JAM PROTECTION AND ALLEVIATION FOR CONTROL SURFACE LINKAGE MECHANISMS
摘要
A flaperon mechanism that provides jam protection while preventing the component departing from the airplane or causing unacceptable collateral damage. The jam protection feature comprises a controlled failure (fused) mechanism that is associated with the flaperon and flaperon hinge panel and maintains functional movement of the devices. Additional features can be added to the mechanism to block, shield, allow runout and shed other obstruction avenues.
申请公布号
WO2013081697(A3)
申请公布日期
2014.11.27
申请号
WO2012US52624
申请日期
2012.08.28
申请人
THE BOEING COMPANY;MACLEAN, ROBERT DOUGLAS;KORDEL, JAN A.;STEYAERT, WARREN H.;BOES, DAVID DOUGLAS
发明人
MACLEAN, ROBERT DOUGLAS;KORDEL, JAN A.;STEYAERT, WARREN H.;BOES, DAVID DOUGLAS