Seal assembly for a turbine engine

A turbine engine, comprising:

• a rotor;
• a stator comprising an aft wall;
• a seal assembly comprising a plurality of seal segments disposed between the rotor and the stator, wherein the rotor, the stator, and the seal assembly are arranged together to define a high pressure region and a low pressure region;
• and
• at least one biasing member engaged with one or more of the plurality of seal segments,
• wherein the plurality of seal segments comprise a primary seal segment and a secondary seal segment connected together via a flexible joint, and
• wherein the flexible joint comprises at least one of a pivot joint, a hinge joint, or a pin joint to allow for angular misalignment between the primary seal segment and the secondary seal segment, thereby allowing the primary seal segment to move with the rotor while the secondary seal segment maintains contact with the aft wall of the stator.