A ceramic shroud assembly suitable for use in a gas turbine engine comprises a metal clamp ring shrink fitted around a ceramic shroud ring and an insulating and compliant interlayer. The interlayer is positioned between the metal clamp ring and the ceramic shroud ring.
申请公布号
US2010104433(A1)
申请公布日期
2010.04.29
申请号
US20060502212
申请日期
2006.08.10
申请人
UNITED TECHNOLOGIES CORPORATION ONE FINANCIAL PLAZA
