Methods and apparatus for radially compliant component mounting
摘要
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.
申请公布号
US8141370(B2)
申请公布日期
2012.03.27
申请号
US20060463142
申请日期
2006.08.08
申请人
BULMAN DAVID EDWARD;DARKINS, JR. TOBY GEORGE;STUMPF JAMES ANTHONY;SCHRODER MARK S.;LIPINSKI JOHN JOSEPH;GENERAL ELECTRIC COMPANY
发明人
BULMAN DAVID EDWARD;DARKINS, JR. TOBY GEORGE;STUMPF JAMES ANTHONY;SCHRODER MARK S.;LIPINSKI JOHN JOSEPH