Analysis of wind turbines in yaw
The yaw problems of a three-bladed, downwind, horizontal axis wind turbine are examined in this report. A four-degree-of-freedom system was chosen to model the turbine. Linearized equations of rotor and nacelle motion were developed using the energy method and Lagrange's equations. Quasi-steady blade element and momentum theories were used in developing the axial induction factor and aerodynamic loads. A computer code was developed to obtain the numerical values of coefficients of the equations of motion, thus allowing the cause of yaw instability to be studied. The study indicated that yaw tracking error is primarily caused by tower shadow. However, the wind turbine studied - besides being unstable in yaw under normal operating conditions - has an additional problem in that the nacelle shape contributes to additional instability. Blade coning, in the present design, is inadequate to overcome this instability. The sensitivity of the system stiffness coefficients to the selected input parameters was studied, and results indicate that the system stiffness coefficient is highly sensitive to the coning angle. Increasing the coning angle could significantly increase the stiffness coefficient and lead to improvement of system stability.
- Research Organization:
- Oregon State Univ., Corvallis (USA). Dept. of Mechanical Engineering
- DOE Contract Number:
- AC04-76DP03533
- OSTI ID:
- 7074641
- Report Number(s):
- RFP-3678; ON: DE84013620
- Country of Publication:
- United States
- Language:
- English
Similar Records
Linearized model for wind turbines in yaw
A computer analysis of wind turbine blade dynamic loads
Computer analysis of wind turbine blade dynamic loads
Thesis/Dissertation
·
Sat Dec 31 23:00:00 EST 1983
·
OSTI ID:6029799
A computer analysis of wind turbine blade dynamic loads
Journal Article
·
Fri Jan 31 23:00:00 EST 1986
· J. Sol. Energy Eng.; (United States)
·
OSTI ID:5982053
Computer analysis of wind turbine blade dynamic loads
Conference
·
Wed Oct 31 23:00:00 EST 1984
·
OSTI ID:6030901