F05B2250/70

WIND TURBINE BLADE WITH ANCHORING SITES
20180230966 · 2018-08-16 ·

The invention relates to a wind turbine blade having integrated thermoplastic anchoring sites for attachment of surface mounted devices, a method for producing such blade and a wind turbine equipped with such blade.

WAVE ENERGY DEVICE WITH CONSTRICTED TUBE AND GENERATOR POD
20180058420 · 2018-03-01 ·

A wave energy converter utilizes a flotation module that rises and falls with the passage of waves, a submerged tube containing a constriction which multiplies the speed of the water passing therethrough, a turbine (or other hydrokinetic apparatus) positioned so as to extract energy from the accelerated flow of water within and/or through the tube, and a submerged gas- or liquid-filled chamber housing one or more energy conversion components (e.g. generators, transformers, rectifiers, inverters). By providing a chamber in proximity to the turbine, generators can be placed in closer proximity to the turbine that turns them, and the shared shaft can be shorter than if the generators were placed in the buoy adjacent to the surface.

PSP BLADES WITH DIHEDRAL ANGLES, COMPRISING A LONGITUDINAL DEPRESSION
20180045175 · 2018-02-15 ·

The invention relates to a novel rhomboidal wind turbine blade with a dihedral angle, as a supplement to another invention filed by the same applicant in 2013, said blade originally comprising four planar rhomboidal sides and a dihedral angle, and now including a longitudinal depression in the side forming the dihedral angle, from the center of the major axis of the blade, which traps more wind with a concave shape and directs same to the vertex of the angle, compressing the wind which rebounds from the vertex of the angle and powering the rotary movement with two sets of two blades per generator, as well as including an automatic safety system allowing the position of the blades to be changed in the event of high-speed winds by a computer system between a motor and a wind speed sensor, with the blades being coupled to the rotor with an angle that can be varied in response to high-speed winds.

COMPRESSOR BLADE FOR A GAS TURBINE ENGINE

An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

COMPRESSOR BLADE FOR A GAS TURBINE ENGINE

An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

COMPRESSOR BLADE FOR A GAS TURBINE ENGINE

An article of manufacture having a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table, the scalable table selected from the group of tables consisting of TABLE 1, wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying the Cartesian coordinate values of X, Y and Z by a number, and wherein X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height, the airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.

Self-starting savonius wind turbine
09752555 · 2017-09-05 ·

A self-starting Savonius wind turbine includes a frame, a rotor assembly that is rotatable about a central axis of rotation and an energy utilizing device operably connected to the rotor assembly. The rotor assembly has at least two rotors, each rotor having at least two rotor blades. Rotation of the rotor assembly is initiated by wind coming from any direction blowing on any one of the plurality of blades. The rotors are configured in a stacked orientation with the blades fixed at a rotated angular position relative to one another to start rotation of the rotor assembly in variable wind conditions. The rotor assembly is made of a composite laminate and the frame is made of a durable, lightweight material. The frame and the rotor assembly are assembled into a single unit for transportation and utilization.

Flexible Wind Turbine Apparatus
20170211544 · 2017-07-27 ·

An airfoil for a wind turbine apparatus includes an airfoil body having an arcuate shape extending between a first end and a second end and an airfoil support secured to a midpoint on the airfoil body and connected to the outer end of the support arm. The airfoil body includes a first portion adjacent to the first end and a second portion adjacent to the second end. The first end and the second end are secured to the support arm, and the body of the airfoil is comprised of material capable of flexing in response to wind pressure. The first and second portions of the airfoil body extend away from each other in an extended position and collapse together in a collapsed position, and the orientation of the airfoil relative to the direction of the wind causes the airfoil to move between the open and closed positions.

HYDRAULIC TURBINE
20250067239 · 2025-02-27 ·

A runner for a hydraulic turbine configured to reduce fish mortality. The runner includes a hub and a plurality of blades extending from the hub. Each blade includes a root connected to the hub and a tip opposite the root. Each blade further includes a leading edge opposite a trailing edge, and a ratio of a thickness of the leading edge to a diameter of the runner can range from about 0.06 to about 0.35. Further, each blade has a leading edge that is curved relative to a radial axis of the runner.

ROTATING BLADE BODY FOR TURBINES USING THE MAGNUS EFFECT, IN PARTICULAR TURBINES WITH AN AXIS OF ROTATION PARALLEL TO THE DIRECTION OF THE MOTOR FLUID
20170130694 · 2017-05-11 ·

The present invention relates to a rotating blade body for turbines using the Magnus effect with an axis of rotation of the turbine parallel to the direction of the motor fluid, characterised in that it is defined by a first sector or end head, more distant from said axis of rotation of the turbine, and by a second sector or rod, connecting said first sector and said axis of rotation of the turbine, said second sector having an average diameter smaller than the diameter of said first sector, said first sector being inscribed within a solid of revolution whose profile is determined so as to maintain a constant value of lift in each section.