GB885399A - Improvements in or relating to turbines - Google Patents
Improvements in or relating to turbinesInfo
- Publication number
- GB885399A GB885399A GB1394459A GB1394459A GB885399A GB 885399 A GB885399 A GB 885399A GB 1394459 A GB1394459 A GB 1394459A GB 1394459 A GB1394459 A GB 1394459A GB 885399 A GB885399 A GB 885399A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring member
- ring
- turbine
- casing
- flange
- 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
- F01D9/045—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial flow machines or engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
885,399. Radial flow turbines. BUCHI, A. J. April 23, 1959, No. 13944/59. Addition to 825,596. Class 110 (3). A turbine comprises a casing A, at least one row of stator blades 1, a bladed rotor C and a ring member B<SP>1</SP> which forms one wall of the space in which the bladed rotor operates. First means are provided for detachably securing the ring member B<SP>1</SP> to the turbine casing A and second means separate from the first are provided for detachably securing the stator blade ring B to the ring member B<SP>1</SP>, thus permitting rotors of different sizes to be used with the same casing by utilizing ring members of different sizes. The turbine shown is an inward radialflow exhaust gas turbine and the ring member B<SP>1</SP> is formed with a flange 6 which is secured by means of studs 4 to the face 7 of the casing A. The stator blade ring B carries a row of stator blades 1 and is secured against circumferential movement with respect to the ring member B<SP>1</SP> by means of pins 7<SP>1</SP>. The blades 1 have cylindrical root portions 1b which are secured to the ring B by means of welding. The turbine exhaust duct D is formed with a radial flange 5 which is secured against the flange 6 of the ring member B<SP>1</SP> by means of the nuts 8 on the studs 4. Specification 823,226 also is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1394459A GB885399A (en) | 1959-04-23 | 1959-04-23 | Improvements in or relating to turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1394459A GB885399A (en) | 1959-04-23 | 1959-04-23 | Improvements in or relating to turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB885399A true GB885399A (en) | 1961-12-28 |
Family
ID=10032198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1394459A Expired GB885399A (en) | 1959-04-23 | 1959-04-23 | Improvements in or relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB885399A (en) |
-
1959
- 1959-04-23 GB GB1394459A patent/GB885399A/en not_active Expired
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