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U.S. Department of Energy
Office of Scientific and Technical Information

Methods and apparatus for radially compliant component mounting

Patent ·
OSTI ID:1039557

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.

Research Organization:
National Energy Technology Laboratory (NETL), Pittsburgh, PA, and Morgantown, WV (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-00CH11047
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,141,370
Application Number:
11/463,142
OSTI ID:
1039557
Country of Publication:
United States
Language:
English

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