Abstract: The bearing assembly can extend between a rotor and a housing, have a plurality of bearing rolling elements mounted for rotation within a bearing ring, an oil damper cavity between the bearing ring and the housing, an oil inlet path to feed the oil damper cavity, and at least one damper ring defining a corresponding axial limit to the oil damper cavity and having a radially inner edge received in a corresponding annular groove defined in the bearing ring, and a radially outer edge having at least one arc portion extending radially outwardly relative the annular groove and engaging the housing, and at least one controlled leakage portion radially recessed from the housing and forming a leakage path leading axially out from the oil damper cavity.

Abstract: The gas turbine engine assembly can include a first component having a male fit perimeter, a second component having a female fit perimeter forming an interference fit with the male fit perimeter, one of the first component and the second component having a pulling lip spanning transversally and further spanning peripherally, and a structure holding the pulling lip transversally offset from the interference fit, the structure having a bending portion extending at least partially transversally.

Abstract: The gas turbine engine assembly can include a first component having a male fit perimeter, a second component having a female fit perimeter forming an interference fit with the male fit perimeter, one of the first component and the second component having a pulling lip spanning transversally and further spanning peripherally, and a structure holding the pulling lip transversally offset from the interference fit, the structure having a bending portion extending at least partially transversally.

Abstract: The bearing assembly can extend between a rotor and a housing, have a plurality of bearing rolling elements mounted for rotation within a bearing ring, an oil damper cavity between the bearing ring and the housing, an oil inlet path to feed the oil damper cavity, and at least one damper ring defining a corresponding axial limit to the oil damper cavity and having a radially inner edge received in a corresponding annular groove defined in the bearing ring, and a radially outer edge having at least one arc portion extending radially outwardly relative the annular groove and engaging the housing, and at least one controlled leakage portion radially recessed from the housing and forming a leakage path leading axially out from the oil damper cavity.