FR944756A - Perfectionnements aux aubes de guidage des compresseurs et turbines du type axial - Google Patents
Perfectionnements aux aubes de guidage des compresseurs et turbines du type axialInfo
- Publication number
- FR944756A FR944756A FR944756DA FR944756A FR 944756 A FR944756 A FR 944756A FR 944756D A FR944756D A FR 944756DA FR 944756 A FR944756 A FR 944756A
- Authority
- FR
- France
- Prior art keywords
- compressors
- guide vanes
- axial type
- type turbines
- turbines
- 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
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB257532X | 1946-04-05 | ||
| GB30147X | 1947-01-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR944756A true FR944756A (fr) | 1949-04-14 |
Family
ID=26237928
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR944756D Expired FR944756A (fr) | 1946-04-05 | 1947-04-05 | Perfectionnements aux aubes de guidage des compresseurs et turbines du type axial |
Country Status (5)
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1278178B (de) * | 1966-06-10 | 1968-09-19 | Rolls Royce | Eintrittsleitschaufelkranz fuer Axialverdichter von Gasturbinentriebwerken |
Families Citing this family (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2654566A (en) * | 1950-02-11 | 1953-10-06 | A V Roe Canada Ltd | Turbine nozzle guide vane construction |
| US2932485A (en) * | 1954-10-01 | 1960-04-12 | United Aircraft Corp | Stator construction |
| DE1067971B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * | 1955-10-18 | 1959-10-29 | ||
| US2915280A (en) * | 1957-04-18 | 1959-12-01 | Gen Electric | Nozzle and seal assembly |
| NL104794C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * | 1957-08-16 | |||
| US3072380A (en) * | 1959-02-05 | 1963-01-08 | Dresser Ind | Stator blade carrier assembly mounting |
| US3075744A (en) * | 1960-08-16 | 1963-01-29 | United Aircraft Corp | Turbine nozzle vane mounting means |
| US3423071A (en) * | 1967-07-17 | 1969-01-21 | United Aircraft Corp | Turbine vane retention |
| GB2192233B (en) * | 1986-07-02 | 1990-11-28 | Rolls Royce Plc | A gas turbine engine load transfer structure |
| US4861229A (en) * | 1987-11-16 | 1989-08-29 | Williams International Corporation | Ceramic-matrix composite nozzle assembly for a turbine engine |
| US5494402A (en) * | 1994-05-16 | 1996-02-27 | Solar Turbines Incorporated | Low thermal stress ceramic turbine nozzle |
| US6517313B2 (en) * | 2001-06-25 | 2003-02-11 | Pratt & Whitney Canada Corp. | Segmented turbine vane support structure |
| US8096746B2 (en) * | 2007-12-13 | 2012-01-17 | Pratt & Whitney Canada Corp. | Radial loading element for turbine vane |
| FR2935430B1 (fr) * | 2008-08-26 | 2012-03-09 | Snecma | Turbine haute-pression de turbomachine amelioree, secteur de distributeur et moteur d'aeronef associes |
| US9702252B2 (en) * | 2012-12-19 | 2017-07-11 | Honeywell International Inc. | Turbine nozzles with slip joints and methods for the production thereof |
| US20140255174A1 (en) * | 2012-12-21 | 2014-09-11 | United Technologies Corporation | Manufacture of full ring strut vane pack |
| US9816387B2 (en) | 2014-09-09 | 2017-11-14 | United Technologies Corporation | Attachment faces for clamped turbine stator of a gas turbine engine |
| EP3763917A1 (de) * | 2019-07-08 | 2021-01-13 | MTU Aero Engines GmbH | Leitschaufelsegment mit stützabschnittsrippe |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB191016889A (en) * | 1910-07-15 | 1910-10-20 | James Howden | Improvements in Means for Fixing Blades in Turbines. |
| US2402418A (en) * | 1943-01-20 | 1946-06-18 | Westinghouse Electric Corp | Turbine apparatus |
| US2427244A (en) * | 1944-03-07 | 1947-09-09 | Gen Electric | Gas turbine |
-
0
- BE BE487115D patent/BE487115A/xx unknown
-
1946
- 1946-04-05 GB GB10630/46A patent/GB611326A/en not_active Expired
-
1947
- 1947-01-31 CH CH257532D patent/CH257532A/de unknown
- 1947-02-10 US US727520A patent/US2605997A/en not_active Expired - Lifetime
- 1947-04-05 FR FR944756D patent/FR944756A/fr not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1278178B (de) * | 1966-06-10 | 1968-09-19 | Rolls Royce | Eintrittsleitschaufelkranz fuer Axialverdichter von Gasturbinentriebwerken |
Also Published As
| Publication number | Publication date |
|---|---|
| US2605997A (en) | 1952-08-05 |
| CH257532A (de) | 1948-10-15 |
| GB611326A (en) | 1948-10-28 |
| BE487115A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) |
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