Invention Application
US20090074562A1 NOZZLE GUIDE VANES 有权
喷嘴指南

NOZZLE GUIDE VANES
Abstract:
A turbine nozzle guide vane 10 with passages 28 leading from a hollow core 32 to respective seal strip slots 20, to deliver cooling air to abutment faces 18 on each end of the vane 10.
Public/Granted literature
Information query
Patent Agency Ranking
0/0