Propeller blade
A propeller blade comprising a composite member. The composite member comprises a stack of plies and a matrix in which the stack of plies is embedded. At least one ply comprises a plurality of first yarns aligned in a first direction defining a plane of the ply and a plurality of second yarns extending transverse to the plane of the ply. Each second yarn does not extend through more than one ply. Also provided is a propelling system comprising the propeller blade, a composite propeller blade prepreg, and a method of forming a propeller blade.
1. A propeller blade comprising:
a composite member comprising a stack of plies, at least one ply comprising:
a plurality of first yarns aligned in a first direction defining a plane of the at least one ply; and
a plurality of second yarns ( 106 ) extending transverse to the plane of the at least one ply; wherein each second yarn does not extend through more than one ply, wherein the second yarns pass though the plane of the at least one ply; and
a matrix in which the stack of plies is embedded.
2. The propeller blade of claim 1 , wherein each of the plurality of second yarns extends beyond the ply by between 50 and 1000 microns.
3. The propeller blade of claim 1 , wherein one of the at least one plies includes a plurality of second yarns extending transverse to the plane of the ply forms an outermost ply of the ply stack;
the blade further comprising:
a second member disposed adjacent to the outermost ply of the stack of plies.
4. The propeller blade of claim 3 , wherein the second member comprises a textured surface and wherein the plurality of second yarns interact with the textured surface.
5. The propeller blade of claim 4 , wherein the textured surface is textured on at least one of the micro and nano scale.
6. The propeller blade of claim 3 , wherein the plurality of second yarns is joined to the second member by an adhesive.
7. The propeller blade of claim 3 , wherein the second member is a metallic blade root.
8. The propeller blade of claim 7 , wherein the root and the composite member overlap along a partial axial extent of the blade.
9. The propeller blade of claim 3 , wherein the second member is one of a foam insert, a glass ply, an aramid shell, an I-beam or a metal sheath.
10. The propeller blade of claim 1 , further comprising:
a spar, the composite member forming at least part of the spar.
11. The propeller blade of claim 3 , wherein the second member is a metallic leading edge member.
12. The propeller blade of claim 1 , further comprising:
a leading edge member defining at least part of a leading edge of the propeller blade and wherein the composite member defines the leading edge member.
13. The propeller blade of claim 12 , wherein the leading edge member extends from a base end of the propeller blade to a tip of the propeller blade.
14. The propeller blade of claim 12 , further comprising:
a leading edge insert, wherein the leading edge member overlays the leading edge insert.
15. A propelling system comprising:
a propeller blade of claim 1 .