REVERSIBLY MOUNTABLE BLADE PLATFORM SEAL

摘要

A rotatable sealing structure for a gas turbine engine (20) includes a first blade (64) and a second blade (64). A seal (80) is arranged between the blades (64) and has a body (80) that is configured for operative association with the first and second blades (64) in a first orientation and in a second orientation to seal a gap (76) defined between the blades (64).