Gas turbine engine stator vane base shape
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
-
Mar 29, 2022
Grant Date -
Dec 12, 2019
app pub date -
Jun 6, 2018
filing date -
Jun 6, 2018
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A stator assembly for use in a gas turbine engine is provided. The stator assembly including: a conical stator shroud including a radially inward surface and a radially outward surface opposite the radially inward surface; and a plurality of stator vanes integrally attached to the conical stator shroud, each of the plurality of stator vanes being integrally attached to the conical stator shroud at a base of the stator vane, wherein radially outward surface of the base of the stator vane mates flush with the radially inward surface of the conical stator shroud.
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Family
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