Patent ID: 7647775

Claim:
A turbine engine augmentor comprising: a centerbody within a gas flowpath from upstream to downstream and having a downstream tailcone; and a plurality of vanes positioned in the gas flowpath outboard of the centerbody and having first and second sides; an augmentor fueling system comprising: a plurality of spray bars, each spray bar at least partially within an associated at least one of said vanes, comprising: a conduit; and a plurality of nozzles coupled to the conduit, each nozzle positioned to discharge an associated fuel stream from one of the sides of the associated vane; and a plurality of blocks, each block mounted within the associated vane relative to an associated one of the nozzles for a range of motion relative thereto between an inward extreme and an outward extreme and movably cooperating with the associated vane, wherein there are nozzles along each of the first side and second side of each of the vanes and each said vane contains a plurality of said blocks, each said block mounted to the associated said nozzle.