Invention Grant
US08506252B1 Turbine blade with multiple impingement cooling 有权
涡轮叶片具有多次冲击冷却

Turbine blade with multiple impingement cooling
Abstract:
A turbine rotor blade with a cooling air channel formed in a mid-chord region, the channel includes a number of rows of semi-circular shaped ribs that extend across the channel and open toward the blade tip. Adjacent ribs form metering and impingement passages that discharge a jet of cooling air against the rib above it. The open ends of the ribs form vortex generating passages in which the impingement cooling air flows into to form a vortex flow pattern in the cooling air.
Information query
Patent Agency Ranking
0/0