Automated variable pitch propeller blade

1 . A propeller blade comprising:

a first material comprising fibers that extend through the propeller blade in a longitudinal direction to form a longitudinal fiber structure or extend along a chord line of a cross-section of the propeller blade; and

a second material different from the first material, wherein the fibers are interspersed through the second material,

wherein the propeller blade includes multiple sections comprising:

a first section where the fibers are substantially uniformly oriented between a leading edge and a trailing edge of the propeller blade; and

a second section where a volume fraction of the first material decreases from the leading edge to the trailing edge.

2 . The propeller blade of claim 1 , wherein the leading edge comprises 66% carbon fiber and 34% polycarbonate and the trailing edge comprises 4% carbon fiber and 96% polycarbonate.

3 . The propeller blade of claim 1 , wherein the multiple sections of the fibers are three or more sections.

4 . The propeller blade of claim 1 , wherein the first material includes carbon fibers and the second material is a polycarbonate matrix.

5 . The propeller blade of claim 4 , wherein the propeller blade includes the carbon fibers in an amount of 4% by volume and the polycarbonate matrix an amount of 96% by volume.

6 . The propeller blade of claim 1 , wherein the first material comprises any of carbon fibers and glass fibers and the second material comprises any of polycarbonate and nylon.

7 . The propeller blade of claim 1 , wherein the longitudinal direction extends longitudinally between a blade root and a blade tip.

8 . The propeller blade of claim 1 , wherein the multiple sections comprise:

a third section located at a tip of the propeller blade, the third section comprising:

a blade pitch of 1-20 degrees.

9 . A propeller blade comprising:

multiple sections, wherein the multiple sections comprise:

a first material comprising fibers;

a second material different from the first material;

a first section where the fibers are substantially uniformly oriented between a leading edge and a trailing edge of the propeller blade; and

a second section where a volume fraction of the first material decreases from the leading edge to the trailing edge,

wherein the fibers of the first material are interspersed through the second material in a longitudinal direction to form a longitudinal fiber structure or extend along a chord line of a cross-section of the propeller blade.

10 . The propeller blade of claim 9 , wherein the multiple sections of the propeller blade are located along a length of the propeller blade and have substantially a same intrinsic parameter.

11 . The propeller blade of claim 9 , wherein the multiple sections further comprise:

a third section where the volume fraction of the first material decreases from the leading edge to the trailing edge.

12 . The propeller blade of claim 11 , wherein the volume fraction of the first section is substantially uniform from the leading edge to the trailing edge and the volume fraction of the first section is greater than that of the second section and that of the third section.

13 . The propeller blade of claim 11 , wherein the third section has a blade pitch that is lower than the first section and the second section.

14 . The propeller blade of claim 9 , wherein the longitudinal direction extends longitudinally between a blade root and a blade tip.

15 . The propeller blade of claim 9 , wherein the longitudinal direction extends longitudinally between a blade root and a blade tip and a blade pitch of the propeller blade decreases from the blade root to the blade tip.

16 . A propeller blade comprising:

a first material comprising fibers that extend in a longitudinal direction to form a longitudinal fiber structure;

a second material different from the first material, wherein the fibers of the first material are interspersed through the second material;

a first segment where the fibers are substantially uniformly oriented between a leading edge and a trailing edge of the propeller blade; and

a second segment where a volume fraction of the first material decreases from the leading edge to the trailing edge.

17 . The propeller blade of claim 16 , wherein the propeller blade further comprises:

multiple segments along a length of the propeller blade, wherein the multiple segments comprise the first segment and the second segment.

18 . The propeller blade of claim 17 , wherein the multiple segments along the length of the propeller blade comprise:

the first segment comprising a root of the propeller blade;

the second segment comprising a midsection of the propeller blade; and

a third segment comprising a tip of the propeller blade.

19 . The propeller blade of claim 18 , wherein a pitch of the first segment is from 35-45 degrees.

20 . The propeller blade of claim 18 , wherein a pitch of the second segment is from 20-30 degrees.