FIELD: vane-type wind-driven power plants at horizontal axis of rotation.
SUBSTANCE: proposed wind-driven power plant has blades, automatic power control unit, wind vane, wind direction control system, electric generator and support. Blades are mounted at angle of attack α≥7°; trailing and leading edges of blades are made according to formula of two parabolas: Y1=K1X1/2; Y2=K2X 1/2+2Ro which are tangent to circle at radius of R≥Ro; center of this circle is located at distance l≥2/3L, where Ro is preset radius of circle; L is projection of blade length on coordinate X; coefficients K1 and K2 are calculated by the following formulae: K1=Y1A/X1A 1/2; K2=(Y2B-2Ro)X2B 1/2, where A and B are points of tangency by parabolas Y1 and Y2, respectively of circle at radius R. Profiles of lower and upper surfaces of blades are formed by intersection on line of trailing edge of two parabolas: Y3=K3X1/2 and Y4=K4X1/2+2Ro, where K3≥1; K4=(0.4-0.8)K3. Blade tip is bent through angle β≥60°. Besides that, plant may be provided with lightning-discharge protector in form of receptors at the blade tip. Parabola-shaped blade of wind-driven power plant increases wind efficiency due to increased area of blades. Mechanical power control system and wind protection reduce cost of wind-driven plant. Longitudinal and transverse oscillations are reduced by more than 20%.
EFFECT: enhanced efficiency and reliability; enhanced lightning protection.
2 cl,, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOJET ENGINE | 2007 |
|
RU2367798C2 |
PROPELLER BLADE | 2004 |
|
RU2278058C2 |
AIR PROPELLER | 2006 |
|
RU2318698C1 |
FLAPPING-WING AIRCRAFT | 2006 |
|
RU2323129C2 |
AIRCRAFT | 2005 |
|
RU2307048C1 |
HELICOPTER | 2006 |
|
RU2333867C2 |
ROTOR WIND ELECTRIC ASSEMBLY | 2006 |
|
RU2325552C1 |
AXIAL-BLOW BLOWER | 2007 |
|
RU2362911C2 |
HELICOPTER | 2006 |
|
RU2309873C1 |
PROPELLER | 2006 |
|
RU2314968C1 |
Authors
Dates
2007-10-27—Published
2006-05-05—Filed