Methods and apparatus for radially compliant component mounting

Methods and apparatus for radially compliant component mounting

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...

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Hauptverfasser: Bulman, David Edward, Darkins, Jr, Toby George, Stumpf, James Anthony, Schroder, Mark S, Lipinski, John Joseph
Format: Patent
Sprache:eng
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creator Bulman, David Edward
Darkins, Jr, Toby George
Stumpf, James Anthony
Schroder, Mark S
Lipinski, John Joseph
description 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.
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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.</abstract><oa>free_for_read</oa></addata></record>
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title Methods and apparatus for radially compliant component mounting
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