GB1336400A - Final stage of a gas or steam turbine - Google Patents
Final stage of a gas or steam turbineInfo
- Publication number
- GB1336400A GB1336400A GB1336400DA GB1336400A GB 1336400 A GB1336400 A GB 1336400A GB 1336400D A GB1336400D A GB 1336400DA GB 1336400 A GB1336400 A GB 1336400A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- housing
- gas
- ordena
- steam turbine
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
-
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/04—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1336400 Turbine exhaust ducts MOSKOVSKOE ORDENA LENINA I ORDENA TRUDOVOGO KRASNOGO ZMANENI VYSSHEE TEKHNICHESKOE UCHILISCHE IMENI N E BAUMANA 16 May 1972 22836/72 Heading FIT [Also in Division F2] To prevent separation of the boundary layer from the convex wall 8 of a diffuser 4 downstream of the last stage of a steam or gas turbine, the rotor blades 3 of the latter are surrounded by a stationary ring 6 which defines with the housing 1 a convergent annular passage 7 through which some of the working fluid is by-passed around the blades 3 and directed against wall 8. Ring 6 is secured to housing 1 or to stator blades 2.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH708872 | 1972-05-12 | ||
GB2283672 | 1972-05-16 | ||
DE2225615A DE2225615B2 (en) | 1972-05-12 | 1972-05-26 | Output stage of a gas or steam turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1336400A true GB1336400A (en) | 1973-11-07 |
Family
ID=27175697
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1336400D Expired GB1336400A (en) | 1972-05-12 | 1972-05-16 | Final stage of a gas or steam turbine |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH539774A (en) |
DE (1) | DE2225615B2 (en) |
GB (1) | GB1336400A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT383396B (en) * | 1984-08-17 | 1987-06-25 | Proizv Ob Turbostroenia | LOW PRESSURE CYLINDERS OF A STEAM TURBINE |
-
1972
- 1972-05-12 CH CH708872A patent/CH539774A/en not_active IP Right Cessation
- 1972-05-16 GB GB1336400D patent/GB1336400A/en not_active Expired
- 1972-05-26 DE DE2225615A patent/DE2225615B2/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE2225615B2 (en) | 1974-10-24 |
DE2225615A1 (en) | 1973-12-06 |
CH539774A (en) | 1973-09-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |