WO2011020458A4 - Rotor element for a fluid to flow around and rotor - Google Patents

Rotor element for a fluid to flow around and rotor Download PDF

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Publication number
WO2011020458A4
WO2011020458A4 PCT/DE2010/000917 DE2010000917W WO2011020458A4 WO 2011020458 A4 WO2011020458 A4 WO 2011020458A4 DE 2010000917 W DE2010000917 W DE 2010000917W WO 2011020458 A4 WO2011020458 A4 WO 2011020458A4
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
flow guide
rotor blade
flow
guide surface
Prior art date
Application number
PCT/DE2010/000917
Other languages
German (de)
French (fr)
Other versions
WO2011020458A3 (en
WO2011020458A2 (en
Inventor
Konrad Buckel
Original Assignee
Konrad Buckel
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 Konrad Buckel filed Critical Konrad Buckel
Publication of WO2011020458A2 publication Critical patent/WO2011020458A2/en
Publication of WO2011020458A3 publication Critical patent/WO2011020458A3/en
Publication of WO2011020458A4 publication Critical patent/WO2011020458A4/en

Links

Classifications

    • 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
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • 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
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2210/00Working fluid
    • F05B2210/16Air or water being indistinctly used as working fluid, i.e. the machine can work equally with air or water without any modification
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/10Geometry two-dimensional
    • F05B2250/14Geometry two-dimensional elliptical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/70Shape
    • F05B2250/71Shape curved
    • F05B2250/711Shape curved convex
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00Geometry
    • F05B2250/70Shape
    • F05B2250/71Shape curved
    • F05B2250/712Shape curved concave
    • 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
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Abstract

The invention relates to a rotor element (10) for a fluid to flow around and for a rotor (20). Said rotor element comprises a rotor blade (12) having two lateral surfaces and a flow conduction surface (14) associated with the rotor blade (12), the wake of said flow conduction surface influencing the flow impacting one of the lateral surfaces of the rotor blade (12) at least to some extent.

Claims

11  11
GEÄNDERTE ANSPRÜCHE CHANGED CLAIMS
beim Internationalen Büro eingegangen am  received at the International Bureau on
11. August 2011 (11.08.2011)  August 11th, 2011 (11.08.2011)
Rotorelement (10) zur Umströmung durch ein Fluid und für einen Rotor (20), mit einem Rotorblatt (12), das zwei Seitenflächen aufweist, und einem dem Rotorblatt (12) zugeordneten Strömungsleitelement, wobei Rotor element (10) for flow around a fluid and for a rotor (20), with a rotor blade (12) which has two side surfaces, and a flow guide element associated with the rotor blade (12)
das Strömungsleitelement eine Strömungsleitfläche (14) ist, deren Nachlauf wenigstens teilweise die Anströmung an einer der Seitenflächen des Rotorblattes (12) beeinflusst, the flow guide element is a flow guide surface (14), the wake of which at least partially influences the flow on one of the side surfaces of the rotor blade (12),
dadurch gekennzeichnet, characterized,
dass die eine Seitenfläche des Rotorblattes (12) konkav und/oder die andere Seitenfläche des Rotorblatts (12) konvex geformt ist und die Strömungsleitfläche (14) der konkaven Seitenfläche des Rotorblatts (12) gegenüberliegend im the one side surface of the rotor blade (12) is concave and / or the other side surface of the rotor blade (12) is convexly shaped and the flow guide surface (14) is opposite to the concave side surface of the rotor blade (12)
Wesentlichen senkrecht zur konkaven Seitenfläche des Rotorblatts (12) angeordnet ist. Is arranged substantially perpendicular to the concave side surface of the rotor blade (12).
Rotorelement (10) gemäß Anspruch 1, Rotor element (10) according to claim 1,
dadurch gekennzeichnet, characterized,
dass sich eine lange Maßstrecke der Strömungsleitfläche (14) entlang einer that a long Maßstrecke the flow guide (14) along a
Längsachse des Rotorblattes (12) erstreckt und/oder dass die Strömungsleitfläche (14) innerhalb einer Schattenprojektion entlang einer Richtung eines Flächenvektors des Rotorblattes (12) liegt. Longitudinal axis of the rotor blade (12) extends and / or that the flow guide surface (14) within a shadow projection along a direction of a surface vector of the rotor blade (12).
Rotorelement (10) gemäß Anspruch 1 oder 2, Rotor element (10) according to claim 1 or 2,
dadurch gekennzeichnet, characterized,
dass die Strömungsleitfläche (14) zwei konvexe Seitenflächen und/oder the flow guide surface (14) has two convex side surfaces and / or
ellipsenförmigen Querschnitt aufweist. having elliptical cross-section.
Rotorelement (10) gemäß einem der vorstehenden Ansprüche, Rotor element (10) according to one of the preceding claims,
dadurch gekennzeichnet, characterized,
dass das Rotorblatt (12) und die Strömungsleitfläche (14) fest voneinander in that the rotor blade (12) and the flow guide surface (14) are fixedly spaced from one another
GEÄNDERTES BLATT (ARTIKEL 19) 12 MODIFIED SHEET (ARTICLE 19) 12
beabstandet sind und/oder gemeinsam in fester relativer Lage zueinander bewegbar sind. are spaced apart and / or together in a fixed relative position to each other are movable.
Rotorelement (10) gemäß einem der vorstehenden Ansprüche, Rotor element (10) according to one of the preceding claims,
dadurch gekennzeichnet, characterized,
dass das Rotorblatt (12) und die Strömungsleitfläche (14) miteinander durch Streben verbunden oder gemeinsam an einer Rotorbasis (24) aufgenommen sind. in that the rotor blade (12) and the flow guide surface (14) are connected to one another by struts or are accommodated together on a rotor base (24).
Rotorelement (10) gemäß einem der vorstehenden Ansprüche, Rotor element (10) according to one of the preceding claims,
dadurch gekennzeichnet, characterized,
dass in Längsrichtung des Rotorblatts (12) der Abstand einer Kante der in the longitudinal direction of the rotor blade (12), the distance of an edge of the
Strömungsleitfläche (14) von der Seitenfläche des Rotorblatts (12) monoton zunimmt. Flow guide surface (14) of the side surface of the rotor blade (12) monotonically increases.
Rotor (20) mit einer Mehrzahl von Rotorelementen (10) zur Umströmung durch ein Fluid, Rotor (20) with a plurality of rotor elements (10) for flow around a fluid,
gekennzeichnet durch marked by
wenigstens ein Rotorelement (10) gemäß einem der vorstehenden Ansprüche. at least one rotor element (10) according to one of the preceding claims.
Rotor (20) gemäß Anspruch 7, Rotor (20) according to claim 7,
dadurch gekennzeichnet, characterized,
dass aus der Drehrichtung des Rotors (20) gesehen die Strömungsleitfläche (14) im Windschatten des Rotorblatts (12) liegt. that seen from the direction of rotation of the rotor (20), the flow guide surface (14) lies in the slipstream of the rotor blade (12).
Rotor (20) gemäß Anspruch 7 oder 8, Rotor (20) according to claim 7 or 8,
dadurch gekennzeichnet, characterized,
dass die Winkelstellungen der Rotorblätter (12) und/oder der Strömungsleitflächen (14) um ihre jeweiligen Längsachsrichtungen einstellbar, insbesondere steuerbar oder regelbar, sind. the angular positions of the rotor blades (12) and / or the flow guide surfaces (14) are adjustable, in particular controllable or controllable, about their respective longitudinal axis directions.
Kraftmaschine zur Umwandlung der Strömungsenergie eines Fluids in eine andere Energieform, insbesondere in elektrische Energie, mit einem Rotor (20), dessen Engine for converting the flow energy of a fluid into another form of energy, in particular into electrical energy, with a rotor (20) whose
GEÄNDERTES BLATT (ARTIKEL 19) 13 MODIFIED SHEET (ARTICLE 19) 13
Drehachse im Wesentlichen in Strömungsrichtung anstellbar ist, Is pivotable axis substantially in the flow direction,
dadurch gekennzeichnet,  characterized,
dass der Rotor (20) ein Rotor gemäß einem der Ansprüche 7 bis 9 ist.  in that the rotor (20) is a rotor according to one of claims 7 to 9.
11. Kraftmaschine gemäß Anspruch 10, 11. Engine according to claim 10,
dadurch gekennzeichnet,  characterized,
dass das Fluid ein Gas, insbesondere Luft, oder eine Flüssigkeit, insbesondere Wasser, ist.  the fluid is a gas, in particular air, or a liquid, in particular water.
12. Propellerantrieb zur Erzeugung eines Vortriebs in einem Fluid,12. propeller drive for producing a propulsion in a fluid,
ekennzeichnet durch  characterized by
wenigstens einen Rotor (20) gemäß einem der Ansprüche 7 bis 9.  at least one rotor (20) according to one of claims 7 to 9.
13. Propellerantrieb gemäß Anspruch 12 , 13. propeller drive according to claim 12,
dadurch gekennzeichnet,  characterized,
dass in der Drehebene des Rotors (20) gesehen die Strömungsleitfläche (14) vor dem Rotorblatt (12) liegt.  that in the plane of rotation of the rotor (20) seen the flow guide surface (14) in front of the rotor blade (12).
GEÄNDERTES BLATT (ARTIKEL 19) MODIFIED SHEET (ARTICLE 19)
PCT/DE2010/000917 2009-08-19 2010-08-03 Rotor element for a fluid to flow around and rotor WO2011020458A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009038076A DE102009038076A1 (en) 2009-08-19 2009-08-19 Rotor element for flow around a fluid and rotor
DE102009038076.0 2009-08-19

Publications (3)

Publication Number Publication Date
WO2011020458A2 WO2011020458A2 (en) 2011-02-24
WO2011020458A3 WO2011020458A3 (en) 2011-09-15
WO2011020458A4 true WO2011020458A4 (en) 2011-11-10

Family

ID=43495424

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2010/000917 WO2011020458A2 (en) 2009-08-19 2010-08-03 Rotor element for a fluid to flow around and rotor

Country Status (2)

Country Link
DE (1) DE102009038076A1 (en)
WO (1) WO2011020458A2 (en)

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EP2691644A4 (en) * 2011-03-22 2014-09-03 Univ Tufts Systems, devices and methods for improving efficiency of wind power generation systems
US11300003B2 (en) 2012-10-23 2022-04-12 General Electric Company Unducted thrust producing system
EP2948633A1 (en) 2012-10-23 2015-12-02 General Electric Company Vane assembly for an unducted thrust producing system
FR3012180B1 (en) * 2013-10-18 2018-02-16 Sebastien Manceau HORIZONTAL ROTATING AXLE WIND MACHINE COMPRISING FAMILIES OF BLADES
US11391298B2 (en) 2015-10-07 2022-07-19 General Electric Company Engine having variable pitch outlet guide vanes
DE102018100511A1 (en) 2018-01-11 2019-07-11 Mehmet Güncü Rotor blade for wind turbines
DE102019111123A1 (en) * 2019-04-30 2020-11-05 Wobben Properties Gmbh Rotor for a wind turbine and wind turbine
US11492918B1 (en) 2021-09-03 2022-11-08 General Electric Company Gas turbine engine with third stream
US11834995B2 (en) 2022-03-29 2023-12-05 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
US11834954B2 (en) 2022-04-11 2023-12-05 General Electric Company Gas turbine engine with third stream
US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
US11680530B1 (en) 2022-04-27 2023-06-20 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine

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Publication number Priority date Publication date Assignee Title
GB176842A (en) * 1921-07-04 1922-03-23 Richard George Oliver Improvements in propellers and fans
GB388827A (en) * 1932-05-23 1933-03-09 James Carter Gray Improvements in and relating to screw propellers and the like
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Also Published As

Publication number Publication date
WO2011020458A3 (en) 2011-09-15
WO2011020458A2 (en) 2011-02-24
DE102009038076A1 (en) 2011-02-24

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