Invention Grant
US08205458B2 Duplex turbine nozzle 有权
双相涡轮喷嘴

Duplex turbine nozzle
Abstract:
A duplex turbine nozzle includes a row of different first and second vanes alternating circumferentially between radially outer and inner bands in vane doublets having axial splitlines therebetween. The vanes have opposite pressure and suction sides spaced apart in each doublet to define an inboard flow passage therebetween, and corresponding outboard flow passages between doublets. The vanes have different patterns of film cooling holes with larger cooling flow density along the outboard passages than along the inboard passages.
Public/Granted literature
Information query
Patent Agency Ranking
0/0