Gas turbine engine assemblies with recirculated hot gas ingestion
AssigneeHoneywell International Inc.
InventorsMark C. Morris, Jeff Howe, Greg Heitland, Jason Smoke
Life of this patent
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AssigneeHoneywell International Inc.
InventorsMark C. Morris, Jeff Howe, Greg Heitland, Jason Smoke
Estimating the term…
A gas turbine engine assembly includes a housing including an annular duct wall that at least partially defines a mainstream hot gas flow path configured to receive mainstream hot gas flow. The assembly further includes a stator assembly including a stator vane that extends into the mainstream hot gas flow path and a turbine rotor assembly downstream of the stator assembly that includes a turbine disk and a turbine blade extending from the turbine disk into the mainstream hot gas flow path. The stator assembly and turbine assembly define a turbine disk cavity, and the turbine disk cavity includes a recirculation cavity configured to recirculate gas ingested from the mainstream hot gas flow path back into the mainstream hot gas flow path.
A gas turbine engine assembly, comprising:
An assembly for recirculating gas ingested from a mainstream hot gas flow into a turbine disk cavity between a stator assembly and a turbine assembly in a gas turbine engine, comprising:
A gas turbine engine assembly, comprising:
Dependencies are inferred from the claim text.