Engine component
An engine component for a turbine engine. The engine component has a composite structure and a cover structure. The composite structure has a composite structure outer wall, a composite structure edge, and a channel. The channel is provided along the composite structure edge. The cover encases at least a portion of the composite structure outer wall. The cover has a main body and an extension.
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 from the composite structure edge, with respect to the centerline, the extension received within the channel;
wherein at least a portion of the composite structure is located radially between opposite sides of the extension and the main body, with respect to the centerline.
2 . The engine component of claim 1 , wherein the main body extends along at least a portion of the composite structure outer wall that is axially spaced aft of the composite structure edge.
3 . The engine component of claim 1 , wherein the main body extends along at least a portion of the composite structure outer wall that is axially spaced forward of the composite structure edge.
4 . The engine component of claim 3 , wherein the turbine engine comprises a fan section, and the composite structure is a fan casing of the fan section.
5 . The engine component of claim 4 , wherein the turbine engine includes an engine casing, and wherein the cover structure couples the fan casing to the engine casing.
6 . The engine component of claim 1 , wherein:
the composite structure includes an airfoil portion having an outer wall defining the composite structure outer wall; and
the composite structure outer wall extends between a composite structure root and a composite structure tip, and between a composite structure leading edge and a composite structure trailing edge, with the composite structure edge being at least one of the composite structure tip, the composite structure leading edge, or the composite structure trailing edge.
7 . The engine component of claim 1 , wherein the engine component is an airfoil assembly having an airfoil portion extending between a root and a tip, and a midspan shroud extending from the airfoil assembly, the midspan shroud being the composite structure.
8 . The engine component of claim 7 , wherein the composite structure outer wall extends between a composite structure leading edge and a composite structure trailing edge, the midspan shroud includes a midspan distal end interconnecting the composite structure trailing edge and the composite structure leading edge, with the cover structure overlying at least a portion of the midspan distal end.
9 . The engine component of claim 7 , wherein:
the turbine engine has an engine centerline;
the airfoil assembly includes two adjacent airfoil portions circumferentially spaced with respect to the engine centerline;
the midspan shroud extends non-continuously between the two adjacent airfoil portions to define circumferentially opposing midspan distal ends; and
the cover structure is provided along the circumferentially opposing midspan distal ends.
10 . The engine component of claim 1 , wherein the composite structure comprises an alignment channel provided along the composite structure outer wall, and the cover structure comprises an aligner provided along the main body, the aligner being received within the alignment channel.
11 . The engine component of claim 1 , wherein:
the main body extends a first centerline length axially with respect to the centerline; and
the extension extends a second centerline length axially with respect to the centerline, the second centerline length being greater than or equal to 10% and less than or equal to 100% of the first centerline length.
12 . The engine component of claim 1 , wherein the extension includes a set of barbs extending into the composite structure.
13 . The engine component of claim 1 , wherein the extension includes a triangular shape when viewed along a plane locally perpendicular to the composite structure edge and intersecting the extension.
14 . The engine component of claim 1 , wherein at least a portion of the extension is bifurcated.
15 . The engine component of claim 1 , wherein the extension includes a rectangular shape when viewed along a plane locally perpendicular to the composite structure edge and intersecting the extension.
16 . The engine component of claim 1 , wherein the cover structure includes at least one of a metallic material or a plastic material.
17 . 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 from the composite structure edge, with respect to the centerline, the extension received within the channel;
wherein:
the main body and the extension are integrally formed;
the channel extends into the composite structure in a first direction, with respect to the centerline; and
the extension has a cross-sectional area when viewed along a plane extending along the centerline and intersecting the cover structure, the cross-sectional area of the extension being non-constant in a second direction, transverse the first direction, within the channel.
18 . 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, the extension received within the channel;
wherein:
the main body terminates at a main body distal end that is spaced a first centerline length axially from the composite structure edge in an axial direction, with respect to the centerline; and
the extension terminates at an extension distal end that is spaced a second centerline length axially from the composite structure edge in the axial direction, with respect to the centerline, the second centerline length being less than or equal to the first centerline length.
19 . The engine component of claim 18 , wherein the main body extends along at least a portion of the composite structure outer wall that is axially spaced aft of the composite structure edge.
20 . The engine component of claim 18 , wherein the engine component is one of an airfoil or a fan casing.