Rotary kinetic fluid motors or pumps
Bearing, seal, or liner between runner portion and static part
Between axial flow runner and vane or vane diaphragm structure
Inventor
active
Centrifugally operated axial and torsional vibration reducer for
Control apparatus for gas turbine
Gas turbine combustor
Gas turbine combustor
Gas turbine combustor by-pass valve device
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Profile ID: LFUS-PAI-P-1153067