<p>A catcher for a gas turbine engine includes a central hub, a plurality of struts, and a first ring. The plurality of struts are connected to and extend outward from the central hub. The first ring is connected to a mid-section of the plurality of struts and extends therebetween.</p>
申请公布号
WO2014004825(A1)
申请公布日期
2014.01.03
申请号
WO2013US48173
申请日期
2013.06.27
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ALEXANDER, ERIC, J.;HAGSHENAS, BEHZAD;ELGIN, RICHARD, L.
