Turbine blade basics. Calculation of Wind Power Where P = power, measured in watts (W) or joules per second (J/s)  = density of fluid, measured in.

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Presentation transcript:

Turbine blade basics

Calculation of Wind Power Where P = power, measured in watts (W) or joules per second (J/s)  = density of fluid, measured in kilogram per cubic meter (kg / m 3 ) A = swept area of blades, =  r 2, measured in square meters (m 2 ) v = wind speed, measured in meters per second (m/s) r P wind = ½ ρ Av 3

Parts of an airfoil Angle of attack,  : Angle between chord line and relative wind Camber: Curvature in airfoil Chord: Imaginary line from center of leading edge to back of trailing edge.

Airfoil Shape Just like the wings of an airplane, wind turbine blades use the airfoil shape to create lift and maximize efficiency.

Lift & Drag Forces The Lift Force is perpendicular to the direction of motion. We want to make this force BIG. The Drag Force is parallel to the direction of motion. We want to make this force small. α = low α = medium <10 degrees α = High Stall!! For particular speeds of relative wind, there is an optimum angle of attack which creates the highest lift-to-drag ratio.

Tip-Speed Ratio Tip-speed ratio is the ratio of the speed of the rotating blade tip to the speed of the relative wind.  r v TSR = Where,  = rotational speed in radians /sec  radians = 180  2  radians = 360  r = rotor radius v = speed of relative wind rr d

Twist & Taper Speed through the air of a point on the blade changes with distance from hub Therefore, tip speed ratio varies as well To optimize angle of attack all along blade, it must twist from root to tip Fast Faster Fastest

Performance Over Range of Tip Speed Ratios Power Coefficient Varies with Tip Speed Ratio Characterized by Cp vs Tip Speed Ratio Curve

Betz Limit All wind power cannot be captured by rotor or air would be completely still behind rotor and not allow more wind to pass through. Theoretical limit of rotor efficiency is 59% Most modern wind turbines are in the 35 – 45% range

Rotor Solidity Solidity is the ratio of total rotor planform area to total swept area Low solidity (0.10) = high speed, low torque High solidity (>0.80) = low speed, high torque A a Solidity = 3a/A

Some innovative ideas…

Building a tapered blade Cardboard Tube for twisted blades Airfoil Blades