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Flowpath component for a gas turbine engine including a chordal seal
Flowpath component for a gas turbine engine including a chordal seal
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机译:包括弦密封的燃气涡轮发动机的流路部件
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摘要
A flow path component includes a platform having at least one radially aligned face. A chordal seal extends axially from the radially aligned face. The chordal seal includes a first curved face configured to prevent edge line contact under deflection conditions while the flow path component is installed in an engine.
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