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A wind turbine for capturing energy from a fluid flow comprises a rotor having a rotational axis and a plurality of rotor blades 104 arranged for rotation about the rotational axis. The rotor blades extend longitudinally in a direction substantially parallel to the rotational axis. A shield member V

A wind turbine for capturing energy from a fluid flow comprises a rotor having a rotational axis and a plurality of rotor blades 104 arranged for rotation about the rotational axis. The rotor blades extend longitudinally in a direction substantially parallel to the rotational axis. A shield member V3 is arranged to shield some of the rotor blades from an oncoming wind where incidence of the wind on those rotor blades would act against rotation of the rotor in the direction of rotation. The rotor blades 104 are distributed about the circumference of the rotor and are spaced from the rotational axis, defining a substantially cylindrical space within the rotor through which the wind passes. The shield member V3 is defined by a radially inward surface and a radially outward surface. The radially inward surface follows substantially a portion of the circumference of the rotor. The radially outward surface of the shield member V3 comprises a first portion which meets the radially inward surface. In the region of the interface with the radially inward surface, the first portion extends in a first direction n that makes an angle of at least 0 degrees and up to 90 degrees in the contra-rotational direction with the radial direction of the rotor. The radially outward surface of the shield member V3 comprises a second portion which meets the first portion. At least a portion of the second portion extends in a second direction p that makes an angle of more than 0 degrees in the contra-rotational direction with the first direction n. The turbine has improved power output and efficiency compared to earlier similar designs.

대표청구항 ▼

1. A turbine for capturing energy from an oncoming fluid flow, the turbine comprising: a rotor having a rotational axis and a plurality of rotor blades arranged for rotation about the rotational axis in a direction of rotation and extending longitudinally in a direction substantially parallel to the

1. A turbine for capturing energy from an oncoming fluid flow, the turbine comprising: a rotor having a rotational axis and a plurality of rotor blades arranged for rotation about the rotational axis in a direction of rotation and extending longitudinally in a direction substantially parallel to the rotational axis;a shield member (V3) arranged to shield, in use, a plurality of the rotor blades at a windward side of the rotor from an oncoming fluid flow where incidence of the fluid on those rotor blades would act against rotation of the rotor in the direction of rotation,wherein the rotor blades are distributed about the circumference of the rotor and are spaced from the rotational axis, whereby to define a substantially cylindrical space within the rotor through which space the fluid flow passes, in use of the turbine;wherein the shield member is defined by a radially inward surface and a radially outward surface, the radially inward surface substantially following a portion of the circumference of the rotor;wherein the radially outward surface of the shield member comprises a first portion which meets the radially inward surface and in the region of the interface with the radially inward surface, the first portion extends in a first direction (n) that makes an angle of at least 0 degrees and up to 90 degrees with a radial direction (r1) of the rotor measured in the contra-rotational direction from the radial direction (r1) to the first direction (n);wherein the radially outward surface of the shield member comprises a second portion which meets the first portion and the angle between the first direction and a second direction (p) which follows at least a portion of the surface of the second portion is more than 0 degrees and less than 100 degrees measured in the contra-rotational direction from the first direction (n) to the second direction (p);wherein the radially outward surface of the shield member comprises a third portion which meets the second portion and at least a portion of the third portion extends in a third direction (q) that makes an angle of more than 30 degrees with the second direction (p) measured in the rotational direction from the second direction (p) to the third direction (q); andwherein the rotor is open on a side of the turbine opposite the shield member about an axis parallel to a direction of the oncoming fluid flow. 2. A turbine as claimed in claim 1, wherein said angle between the first direction (n) and the radial direction (r1) of the rotor is greater than 0 degrees and less than 90 degrees. 3. A turbine as claimed in claim 1, wherein the angle between the first direction (n) and the second direction (p) is greater than 40 degrees and less than 100 degrees. 4. A turbine as claimed in claim 1, wherein the angle between the second direction (p) and the third direction (q) is less than 90 degrees. 5. A turbine as claimed in claim 1, wherein the third portion has a length greater than half the radius of the rotor and less than three times the radius of the rotor. 6. A turbine as claimed in claim 1, wherein the rotor blades are arcuate in cross-section and a chord line (m) between the ends of the arcuate cross-section of the blades makes an angle of more than 0 degrees and less than 45 degrees in the contra-rotational direction with an outward radial direction of the rotor. 7. A turbine as claimed in claim 1 comprising more than five rotor blades and fewer than 19 rotor blades. 8. A turbine as claimed in claim 1, wherein the extent of the rotor blades in the radial direction of the rotor is greater than 10% of the radius of the rotor and less than 50% of the radius of the rotor. 9. A turbine as claimed in claim 1 further comprising a flow-directing member (V2) within the substantially cylindrical space. 10. A turbine as claimed in claim 9, wherein the flow-directing member has a radially outward surface which follows substantially a portion of the circumference of the substantially cylindrical space. 11. A turbine as claimed in claim 10, wherein the flow-directing member has a radially inward surface that substantially mirrors the radially outward surface.