Methods and apparatus to facilitate sealing between rotating turbine shafts

A seal assembly (60) for a gas turbine engine includes a first rotatable shaft (42) and a second rotatable shaft (44). the seal assembly comprises a brush seal (70) and a plurality of seal projections (72) extending outwardly from the brush seal. the brush seal is sealingly coupled to the first rotatable shaft such that the plurality of seal projections contact the second rotatable shaft to facilitate sealing between the first and second rotatable shafts.