Invention Application
- Patent Title: FLOWPATH COMPONENT FOR A GAS TURBINE ENGINE INCLUDING A CHORDAL SEAL
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Application No.: US15267632Application Date: 2016-09-16
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Publication No.: US20180080334A1Publication Date: 2018-03-22
- Inventor: Mark A. Boeke , Jeffrey J. DeGray , Richard M. Salzillo, JR.
- Applicant: United Technologies Corporation
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F02C3/04 ; F01D5/06 ; F01D9/04
Abstract:
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.
Public/Granted literature
- US10329937B2 Flowpath component for a gas turbine engine including a chordal seal Public/Granted day:2019-06-25
Information query
