US 12,410,716 B1
Engine component
Ming Xie, Dayton, OH (US); Arthur W. Sibbach, Boxford, MA (US); and Nicholas J. Kray, Mason, OH (US)
Assigned to General Electric Company, Evendale, OH (US)
Filed by General Electric Company, Schenectady, NY (US)
Filed on May 3, 2024, as Appl. No. 18/654,134.
Int. Cl. F01D 5/14 (2006.01); F01D 5/28 (2006.01)
CPC F01D 5/147 (2013.01) [F01D 5/282 (2013.01); F05D 2240/303 (2013.01); F05D 2240/304 (2013.01); F05D 2250/12 (2013.01)] 20 Claims
OG exemplary drawing
 
1. An engine component for a turbine engine, the engine component comprising:
a composite structure having a composite structure outer wall, a composite structure edge, and a channel provided along the composite structure edge, the composite structure having a centerline extending from the composite structure edge; and
a cover structure encasing at least a portion of the composite structure outer wall, the cover structure including a main body and an extension, the main body extending along at least a portion of the composite structure outer wall that is axially spaced aft of the composite structure edge, with respect to the centerline, the extension received within the channel.