An armor system includes a ceramic armor layer (12) and a ceramic composite armor layer (14) adjacent to the ceramic armor layer. The ceramic composite armor layer includes a ceramic matrix (34) and unidirectionally oriented fibers (36) disposed within the ceramic matrix (34).
申请公布号
EP2108915(A2)
申请公布日期
2009.10.14
申请号
EP20090005121
申请日期
2009.04.07
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
HOLOWCZAK, JOHN E.;TREDWAY, WILLIAM K.;BARTH, ROBER A.
