Aerodynamic component for a gas turbine engine
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
-
Mar 12, 2024
Grant Date -
N/A
app pub date -
Nov 24, 2021
filing date -
Nov 24, 2021
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aerodynamic component of a gas turbine engine is provided and is fittable to a shell having a shell shape. The aerodynamic component includes a body having a component shape initially deviating from the shell shape prior to an assembly operation in which the aerodynamic component is to be fit to the shell. Deviation of the component shape from the shell shape aids in an establishment of a final desired shape of the aerodynamic component following the assembly operation.
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International Classification(s)
- 2021 Application Filing Year
- F23M Class
- 16 Applications Filed
- 8 Patents Issued To-Date
- 50 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F23M Class
- 0 % this patent is cited more than
- 1 Age
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