Disclosed is a linkage assembly for a gas turbine engine (20) having a link (102a-102d) having a first end (104a), a second end (104b), and a rod (106) extending therebetween, the first end having a first sliding bearing (108) disposed within a first sliding bearing housing (107), a fastener (118) comprising a first flange (126a) and a second flange (126b), a pin (120) extending between the first flange and the second flange, wherein the first sliding bearing is pivotally connected to the pin; and a biasing member (136a, 136b) secured between the first flange and the sliding bearing housing, the biasing member contacting the sliding bearing housing and biasing the link against rotation about a center axis for the rod of the link.
LINKAGE ASSEMBLY
GESTÄNGEANORDNUNG
ENSEMBLE DE LIAISON
2021-08-25
Patent
Elektronische Ressource
Englisch