FLOWPATH COMPONENT FOR A GAS TURBINE ENGINE INCLUDING A CHORDAL SEAL

摘要

A flow path component (100) includes a platform (110,120) having at least one radially aligned face (114,124). A chordal seal (160,170) extends axially from the radially aligned face (114,124). The chordal seal (160,170) includes a first curved face (162,172) configured to prevent edge line contact under deflection conditions while the flow path component (100) is installed in an engine (20).