GB776988A - Means for fixing nozzles in turbine casings - Google Patents
Means for fixing nozzles in turbine casingsInfo
- Publication number
- GB776988A GB776988A GB2893454A GB2893454A GB776988A GB 776988 A GB776988 A GB 776988A GB 2893454 A GB2893454 A GB 2893454A GB 2893454 A GB2893454 A GB 2893454A GB 776988 A GB776988 A GB 776988A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- retaining ring
- ring
- blocks
- face
- 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
- F01D9/047—Nozzle boxes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
776,988. Turbines. BRITISH THOMSONHOUSTON CO., Ltd. Sept. 27, 1955 [Oct. 7, 1954], No. 28934/54. Class 110 (3). Means for fixing nozzles in a turbine casing comprises a nozzle ring 2 having inner and outer peripheries 4, 5 constituting oppositely directed conical surfaces with the inner surface 4 tapering toward the inlet side of the nozzle and located in a corresponding shaped recess 6 in the turbine casing 1, a retaining ring 7 having inwardly tapering faces 8, 9, with a face 8 tapered at an angle to correspond and mate with the outer periphery of the nozzle ring 2 and a plurality of location blocks 10 each having a tapered face in contact with the retaining ring and an opposite face in contact with an abutment 11 on the casing and radially disposed screw means 12 for forcing the blocks radially outward to tighten the retaining ring against the nozzle ring. The nozzle and retaining rings are conveniently made in semi-circular segments for ease of assembly, but either of these rings may be made of three or more segments. The clearance holes through the blocks 10 are tapped at 13 to facilitate removal. In a modification, the retaining ring is extended axially and used to support an inter-stage set of fixed blades.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2893454A GB776988A (en) | 1954-10-07 | 1954-10-07 | Means for fixing nozzles in turbine casings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2893454A GB776988A (en) | 1954-10-07 | 1954-10-07 | Means for fixing nozzles in turbine casings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB776988A true GB776988A (en) | 1957-06-12 |
Family
ID=10283560
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2893454A Expired GB776988A (en) | 1954-10-07 | 1954-10-07 | Means for fixing nozzles in turbine casings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB776988A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3817655A (en) * | 1972-11-22 | 1974-06-18 | Carrier Corp | Stator blade mounting structure for turbomachines |
US4097188A (en) * | 1976-04-15 | 1978-06-27 | Terence Owen Forster | Nozzle insert for a turbine |
EP0359986A1 (en) * | 1988-09-06 | 1990-03-28 | Westinghouse Electric Corporation | Apparatus for supporting the torque load on a gasturbine vane |
-
1954
- 1954-10-07 GB GB2893454A patent/GB776988A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3817655A (en) * | 1972-11-22 | 1974-06-18 | Carrier Corp | Stator blade mounting structure for turbomachines |
US4097188A (en) * | 1976-04-15 | 1978-06-27 | Terence Owen Forster | Nozzle insert for a turbine |
EP0359986A1 (en) * | 1988-09-06 | 1990-03-28 | Westinghouse Electric Corporation | Apparatus for supporting the torque load on a gasturbine vane |
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