Abstract: A turbine engine fan casing for containing a separated blade fragment comprising a support case having an axially extending impact zone, a substantially structurally continuous penetrable covering circumscribing the impact zone; and a containment covering circumscribing the penetrable covering. The containment covering comprises a textile fabric containing threads in a warp direction and a fill direction, wherein the threads in the warp direction are of a different denier than the threads in the fill direction.
Type:
Grant
Filed:
June 1, 2006
Date of Patent:
April 14, 2009
Assignee:
Unied Technologies Corporation
Inventors:
Mark W. Costa, Jan B. Kowza, Curt R. Hetherington, Wendy P. Lopardi, Douglas Welch