A hollow camshaft (19) lubrication system for aircraft engines that supplies lubricant (14) to cam lobe surfaces (25) from the interior surface (22) of the hollow camshaft (19) even during periods when aircraft operation moves the rotation axis of the hollow camshaft (19) from horizontal.
申请公布号
WO0210559(A1)
申请公布日期
2002.02.07
申请号
WO2001US23977
申请日期
2001.07.31
申请人
FIREWALL FORWARD TECHNOLOGIES, LLC.;EHRESMAN, THOMAS, E.;SEADER, MARK, E.
