Turbine with yaw brake mechanism having a rotor lock and a corresponding receptacle

Patent metadata

Field	Value
Publication number	US-2016245258-A1
Application number	US-201514629653-A
Country	US
Kind code	A1
Filing date	Feb 24, 2015
Priority date	Feb 24, 2015
Publication date	Aug 25, 2016
Grant date	—

Abstract

A yaw brake mechanism is described for maintaining a yawing structure, such as a nacelle of a fluid turbine, at a desired orientation or azimuthal heading about a reference or yaw axis. The yaw brake mechanism uses one or more rotor locks and one or more receptacles that cooperate with one another to achieve the locking function. One of the rotor locks is actuatable so that a portion thereof can be engaged in one of the receptacles to lock the yawing structure. The number of rotor locks and receptacles can be selected to allow the yawing structure to achieve any azimuth heading around the full 360 degrees of the yaw axis with various degrees of accuracy. The yaw brake mechanism allows the yawing structure to maintain multiple headings while being subjected to extreme moment and force loads in a low mass, low height, low cost solution.

First claim

1 . A yaw brake mechanism of a yawing structure that is rotatably mounted on a non-rotatable structure and that is rotatable about a yaw axis of the non-rotatable structure, comprising:
at least one rotor lock that is actuatable between an engaged condition and a disengaged condition; a lock plate that cooperates with the at least one rotor lock for fixing the yawing structure in a desired orientation about the yaw axis; the lock plate includes at least one receptacle that can receive a portion of the at least one rotor lock therein when the at least one rotor lock is actuated to the engaged condition; and the lock plate and the at least one rotor lock are positioned relative to each other whereby the portion of the at least one rotor lock is disposed within the at least one receptacle of the lock plate when the at least one rotor lock is actuated to the engaged condition thereby preventing rotation of the yawing structure about the yaw axis and the portion of the at least one rotor lock is removed from the at least one receptacle of the lock plate when the at least one rotor lock is actuated to the disengaged condition thereby permitting rotation of the yawing structure about the yaw axis.

2 . The yaw brake mechanism of claim 1 , comprising a plurality of the rotor locks and a plurality of the receptacles.

3 . The yaw brake mechanism of claim 1 , wherein the at least one rotor lock is mounted to one of the yawing structure or the non-rotatable structure, and the lock plate is mounted to the other of the yawing structure or the non-rotatable structure.

4 . The yaw brake mechanism of claim 2 , wherein the lock plate has a central axis that is substantially parallel to the yaw axis, and the receptacles are formed at circumferentially spaced locations around the central axis of the lock plate.

5 . The yaw brake mechanism of claim 4 , wherein the receptacles are disposed around the entire circumference of the lock plate.

6 . The yaw brake mechanism of claim 2 , wherein the number of the receptacles is greater than the number of the rotor locks.

7 . The yaw brake mechanism of claim 4 , wherein the lock plate includes an inner perimeter that is formed with gear teeth, and the lock plate forms an inner race of a slew bearing.

8 . The yaw brake mechanism of claim 2 , wherein the rotor locks and the receptacles permit the yawing structure to achieve any yawing angle between 0 to 360 degrees in multiples of a predetermined amount of degrees.

9 . A fluid turbine, comprising:
a tower having a yaw axis; a nacelle rotatably mounted on the tower and rotatable about the yaw axis to change an orientation of the nacelle about the yaw axis; a rotor rotatably mounted on the nacelle for rotation about a rotation axis; a yaw drive mechanism connected to the nacelle for rotating the nacelle about the yaw axis; a yaw brake mechanism for fixing the orientation of the nacelle about the yaw axis, the yaw brake mechanism including:
at least one rotor lock mounted to either the nacelle or the tower that is actuatable between an engaged condition and a disengaged condition;
a lock plate that cooperates with the at least one rotor lock for fixing the nacelle in a desired orientation about the yaw axis, the lock plate is mounted to either the tower or the nacelle;
the lock plate includes at least one receptacle that can receive a portion of the at least one rotor lock therein when the at least one rotor lock is actuated to the engaged condition; and
the lock plate and the at least one rotor lock are positioned relative to each other whereby the portion of the at least one rotor lock is disposed within the at least one receptacle of the lock plate when the at least one rotor lock is actuated to the engaged condition thereby preventing rotation of the nacelle about the yaw axis and the portion of the at least one rotor lock is removed from the at least one receptacle of the lock plate when the at least one rotor lock is actuated to the disengaged condition thereby permitting rotation of the nacelle about the yaw axis.

10 . The fluid turbine of claim 9 , comprising a plurality of the rotor locks and a plurality of the receptacles.

11 . The fluid turbine of claim 10 , wherein the lock plate has a central axis that is substantially parallel to the yaw axis, and the receptacles are formed at circumferentially spaced locations around the central axis of the lock plate.

12 . The fluid turbine of claim 11 , wherein the receptacles are disposed around the entire circumference of the lock plate.

13 . The fluid turbine of claim 10 , comprising more than two of the rotor locks and more than two of the receptacles.

14 . The fluid turbine of claim 10 , wherein the number of the receptacles is greater than the number of the rotor locks.

15 . The fluid turbine of claim 9 , wherein the lock plate includes an inner perimeter that is formed with gear teeth, and the lock plate forms an inner race of a slew bearing.

16 . The fluid turbine of claim 10 , wherein the rotor locks and the receptacles permit the nacelle to achieve any yawing angle between 0 to 360 degrees in multiples of a predetermined amount of degrees.

17 . The fluid turbine of claim 9 , wherein the fluid turbine comprises a tidal turbine, a water turbine or a wind turbine.

Assignees

• Lockheed Corp

Inventors

• Firkser Stephen
• Mcguigan Thomas E

Classifications

• F03D80/70

  Bearing or lubricating arrangements · CPC title

• F03D7/0212 Primary

  the rotating axis remaining horizontal · CPC title

• F16D63/006 Primary

  Positive locking brakes · CPC title

• F05B2270/329

  Azimuth or yaw angle · CPC title

• F03D7/0248 Primary

  by mechanical means acting on the power train · CPC title