Advanced Wind Turbine Program Next Generation Turbine ... - NREL
Advanced Wind Turbine Program Next Generation Turbine ... - NREL
Advanced Wind Turbine Program Next Generation Turbine ... - NREL
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Figure 22. POC Main Control Cabinet ........................................................................................ 49<br />
Figure 23. POC 34-m Blade Planform......................................................................................... 51<br />
Figure 24. NGT POC Airfoil Family........................................................................................... 52<br />
Figure 25. 18% Airfoil Model in the WSU <strong>Wind</strong> Tunnel Test .................................................... 52<br />
Figure 26. Prototype Set of the GE34a Blades at Tecsis ............................................................. 53<br />
Figure 27. Static Blade Tests ........................................................................................................ 54<br />
Figure 28. Static Blade Test Setup................................................................................................ 54<br />
Figure 29. NWTC Fatigue Test Setup ......................................................................................... 55<br />
Figure 30. POC Hub ..................................................................................................................... 56<br />
Figure 31. POC <strong>Turbine</strong> Rotor Being Installed ........................................................................... 57<br />
Figure 32. POC <strong>Turbine</strong> Installed in Tehachapi, California ......................................................... 57<br />
Figure 33. Comparison of Theoretical and Measured POC Power Curves .................................. 58<br />
Figure 34. Comparison of the POC Noise Levels to Historical Levels ........................................ 59<br />
Figure 35. Comparison of Noise Levels and Rotor Tip Speeds ................................................... 60<br />
Figure 36. Benefits to COE from Increasing Rotor Size and <strong>Turbine</strong> Rating .............................. 64<br />
Figure 37. Predicted Power Performance for the EMD1.5/77 <strong>Turbine</strong> ....................................... 65<br />
Figure 38. EMD 37-m (GE37a) Blade.......................................................................................... 66<br />
Figure 39. EMD Tower-Top Accelerometer Package ................................................................. 68<br />
Figure 40. Flowchart of the EMD Tower Top Accelerometer Feedback .................................... 68<br />
Figure 41. EMD <strong>Turbine</strong> Installed in Tehachapi, California........................................................ 71<br />
Figure 42. Comparison of Theoretical and Measured EMD Power Curves ................................. 71<br />
Figure 43. Comparison of the EMD Noise Levels to Historical Levels ....................................... 73<br />
Figure 44. Leverage of USDOE R&D Funding by GE <strong>Wind</strong> Energy.......................................... 74<br />
Figure 45. Return on Investment of <strong>NREL</strong> Funds in GE <strong>Wind</strong>................................................... 74<br />
List of Tables<br />
Table 1. Summary of the Key Drive Train Design Parameters and Configurations Options......... 6<br />
Table 2. Summary of Drivetrain Configurations Investigated........................................................ 7<br />
Table 3. Proof of Concepts <strong>Turbine</strong> Configuration Description................................................... 42<br />
Table 4. Summary of Required Airfoil Characteristics ................................................................ 51<br />
Table 5. Test Equivalent Damage ................................................................................................. 56<br />
Table 6. Engineering & Manufacturing Development <strong>Turbine</strong> Configuration ............................ 62<br />
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