Precision blade pitch adjustment

1. A blade pitch adjustment mechanism for fixing a rotor blade to a rotor hub, the blade pitch adjustment mechanism comprising:

a pitch cylinder having a first face and pitch slots extending longitudinally from the first face, and a pitch plate circumscribing the first face, wherein the first face is recessed inboard from the pitch plate;

a blade sleeve having a second face and a blade slot extending longitudinally from the second face, the blade sleeve configured to be rotationally positioned in the pitch cylinder with the second face located with the first face; and

the blade slot is cooperative with each pitch slot of the pitch slots to form keyways, whereby a keyway of the keyways is opened at the each pitch slot when the blade slot is circumferentially aligned with the each pitch slot.

2. The blade pitch adjustment mechanism of claim 1 , wherein the blade slot comprises blade slots.

3. The blade pitch adjustment mechanism of claim 1 , wherein the keyways are circumferentially located at increments of about 1 degree.

4. The blade pitch adjustment mechanism of claim 1 , wherein the keyways are circumferentially located at increments of about 0.08 and 1.2 degrees.

5. The blade pitch adjustment mechanism of claim 1 , wherein the keyways are circumferentially located at increments of greater than about 1.2 degrees.

6. The blade pitch adjustment mechanism of claim 1 , further comprising a key configured to mate with the keyway.

7. A rotor blade assembly, comprising:

a hub having a rotational axis and an outboard wall parallel to the rotational axis;

a pitch cylinder fixed to the hub and extending inboard with a first face exposed at the outboard wall, and a pitch plate positioned at the outboard wall and circumscribing the first face, wherein the first face is recessed inboard from the pitch plate;

pitch slots spaced circumferentially and extending inboard from the first face;

a blade sleeve fixed to a blade and positioned in the pitch cylinder with a second face located at the outboard wall;

a blade slot extending inboard from the second face, wherein the blade slot is cooperative with each pitch slot of the pitch slots to form keyways, wherein each keyway of the keyways is formed at the each pitch slot when the blade slot is circumferentially aligned with the each pitch slot; and

a key configured to be disposed in the keyway thereby fixing the blade sleeve to the pitch cylinder.

8. The rotor blade assembly of claim 7 , wherein the blade slot comprises blade slots.

9. The rotor blade assembly of claim 7 , wherein the keyway corresponds to a determined blade pitch; and

the keyways are circumferentially located at increments of about 0.5 to 1.5 degrees.

10. The rotor blade assembly of claim 9 , wherein the increments are about 1.0 degrees.

11. The rotor blade assembly of claim 7 , further comprising a stop connected to the pitch cylinder proximate the first face, the stop holding the key in the keyway.

12. A method, comprising:

adjusting a blade pitch in a rotor blade assembly comprising a hub having a rotational axis and an outboard wall parallel to the rotational axis, a pitch cylinder fixed to the hub and extending inboard from a first face, pitch slots spaced circumferentially and extending inboard from the first face, a pitch plate positioned at the outboard wall and circumscribing the first face, wherein the first face is recessed inboard from the pitch plate, a blade sleeve fixed to a blade and positioned in the pitch cylinder with a second face located with the first face, a blade slot extending inboard from the second face;

rotating the blade sleeve until the blade slot is aligned with a first pitch slot of the pitch slots forming a first keyway corresponding to a first blade pitch; and

fixing the blade at the first blade pitch by positioning a key in the first keyway.

13. The method of claim 12 , further comprising testing the rotor blade assembly by rotating the rotor blade assembly with the first blade pitch.

14. The method of claim 12 , wherein the rotor blade assembly comprises six or more blades.

15. The method of claim 12 , further comprising:

testing the rotor blade assembly by rotating the rotor blade assembly with the first blade pitch;

removing the key from the first keyway;

rotating the blade sleeve until the blade slot is aligned with a second pitch slot of the pitch slots thereby forming a second keyway corresponding to a second blade pitch;

fixing the blade at the second blade pitch by positioning a key in the second keyway; and

testing the rotor blade assembly by rotating the rotor blade assembly with the second blade pitch.

16. The method of claim 15 , wherein the rotor blade assembly comprises six or more blades.