GB758669A - Improvements in or relating to axial-flow compressors - Google Patents
Improvements in or relating to axial-flow compressorsInfo
- Publication number
- GB758669A GB758669A GB30854/53A GB3085453A GB758669A GB 758669 A GB758669 A GB 758669A GB 30854/53 A GB30854/53 A GB 30854/53A GB 3085453 A GB3085453 A GB 3085453A GB 758669 A GB758669 A GB 758669A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flanges
- axial
- casing
- ring
- reinforcing webs
- 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
- 230000003014 reinforcing effect Effects 0.000 abstract 3
- 229910045601 alloy Inorganic materials 0.000 abstract 2
- 239000000956 alloy Substances 0.000 abstract 2
- 239000012530 fluid Substances 0.000 abstract 1
- 229910001234 light alloy Inorganic materials 0.000 abstract 1
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)
- Applications Or Details Of Rotary Compressors (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE533039D BE533039A (enrdf_load_stackoverflow) | 1953-11-06 | ||
GB30854/53A GB758669A (en) | 1953-11-06 | 1953-11-06 | Improvements in or relating to axial-flow compressors |
US464511A US2833463A (en) | 1953-11-06 | 1954-10-25 | Stator construction for axial flow compressor |
FR1111000D FR1111000A (fr) | 1953-11-06 | 1954-10-27 | Perfectionnements aux compresseurs axiaux |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB30854/53A GB758669A (en) | 1953-11-06 | 1953-11-06 | Improvements in or relating to axial-flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB758669A true GB758669A (en) | 1956-10-10 |
Family
ID=10314175
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30854/53A Expired GB758669A (en) | 1953-11-06 | 1953-11-06 | Improvements in or relating to axial-flow compressors |
Country Status (4)
Country | Link |
---|---|
US (1) | US2833463A (enrdf_load_stackoverflow) |
BE (1) | BE533039A (enrdf_load_stackoverflow) |
FR (1) | FR1111000A (enrdf_load_stackoverflow) |
GB (1) | GB758669A (enrdf_load_stackoverflow) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1054202B (de) * | 1956-12-18 | 1959-04-02 | Gen Electric | Leitschaufelanordnung fuer Axialverdichter von Gasturbinen |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB799896A (en) * | 1955-10-21 | 1958-08-13 | Rolls Royce | Improvements in or relating to axial-flow compressors |
GB938189A (en) * | 1960-10-29 | 1963-10-02 | Ruston & Hornsby Ltd | Improvements in the construction of turbine and compressor blade elements |
US3269702A (en) * | 1964-01-13 | 1966-08-30 | United Aircraft Corp | Nozzle vane assembly |
US4460315A (en) * | 1981-06-29 | 1984-07-17 | General Electric Company | Turbomachine rotor assembly |
US4907944A (en) * | 1984-10-01 | 1990-03-13 | General Electric Company | Turbomachinery blade mounting arrangement |
US4688992A (en) * | 1985-01-25 | 1987-08-25 | General Electric Company | Blade platform |
US5141395A (en) * | 1991-09-05 | 1992-08-25 | General Electric Company | Flow activated flowpath liner seal |
US8128354B2 (en) * | 2007-01-17 | 2012-03-06 | Siemens Energy, Inc. | Gas turbine engine |
US8894370B2 (en) * | 2008-04-04 | 2014-11-25 | General Electric Company | Turbine blade retention system and method |
FR2978197B1 (fr) * | 2011-07-22 | 2015-12-25 | Snecma | Distributeur de turbine de turbomachine et turbine comportant un tel distributeur |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE488535A (enrdf_load_stackoverflow) * | 1947-02-17 | |||
US2638743A (en) * | 1949-04-29 | 1953-05-19 | Ruston & Hornsby Ltd | Construction of turbine-inlet and stator elements of gas turbines |
-
0
- BE BE533039D patent/BE533039A/xx unknown
-
1953
- 1953-11-06 GB GB30854/53A patent/GB758669A/en not_active Expired
-
1954
- 1954-10-25 US US464511A patent/US2833463A/en not_active Expired - Lifetime
- 1954-10-27 FR FR1111000D patent/FR1111000A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1054202B (de) * | 1956-12-18 | 1959-04-02 | Gen Electric | Leitschaufelanordnung fuer Axialverdichter von Gasturbinen |
Also Published As
Publication number | Publication date |
---|---|
BE533039A (enrdf_load_stackoverflow) | |
FR1111000A (fr) | 1956-02-20 |
US2833463A (en) | 1958-05-06 |
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