GB673062A - Improvements in guiding means for annular flow of fluids - Google Patents
Improvements in guiding means for annular flow of fluidsInfo
- Publication number
- GB673062A GB673062A GB34939/47A GB3493947A GB673062A GB 673062 A GB673062 A GB 673062A GB 34939/47 A GB34939/47 A GB 34939/47A GB 3493947 A GB3493947 A GB 3493947A GB 673062 A GB673062 A GB 673062A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- flow
- turbine
- helical
- admission
- 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
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/0015—Whirl chambers
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/16—Stators
- F03B3/18—Stator blades; Guide conduits or vanes, e.g. adjustable
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
Abstract
673,062. Hydraulic turbines; radial-flow pumps. ABBEY, A. (Soc. Financiere d-Expansion Commerciale et Industrielle Soc. Anon Sfinder). Dec. 31, 1947, No. 34939/47. Classes 110(i) and 110(iii) [Also in Groups XI and XXIX] Annular flow of fluid takes place between two surfaces of revolution and a helical surface which has at least one thread. and is constant in pitch over the range of regulation, at least one of the surfaces having a helical movement with respect to the others with a pitch equal to that of the helical surface, for the purpose of regulating the flow. Fig. 8 shows a Kaplan turbine in which the inlet guide comprises a conical surface 1 and helical surface 3, regulation being effected by a screwing movement of :a control surface 2. In the turbine shown in Fig. 9, the control surface 2 is formed by the free surface 29 of the water or other working fluid. The free surface is adjusted by varying the pressure of air within a bell 25. Instead of air, mercury or other plastic liquid or gaseous merium which does not mix or emulsify with the working fluid and is substantially different in density from it may be used. Fig. 10 shows a turbine in which admission is regulated by simultaneous adjustment of members 40 and 41. The flow through the rotor is bounded at its inner periphery by a free surface 45, the position of which is determined by the volume of flow. The flow may be'directed outwardly instead of inwardly as shown. In the turbine (which may be modified to act as a pump) shown in Fig. 6, the working fluid from an annular nozzle 6 passes through rotor passages 9, 10 and is discharged through a pipe 12. Admission is 'varied by admitting pressure water to the space above a cover 24 so as to cause axial displacement of the rotor 17 and thus of a control surface 8 and a control member 11, both of which are carried by the rotor. To avoid impact losses consequent upon alteration of the pressure at the turbine inlet, the positions of a control member 7 with respect to the :surface 8 and of the control member 11 with respect to a surface 14 are automically regulated by the admission of pressure water to chambers 20, 21 and 22, 23 in accordance with the pressure difference set up at the inlet edges 18, 19 of the spiral surfaces of the rotor and charge pipe, respectively. The regulation of the spiral surfaces of the rotor and dismay be effected through a servomotor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34939/47A GB673062A (en) | 1947-12-31 | 1947-12-31 | Improvements in guiding means for annular flow of fluids |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34939/47A GB673062A (en) | 1947-12-31 | 1947-12-31 | Improvements in guiding means for annular flow of fluids |
Publications (1)
Publication Number | Publication Date |
---|---|
GB673062A true GB673062A (en) | 1952-06-04 |
Family
ID=10371821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34939/47A Expired GB673062A (en) | 1947-12-31 | 1947-12-31 | Improvements in guiding means for annular flow of fluids |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB673062A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0017829A1 (en) * | 1979-04-09 | 1980-10-29 | Arthur Milz | Centrifugal pump and its housing |
GB2128107A (en) * | 1982-10-01 | 1984-04-26 | Spraying Systems Co | Whirl spray nozzle |
US4664314A (en) * | 1982-10-01 | 1987-05-12 | Spraying Systems Co. | Whirl spray nozzle |
RU2563287C2 (en) * | 2010-08-18 | 2015-09-20 | Владимир Григорьевич Иванов | Water-pressure engine |
-
1947
- 1947-12-31 GB GB34939/47A patent/GB673062A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0017829A1 (en) * | 1979-04-09 | 1980-10-29 | Arthur Milz | Centrifugal pump and its housing |
GB2128107A (en) * | 1982-10-01 | 1984-04-26 | Spraying Systems Co | Whirl spray nozzle |
US4664314A (en) * | 1982-10-01 | 1987-05-12 | Spraying Systems Co. | Whirl spray nozzle |
RU2563287C2 (en) * | 2010-08-18 | 2015-09-20 | Владимир Григорьевич Иванов | Water-pressure engine |
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