Fold-lock and pitch-lock systems

Patent metadata

Field	Value
Publication number	US-12534186-B2
Application number	US-202318472897-A
Country	US
Kind code	B2
Filing date	Sep 22, 2023
Priority date	Sep 22, 2023
Publication date	Jan 27, 2026
Grant date	Jan 27, 2026

Abstract

A rotor-blade assembly has a lock system to enable and disable a folding degree of freedom and a pitching degree of freedom of a rotor blade. A grip couples a blade to a hub, the blade being pivotable about a fold axis relative to the grip, the blade and grip being pivotable together about a pitch axis relative to the hub. A fold lock prevents folding of the blade in a fold-lock position and allows folding of the rotor blade in a pitch-lock position, and a pitch lock allows pitch movement of the rotor blade in a fold-lock position and prevents pitch movement of the rotor blade in the pitch-lock position. A rotary actuator carried by the grip has actuator arms coupled through linkage to the pitch lock and fold lock, and the actuator is configured for moving the pitch lock and fold lock between the fold-lock and pitch-lock positions.

First claim

What is claimed is:

1 . A rotor-blade assembly having a lock system to enable and disable a folding degree of freedom and a pitching degree of freedom of a rotor blade, the system comprising:
a blade grip coupled to a hub, the blade grip being rotatable relative to the hub about a pitch axis; a rotor blade coupled to the blade grip, the blade being pivotable about a fold axis relative to the grip, the blade and grip being pivotable together about the pitch axis; a fold lock that prevents folding of the blade in a fold-lock position and allows folding of the blade in a pitch-lock position; a pitch lock that allows pitch movement of the rotor blade in the fold-lock position and prevents pitch movement of the rotor blade in the pitch-lock position; and a rotary actuator carried by the grip and having an actuator arm; a linkage comprising a first link and a second link, each link having opposing ends, the first link pivotably connected at one end to the actuator arm and pivotably connected at its opposing end to the fold lock, and the second link pivotably connected at one end to the pitch lock and pivotably connected at its opposing end to the actuator arm; wherein the actuator is configured for moving the pitch lock and the fold lock between the fold-lock and pitch-lock positions.

2 . The rotor-blade assembly of claim 1 , wherein the actuator is carried in a bolt coupling the blade to the hub.

3 . The rotor-blade assembly of claim 1 , wherein the actuator is carried on a leading portion of the grip.

4 . The rotor-blade assembly of claim 1 , wherein the actuator is carried on a trailing portion of the grip.

5 . The rotor-blade assembly of claim 1 , wherein the linkage provides passive, overcenter locking in the pitch-lock position.

6 . The rotor-blade assembly of claim 1 , wherein the linkage provides passive, overcenter locking in the fold-lock position.

7 . The rotor-blade assembly of claim 1 , further comprising:
a blade-fold link coupled to the rotor blade, wherein the fold lock enables and disables the folding degree of freedom by unlocking and locking the blade-fold link.

8 . The rotor-blade assembly of claim 1 , further comprising:
a blade-stop tab; wherein the pitch lock enables and disables the pitching degree of freedom by engaging and disengaging the blade-stop tab.

9 . A rotor-blade assembly having a lock system to enable and disable a folding degree of freedom and a pitching degree of freedom of a rotor blade, the system comprising:
a blade grip coupled to a hub, the blade grip being rotatable relative to the hub about a pitch axis; a rotor blade coupled to the blade grip, the blade being pivotable about a fold axis relative to the grip, the blade and grip being pivotable together about the pitch axis; a fold lock that prevents folding of the blade in a fold-lock position and allows folding of the rotor blade in a pitch-lock position; a pitch lock that allows pitch movement of the rotor blade in the fold-lock position and prevents pitch movement of the rotor blade in the pitch-lock position; and a rotary actuator carried in a bolt coupling the blade to the hub and having an actuator arm; a linkage comprising a first link and a second link, each link having opposing ends, the first link pivotably connected at one end to the actuator arm and pivotably connected at its opposing end to the fold lock, and the second link pivotably connected at one end to the pitch lock and pivotably connected at its opposing end to the actuator arm; wherein the actuator is configured for moving the pitch lock and the fold lock between the fold-lock and pitch-lock positions.

10 . The rotor-blade assembly of claim 9 , wherein the linkage provides passive, overcenter locking in the pitch-lock position.

11 . The rotor-blade assembly of claim 9 , wherein the linkage provides passive, overcenter locking in the fold-lock position.

12 . The rotor-blade assembly of claim 9 , further comprising:
a blade-fold link coupled to the rotor blade, wherein the fold lock enables and disables the folding degree of freedom by unlocking and locking the blade-fold link.

13 . The rotor-blade assembly of claim 9 , further comprising:
a blade-stop tab; wherein the pitch lock enables and disables the pitching degree of freedom by engaging and disengaging the blade-stop tab.

14 . The rotor-blade assembly of claim 9 , further comprising:
a second actuator carried on a leading portion of the grip and coupled to at least one actuator arm, the second actuator being configured for moving the pitch lock and the fold lock between the fold-lock and pitch-lock positions.

15 . The rotor-blade assembly of claim 9 , further comprising:
a second actuator carried on a trailing portion of the grip and coupled to at least one actuator arm, the second actuator being configured for moving the pitch lock and the fold lock between the fold-lock and pitch-lock positions.

16 . A rotor assembly having a lock system to enable and disable a pitching degree of freedom of a rotor blade, the system comprising:
a rotor mast rotatable about a mast axis; a rotor blade coupled to the mast for rotation therewith about the mast axis, the blade also being rotatable relative to the mast about a pitch axis; a pitch lock that allows pitch movement of the rotor blade in an unlock position and prevents pitch movement of the rotor blade in a lock position; a ring carried by the mast and rotatable relative to the mast about the mast axis, a lock linkage coupling the ring to the pitch lock; an actuator configured for rotating the ring about the mast axis; wherein operation of the actuator rotates the ring about the mast axis for moving the pitch lock between the lock and unlock positions.

17 . The rotor assembly of claim 16 , wherein the lock linkage provides passive, overcenter locking in the lock position.

18 . The rotor assembly of claim 16 , wherein a ring linkage couples the actuator to the ring.

19 . The rotor assembly of claim 18 , wherein the ring linkage provides passive, overcenter locking in the unlock position.

20 . The rotor assembly of claim 16 , wherein the ring comprises gear teeth and the actuator comprises a gear engaged with the teeth.

Assignees

• Textron Innovations Inc

Inventors

• Cravener Kyle
• Harloff Andrew
• Halcom Lancer Drake
• Maresh Andrew

Classifications

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• B64C11/28 Primary

  Collapsible or foldable blades · CPC title

• B64C27/50

  Blades foldable to facilitate stowage of aircraft · CPC title