
PCT/US1991/008298 WO1992010656A1 (en) | 1990-12-13 | 1991-11-06 | Diaphragm seal plate |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69116137D1 true DE69116137D1 (de) | 1996-02-15 |
DE69116137T2 DE69116137T2 (de) | 1996-05-15 |
Family
ID=24512833
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69116137T Expired - Fee Related DE69116137T2 (de) | 1990-12-13 | 1991-11-06 | Abdichtung für das diaphragma einer turbine |
Country Status (5)
Country | Link |
---|---|
US (1) | US5125228A (de) |
EP (1) | EP0515613B1 (de) |
JP (1) | JPH05504812A (de) |
DE (1) | DE69116137T2 (de) |
WO (1) | WO1992010656A1 (de) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5549449A (en) * | 1993-07-02 | 1996-08-27 | Wrr Industries, Inc. | Turbomachinery incorporating heat transfer reduction features |
US5793701A (en) * | 1995-04-07 | 1998-08-11 | Acuson Corporation | Method and apparatus for coherent image formation |
US5664413A (en) * | 1995-03-29 | 1997-09-09 | Alliedsignal Inc. | Dual pilot ring for a gas turbine engine |
US6168375B1 (en) * | 1998-10-01 | 2001-01-02 | Alliedsignal Inc. | Spring-loaded vaned diffuser |
KR100388956B1 (ko) * | 2000-10-13 | 2003-06-25 | 삼성테크윈 주식회사 | 인터스테이지 실링 구조체를 갖는 가스터빈 엔진 |
KR100378484B1 (ko) * | 2000-10-13 | 2003-03-29 | 삼성테크윈 주식회사 | 인터스테이지 실링 구조체를 갖는 가스터빈 엔진 |
US6867383B1 (en) | 2003-03-28 | 2005-03-15 | Little Giant Pump Company | Liquid level assembly with diaphragm seal |
JP6817330B2 (ja) * | 2016-12-13 | 2021-01-20 | 三菱パワー株式会社 | ガスタービンの分解組立方法、シール板組立体及びガスタービンロータ |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB750597A (en) * | 1952-06-27 | 1956-06-20 | Kloeckner Humboldt Deutz Ag | Rotors for gas turbine installations and exhaust gas turboblower installations |
US3163003A (en) * | 1954-10-25 | 1964-12-29 | Garrett Corp | Gas turbine compressor |
US2946192A (en) * | 1958-05-16 | 1960-07-26 | Standard Motor Co Ltd | Gas turbine power plant |
US3116908A (en) * | 1961-04-04 | 1964-01-07 | Solar Aircraft Co | Split wheel gas turbine assembly |
GB970188A (en) * | 1963-01-31 | 1964-09-16 | Rolls Royce | Gas turbine vertical lift engine |
US3285005A (en) * | 1964-05-28 | 1966-11-15 | Continental Aviat & Eng Corp | Turbine engine construction |
US3263424A (en) * | 1965-03-25 | 1966-08-02 | Birmann Rudolph | Turbine-compressor unit |
US4040249A (en) * | 1975-06-24 | 1977-08-09 | Deere & Company | Single shaft gas turbine engine with axially mounted disk regenerator |
US4009568A (en) * | 1975-10-30 | 1977-03-01 | General Motors Corporation | Turbine support structure |
US4030288A (en) * | 1975-11-10 | 1977-06-21 | Caterpillar Tractor Co. | Modular gas turbine engine assembly |
US4712370A (en) * | 1986-04-24 | 1987-12-15 | The United States Of America As Represented By The Secretary Of The Air Force | Sliding duct seal |
US4932207A (en) * | 1988-12-28 | 1990-06-12 | Sundstrand Corporation | Segmented seal plate for a turbine engine |
US5033263A (en) * | 1989-03-17 | 1991-07-23 | Sundstrand Corporation | Compact gas turbine engine |
-
1990
- 1990-12-13 US US07/627,019 patent/US5125228A/en not_active Expired - Lifetime
-
1991
- 1991-11-06 EP EP92900421A patent/EP0515613B1/de not_active Expired - Lifetime
- 1991-11-06 DE DE69116137T patent/DE69116137T2/de not_active Expired - Fee Related
- 1991-11-06 WO PCT/US1991/008298 patent/WO1992010656A1/en active IP Right Grant
- 1991-11-06 JP JP4501889A patent/JPH05504812A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0515613A4 (en) | 1993-08-04 |
DE69116137T2 (de) | 1996-05-15 |
EP0515613A1 (de) | 1992-12-02 |
US5125228A (en) | 1992-06-30 |
WO1992010656A1 (en) | 1992-06-25 |
EP0515613B1 (de) | 1996-01-03 |
JPH05504812A (ja) | 1993-07-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Free format text: PATENTANWAELTE RUFF, WILHELM, BEIER, DAUSTER & PARTNER, 70173 STUTTGART |
|
8339 | Ceased/non-payment of the annual fee |