IP Library Granted Patent US 12,297,747
Granted Patent B1
US 12,297,747 · App. 18/406,289 · Granted May 13, 2025

Inlet protector for vane coupling hole

Inventors: Michael G. McCaffrey (Windsor, CT); Paul M. Lutjen (Kennebunkport, ME); Mark F. Zelesky (Bolton, CT)
Assignee: RTX Corporation
F01D5/187F01D9/065F01D11/005F01D25/12F05D2260/607
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Quick Facts
Patent No.
US 12,297,747
App. No.
18/406,289
Granted
May 13, 2025
Kind
B1
Abstract

An inlet protector for a vane cooling air passage inlet including a vane including a vane cooling air inlet; an inlet protector fluidly coupled to the vane cooling air inlet, the inlet protector comprising a protector body having a discharge portion and a suction portion, an interior flow passage fluidly coupling the suction portion with the discharge portion; the discharge portion fluidly coupled with the vane cooling air inlet; and a suction inlet formed in the suction portion, wherein the suction inlet is located distally from the vane cooling air inlet.

Claims (39)

1. An inlet protector for a vane cooling air passage inlet comprising:

a vane comprising a vane cooling air inlet;

an inlet protector fluidly coupled to the vane cooling air inlet, the inlet protector comprising a protector body having a discharge portion and a suction portion, an interior flow passage fluidly coupling the suction portion with the discharge portion;

the discharge portion fluidly coupled with the vane cooling air inlet; and

a suction inlet formed in the suction portion, wherein the suction inlet is located distally from the vane cooling air inlet;

a seal proximate the vane cooling air inlet;

an anti-rotation lug proximate the vane cooling air inlet; wherein the suction inlet of the inlet protector extends radially outboard the seal and radially outboard the anti-rotation lug in the internal cavity.

2. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the interior flow passage fluidly communicates the suction inlet to a discharge exit formed in the discharge portion, the discharge exit being fluidly coupled with the vane cooling air inlet.

3. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the suction inlet comprises a bell-mouth shape.

4. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the suction inlet comprises a cross-sectional area 20 percent larger than the vane cooling air inlet.

5. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the discharge exit comprises a cross sectional area equal to the vane cooling air inlet.

6. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the inlet protector attaches to the vane along a vane face proximate the vane cooling air inlet.

7. The inlet protector for a vane cooling air passage inlet according to claim 1 , wherein the vane cooling air inlet comprises a second vane feed hole.

8. An inlet protector for a vane cooling air passage inlet comprising:

a gas turbine engine internal cavity;

a vane proximate the internal cavity, the vane comprising a vane cooling air inlet;

an anti-rotation lug proximate the vane cooling air inlet;

a seal proximate the vane cooling air inlet;

an inlet protector fluidly coupled to the vane cooling air inlet, the inlet protector comprising a protector body having a discharge portion and a suction portion, an interior flow passage fluidly coupling the suction portion with the discharge portion, the discharge portion fluidly coupled with the vane cooling air inlet; and

a suction inlet formed in the suction portion, wherein the suction inlet is located within the internal cavity distally from the vane cooling air inlet; wherein the suction inlet of the inlet protector extends radially outboard the seal and radially outboard the anti-rotation lug in the internal cavity.

9. The inlet protector for a vane cooling air passage inlet according to claim 8 , further comprising:

a vane-lug gap formed in the internal cavity between the anti-rotation lug and the vane cooling air inlet.

10. The inlet protector for a vane cooling air passage inlet according to claim 8 , wherein the suction inlet comprises a bell-mouth shape formed from the suction inlet into the interior flow passage, the bell-mouth shape comprising a relatively larger cross-sectional area that gradually reduces along the interior flow passage to form a relatively low flow velocity region.

11. The inlet protector for a vane cooling air passage inlet according to claim 8 , wherein the inlet protector attaches to the vane along a vane face proximate the vane cooling air inlet.

12. The inlet protector for a vane cooling air passage inlet according to claim 8 , wherein the interior flow passage fluidly communicates the suction inlet to a discharge exit formed in the discharge portion, the discharge exit being fluidly coupled with the vane cooling air inlet.

13. A process for preventing debris with an inlet protector for a vane cooling air passage inlet comprising:

a vane comprising a vane cooling air inlet;

fluidly coupling an inlet protector to the vane cooling air inlet, the inlet protector comprising a protector body having a discharge portion and a suction portion, an interior flow passage fluidly coupling the suction portion with the discharge portion; and

fluidly coupling the discharge portion with the vane cooling air inlet;

forming a suction inlet in the suction portion, wherein the suction inlet is located distally from the vane cooling air inlet;

fluidly communicating the interior flow passage between the suction inlet and a discharge exit formed in the discharge portion;

fluidly coupling the discharge exit with the vane cooling air inlet;

forming a bell-mouth shape from the suction inlet into the interior flow passage, the bell-mouth shape comprising a relatively larger cross-sectional area that gradually reduces along the interior flow passage;

forming a relatively low flow velocity region proximate the suction inlet; and

extending the suction inlet of the inlet protector radially outboard a seal and radially outboard an anti-rotation lug in an internal cavity proximate the vane.

14. The process of claim 13 , further comprising:

attaching the inlet protector to the vane along a vane face proximate the vane cooling air inlet.

15. The process of claim 14 , further comprising:

forming the suction inlet with a cross-sectional area 20 percent larger than the vane cooling air inlet.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 8, 2024
From: MCCAFFREY, MICHAEL G.; LUTJEN, PAUL M.; ZELESKY, MARK F.
To: RTX CORPORATION
Reel/Frame 066045/0715 →
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