GB1123886A - Double opposed axial-flow elastic fluid turbines - Google Patents
Double opposed axial-flow elastic fluid turbinesInfo
- Publication number
- GB1123886A GB1123886A GB19623/67A GB1962367A GB1123886A GB 1123886 A GB1123886 A GB 1123886A GB 19623/67 A GB19623/67 A GB 19623/67A GB 1962367 A GB1962367 A GB 1962367A GB 1123886 A GB1123886 A GB 1123886A
- Authority
- GB
- United Kingdom
- Prior art keywords
- annular wall
- radial
- shrouds
- seals
- rows
- 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
- F01D25/26—Double casings; Measures against temperature strain in casings
-
- 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
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
- F01D3/02—Machines or engines with axial-thrust balancing effected by working-fluid characterised by having one fluid flow in one axial direction and another fluid flow in the opposite direction
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,123,886. Elastic-fluid turbines. WESTINGHOUSE ELECTRIC CORP. April 28, 1967 [June 28, 1966], No. 19623/67. Heading F1T. A central admission double opposed-flow axialflow plastic-fluid turbine comprises a pair of rows of stator vanes 16, 20, Fig. 5, co-operating with a pair of rows of first-stage rotor blades 18 and having shrouds 40, 42 which jointly define in part an annular space 28 into which the motive fluid is admitted, a stationary annular wall 44 spanning the axial space between the rows of stator vanes and having axially opposed peripheral marginal portions 45, 46 disposed in lapping relation with the shrouds 40, 42 with seals 50, 51 interposed between them, the seals being carried by either the shrouds or, as shown, the marginal portions. The seals 50, 51, which permit relative thermal expansion of the parts, are of arcuate segmental form, and located in peripheral grooves 47, 48, each segment being pressed outwards by a leaf spring 52, Figs. 4 and 5, located in the groove. The upper and lower halves 44a, 44b of the annular wall 44 are provided with pairs of diametricallyopposed radial struts 61, 55 respectively which are bolted together to unite the two halves. Each strut 55 has a slot 58 engaged by a key 59 and a bolt 57 carried by a flange 56 fixed to the lower half 21b of the outer casing of the turbine whereby movement of the strut is restricted in all but the radial direction. Additionally, each annular wall half 44a, 44b has a vertical dowel (69), Fig.3 (not shown), engaging a radial bore in a member (67) carried by the outer casing and permitting radial movement only. Radial expansion of the annular wall 44 is thereby allowed.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US561207A US3408045A (en) | 1966-06-28 | 1966-06-28 | Turbine nozzle seal structure |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1123886A true GB1123886A (en) | 1968-08-14 |
Family
ID=24241073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB19623/67A Expired GB1123886A (en) | 1966-06-28 | 1967-04-28 | Double opposed axial-flow elastic fluid turbines |
Country Status (2)
Country | Link |
---|---|
US (1) | US3408045A (en) |
GB (1) | GB1123886A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2512106A1 (en) * | 1981-09-03 | 1983-03-04 | Sud Ouest Ind Cie Fse Develop | Axial flow thermodynamic turbine - has central inlet between two sets of vaned wheels on common shaft |
GB2425809A (en) * | 2005-05-06 | 2006-11-08 | Gen Electric | Mounting a diaphragm within a steam turbine casing |
CN109477398A (en) * | 2016-08-16 | 2019-03-15 | 通用电器技术有限公司 | With the axial-flow turbine in the punishment of horizontal composition plane at the flow guiding disc of two half-unit |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE312813B (en) * | 1967-07-11 | 1969-07-28 | Stal Laval Turbin Ab | |
US3529901A (en) * | 1968-11-18 | 1970-09-22 | Westinghouse Electric Corp | Turbine motive fluid inlet seal structure |
US4479756A (en) * | 1978-08-21 | 1984-10-30 | Roy E. Roth Company | Multi-stage pump |
US4871295A (en) * | 1983-04-19 | 1989-10-03 | Ormat Turbines (1965) Ltd. | Modular rankine cycle vapor turbine |
US4764084A (en) * | 1987-11-23 | 1988-08-16 | Westinghouse Electric Corp. | Inlet flow guide for a low pressure turbine |
US4863341A (en) * | 1988-05-13 | 1989-09-05 | Westinghouse Electric Corp. | Turbine having semi-isolated inlet |
EP2772617B1 (en) * | 2013-02-27 | 2018-11-28 | Ansaldo Energia Switzerland AG | Rotary flow machine with support means |
US10385832B2 (en) * | 2013-06-28 | 2019-08-20 | Exxonmobil Upstream Research Company | Systems and methods of utilizing axial flow expanders |
WO2014208777A1 (en) | 2013-06-28 | 2014-12-31 | Mitsubishi Heavy Industries Compressor Corporation | Axial flow expander |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL302648A (en) * |
-
1966
- 1966-06-28 US US561207A patent/US3408045A/en not_active Expired - Lifetime
-
1967
- 1967-04-28 GB GB19623/67A patent/GB1123886A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2512106A1 (en) * | 1981-09-03 | 1983-03-04 | Sud Ouest Ind Cie Fse Develop | Axial flow thermodynamic turbine - has central inlet between two sets of vaned wheels on common shaft |
GB2425809A (en) * | 2005-05-06 | 2006-11-08 | Gen Electric | Mounting a diaphragm within a steam turbine casing |
US7329098B2 (en) | 2005-05-06 | 2008-02-12 | Geenral Electric Company | Adjustable support bar with adjustable shim design for steam turbine diaphragms |
GB2425809A8 (en) * | 2005-05-06 | 2010-07-07 | Gen Electric | Adjustable support bar with adjustable shim designfor steam turbine diaphragms |
CN109477398A (en) * | 2016-08-16 | 2019-03-15 | 通用电器技术有限公司 | With the axial-flow turbine in the punishment of horizontal composition plane at the flow guiding disc of two half-unit |
CN109477398B (en) * | 2016-08-16 | 2022-02-15 | 通用电器技术有限公司 | Axial turbine with a diaphragm divided into two halves at a horizontal joint plane |
Also Published As
Publication number | Publication date |
---|---|
US3408045A (en) | 1968-10-29 |
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