Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud

• US 7,665,959 B2
• Filed: 07/20/2005
• Issued: 02/23/2010
• Est. Priority Date: 07/20/2005
• Status: Expired due to Fees

• Current Assignee: Raytheon Technologies Corporation d/b/a RTX (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Tirone, John P. III, Giaimo, John A.
• Primary Examiner(s): VERDIER, CHRISTOPHER M
• Application Number:
  US11/185,622
• Publication Number:
  US 20070020090A1
• Time in Patent Office: 1,679 Days
• Field of Search: 415/150, 415159-166
• US Class Current: 415/160
• CPC Class Codes: F01D 17/162 for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F04D 27/0246 by varying geometry within the pumps, e.g. by adjusting vanes
• CPC Class Codes: F04D 29/563 specially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2260/4031 as in toothed gearing

Abstract

An inner diameter vane shroud of a variable vane assembly accommodates a synchronization mechanism for coordinating rotation of an array of variable vanes. The inner diameter vane shroud has a gear track that runs circumferentially through the vane shroud. An array of variable vanes is rotatably mounted in the vane shroud at an inner end. Each vane has a gear pinion at its inner end, which interfaces with the gear track. As one of the individual variable vanes is rotated by an actuation source, the other variable vanes of the variable vane array are rotated a like amount by the rack and pinion gear interface.

Claims

1. A variable vane shroud mechanism for use in a turbine engine, the vane shroud mechanism comprising:

an inner diameter vane shroud for receiving inner diameter ends of an away of variable vanes, the shroud comprising;

a plurality of radially extending vane sockets;

an internal synchronizing cavity extending circumferentially across a width of the vane shroud adjacent the plurality of sockets;

an arcuate body portion comprising a forward shroud component and an aft shroud component each comprising;

a mating surface comprising;

a plurality of partial vane sockets; and

an internal surface defining a portion of the internal synchronizing cavity;

wherein the mating surfaces of the forward and aft shroud components mate such that the plurality of partial vane sockets form the plurality of radially extending sockets, and the internal surfaces form the internal synchronizing cavity; and

a three-sided gear track extending axially from the plurality of partial vane sockets on the aft shroud component, the internal surface of the aft shroud component comprising a portion of the gear track; and

a synchronizing mechanism positioned internally within the variable vane shroud to interface with the inner diameter ends of the away of variable vanes such that rotation of individual variable vanes comprising the away of variable vanes is coordinated.

2. A variable vane assembly comprising:

an inner diameter vane shroud comprising;

an arcuate shroud body;

a plurality of sockets extending radially into an interior of the shroud body; and

a rack channel extending circumferentially through an interior of the shroud body and intersecting the plurality of sockets;

a drive vane comprising;

an inner diameter trunnion rotatably disposed in one of the plurality of sockets in the inner diameter vane shroud; and

a pinion extending axially from the trunnion that rides within the rack channel;

a plurality of follower vanes each comprising;

an inner diameter trunnion rotatably disposed in one of the plurality of sockets in the inner diameter vane shroud; and

a pinion extending axially from the trunnion that rides within the rack channel; and

an arcuate gear rack slidably located in the rack channel within the interior of the arcuate shroud body to interface with the pinions of the drive vane and the follower vanes such that when the drive vane is rotated an amount, the plurality of follower vanes are rotated a like amount by the gear rack.

3. The variable vane assembly of claim 2 wherein the inner diameter vane shroud comprises a forward vane shroud component and an aft vane shroud component.

4. The variable vane assembly of claim 3 wherein the aft shroud component includes a three-sided rack channel.

5. The variable vane assembly of claim 2 wherein the drive vane and each of the follower vanes include a button positioned radially inward from the inner diameter trunnion to secure the vanes within the interior of the inner diameter vane shroud.

6. The variable vane assembly of claim 2 wherein the interior rack channel bounds the pinions and the gear rack to prevent radial and axial disengagement of the pinions from the gear rack.