发明名称 Turbine blade angel wing with pumping features
摘要 A gas turbine engine, including: a plurality of blades (60) assembled into an annular row of blades and partly defining a hot gas path (26) and a cooling fluid path (24), wherein the cooling fluid path extends from a rotor cavity (22) to the hot gas path; an angel wing assembly (99) disposed on a side (74) of a base (76) of the row of blades; and pumping features (130) distributed about the angel wing assembly configured to impart, at a narrowest gap (42) of the cooling fluid path, motion to a flow of cooling fluid flowing there through. The plurality of pumping features, the angel wing assembly, and the base of the row of blades are effective to produce a helical motion to the flow of cooling fluid as it enters the hot gas path.
申请公布号 US8926283(B2) 申请公布日期 2015.01.06
申请号 US201213688411 申请日期 2012.11.29
申请人 Siemens Aktiengesellschaft 发明人 Lee Ching-Pang;Tham Kok-Mun;Vitt Paul H.;Schroeder Eric
分类号 F01D11/00;F01D5/14;F01D11/02 主分类号 F01D11/00
代理机构 代理人
主权项 1. A gas turbine engine, comprising: a plurality of blades assembled into an annular row of blades about a gas turbine engine longitudinal axis and partly defining both a hot gas path and a cooling fluid path, wherein the cooling fluid path extends from a rotor cavity, past a side of a radially inward base of the row of blades where the side is upstream with respect to a flow of hot gases in the hot gas path, and leads to the hot gas path; an angel wing assembly disposed on the side of the base of the row of blades; and a plurality of pumping features, each comprising a single pumping surface and a complementary surface, distributed about the angel wing assembly configured to impart, at a narrowest gap of the cooling fluid path defined by the angel wing, motion to a flow of cooling fluid flowing there through, wherein the plurality of pumping features, the angel wing assembly, and the base of the row of blades are effective to produce a helical motion about the gas turbine engine longitudinal axis to the flow of cooling fluid as it enters the hot gas path, and wherein the single pumping surface and the complementary surface are disposed radially inward of and transverse to a radially outer surface of the angel wing assembly and circumferentially adjacent to each other.
地址 München DE