Rotorcraft flapping lock

Patent metadata

Field	Value
Publication number	US-9327831-B2
Application number	US-201313949766-A
Country	US
Kind code	B2
Filing date	Jul 24, 2013
Priority date	May 22, 2013
Publication date	May 3, 2016
Grant date	May 3, 2016

Abstract

According to one embodiment, a flapping lock for a rotor system includes a downstop, a flapping stop, and an actuator. The downstop is in mechanical communication with a shaft. The flapping stop is in mechanical communication with a rotor hub. The actuator is operable to move the downstop towards the flapping stop.

First claim

What is claimed is:

1. A rotorcraft, comprising:
a body;
a wing coupled to the body;
a power train coupled to at least one of the body or the wing and comprising a power source and a shaft in mechanical communication with the power source;
a tiltrotor assembly pivotally coupled to the wing and
in mechanical communication with the shaft, the tiltrotor assembly comprising:
a hub in mechanical communication with the shaft;
a rotor blade in mechanical communication with the hub;
a flapping lock deployable in a locked position in an unlocked position, the flapping lock operable in the locked position to prevent at least some flapping movement of the hub relative to the shaft, the flapping lock operable in the unlocked position to allow the at least some flapping movement of the hub relative to the shaft; and
the flapping lock comprising an actuator, a downstop in mechanical communication with the shaft, and a flapping stop in mechanical communication with the hub.

2. The rotorcraft of claim 1 , the actuator operable to deploy the flapping lock in the locked position by moving the downstop towards the flapping stop.

3. The rotorcraft of claim 1 , the flapping lock further comprising a load absorber positioned between the downstop and the flapping stop.

4. The rotorcraft of claim 3 , wherein the load absorber is comprised of an elastomeric material.

5. The rotorcraft of claim 3 , wherein the load absorber is coupled to the downstop.

6. The rotorcraft of claim 5 , the flapping lock further comprising a second load absorber coupled to the flapping stop.

7. The rotorcraft of claim 1 , wherein the flapping lock in the locked position substantially maintains the hub perpendicular to the shaft.

8. The rotorcraft of claim 1 , wherein the flapping lock in the unlocked position allows the shaft to move conically relative to a pivot point and the hub to move spherically about a spherical element.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Schank Troy
• Stamps Frank B

Classifications

• B64C27/605

  including swash plate, spider or cam mechanisms · CPC title

• B64C27/32

  Rotors · CPC title

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• B64C11/28

  Collapsible or foldable blades · CPC title

• B64C27/41

  with flapping hinge or universal joint, common to the blades · CPC title