GB673062A - Improvements in guiding means for annular flow of fluids - Google Patents

Improvements in guiding means for annular flow of fluids

Info

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
Application number
GB34939/47A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SFINDEX
Original Assignee
SFINDEX
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SFINDEX filed Critical SFINDEX
Priority to GB34939/47A priority Critical patent/GB673062A/en
Publication of GB673062A publication Critical patent/GB673062A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15DFLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00Influencing flow of fluids
    • F15D1/0015Whirl chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141Final 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/16Stators
    • F03B3/18Stator blades; Guide conduits or vanes, e.g. adjustable
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro 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.
GB34939/47A 1947-12-31 1947-12-31 Improvements in guiding means for annular flow of fluids Expired GB673062A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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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