Rotary kinetic fluid motors or pumps
Bearing, seal, or liner between runner portion and static part
Between blade edge and static part
Inventor
active
Brush seal segment having bristle damping
Controlled leakage shroud panel
Curved film cooling holes for gas turbine engine vanes
External cooling system for turbine frame
Gas turbine engine bleed scoops
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Profile ID: LFUS-PAI-P-122688