发明名称 Nozzle blade
摘要 This relates to a nozzle blade in which the leading edge shape has a curved-line shape that is formed by the distance from the rotation axis of the nozzle blade to the leading edge changing depending on the nozzle blade height position, and the trailing edge shape has a straight-line shape that is formed by the distance from the rotation axis of the nozzle blade to the trailing edge being constant irrespective of the nozzle blade height position.
申请公布号 US9528386(B2) 申请公布日期 2016.12.27
申请号 US201214116462 申请日期 2012.05.24
申请人 IHI CORPORATION 发明人 Morita Isao
分类号 F01D17/16;F01D5/14;F01D9/04;F02B37/24;F02C6/12 主分类号 F01D17/16
代理机构 Ostrolenk Faber LLP 代理人 Ostrolenk Faber LLP
主权项 1. A variable-capacity turbocharger comprising: a turbine impeller which includes turbine blades; a plurality of nozzle blades, each rotatable around a respective shaft portion of each of the nozzle blades, disposed at the periphery of the turbine impeller; a shroud surrounding a tip side of the turbine blades; an opposing wall that is separated from the shroud in a height direction of the nozzle blades; and a nozzle sandwiched by the shroud and the opposing wall, the nozzle being provided with the nozzle blades, wherein a leading edge of the nozzle blades in the height direction of the nozzle blades has a curved-line shape over the entire length of the leading edge relative to a distance from the shaft portion of the nozzle blades to the leading edge which changes depending on a height position of the nozzle blades, anda trailing edge of the nozzle blades in the height direction of the nozzle blades has a straight-line shape such that a distance from the shaft portion of the nozzle blades to the trailing edge being constant irrespective of the height position of the nozzle blades.
地址 JP