Flow guides for internal cooling of a CMC airfoil
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
-
Feb 25, 2025
Grant Date -
Dec 21, 2023
app pub date -
Jun 17, 2022
filing date -
Jun 17, 2022
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A component for a gas turbine engine includes a matrix composite component having a radially outer end and a radially inner end. The ceramic matrix component having an internal chamber defined by an inner surface. A spar is received within the internal cavity, and spaced from an inner surface of the matrix component defining a chamber with the inner surface. Flow guides are formed on one of an outer surface of the spar and the inner surface of the matrix component. The flow guides direct airflow towards a portion of the inner surface. An air inlet chamber is formed at one radial end of the spar and an air outlet chamber formed at an opposed radial end of the spar. The air inlet chamber is defined such that air will flow into the internal chamber, outwardly of the spar, and inwardly of the inner surface of the matrix component. A gas turbine engine is also disclosed.
First Claim
Other Claims data not available
Family
International Classification(s)
- 2022 Application Filing Year
- F23R Class
- 253 Applications Filed
- 151 Patents Issued To-Date
- 59.69 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F23R Class
- 0 % this patent is cited more than
- < 1 Age
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