Fixed geometry self starting transverse axis wind turbine

Claim 2

In a fixed geometry wind turbine: a blade, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, said blade being mounted for rotation about a vertical axis, said blade having two sides, the first of which faces said axis and the second of which, faces away from said axis, the improvement comprising: said blade having a representative cross-section in a plane transverse to said axis, that includes a cambered profile, the median of said blade cross-section profile being substantially represented by the arc of a circle whose center is at or near said axis of rotation, said blade having a well rounded leading edge in combination with a trailing edge which is thin compared to the leading edge, such leading and trailing edges being connected by smooth continuous contours of thickness distribution most conducive to high lift to drag ratio, said blade having a thickness normal to said axis, at the maximum point, of about 19% of the chord width in said cross-section, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means providing high lift to drag ratios having high drag characteristics in reversed flows and large center of pressure travels, so that said turbine will start at low wind speed, will accelerate through the intermediate rotational speed range, and will run at high rotational speeds in response to un-altered naturally occurring winds.

Claim 3

In a fixed geometry wind turbine, a blade, said blade having a chord, said blade being mounted for rotation about a vertical axis, and comprising an upwardly extending elongated fixed geometry element that is long compared to its width and thickness, said blade having a thickness normal to said axis, at its maximum point, of about 19% of said chord, so as to provide improved self-starting and accelerating capability, said blade having a curved camber line, said camber line having a concave side which faces said axis, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means providing high lift to drag ratios having high drag characteristics in reversed flows and large center of pressure travels, whereby the blade will tend to start rotating at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at high rotational speeds, in response to un-altered naturally occurring winds, where U/V exceeds 1, with U being the tip speed of the blade and V being the velocity of the ambient wind.

Claim 4

In a fixed geometry wind turbine, a blade, said blade having a chord, said blade being mounted for rotation about a vertical axis, and comprising an upwardly extending elongated fixed geometry element that is long compared to its width and thickness, said blade having a thickness normal to said axis, at its maximum point, of about 19% of said chord, so as to provide improved self-starting and accelerating capability, said blade having a curved camber line, said camber line having a concave side which faces said axis, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means providing high lift to drag ratios having high drag characteristics in reversed flows and large center of pressure travels, whereby the blade will tend to start rotating at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at high rotational speeds, in response to un-altered naturally occurring winds, where U/V exceeds 1, with U being the tip speed of the blade and V being the velocity of the ambient wind.

Claim 5

In a fixed geometry wind turbine, a blade, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, said blade being mounted for rotation about an axis transverse to the direction of the wind, said blade having cross-section means comprising a well rounded leading edge, and a smoothly contoured profile including a camber to the mean line of said blades cross-sectional profile having a concave side which faces said axis, thereby to provide a high lift to drag ratio and high drag in reversed flows, said blade having a chord width of about 24 to 40% of the radius of blade rotation and having a thickness normal to said axis of about 19% of the chord width, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means so that said turbine will start rotating at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at high rotational speeds, in response to naturally occurring winds, whereby to provide improved self-starting and accelerating capability.

Claim 6

In a fixed geometry wind turbine, a blade, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, said blade being mounted for rotation about an axis transverse to the direction of the wind, said blade having cross-section means comprising a well rounded leading edge, and a smoothly contoured profile including a camber to the mean line of said blades cross-sectional profile having a concave side which faces said axis, thereby to provide a high lift to drag ratio and high drag in reversed flows, said blade having a chord width of about 24 to 40% of the radius of blade rotation and having a thickness normal to said axis of about 19% of the chord width, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means so that said turbine will start rotating at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at high rotational speeds, in response to naturally occurring winds, whereby to provide improved self-starting and accelerating capability.

Claim 7

In a wind turbine, as defined in claims 1, 2 or 3 in which there are a plurality of said blades angularly spaced equally around said axis, to provide said turbine with self-starting capability.

Claim 8

In a fixes geometry wind turbine, a blade, having a chord, said blade being mounted for rotation about a vertical axis, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, said blade having a chord on the order of 24 to 40% of the blade radius, to provide self-starting capability, said blade having a maximum thickness on the order of 19% of the chord of the blade, said blade having cross-section means comprising leading and trailing edges and a curved camber line having a concave side which faces inwardly and providing high lift to drag ratios with high drag in reverse flows, whereby to provide self-starting capability, said blade having an angle of attack, negative to the circular path traveled by the said blade about its own axis of rotation, to provide a controlled ratio of rotor blade velocity to wind stream velocity, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means so that said blade will start at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at controlled high rotational speeds in response to un-altered naturally occurring winds.

Claim 9

In a fixes geometry wind turbine, a blade, having a chord, said blade being mounted for rotation about a vertical axis, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, said blade having a chord on the order of 24 to 40% of the blade radius, to provide self-starting capability, said blade having a maximum thickness on the order of 19% of the chord of the blade, said blade having cross-section means comprising leading and trailing edges and a curved camber line having a concave side which faces inwardly and providing high lift to drag ratios with high drag in reverse flows, whereby to provide self-starting capability, said blade having an angle of attack, negative to the circular path traveled by the said blade about its own axis of rotation, to provide a controlled ratio of rotor blade velocity to wind stream velocity, all of the parts of said wind turbine rotor comprising a fixed geometry unit, said blade comprising means so that said blade will start at low wind speeds, will accelerate through the intermediate rotational speed range, and will run at controlled high rotational speeds in response to un-altered naturally occurring winds.

Claim 10

A wind turbine, as described in claim 5, to provide an improved and highly sensitive flow meter, wind speed indicator and the like.

Claim 11

In a fixed geometry wind turbine, a blade, means mounting said blade for rotation about an axis perpendicular to the direction of the wind, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, the improvement comprising: said blade characterized by high lift to drag ratios and high drag in reversed flow and including a means, to provide the self-starting characteristics of the turbine, comprising a convex leading portion which increases to a maximum blade thickness which is greater than 10% of the chord of the blade and then decreases in thickness to its trailing end, said blade having a curved camber line having a concave side which faces said axis, the combination thereby to provide such excursions of the center of pressure of said airfoil so that said blade will start and accelerate through intermediate speeds into the high speed range of operation due to un-altered naturally occurring wind, said blade, and said means for mounting the same for rotation, comprising a fixed geometry unit.

Claim 12

In a fixed geometry wind turbine, a blade, means mounting said blade for rotation about an axis perpendicular to the direction of the wind, said blade comprising a fixed geometry upwardly extending elongated element which is relatively long as compared to its width and thickness, the improvement comprising: said blade characterized by high lift to drag ratios and high drag in reversed flow and including a means, to provide the self-starting characteristics of the turbine, comprising a convex leading portion which increases to a maximum blade thickness which is greater than 10% of the chord of the blade and then decreases in thickness to its trailing end, said blade having a curved camber line having a concave side which faces said axis, the combination thereby to provide such excursions of the center of pressure of said airfoil so that said blade will start and accelerate through intermediate speeds into the high speed range of operation due to un-altered naturally occurring wind, said blade, and said means for mounting the same for rotation, comprising a fixed geometry unit.

Claim 13

A fixed geometry wind turbine as defined in claim 7 in which said convex leading portion increases to a maximum blade thickness which is on the order of 19% of the chord of the blade and having a large center of pressure travel.

Claim 14

In a fixed geometry wind turbine as defined in claim 8, said blade having a chord on the order of 24 to 40% of the distance of said blade from said axis.

Claim 15

In a fixed geometry wind turbine as defined in claims 7, 8 or 9 in which there are at least two of said blades located at different angular positions about said axis, to improve the self-starting capability.

Claim 16

In a fixed geometry wind turbine, support means, blade means mounted for rotation, upon said support means, about a vertical axis, said blade means comprising an elongated upwardly extending fixed geometry wind driven blade element having leading and trailing edges being connected by smooth continuous contours of thickness distribution providing high lift to drag characteristics with large excursions in the center of pressure, said contours comprising two surfaces one of which faces said vertical axis, said blade having a curved camber line having a concave side which faces inwardly, said blade means having a contour and a thickness to chord ratio which will allow the blade to accelerate the blade means from a standstill to a tip speed ratio substantially within the high speed range of rotation in response to un-altered naturally occurring wind flow acting as the only power source for accelerating said blade means and including chord, camber, thickness, and thickness distribution, interrelated to achieve such acceleration.

Claim 17

In a fixed geometry wind turbine, support means, blade means mounted for rotation, upon said support means, about a vertical axis, said blade means comprising an elongated upwardly extending fixed geometry wind driven blade element having leading and trailing edges being connected by smooth continuous contours of thickness distribution providing high lift to drag characteristics with large excursions in the center of pressure, said contours comprising two surfaces one of which faces said vertical axis, said blade having a curved camber line having a concave side which faces inwardly, said blade means having a contour and a thickness to chord ratio which will allow the blade to accelerate the blade means from a standstill to a tip speed ratio substantially within the high speed range of rotation in response to un-altered naturally occurring wind flow acting as the only power source for accelerating said blade means and including chord, camber, thickness, and thickness distribution, interrelated to achieve such acceleration.

Claim 18

In a fixed geometry wind turbine as defined in claim 11: said blade means having a cross-section profile camber which conforms substantially to the arc of a circle having the concave side facing said vertical axis.

Claim 19

In a fixed geometry wind turbine, as defined in claim 11: said blade means including means which will accelerate the blade means from a standstill through an intermediate speed where the tip speed ratio is about 1 to a speed of substantially higher order in response to free unconfined air wind flow acting as the only energy source for accelerating said blade means and including chord, camber, thickness, and thickness distribution, interrelated to achieve such acceleration.

Claim 20

In a fixed geometry high speed wind turbine as defined in claim 13: said blade means having a cross-section profile camber line which conforms substantially to the arc of a circle and having the concave side facing said vertical axis, to provide said center of pressure excursions.

Claim 21

In a transverse axis wind turbine providing an improved fixed geometry rotor, said fixed geometry rotor having means for rotation about said axis, including means mounting at least one fixed geometry blade for rotation about said axis, said blade being mounted for rotation about said axis to circumscribe a volume of space, the rotor improvements comprising: said blade having a cross-section profile representative of a family of airfoils having thickness distribution conducive to high lift, low drag, large center of pressure travel, and a high drag characteristic in reversed flows, said blade having a representative cross-section profile; and having a curved median or camber line having a concave curvature which faces said axis and provided with smooth continuous curvature on both the outermost and innermost surfaces, said cambered airfoil having excursions in the center of pressure travel to provide variations in the pitching moment and thereby effect increasing rotational oscillations leading to forward rotation from the standing position, said airfoil having sufficiently high lift and sufficiently low drag characteristics to provide adequate torque in the intermediate range of rotor speeds to accelerate the rotor through the intermediate into the high speed range of rotation, said rotor improvements including a thickness to chord ratio which together with the other of said rotor improvements provide the inherent ability to consistently initiate forward rotation and accelerate through the intermediate into the high speed range of rotation.

Claim 22

In a transverse axis wind turbine providing an improved fixed geometry rotor, said fixed geometry rotor having means for rotation about said axis, including means mounting at least one fixed geometry blade for rotation about said axis, said blade being mounted for rotation about said axis to circumscribe a volume of space, the rotor improvements comprising: said blade having a cross-section profile representative of a family of airfoils having thickness distribution conducive to high lift, low drag, large center of pressure travel, and a high drag characteristic in reversed flows, said blade having a representative cross-section profile; and having a curved median or camber line having a concave curvature which faces said axis and provided with smooth continuous curvature on both the outermost and innermost surfaces, said cambered airfoil having excursions in the center of pressure travel to provide variations in the pitching moment and thereby effect increasing rotational oscillations leading to forward rotation from the standing position, said airfoil having sufficiently high lift and sufficiently low drag characteristics to provide adequate torque in the intermediate range of rotor speeds to accelerate the rotor through the intermediate into the high speed range of rotation, said rotor improvements including a thickness to chord ratio which together with the other of said rotor improvements provide the inherent ability to consistently initiate forward rotation and accelerate through the intermediate into the high speed range of rotation.

Claim 23

A wind turbine as defined in claim 15 in which said volume of space is defined by a line of revolution about said axis, said line extending from one point on said axis to another point on said axis and comprising a concave configuration facing said axis and extending between said points.

Claim 24

A wind turbine as defined in claim 15 in which said volume of space is cylindrical.

Claim 25

A wind turbine as defined in claim 15 in which said volume of space is a frustum of a cone.

Claim 26

A wind turbine as described in claim 15 having a single blade thereby to provide maximum torque per square foot of blade area.

Claim 27

A wind turbine as described in claim 15 having two blades thereby to combine the forces acting on the upstream and downstream facing blades and provide more improved starting and accelerating capability.

Claim 28

A wind turbine as described in claim 15 having three blades thereby to provide greater low speed torque.

Claim 29

A wind turbine as described in claim 15 having a blade chord width of about 12 to 20% of said rotor diameter and a blade maximum thickness of about 19% of said blade chord width, the combination to provide improved self-starting and accelerating capability.

Claim 30

A wind turbine as described in claim 15 wherein said blade chord width may be from 20% of said turbine's diameter to 12% or less of said turbine's diameter, said blade cross-section profile of 20% chord to diameter ratio having on the order of 19% maximum thickness to chord width to provide said blade with large center of pressure travel and high drag in reversed flow thereby generating a forward rotational force in such part of the rotor blade that is moving less than the ratio of blade speed to wind speed of 1 to 1, said cross-section profile of 12% or less chord diameter ratio having a maximum blade profile thickness of 10 to 12% of said chord width thereby to increase said turbine's rotational speed capability in such part of the rotor blade as is moving at the high speed ratio range.

Claim 31

A wind turbine as described in claim 15 having a blade chord to turbine diameter ratio of 12 to 20% and thickness to chord ratio of 10 to 19% thereby to provide a turbine of capability to initiate rotational motion from a standing position and accelerating therefrom into the high speed range of rotational speed.

Claim 32

A wind turbine as defined in claim 22 in which the turbine has only one blade.