Invention Grant
US09574460B2 Support arrangement for a transition piece of a gas turbine engine 有权
用于燃气涡轮发动机的过渡件的支撑装置

Support arrangement for a transition piece of a gas turbine engine
Abstract:
A support arrangement (10) for a transition piece (12) of a gas turbine engine (14). The support arrangement includes a mounting bracket (16) for the transition piece and a pin (18) supporting the mounting bracket in an interior (20) of the gas turbine engine and extending through an opening (22) in a casing (24) to an exterior (26) of the gas turbine engine. The support arrangement further includes a spherical washer (28, 38) positioned between the pin and either the mounting bracket or the casing.
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