Invention Grant
US08453463B2 Anti-vortex device for a gas turbine engine compressor 有权
用于燃气涡轮发动机压缩机的防涡流装置

Anti-vortex device for a gas turbine engine compressor
Abstract:
An anti-vortex device for use in a compressor rotor assembly of a gas turbine engine is described. Spaced-apart radial passageways extend from an axially extending passage provided in a central area of the device to an outer peripheral rim surface thereof. The radial passageways channel air from the primary gaspath about the rotor assembly to the axially extending passage where the air is directed into a central axial passage of the rotor assembly.
Public/Granted literature
Information query
Patent Agency Ranking
0/0