Design and Fabrication of Dual rotor counter wind turbine

Multi-rotor turbines can surpass the Betz limit. Further addition of rotor stages gives diminishing returns. It is because of the added cost and the complexity that?s why multi rotor are not used widely. In order to implement a practical and long-term benefit use dual rotor concept is prop

2025-06-28 16:26:20 - Adil Khan

Project Title

Design and Fabrication of Dual rotor counter wind turbine

Project Area of Specialization Electrical/Electronic EngineeringProject Summary

Multi-rotor turbines can surpass the Betz limit. Further addition of rotor stages gives diminishing returns. It is because of the added cost and the complexity that’s why multi rotor are not used widely. In order to implement a practical and long-term benefit use dual rotor concept is proposed. Main corncern is to minimize the ground root losses and wake losses. The second main target is to improve the efficiency through the use of aerodynamically optimized secondary rotor. To see the feasibility of this concept many models were prescribed however the most effective one was the RANS model. The ability of the RANS model to simulate multiple rotors is ?rst veri?ed for a canonical case by comparing against analytical results for a four, equal-size and uniformly loaded rotors. Fair agreement is observed between theory and simulation although the simulations in general predict higher power for downstream disks. The analytical results ignore wake mixing. Comparisons were also made for two-disk and three-disk turbines with similar accuracy. In order to enhance the model of RANS new approach with an actuator disk representation of a turbine rotor is uses to carry out parametric sweeps. In the ?rst parametric sweep, the secondary rotor size and tip speed ratio are varied while holding ?xed the axial spacing between the main and secondary rotors. In the second parametric sweep, the axial spacing and the secondary rotor tip speed ratio are varied while holding the secondary rotor tip radius at the optimum value of 0.25 found in the ?rst parametric sweep. The RANS based optimization study suggest that an increase in CP of about 0.035, which is about a 7% increase in aerodynamic e?ciency, is attainable with the DRWT concept. This improvement is primarily due to e?cient extraction of energy ?owing near the hub of the main rotor, but in part also due to the addition of another energy extracting device. A net bene?t of 7% in CPis predicted by RANS calculations for the optimized DRWT design. Wake comparisons con?rm e?cient extraction of energy in the root region by the DRWT. However, increase in vertical entrainment of energy, which would reduce turbine wake losses, is not clearly observed in the simulations

Project Objectives

Objectives of Dual rotor wind turine are:

Project Implementation Method

Wind turbine is vast field but the need is to what changes are needed to do?Wind turbines blades are similar to the wings and are constructed from set of aerofoils. To increase the efficiency of power generated from wind turbine many alternations are installed with the passage of time. Many researches are made in order to boast up the power generated from wind source. Although wind turbine production power is mainly divided into two categories. One is the testing and designing and the second step is most important in which assembling of the parts take place. 

Wind turbines work on the principle of aerodynamics as a result pressure distributed on a aerofoils can be integrated to give lift and drag forces. Blade pitch mechanism is mostly used to adjust the rotation speed and power generation. The blow wind causes the blades to moves as they have many aerofils spaces as a result the rotor start moving which move the turbine and power is produced. As we all know the typically the blades of turbines rotates very slow rpm mainly due to the noise and mechanical strenghth. The net power produced is low as a result gearbox is attached which helps to maxmize the power ratio. 

Benefits of the Project

Dual rotor wind turbines have many advantages:

This modication of the single rotor to the double rotor helps to improve the power sector and also improve the capacity of  generation of electricity.  

Technical Details of Final Deliverable

As the dual rotor have two rotor attached having 6 blades on a single tower which ultimately boast up the efficiency of the power. Dual rotor turbine also helpful in improving the performance of power system and initial power of the system. Although the initial cost of dual rotor wind turbine is expensive but it has long lasting impacts on the power sector economy. As Pakistan power sector is badly hit due to numerous reasons so need is to have a friendly power fuel which also because the source of income. There is need of constructive stages so the idea of wind turbine is best way to flourish the economy and energy sectors. As this concept of energy is widely adopted by many foreign countries so need is to initiate this project widely.                         

Final Deliverable of the Project Hardware SystemCore Industry Energy Other Industries Education , Others Core Technology Shared EconomyOther Technologies Wearables and ImplantablesSustainable Development Goals No PovertyRequired Resources
Item Name Type No. of Units Per Unit Cost (in Rs) Total (in Rs)
Total in (Rs) 60600
Rotor Equipment225005000
Blades Equipment615009000
Tower Equipment120002000
Motor Equipment115001500
Gear box Equipment130003000
AC Generator Equipment150005000
Shafts Equipment415006000
Brakes Equipment213002600
Cooling System Equipment110001000
Nacelle Equipment115001500
Gravity Foundation ground Equipment120002000
Controller Equipment110001000
Pitch Equipment210002000
Yaw Drive Equipment110001000
Wind Wane Equipment110001000
Turbine Equipment125002500
Connection to electric grid Equipment130003000
Filters Equipment110001000
Wires Equipment50502500
Step down Transformer Equipment125002500
Base of project Miscellaneous 110001000
Stationary Miscellaneous 110001000
Printing Miscellaneous 115001500
Decoration Miscellaneous 120002000

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