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A fluid damper for attenuating high amplitudes occasioned by shaft unbalance of a main engine shaft of an aircraft turbine type power plant comprising a full ring with circumferentially spaced fluid cavities surrounding the radial bearing and characterized as being simpler and less costly than heret

A fluid damper for attenuating high amplitudes occasioned by shaft unbalance of a main engine shaft of an aircraft turbine type power plant comprising a full ring with circumferentially spaced fluid cavities surrounding the radial bearing and characterized as being simpler and less costly than heretofore used curve beam fluid dampers.

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For a shaft being supported by a radial bearing including an inner race, an outer race and roller bearings supported therebetween, fluid damper means including a one-piece nonrotating support member surrounding said outer race and mounted adjacent thereto, a fixed support housing having wall means d

For a shaft being supported by a radial bearing including an inner race, an outer race and roller bearings supported therebetween, fluid damper means including a one-piece nonrotating support member surrounding said outer race and mounted adjacent thereto, a fixed support housing having wall means defining, a compartment for supporting said bearing, said wall means defining an inner annular surface said nonrotating support member having an outer annular surface complementing said inner annular surface of said fixed housing, a plurality of circumferentially spaced cavities formed in said outer annular surface, means for supplying oil to each of said cavities and means for draining oil from said cavities, the rate of flow into and out of said cavities being selected to create a hydrodynamic force in each of said cavities for damping unbalance loads and sealing means formed around each of said cavities.