Variable geometry windturbine

Claim 2

A power generating device comprising: fluid impact impellers for converting fluid energy into mechanical energy; a fluid flow accelerator surface having an outer structure and a shape substantially that of a partial inner concentric section of a hollow toroid providing thereby open channel means about the exterior periphery of said fluid flow accelerator; wherein said fluid impact impellers are mounted within said fluid flow accelerator channel means for the purpose of energy extraction from accelerated fluid velocity fields within said channel means.

Claim 3

A power generating device according to claim 1, wherein the power generating device is an omnidirectional turbine providing a rotational output in response to a fluid flow approaching the turbine from any direction to a plane of rotation, and wherein said fluid impact impellers comprise a plurality of deflector means, each having variable geometry so constructed that points lying on an impeller surface structure equidistant from a centroidal axis of said impeller and in a plane perpendicular to said axis, will have substantially 360 degree and 3-dimensional interdependent symmetry of motion during operational stages of deployment and that each blossoms open into a dominant maximum resistance fluid impact surface when rotating substantially with the fluid and collapses into a closed folded configuration of minimal parasite drag when rotating substantially into the flow field for providing a net torque of a first sense to a hub means in response to fluid flow in any direction to a plane perpendicular to an axis of rotation.

Claim 4

A power generating device according to claim 1, wherein the fluid flow accelerator surface is substantially of circular horizontal cross-section and positioned concentric and interior to a revolutionary path of working elements.

Claim 5

The omnidirectional turbine of claim 2 wherein said plurality of variable geometry deflector means comprises a plurality of umbrella-like elements, and wherein the fluid flow accelerator has its periphery substantially circular in a horizontal plane.

Claim 6

The omnidirectional turbine of claim 2 wherein the fluid flow accelerator is connected to the fluid impact impeller working elements and rotating with the working elements.

Claim 7

A power generating device according to claim 1, wherein the flow accelerator has closing covers at either verticle end of said fluid flow accelerator.

Claim 8

A power generating device according to claim 1, wherein said fluid impact impeller working elements may revolve with respect to said fluid flow accelerator body within said fluid flow accelerator channel means.

Claim 9

A power generating device according to claim 1, wherein said fluid impact impellers are rigidly mounted to and fixed with respect to said fluid flow accelerator structure within said channel means of said fluid flow accelerator, and wherein said fluid flow accelerator may rotate about a central axis in response to fluid flow into an optimum position for energy extraction by said impact impellers.

Claim 10

A power generating device according to claim 1, wherein said fluid impact impellers comprise two horizontal axis rotors mounted rigidly to and fixed with respect to said fluid flow accelerator body within said channel means; wherein each horizontal axis rotor is located substantially at an opposite extreme with respect to the other rotor within the peripheral channel means of said fluid flow accelerator; wherein said fluid flow accelerator body may rotate about a central axis in response to fluid flow.

Claim 11

A power generating device according to claim 7, wherein said fluid impact impellers comprise two horizontal axis rotors located substantially at opposite extremes within said channel means with respect to each other; wherein said horizontal axis rotors may revolve jointly in unison within said channel means.

Claim 12

A power generating device according to claim 8, wherein said fluid impact impellers comprise verticle axis rotors; wherein said verticle axis rotors are located substantially at opposite extremes with respect to each other within said fluid flow accelerator channel means.