GB704609A - Improvements in or relating to multi-stage axial-flow compressors or turbines - Google Patents
Improvements in or relating to multi-stage axial-flow compressors or turbinesInfo
- Publication number
- GB704609A GB704609A GB1918050A GB1918050A GB704609A GB 704609 A GB704609 A GB 704609A GB 1918050 A GB1918050 A GB 1918050A GB 1918050 A GB1918050 A GB 1918050A GB 704609 A GB704609 A GB 704609A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shell
- discs
- slots
- secured
- blades
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
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)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1918050A GB704609A (en) | 1950-08-01 | 1950-08-01 | Improvements in or relating to multi-stage axial-flow compressors or turbines |
FR1057994D FR1057994A (fr) | 1950-08-01 | 1952-04-08 | Perfectionnements aux rotors de turbo-machines |
CH301115D CH301115A (de) | 1950-08-01 | 1952-04-09 | Rotor für eine axial beaufschlagte Turbomaschine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1918050A GB704609A (en) | 1950-08-01 | 1950-08-01 | Improvements in or relating to multi-stage axial-flow compressors or turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB704609A true GB704609A (en) | 1954-02-24 |
Family
ID=10125074
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1918050A Expired GB704609A (en) | 1950-08-01 | 1950-08-01 | Improvements in or relating to multi-stage axial-flow compressors or turbines |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH301115A (fr) |
FR (1) | FR1057994A (fr) |
GB (1) | GB704609A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3173655A (en) * | 1961-09-08 | 1965-03-16 | Stalker Corp | Bladed rotor |
US7147436B2 (en) * | 2004-04-15 | 2006-12-12 | United Technologies Corporation | Turbine engine rotor retainer |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1095453B (de) * | 1955-07-18 | 1960-12-22 | Rolls Royce | Mehrstufige Axialstroemungsmaschine |
DE1140306B (de) * | 1958-07-17 | 1962-11-29 | Daimler Benz Ag | Trommellaeufer fuer Axialstroemungsmaschinen, insbesondere Verdichter |
US4310286A (en) * | 1979-05-17 | 1982-01-12 | United Technologies Corporation | Rotor assembly having a multistage disk |
-
1950
- 1950-08-01 GB GB1918050A patent/GB704609A/en not_active Expired
-
1952
- 1952-04-08 FR FR1057994D patent/FR1057994A/fr not_active Expired
- 1952-04-09 CH CH301115D patent/CH301115A/de unknown
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3173655A (en) * | 1961-09-08 | 1965-03-16 | Stalker Corp | Bladed rotor |
US7147436B2 (en) * | 2004-04-15 | 2006-12-12 | United Technologies Corporation | Turbine engine rotor retainer |
Also Published As
Publication number | Publication date |
---|---|
CH301115A (de) | 1954-08-31 |
FR1057994A (fr) | 1954-03-12 |
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