MULTI-PIECE INJECTOR NOZZLE FOR A TURBINE ENGINE
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United States of America
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Issued Date -
Mar 20, 2025
app pub date -
Sep 15, 2023
filing date -
Sep 15, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
An apparatus is provided for a turbine engine. This turbine engine apparatus includes an annular nozzle. The annular nozzle includes an inner monolithic body and an outer monolithic body. The inner monolithic body includes an inner shroud and a plurality of vanes. The inner shroud extends axially along and circumferentially around an axis. The vanes are arranged circumferentially about the axis in an array. Each of the vanes projects radially out from the inner shroud to a respective outer distal end. The outer monolithic body is radially outboard of and circumscribes the inner monolithic body. The outer monolithic body is configured as or otherwise includes an outer shroud. The outer shroud extends axially along and circumferentially around the axis. The outer shroud radially engages each of the vanes at the respective outer distal end.
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