The present invention is directed toward a suspension system for mounting an exhaust duct liner within an exhaust duct of a gas turbine engine. An exhaust liner suspension system comprises a hanger, a bracket and a coil pin. The hanger comprises a first end for connecting with an exhaust duct and a second end having a hinge pin socket. The bracket comprises a base for connecting with an exhaust duct liner and a pedestal having a hinge pin bore. The coil pin is insertable in the hinge pin socket and the hinge pin bore thereby pivotably connecting the hanger and the bracket. The coil pin also provides a dampened connection between the hanger and the bracket.
申请公布号
WO2008054436(A2)
申请公布日期
2008.05.08
申请号
WO2007US00406
申请日期
2007.01.05
申请人
UNITED TECHNOLOGIES CORPORATION;FARAH, JORGE, I.;NACKOUL, MICHAEL, E.;CINTRON, JOSE, M.
发明人
FARAH, JORGE, I.;NACKOUL, MICHAEL, E.;CINTRON, JOSE, M.