Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor

摘要

A mounting assembly (36) for an aft end (38) of a liner of a gas turbine engine combustor includes a support member (40). The mounting assembly (36) includes a pin member (46) extending through each one of a plurality of circumferentially spaced openings (42) in a portion of the support member (40) for the combustor and into a plurality of partial openings (44) formed in the aft end (38) of the liner, with each pin member (46) including a head portion (48) at one end thereof, and a device (50) positioned within each opening (42) in the support member (40) so as to retain the pin members (42) therein. The pin members (42) and the support member (40) are able to slide radially and/or axially with respect to the liner aft end (38) as the support member (40) experiences thermal growth greater than the liner.