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A turbine which rotates in the same directional sense for both directions of throughflow of a working medium contains rotor blades possessing an aerofoil-shaped profile which at least over a portion of the length of the rotor blades is subdivided into profile parts or portions in order to improve th

A turbine which rotates in the same directional sense for both directions of throughflow of a working medium contains rotor blades possessing an aerofoil-shaped profile which at least over a portion of the length of the rotor blades is subdivided into profile parts or portions in order to improve the flow of the working medium about the rotor blades. The profile parts of the rotor blades are non-symmetrically constructed or arranged at least in part with respect to each plane which is perpendicular to the momentary throughflow direction of the rotor. It is therefore possible to reduce the dimensions of the turbine with essentially the same power output. Such type of turbine is particularly suitable for extracting energy from the movement of waves of bodies of water, such as the sea water of the ocean, and air moved by the waves alternately in opposite directions serves as the working or flow medium.

대표청구항 ▼

1. A turbine comprising: a rotatable rotor provided with a rotor hub and rotor blades each having a profiled structure defining a substantially aerofoil-shaped profile; a working medium alternately flowing through the rotor in opposite throughflow directions; said rotor rotating in the same dir

1. A turbine comprising: a rotatable rotor provided with a rotor hub and rotor blades each having a profiled structure defining a substantially aerofoil-shaped profile; a working medium alternately flowing through the rotor in opposite throughflow directions; said rotor rotating in the same direction of rotation during both throughflow directions of the working medium; the profiled structure of each of the rotor blades being subdivided at least over a portion of the length of the rotor blades into profile parts in order to improve the flow of the working medium around the rotor blades; each of said profile parts defining a blade member; said blade members being at least in part spaced from one another in the throughflow directions of the working medium; and at least one of the profile parts being non-symmetrical to a plane which is perpendicular to the momentary throughflow direction of the working medium and which plane extends through said at least one profile part. 2. The turbine as defined in claim 1, wherein: the mutual spacing of the profile parts of the rotor blade at a front end of the profile part is different from the mutual spacing of the profile parts at the rear end of said profile parts. 3. The turbine as defined in claim 1, wherein: said profile parts possess a flatter configuration at mutually confronting surfaces thereof than at surfaces of said profile parts which face away from one another. 4. The turbine as defined in claims 1 or 2, wherein: said profile parts of a rotor blade define two equal size profile parts constructed as a primary blade; and said equal size profile parts being arranged behind one another in the flow direction of the working medium through the rotor. 5. The turbine as defined in claim 4, wherein: said profile parts are arranged opposite one another. 6. The turbine as defined in claim 4, wherein: said profile parts are arranged offset with respect to one another in circumferential direction of the rotor. 7. The turbine as defined in claim 4, wherein: the profile parts have a mutual mean spacing from one another in the throughflow direction of the working medium which amounts up to 1.5-fold the chord length of a profile part. 8. The turbine as defined in claim 7, wherein: said mean spacing amounts to about 0.7-fold the chord length of the profile part. 9. The turbine as defined in claims 2 or 3, wherein: said profile parts are symmetrically grouped with respect to a plane which is substantially perpendicular to the throughflow direction of the working medium. 10. The turbine as defined in claim 1, wherein: the lengthwise direction of the rotor blades extends away from the rotor hub of the rotor. 11. The turbine defined in claim 1, wherein: said turbine is used for extracting energy from the movement of the waves of the ocean. 12. The turbine as defined in claim 11, further including: a vessel having an upper vessel throat; said turbine being arranged at the region of the upper throat of said vessel; and said vessel having a lower open end which immerses into the water moved by the waves. 13. The turbine as defined in claim 1, wherein: said turbine is used for extracting energy from a to-and-fro moving body of water. 14. The turbine as defined in claim 1, wherein: the difference of the spacing between the front ends and the rear ends of the profile parts becomes smaller with increasing spacing from the axis of rotation of the rotor. 15. The turbine as defined in claim 1, wherein: said plane extends between opposite ends of said at least one profile part. 16. A turbine comprising: a rotatable rotor provided with a rotor hub and rotor blades each having a profiled structure defining a substantially aerofoil-shaped profile; a working medium alternately flowing through the rotor in opposite throughflow directions; said profiled structure of each said rotor blade being substantially symmetrical relative to a plane which extends normally to said opposite throughflow directions; said rotor rotating in the same direction of rotation during both throughflow directions of the working medium; the profiled structure of each of the rotor blades being subdivided at least over a portion of the length of the rotor blades into a profile parts in order to improve the flow of the working medium around the rotor blades; each of said profile parts defining a blade member; said blade members being at least in part spaced from one another in the throughflow directions of the working medium; and at least one of the profile parts being non-symmetrical to a plane which extends normally to said opposite throughflow directions of the working medium and which plane extends through said at least one profile part.