Three degrees of freedom aft mounting system for gas turbine transition duct
AssigneePower Systems Mfg., LLC
InventorsRobert J. Kraft, Charles Biondo, Brian R. Mack, Mark A. Minnich
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AssigneePower Systems Mfg., LLC
InventorsRobert J. Kraft, Charles Biondo, Brian R. Mack, Mark A. Minnich
Estimating the term…
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.
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:
Dependencies are inferred from the claim text.