公开(公告)号：EP2809933B1

公开(公告)日：2020-09-23

申请号：EP13767469.3

申请日：2013-01-07

申请人： Raytheon Technologies Corporation

发明人： ATASSI, Oliver V. ,  PETRENKO, Oleg

IPC分类号： F02K3/04 ,  F02K1/09

公开(公告)号：EP3825538A1

公开(公告)日：2021-05-26

申请号：EP20215392.0

申请日：2010-11-24

申请人： Raytheon Technologies Corporation

发明人： SCHWARK, JR., Fred W. ,  ATASSI, Oliver V. ,  OWEN, William D.

IPC分类号： F02K1/09 ,  F02K1/72

摘要： A variable area fan nozzle (42) for a high-bypass gas turbine engine (10) includes a first track slider (74) movable relative to the hinge beam (72) along a first interface. A second track slider (76) is movable relative to the first track slider (74) along a second interface that includes a bearing assembly (84). A VAFN cowl (70) is mounted to the second track slider (76).