There is disclosed a reheat assembly (100) for a gas turbine engine, the reheat assembly comprising; a jetpipe casing (102,310) defining a reheat core section (104) configured to duct a core flow of air and a reheat bypass section (106) configured to duct ...

The invention relates to a mixing arrangement for mixing a fuel (13, 15) with a stream of oxygen containing gas flowing along an axis (16) in an axial channel, especially in the second combustor of a gas turbine with sequential combustion. The mixing is im...

One embodiment of the present invention is a gas turbine engine (10), comprising a thrust augmentation system (64) with a fluidic flameholder, which ejects the fuel (82) by generating an obstruction to the exhaust flow of the turbine engine.

A method for fabricating an augmentor (100) includes fabricating an outer casing having at least one channel (133) defined therein, fabricating a centerbody (103) having at least one channel (134) defined therein, fabricating a plurality of turbine frame v...

The strut has a monoblock structure of ceramic material and formed with CERASEP. The structure has two symmetric walls (14, 15) to define a groove (16), end parts (17) joined together to define a base (18), and end parts (19) to define respective flanges (...

The ring (19) has burner ring with an upstream annular envelope forming a gorge in which a fuel injection harness (4) is arranged. The annular envelope has an upstream surface that is in contact with a flow of exhaust gas. Each of multiple ring sectors has...

A turbine engine augmentor (32) has a centerbody (38) within a gas flowpath. A flameholder (42) is positioned in the flowpath outboard of the centerbody (38). A burner (62) within the centerbody (38) has an outlet for expelling combustion products of a fir...

An afterburner apparatus (10) that utilizes a novel swirl generator (30) for rapidly and efficiently atomizing, vaporizing, as necessary, and mixing a fuel into an oxidant. The swirl generator (30) converts an oxidant flow into a turbulent, three-dimension...

A heat shield (20) and support strut (66) for protecting a fuel injection tube (22) of a turbine engine afterburner section (24) are described. The heat shield (20) can be replaced in the afterburner section without moving or disconnecting the fuel injecti...