发明名称 Wind turbine blade and wind turbine generator including the same
摘要 Provided is a wind turbine blade that can improve aerodynamic performance in a blade-tip region and reduce aerodynamic noise. A wind turbine blade includes a blade body having a chord length that decreases from a blade root side to a blade tip side, wherein the blade body includes a blade-tip region in which a dimensionless radial position is within the range of 0.6 to 1.0, inclusive, the dimension less radial position being the ratio of radial position to blade radius (½ of a blade diameter), and a blade-body region in which the dimensionless radial position is smaller than 0.6, and wherein a maximum-blade-thickness position of a blade cross-section in the blade-tip region is closer to a leading edge than a maximum-blade-thickness position of a blade cross-section in the blade-body region.
申请公布号 US8801387(B2) 申请公布日期 2014.08.12
申请号 US201213468205 申请日期 2012.05.10
申请人 Mitsubishi Heavy Industries, Ltd. 发明人 Fukami Koji
分类号 F01D5/14;F03D1/06 主分类号 F01D5/14
代理机构 代理人 Kanesaka Manabu;Hauptman Benjamin J.
主权项 1. A wind turbine blade comprising: a blade body having a chord length that decreases from a blade root side to a blade tip side, wherein the blade body includes a blade-tip region in which a dimensionless radial position is within the range of 0.6 to 1.0, inclusive, the dimensionless radial position being the ratio of radial position to blade radius (½ of a blade diameter), and a blade-body region in which the dimensionless radial position is smaller than 0.6, wherein a maximum-blade-thickness position of a blade cross-section in the blade-tip region is closer to a leading edge than a maximum-blade-thickness position of a blade cross-section in the blade-body region, wherein the leading edge in the blade-tip region is shifted in the direction of the trailing edge such that a maximum-blade-thickness line formed by connecting, in the radial direction, the maximum-blade-thickness positions of the blade cross-sections at radial positions form a substantially straight line, and wherein the leading edge in the blade-tip region is S-shaped such that the leading edge shifts greatly toward the trailing edge in a transition region from the blade-body region to the blade-tip region, shifts gradually in the direction of the trailing edge toward the blade tip in a connecting region, which is connected to the transition region, and shifts in the direction of the trailing edge to finally connect with the blade tip in an end region, which is connected to the connecting region.
地址 Tokyo JP