A generator driven by a wind turbine is required to deliver 12 MW of power at the generator terminals. The turbine is a two-blade propeller rotating about a horizontal axis and the maximum permitted shear stress of the turbine shaft is 55×106 N/m² The rotor is designed to operate at a rotational speed of 20 revolution per seconds .The stage efficiencies are Cp = 0.32, ngb = 0.90, ng = 0.92. . (1) If the turbine delivers its rated power at a wind average speed of 27 m/s, calculate the corresponding diameter of the propeller and its TSR assuming a typical value for the overall efficiency. The air density may be assumed to have a value 1.29
A generator driven by a wind turbine is required to deliver 12 MW of power at the generator terminals. The turbine is a two-blade propeller rotating about a horizontal axis and the maximum permitted shear stress of the turbine shaft is 55×106 N/m² The rotor is designed to operate at a rotational speed of 20 revolution per seconds .The stage efficiencies are Cp = 0.32, ngb = 0.90, ng = 0.92. . (1) If the turbine delivers its rated power at a wind average speed of 27 m/s, calculate the corresponding diameter of the propeller and its TSR assuming a typical value for the overall efficiency. The air density may be assumed to have a value 1.29
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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![A generator driven by a wind turbine is required to deliver 12 MW of power at the generator terminals. The
turbine is a two-blade propeller rotating about a horizontal axis and the maximum permitted shear stress of
the turbine shaft is 55×106 N/m2 The rotor is designed to operate at a rotational speed of 20 revolution per
seconds .The stage efficiencies are Cp = 0.32, ngb = 0.90, ng = 0.92.. (i) If the turbine delivers its rated
power at a wind average speed of 27 m/s, calculate the corresponding diameter of the propeller and its TSR,
assuming a typical value for the overall efficiency. The air density may be assumed to have a value 1.29
kg/m³. (ii) Calculate the torque on the turbine shaft.
Area =
Radius=
Tip speed ratio =
shaft torque](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fbe3c2e01-24d6-474f-8d3e-6dc9b01ea8ec%2F76fb5013-e81f-493e-a690-2bcaa07e3866%2F5lm26hp_processed.png&w=3840&q=75)
Transcribed Image Text:A generator driven by a wind turbine is required to deliver 12 MW of power at the generator terminals. The
turbine is a two-blade propeller rotating about a horizontal axis and the maximum permitted shear stress of
the turbine shaft is 55×106 N/m2 The rotor is designed to operate at a rotational speed of 20 revolution per
seconds .The stage efficiencies are Cp = 0.32, ngb = 0.90, ng = 0.92.. (i) If the turbine delivers its rated
power at a wind average speed of 27 m/s, calculate the corresponding diameter of the propeller and its TSR,
assuming a typical value for the overall efficiency. The air density may be assumed to have a value 1.29
kg/m³. (ii) Calculate the torque on the turbine shaft.
Area =
Radius=
Tip speed ratio =
shaft torque
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