Lightweight cast inner diameter vane shroud for variable stator vanes

• US 7,753,647 B2
• Filed: 07/20/2005
• Issued: 07/13/2010
• 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:
  US11/185,956
• Publication Number:
  US 20070020093A1
• Time in Patent Office: 1,819 Days
• Field of Search: 415/149.4, 415/150, 415159-166, 415189-190, 415/209.2, 415/209.3, 415/209.4, 415/210.1
• 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: F01D 9/042 fixing blades to stators fixing stator-rings in the casing or to each other F01D25/246
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An inner diameter vane shroud for use in a gas turbine engine is comprised of lightweight cast forward and aft shroud components. The forward and aft shroud components are made with an investment casting technique that creates a hollow cavity that runs in a circumferential direction through each component. The forward and aft shroud components are matable to form sockets that receive inner diameter ends of variable stator vanes.

Claims

1. A stator vane section for use in a turbine engine, the stator vane section comprising:

an outer diameter fan case;

a plurality of stator vanes each comprising;

an inner diameter end; and

an outer diameter end for rotating in the outer diameter fan case;

an inner diameter vane shroud comprising;

a forward inner diameter shroud component comprising;

a forward hollow channel running circumferentially through an interior of the forward shroud component;

a forward fastener hole extending through the forward inner diameter vane shroud component to intersect the forward hollow channel; and

a plurality of forward recesses; and

an aft shroud component comprising;

an aft hollow channel running circumferentially through an interior of the aft shroud component;

an aft fastener hole extending into and terminating within the aft shroud component so as to align with the forward fastener hole and not intersect the aft hollow channel; and

a plurality of aft recesses that mate with the forward recesses to receive the inner diameter ends of stator vanes.

2. The stator vane section of claim 1 wherein the aft fastener hole of the aft shroud component includes a locking insert for securing a threaded fastener within the aft fastener hole of the aft shroud component.

3. The stator vane section of claim 1 wherein the forward shroud component comprises an opening to allow access to the forward hollow channel, the opening including a removable cap for sealing the opening.

4. The stator vane section of claim 1 and further comprising an interior cavity positioned between the forward inner diameter shroud component and the aft shroud component and flanked by forward and aft recesses.

5. The stator vane section of claim 1 wherein the forward inner diameter shroud component and the aft shroud component are produced by investment casting.

6. A vane shroud segment comprising:

an arcuate body portion;

a mating surface comprising;

partial sockets for receiving inner diameter ends of stator vanes; and

a weight-reducing depression positioned adjacent each of the partial sockets;

an internal hollow channel extending through an interior of the arcuate body portion and across the length of the arcuate body portion alongside the partial sockets and weight reducing depressions; and

a fastener hole extending into the mating surface radially inward of the partial sockets and weight-reducing depressions so as to not intersect the internal hollow channel.

7. The vane shroud segment of claim 6 wherein the fastener hole includes a locking insert for securing a threaded fastener within the fastener hole.

8. The vane shroud segment of claim 6 wherein the arcuate body portion comprises an opening to allow access to the internal hollow channel, the opening including a removable cap for sealing the opening.

9. The vane shroud segment of claim 6 wherein the arcuate body portion comprises a plurality of holes for receiving threaded fasteners.

10. The vane shroud segment of claim 6 wherein the internal hollow channel is produced by an investment casting process.

11. An inner diameter vane shroud having a forward shroud component and an aft shroud component that mate to form sockets for receiving inner diameter ends of variable stator vanes, the inner diameter vane shroud characterized by:

a forward hollow channel running through an interior of the forward shroud component;

a forward fastener hole extending through the forward shroud component to intersect the forward hollow channel;

an aft hollow channel running through an interior of the aft shroud component; and

an aft fastener hole extending into and terminating within the aft shroud component so as to not intersect the aft hollow channel;

wherein the hollow channels are produced by an investment casting process; and

wherein the sockets are disposed between the forward and aft hollow channels so as to not intersect the channels.

12. The vane shroud of claim 11 wherein the holes of the aft shroud component include locking inserts for securing the threaded fasteners within the holes of the aft shroud component.

13. The vane shroud of claim 11 wherein the forward shroud component comprises an opening to allow access to the forward hollow channel.

14. The vane shroud of claim 13 wherein the forward shroud component includes a removable cap for sealing the opening.

15. The inner diameter vane shroud of claim 11 wherein the inner diameter vane shroud is further characterized by a plurality of weight-reducing depressions positioned along mating surfaces of the forward shroud component and the aft shroud component.