GB208681A - Improvements in and relating to steam or gas turbines, turbocompressors and the like - Google Patents
Improvements in and relating to steam or gas turbines, turbocompressors and the likeInfo
- Publication number
- GB208681A GB208681A GB15918/23A GB1591823A GB208681A GB 208681 A GB208681 A GB 208681A GB 15918/23 A GB15918/23 A GB 15918/23A GB 1591823 A GB1591823 A GB 1591823A GB 208681 A GB208681 A GB 208681A
- Authority
- GB
- United Kingdom
- Prior art keywords
- diaphragms
- diaphragm
- turbocompressors
- turbines
- steam
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
208,681. Erste Br³nner Maschinen Fabriks Ges. Feb. 23, 1923, [Convention date]. Casings.-Relates to the method of mounting the nozzle diaphragms for turbines and' turbocompressors described in Specification 208,664, [Class 110 (iii), Turbines, &c.], in avoiding the use of separate split liners by employing a single diaphragm a<1> as the supporting body for each group of diaphragms a, this diaphragm a<1> having an annular flange z fitting with radial clearance a casing groove f. The diaphragms a may be connected to the supporting diaphragm a<1> by bolts h, as shown to the left of the Figure, or, as shown to the right, the diaphragm a<1> may be constructed as a split bush, and the diaphragms a secured thereto by a series of separate milled' blades e.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT208681X | 1923-02-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB208681A true GB208681A (en) | 1923-12-27 |
Family
ID=3669654
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB15918/23A Expired GB208681A (en) | 1923-02-23 | 1923-06-19 | Improvements in and relating to steam or gas turbines, turbocompressors and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB208681A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2447942A (en) * | 1944-12-05 | 1948-08-24 | Rateau Soc | Turbine distributor and nozzle |
| US5104288A (en) * | 1990-12-10 | 1992-04-14 | Westinghouse Electric Corp. | Dual plane bolted joint for separately-supported segmental stationary turbine blade assemblies |
| WO1997005364A1 (en) * | 1995-07-28 | 1997-02-13 | Siemens Aktiengesellschaft | Guide blade structure and its use in a steam turbine |
-
1923
- 1923-06-19 GB GB15918/23A patent/GB208681A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2447942A (en) * | 1944-12-05 | 1948-08-24 | Rateau Soc | Turbine distributor and nozzle |
| US5104288A (en) * | 1990-12-10 | 1992-04-14 | Westinghouse Electric Corp. | Dual plane bolted joint for separately-supported segmental stationary turbine blade assemblies |
| WO1997005364A1 (en) * | 1995-07-28 | 1997-02-13 | Siemens Aktiengesellschaft | Guide blade structure and its use in a steam turbine |
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