BE570533A - - Google Patents
Info
- Publication number
- BE570533A BE570533A BE570533DA BE570533A BE 570533 A BE570533 A BE 570533A BE 570533D A BE570533D A BE 570533DA BE 570533 A BE570533 A BE 570533A
- Authority
- BE
- Belgium
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
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US679623A US2984454A (en) | 1957-08-22 | 1957-08-22 | Stator units |
Publications (1)
Publication Number | Publication Date |
---|---|
BE570533A true BE570533A (fr) |
Family
ID=24727658
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE570533D BE570533A (fr) | 1957-08-22 |
Country Status (7)
Country | Link |
---|---|
US (1) | US2984454A (fr) |
BE (1) | BE570533A (fr) |
CH (1) | CH362269A (fr) |
DE (1) | DE1114364B (fr) |
FR (1) | FR1211581A (fr) |
GB (1) | GB893579A (fr) |
NL (2) | NL230456A (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3062499A (en) * | 1960-05-18 | 1962-11-06 | United Aircraft Corp | Vane mounting and seal |
US3075744A (en) * | 1960-08-16 | 1963-01-29 | United Aircraft Corp | Turbine nozzle vane mounting means |
GB1086432A (en) * | 1965-09-21 | 1967-10-11 | Bristol Siddeley Engines Ltd | Gas turbine engines |
US3423071A (en) * | 1967-07-17 | 1969-01-21 | United Aircraft Corp | Turbine vane retention |
US3511577A (en) * | 1968-04-10 | 1970-05-12 | Caterpillar Tractor Co | Turbine nozzle construction |
US3730640A (en) * | 1971-06-28 | 1973-05-01 | United Aircraft Corp | Seal ring for gas turbine |
US4425078A (en) * | 1980-07-18 | 1984-01-10 | United Technologies Corporation | Axial flexible radially stiff retaining ring for sealing in a gas turbine engine |
US4478551A (en) * | 1981-12-08 | 1984-10-23 | United Technologies Corporation | Turbine exhaust case design |
US4512712A (en) * | 1983-08-01 | 1985-04-23 | United Technologies Corporation | Turbine stator assembly |
GB2151709B (en) * | 1983-12-19 | 1988-07-27 | Gen Electric | Improvements in gas turbine engines |
US4720236A (en) * | 1984-12-21 | 1988-01-19 | United Technologies Corporation | Coolable stator assembly for a gas turbine engine |
FR2624913B1 (fr) * | 1987-12-16 | 1990-04-20 | Snecma | Dispositif de fixation a vis d'une piece de revolution sur une bride annulaire de turbomachine |
US5411370A (en) * | 1994-08-01 | 1995-05-02 | United Technologies Corporation | Vibration damping shroud for a turbomachine vane |
DE10133393B4 (de) | 2001-07-13 | 2007-08-30 | TransMIT Gesellschaft für Technologietransfer mbH | Röhrchen mit Innendurchmessern im Nanometerbereich |
US6884029B2 (en) * | 2002-09-26 | 2005-04-26 | Siemens Westinghouse Power Corporation | Heat-tolerated vortex-disrupting fluid guide component |
US7527469B2 (en) * | 2004-12-10 | 2009-05-05 | Siemens Energy, Inc. | Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine |
US9963989B2 (en) * | 2013-06-12 | 2018-05-08 | United Technologies Corporation | Gas turbine engine vane-to-transition duct seal |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB589542A (en) * | 1941-09-22 | 1947-06-24 | Karl Baumann | Improvements in internal combustion turbines |
BE471940A (fr) * | 1946-03-20 | |||
BE487120A (fr) * | 1946-03-25 | |||
FR964211A (fr) * | 1947-04-03 | 1950-08-08 | ||
FR965713A (fr) * | 1947-05-07 | 1950-09-20 | ||
US2654566A (en) * | 1950-02-11 | 1953-10-06 | A V Roe Canada Ltd | Turbine nozzle guide vane construction |
GB741138A (en) * | 1952-10-03 | 1955-11-30 | Vickers Electrical Co Ltd | Improvements relating to gas turbines |
US2942844A (en) * | 1952-12-22 | 1960-06-28 | Gen Motors Corp | Turbine nozzle |
BE529252A (fr) * | 1953-06-01 |
-
0
- BE BE570533D patent/BE570533A/xx unknown
- NL NL99435D patent/NL99435C/xx active
- NL NL230456D patent/NL230456A/xx unknown
-
1957
- 1957-08-22 US US679623A patent/US2984454A/en not_active Expired - Lifetime
-
1958
- 1958-08-02 DE DEU5516A patent/DE1114364B/de active Pending
- 1958-08-21 GB GB26924/58A patent/GB893579A/en not_active Expired
- 1958-08-21 FR FR1211581D patent/FR1211581A/fr not_active Expired
- 1958-08-22 CH CH362269D patent/CH362269A/de unknown
Also Published As
Publication number | Publication date |
---|---|
GB893579A (en) | 1962-04-11 |
US2984454A (en) | 1961-05-16 |
NL230456A (fr) | |
CH362269A (de) | 1962-05-31 |
FR1211581A (fr) | 1960-03-17 |
DE1114364B (de) | 1961-09-28 |
NL99435C (fr) |