NO752644L - - Google Patents
Info
- Publication number
- NO752644L NO752644L NO752644A NO752644A NO752644L NO 752644 L NO752644 L NO 752644L NO 752644 A NO752644 A NO 752644A NO 752644 A NO752644 A NO 752644A NO 752644 L NO752644 L NO 752644L
- Authority
- NO
- Norway
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)
- Fats And Perfumes (AREA)
- Polysaccharides And Polysaccharide Derivatives (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US492574A US3918832A (en) | 1974-07-29 | 1974-07-29 | Stator construction for an axial flow compressor |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| NO752644L true NO752644L (de) | 1976-01-30 |
| NO149010B NO149010B (no) | 1983-10-17 |
| NO149010C NO149010C (no) | 1984-01-25 |
Family
ID=23956790
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO75752644A NO149010C (no) | 1974-07-29 | 1975-07-28 | Kompressor. |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US3918832A (de) |
| JP (1) | JPS6050999B2 (de) |
| BR (1) | BR7504846A (de) |
| CA (1) | CA1027870A (de) |
| CH (1) | CH589229A5 (de) |
| DE (1) | DE2532554C2 (de) |
| FR (1) | FR2280812A1 (de) |
| GB (1) | GB1511019A (de) |
| IT (1) | IT1040063B (de) |
| NO (1) | NO149010C (de) |
| SE (1) | SE419260B (de) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5167488A (en) * | 1991-07-03 | 1992-12-01 | General Electric Company | Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments |
| EP0763653B1 (de) * | 1995-09-13 | 2001-07-18 | SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) | Strahlumkehrgitter für eine Schubumkehrvorrichtungsklappe |
| US6234750B1 (en) * | 1999-03-12 | 2001-05-22 | General Electric Company | Interlocked compressor stator |
| US7743497B2 (en) * | 2005-10-06 | 2010-06-29 | General Electric Company | Method of providing non-uniform stator vane spacing in a compressor |
| US10280779B2 (en) | 2013-09-10 | 2019-05-07 | United Technologies Corporation | Plug seal for gas turbine engine |
| WO2015119687A2 (en) | 2013-11-11 | 2015-08-13 | United Technologies Corporation | Segmented seal for gas turbine engine |
| US10634055B2 (en) | 2015-02-05 | 2020-04-28 | United Technologies Corporation | Gas turbine engine having section with thermally isolated area |
| US9920652B2 (en) | 2015-02-09 | 2018-03-20 | United Technologies Corporation | Gas turbine engine having section with thermally isolated area |
| US11248622B2 (en) * | 2016-09-02 | 2022-02-15 | Raytheon Technologies Corporation | Repeating airfoil tip strong pressure profile |
| US10550725B2 (en) * | 2016-10-19 | 2020-02-04 | United Technologies Corporation | Engine cases and associated flange |
| US11629606B2 (en) * | 2021-05-26 | 2023-04-18 | General Electric Company | Split-line stator vane assembly |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2857093A (en) * | 1954-12-02 | 1958-10-21 | Cincinnati Testing & Res Lab | Stator casing and blade assembly |
| GB800098A (en) * | 1955-10-31 | 1958-08-20 | Rolls Royce | Improvements in or relating to multi-stage axial-flow compressors |
| US2997275A (en) * | 1959-03-23 | 1961-08-22 | Westinghouse Electric Corp | Stator structure for axial-flow fluid machine |
| US3302926A (en) * | 1965-12-06 | 1967-02-07 | Gen Electric | Segmented nozzle diaphragm for high temperature turbine |
| US3326523A (en) * | 1965-12-06 | 1967-06-20 | Gen Electric | Stator vane assembly having composite sectors |
| US3773430A (en) * | 1972-03-17 | 1973-11-20 | Ingersoll Rand Co | Gas compressor |
-
1974
- 1974-07-29 US US492574A patent/US3918832A/en not_active Expired - Lifetime
-
1975
- 1975-07-02 CA CA230,590A patent/CA1027870A/en not_active Expired
- 1975-07-16 CH CH927875A patent/CH589229A5/xx not_active IP Right Cessation
- 1975-07-21 DE DE2532554A patent/DE2532554C2/de not_active Expired
- 1975-07-23 SE SE7508371A patent/SE419260B/xx not_active IP Right Cessation
- 1975-07-25 FR FR7523244A patent/FR2280812A1/fr active Granted
- 1975-07-25 GB GB31284/75A patent/GB1511019A/en not_active Expired
- 1975-07-25 IT IT25778/75A patent/IT1040063B/it active
- 1975-07-28 JP JP50091848A patent/JPS6050999B2/ja not_active Expired
- 1975-07-28 NO NO75752644A patent/NO149010C/no unknown
- 1975-07-29 BR BR7504846*A patent/BR7504846A/pt unknown
Also Published As
| Publication number | Publication date |
|---|---|
| GB1511019A (en) | 1978-05-17 |
| CA1027870A (en) | 1978-03-14 |
| DE2532554C2 (de) | 1985-05-23 |
| NO149010B (no) | 1983-10-17 |
| FR2280812A1 (fr) | 1976-02-27 |
| CH589229A5 (de) | 1977-06-30 |
| JPS6050999B2 (ja) | 1985-11-11 |
| JPS5138112A (de) | 1976-03-30 |
| IT1040063B (it) | 1979-12-20 |
| US3918832A (en) | 1975-11-11 |
| SE419260B (sv) | 1981-07-20 |
| BR7504846A (pt) | 1976-07-06 |
| FR2280812B1 (de) | 1980-09-26 |
| NO149010C (no) | 1984-01-25 |
| DE2532554A1 (de) | 1976-02-19 |
| SE7508371L (sv) | 1976-01-30 |