| 摘要 |
PROBLEM TO BE SOLVED: To provide methods and apparatus for radially compliant component mounting. SOLUTION: A mounting assembly is provided for a liner of a gas turbine engine combustor 1 including the combustor liner 9 and a radially outer annular flow sleeve 8. The mounting assembly includes an inner ring 208 surrounding a radially outer surface of the liner and including a plurality of axially extending fingers 210. The mounting assembly also includes a radially outer ring 226 coupled to the inner ring through a plurality of spacers 228 that extend radially from a radially outer surface of the inner ring to the outer ring. COPYRIGHT: (C)2008,JPO&INPIT
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