초록 ▼

The cooling air for the nozzle of an augmentor of a gas turbine engine is maintained uniformly around the circumference to assure the prevention of hot streaks that would be occasioned by the liner “sagging”. A separate end piece having judiciously located gaps for directing air over the nozzles, fl

The cooling air for the nozzle of an augmentor of a gas turbine engine is maintained uniformly around the circumference to assure the prevention of hot streaks that would be occasioned by the liner “sagging”. A separate end piece having judiciously located gaps for directing air over the nozzles, flaps and seals attached to the end of the augmentor duct maintains concentricity during augmentor operation, and affords support to the liner of the duct.

대표청구항 ▼

An augmentor for a gas turbine engine having a gas path for flowing the engine\s working medium including a generally circular shaped duct, a variable nozzle attached to the end of the duct in proximity to the engine\s working medium exiting from said duct, a generally circular shaped liner attached

An augmentor for a gas turbine engine having a gas path for flowing the engine\s working medium including a generally circular shaped duct, a variable nozzle attached to the end of the duct in proximity to the engine\s working medium exiting from said duct, a generally circular shaped liner attached to the end of said engine concentrically disposed relative to said duct and defining an open ended annular flow path for receiving cooling air between said engine\s liner and said duct, said liner terminating in proximity to the exit plane of said duct, the improvement comprising an annular, circumferentially disposed sinusoidally shaped member attached to the end of said liner adjacent the exit end of said duct and extending radially outwardly relative to the engine\s working medium and defining open ended passageways, a separate end piece supported to said duct in proximity to said sinusoidal member for distributing the cooling air discharging from said open ended annular flow path and said open ended passageways of said sinusoidally shaped member to said nozzle for defining a uniform flow path around the circumference of said nozzle and to support the liner, one end of said separate end piece providing an abutment for supporting said sinusoidally shaped member when said sinusoidally shaped member is expanded by said engine working medium and said separate end piece extending axially beyond the exit end of said duct and defining with said duct an annular gap having a predetermined auunlar dimension for providing a predetermined amount of cooling air to flow to said nozzle throughout the operating range of said augmentor.