18965600. SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR (RTX Corporation)
SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR
Organization Name
Inventor(s)
Steven W. Burd of Cheshire CT US
SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR
This abstract first appeared for US patent application 18965600 titled 'SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR
Original Abstract Submitted
An assembly is provided for a turbine engine. This turbine engine assembly includes a supplemental thrust section and a duct. The supplemental thrust section includes a rotating detonation combustor. The duct includes a supplemental thrust section inlet fluidly coupled with and leading to the rotating detonation combustor. The supplemental thrust section inlet has a flow area that decreases as at least a first portion of the supplemental thrust section inlet extends towards the rotating detonation combustor.