Rotary kinetic fluid motors or pumps
Bearing, seal, or liner between runner portion and static part
Between blade edge and static part
Inventor
active
Casing, a compressor, a turbine, and a combustion turbine...
Three-spool by-pass turbojet with a high by-pass ratio
Turbojet architecture with two fans at the front
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Profile ID: LFUS-PAI-P-2836617