摘要:
A retainer (82), in an exemplary embodiment of the invention, is used in a gas turbine engine inter-stage seal assembly to retain an annular seal ring flange (50) of a seal ring (48) against an annular platform flange (60) extending radially inwardly from an inner platform (30) of an annular nozzle stage having nozzle vanes (26). The retainer includes a body having a central portion (92) through which a bore (88) is formed around a bore axis (89) and a central tab (94) extends radially outwardly from the central portion (92) with respect to the bore axis (89). First and second arms (97 and 98), respectively, extend in opposite respective first and second tangential directions, with respect to the bore axis (89), away from the central portion (92) and each other. Axial spacers (104) extend aftwardly from first and second free ends (106 and 108) of the first and second arms (97 and 98), respectively and anti-rotation feet with rounded ends depend from the first and second free ends (106 and 108) in an opposite direction from which the central tab (94) extends. A pedestal assembly (110) extends aft from the central portion (92) and is located aft of the central tab. The retainer (82) is an integrally cast unit.
摘要:
A retainer (82), in an exemplary embodiment of the invention, is used in a gas turbine engine inter-stage seal assembly to retain an annular seal ring flange (50) of a seal ring (48) against an annular platform flange (60) extending radially inwardly from an inner platform (30) of an annular nozzle stage having nozzle vanes (26). The retainer includes a body having a central portion (92) through which a bore (88) is formed around a bore axis (89) and a central tab (94) extends radially outwardly from the central portion (92) with respect to the bore axis (89). First and second arms (97 and 98), respectively, extend in opposite respective first and second tangential directions, with respect to the bore axis (89), away from the central portion (92) and each other. Axial spacers (104) extend aftwardly from first and second free ends (106 and 108) of the first and second arms (97 and 98), respectively and anti-rotation feet with rounded ends depend from the first and second free ends (106 and 108) in an opposite direction from which the central tab (94) extends. A pedestal assembly (110) extends aft from the central portion (92) and is located aft of the central tab. The retainer (82) is an integrally cast unit.
摘要:
A dome assembly for a multiple annular combustor is disclosed as including an annular dome plate (35) having at least two radial domes, wherein each of the radial domes include a plurality of circumferentially spaced openings therein. A heat shield (116) is positioned within each of the openings, with a threaded forward end (173) located upstream of the dome plate and an aft end (204) located downstream of the dome plate. A retainer nut (176) with threads (175) formed on an annular surface thereof is matingly engagable with the forward end (173) of each heat shield. When the retainer nut is tightened onto the heat shield forward end, the heat shield is mechanically attached to the dome plate. Preferably, at least one centerbody extends axially downstream from either the radially outer or inner side of the aft end. The dome assembly includes a ferrule (183) within each of the dome plate openings for receiving an air/fuel mixer (50) therein, the ferrule having an annular sealing flange extending radially therefrom. A retaining ring (184) is positioned upstream of the heat shield forward end to produce a gap therebetween. The ferrule sealing flange (216) is positioned within the gap to prevent air from flowing between the heat shield and the air/fuel mixer.