Sealing ring for gas turbine engines

A rotor assembly comprising a first rotatable member having a surface with a groove formed therein, a second rotatable member concentric with the first member and spaced apart therefrom to define an annular gap therebetween, and an expandable sealing ring located in the groove for sealing the annular gap, the sealing ring comprising:

• a first pair of adjoining surfaces defining a first edge, said first edge being the radially outermost part of the sealing ring, and a second pair of adjoining surfaces defining a second edge diagonally opposite and spaced a predetermined distance from the first edge, and
• an expandable scarf joint connecting circumferential ends of said sealing ring, wherein said predetermined distance is defined to permit, via the centrifugal force generated when the rotor is rotated at high speed, the first edge to sealingly contact the second member, the second edge to sealingly contact the groove, and one of the first pair of adjoining surfaces to contact the groove, wherein the plane of the scarf joint lies between the first and second edges of the ring so that continuous line seal contacts are maintained at both the first and second edges of the ring.