Methods and apparatus for a mounting assembly for a liner of a gas turbine engine combustor are provided. The combustor includes a combustor liner and a radially outer annular flow sleeve. The mounting assembly includes an inner ring surrounding a radially outer surface of the liner and including a plurality of axially extending fingers. The mounting assembly also includes a radially outer ring coupled to the inner ring through a plurality of spacers that extend radially from a radially outer surface of the inner ring to the outer ring.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH & DEVELOPMENT
The invention described herein was made in the performance of work under DOE Case No. S-110,587--Disclosure No. 164632--Contract No. DE-FC26-00CH11047, currently administered by the Department of Energy.