초록 ▼

A multiple directional axes structural support system for use as the aft end mount for a gas turbine transition duct to a turbine inlet is disclosed. The mounting system is configured to withstand high temperature gradients and mechanical loads associated with gas turbine environments while allowing

A multiple directional axes structural support system for use as the aft end mount for a gas turbine transition duct to a turbine inlet is disclosed. The mounting system is configured to withstand high temperature gradients and mechanical loads associated with gas turbine environments while allowing multiple axes adjustment and interface capability between the transition duct and the turbine inlet casing. A spherical ball joint allows for rotation about multiple (three) axes to compensate for relative thermal growth, manufacturing tolerances, and assembly tolerances between mating surfaces. The ball joint is held in place by fitted spacers, bosses, and a through-bolt, that when torqued will dampen out unwanted vibrations in the multi-axis mounting system.

대표청구항 ▼

1. A support system for attaching the aft end of a gas turbine transition duct to a turbine inlet housing to provide three degrees of freedom of relative movement between the duct and the turbine inlet comprising:a) a base member contoured to an outer wall of the transition duct member and rigidly a

1. A support system for attaching the aft end of a gas turbine transition duct to a turbine inlet housing to provide three degrees of freedom of relative movement between the duct and the turbine inlet comprising:a) a base member contoured to an outer wall of the transition duct member and rigidly attachable thereto; b) said base member further including rigidly attached fingers; c) a support assembly including: a central bracket having a central spherical ball mount at one end connected within said base member fingers, providing three degrees of freedom of movement between the base member and the central bracket and a mounting surface at the other end for mating the transition duct to said turbine inlet; a pair of contoured washers sized to mate to said central spherical ball mount and constructed of such material as to absorb wear from said spherical ball mount due to vibrations; a pair of contoured ring mounts to accept said contoured washers and spherical ball mount sized to fit between said contoured washers and said fingers; an interconnecting fastener fitted through said fingers, contoured ring mounts, contoured washers, and central spherical ball mount for retaining said central spherical ball mount with three degrees of freedom; said interconnecting fastener configured such that a force maybe applied to said fingers and contoured ring mounts to resist said motion of said central spherical ball mount with three degrees of freedom.