Adaptive engine with boost spool
AssigneeUnited Technologies Corporation
InventorsPaul R. Hanrahan, Daniel Bernard Kupratis
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AssigneeUnited Technologies Corporation
InventorsPaul R. Hanrahan, Daniel Bernard Kupratis
Estimating the term…
A gas turbine engine includes a first spool, a second spool, a primary combustor, and a diffuser. The first spool includes a first compressor rotationally driven by a first turbine via a first shaft. The second spool includes a second compressor driven by a second turbine via a second shaft. The first compressor, the diffuser, and the primary combustor are arranged in series to provide a compressed airflow discharged from the first compressor to the primary combustor via the diffuser, which includes walls that diverge towards the primary combustor. The second compressor is fluidly coupled to the diffuser to receive at least a portion of the compressed airflow from the diffuser. The second turbine is fluidly coupled to the diffuser to discharge an expanded airflow to the diffuser.
A gas turbine engine comprising:
Dependencies are inferred from the claim text.