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Assessment of a rotor blade extension retrofit as a supplement to the lifetime extension of wind turbines

机译:评估转子叶片延伸改装作为风力涡轮机的寿命延伸的补充剂

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The potential lifetime of wind turbine components is usually not fully utilized as the site conditions are less severe than assumed in the turbine design. Operators of wind farms can make use of the excess fatigue budget to increase the energy yield and thus decrease the levelized cost of energy (LCoE). To achieve this, the lifetime of the turbine can be extended until the fatigue budget is exhausted. Alternatively, a rotor blade extension (RBE) is an option to increase the energy yield of a wind turbine. An RBE increases the blade length and thus the swept area and the energy yield. An RBE also increases the loads on the turbine, however. Higher fatigue loads in turn reduce the fatigue budget of a turbine. This study investigates whether the use of an RBE is advantageous compared with a sole lifetime extension (LTE). As the use case, a commercial 1.5 MW turbine located in northern Germany was investigated. Aeroservoelastic multibody load simulations and simplified static load simulations were verified with each other. These simulations revealed the loads to determine the fatigue budget of the turbine components. Since the blade became the critical component when a certain RBE length was exceeded, the blade was subjected to a structural fatigue analysis. The fatigue analysis focused on the trailing-edge bond line which became critical when lead–lag loads increased with blade length. Finally, the energy production gains due to LTE and RBE were assessed. For the use case turbine, this study revealed an LTE of 8.7?years after a design life of 20?years with an additional energy yield of 43.5 %. Moreover, the extension of the 34 m blade with an RBE length of 0.8 m further increased the yield by 2.3 %.
机译:由于现场条件比在涡轮机设计中假设的假设不太严重,通常不充分利用风力涡轮机部件的潜在寿命。风电场的运营商可以利用多余的疲劳预算来增加能源产量,从而降低能量的调整成本(LCoE)。为此,可以延长涡轮机的寿命,直到疲劳预算耗尽。或者,转子叶片延伸部(RBE)是增加风力涡轮机的能量产量的选项。 RBE增加叶片长度,从而增加扫掠区域和能量产量。然而,RBE也增加了涡轮机上的负载。较高的疲劳负载反过来减少了涡轮机的疲劳预算。该研究研究了与唯一寿命延伸(LTE)相比的RBE的使用是有利的。作为用例,研究了位于德国北部的商业1.5兆瓦涡轮机。 Aeroservoelastic多体重负荷模拟和简化的静载性模拟彼此验证。这些模拟显示了载荷来确定涡轮机部件的疲劳预算。由于当超过某个RBE长度时,刀片成为关键部件,因此刀片经受结构疲劳分析。当带叶片长度的引线载荷增加时,聚焦在后缘键合线上的疲劳分析成为关键的。最后,评估了LTE和RBE引起的能源生产提升。对于用案例涡轮机,本研究揭示了LTE 8.7的设计寿命为20?年,额外的能源收益率为43.5%。此外,具有RBE长度为0.8米的34M叶片的延伸进一步增加了2.3%的产率。

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