Folding spindle and bearing assembly in a folding rotor blade assembly
A folding rotor blade assembly for a tiltrotor aircraft comprising a rotor blade pivotally connected to a grip with dual concentric blade bolts having a common central axis providing a pivotal axis inboard of an outboard bearing. A folding spindle connects the outboard bearing to an outboard tip of a yoke. The outboard bearing and the spindle fold with the rotor blade relative to the yoke. In use, the compact folded arrangement of the rotor blades reduces folded aircraft dimensions in response to ever increasing restricted storage space parameters.
1. A folding rotor blade assembly for a tiltrotor aircraft, comprising:
a drive mast connected to a yoke;
an inboard beam housing an inboard bearing, the inboard bearing connected to the yoke;
an outboard beam housing an outboard bearing, the outboard bearing connected to the yoke outboard of the inboard bearing;
a grip connected to the inboard beam;
a rotor blade connected to the grip at a pivotal connection positioned inboard of the outboard bearing, the rotor blade comprising a first blade tang and a second blade tang connected to the grip at the pivotal connection; and
the outboard beam connected to the rotor blade between the first blade tang and the second blade tang.
2. The folding rotor blade assembly of claim 1 , further comprising a pair of axially aligned blade bolts at the pivotal connection providing a pivot axis of the rotor blade relative to the grip.
3. The folding rotor blade assembly of claim 1 , wherein the outboard beam is connected to the rotor blade at the pivotal connection.
4. The folding rotor blade assembly of claim 3 , further comprising:
a folding spindle connected to the outboard bearing and connected to the yoke at a second pivotal connection; and
a pivot axis of the pivotal connection is collinear with a second pivot axis of the second pivotal connection.
5. The folding rotor blade assembly of claim 1 , further comprising:
a pair of axially aligned blade bolts at the pivotal connection providing a pivot axis of the rotor blade relative to the grip;
a folding spindle connected to the outboard bearing and connected to the yoke at a second pivotal connection providing a second pivot axis of the folding spindle relative to the yoke; and
the pivot axis is collinear with the second pivot axis.
6. The folding rotor blade assembly of claim 1 , further comprising:
a folding spindle connected to the outboard bearing and connected to the yoke at a second pivotal connection; and
a pivot axis of the pivotal connection is collinear with a second pivot axis of the second pivotal connection.
7. The folding rotor blade assembly of claim 1 , wherein the outboard bearing further comprises an outboard shear bearing and an outboard centrifugal force (“CF”) bearing.
8. The folding rotor blade assembly of claim 1 , wherein the inboard bearing further comprises an inboard shear bearing.
9. The folding rotor blade assembly of claim 1 , further comprising;
a folding spindle connected to the outboard bearing and connected to the yoke at a second pivotal connection; and
a lock connected to the folding spindle and releasably engaged with the yoke.
10. A folding rotor blade assembly, comprising:
a yoke including a yoke arm extending radially from a central aperture;
a clamp plate connected to the yoke proximate the central aperture;
an inboard bearing connected to the clamp plate and connected to an inboard beam;
a grip connected to the inboard beam;
a folding spindle connected to the yoke arm at a first pivotal connection;
an outboard bearing connected to the folding spindle and an outboard beam;
a rotor blade comprising a first blade tang and a second blade tang connected to the grip at a second pivotal connection and the outboard beam connected to the rotor blade between the first blade tang and the second blade tang; and
the first pivotal connection and the second pivotal connection positioned inboard of the outboard bearing.
11. The folding rotor blade assembly of claim 10 , further comprising:
a first pivot axis at the first pivotal connection;
a pair of axially aligned blade bolts at the second pivotal connection providing a second pivot axis; and
the first pivot axis is collinear with the second pivot axis.
12. The folding rotor blade assembly of claim 10 , further comprising a lock connected to the folding spindle and releasably engaged with the yoke arm.
13. A method comprising:
pitching a rotor blade of a rotor blade assembly comprising an inboard bearing connected to a yoke and a grip, an outboard bearing connected to the yoke at a first pivotal connection providing a first pivot axis, and a rotor blade connected to the grip at a second pivotal connection providing a second pivot axis inboard of the outboard bearing, the rotor blade having a first blade tang and a second blade tang connected to the grip at the second pivotal connection and the rotor blade connected to an outboard beam between the first blade tang and the second blade tang; and
rotating the rotor blade together with the outboard bearing around the first pivot axis and the second pivot axis.
14. The method of claim 13 , wherein pitching the rotor blade includes axially aligning the first pivot axis with the second pivot axis.
15. The method of claim 14 wherein the first pivot axis and the second pivot axis are both inboard of the outboard bearing.
16. The method of claim 13 , wherein the outboard bearing further comprises an outboard shear bearing and an outboard centrifugal force (“CF”) bearing.
17. The method of claim 13 , further comprising a pair of axially aligned blade bolts at the second pivotal connection.