IP Library Granted Patent US 11,156,112
Granted Patent B2
US 11,156,112 · App. 16/178,677 · Granted Oct 26, 2021

Method and apparatus for mounting a transition duct in a gas turbine engine

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Quick Facts
Patent No.
US 11,156,112
App. No.
16/178,677
Granted
Oct 26, 2021
Kind
B2
Abstract

An apparatus and method for reducing the vibrations to a transition duct and improving the assembly and fit-up of a transition duct relative to a combustion system are disclosed. A damping member is provided between the transition duct and its mounting points to the gas turbine engine. The damping member comprises one or more layers of a composite material positioned between layers of sheet metal. An adjustable mounting system is also provided for the transition duct to allow for movement of a transition duct relative to the combustion liner.

Claims (28)

1. An adjustable mounting system for a transition duct comprising:

a support plate secured to an inlet ring of a transition duct, the support plate comprising a slot and a plurality of clearance holes;

an H-block plate positioned adjacent a forward face of the support plate and having a plurality of first holes and a leg portion extending through the slot in the support plate;

one or more backing plates positioned adjacent an aft face of the support plate, the one or more backing plates each having a second hole; and,

a plurality of fasteners coupling the H-block plate, support plate, and backing plate together, wherein each of the plurality of fasteners couples the H-block, support plate, and backing plate together by passing through each of one of the plurality of clearance holes, one of the plurality of first holes, and the second hole of one of the one or more of the backing plates.

2. The mounting system of claim 1 , wherein the slot of the support plate is U-shaped.

3. The mounting system of claim 1 , wherein the clearance holes of the support plate are non-circular.

4. The mounting system of claim 1 , wherein the plurality of clearance holes in the support plate have a diameter greater than a diameter of the plurality of first holes or the second holes.

5. The mounting system of claim 1 , wherein a position of the transition duct is adjustable in a plane parallel to the support plate.

6. The mounting system of claim 1 , wherein the support plate is welded to the inlet ring of the transition duct.

7. The mounting system of claim 1 , wherein each of the second holes is threaded for coupling to the plurality of fasteners.

8. The mounting system of claim 1 , wherein the one or more backing plates are positioned on opposing sides of the leg portion of the H-block plate.

9. The mounting system of claim 1 further comprising a means for retaining the plurality of fasteners in the adjustable mounting system.

10. An adjustable mounting system for a transition duct comprising:

a support plate having a slot, the support plate secured to an inlet ring of a transition duct;

an H-block plate positioned adjacent a forward face of the support plate and having a plurality of first holes and a leg portion extending through the slot in the support plate;

one or more backing plates positioned adjacent an aft face of the support plate, the one or more backing plates each having a second hole; and

a plurality of fasteners, each of the plurality of fasteners coupling each of the H-block plate, support plate, and one of the one or more backing plates together.

11. The adjustable mounting system of claim 10 , wherein the slot of the support plate is U-shaped.

12. The adjustable mounting system of claim 10 , further comprising a plurality of clearance holes in the support plate.

13. The adjustable mounting system of claim 12 , wherein the plurality of clearance holes of the support plate is non-circular.

14. The adjustable mounting system of claim 13 , wherein the plurality of clearance holes in the support plate have a diameter greater than a diameter of the plurality of first holes or the second holes.

15. The adjustable mounting system of claim 14 , wherein a position of the transition duct is adjustable in a plane parallel to the support plate.

16. The adjustable mounting system of claim 10 , wherein a position of the transition duct is adjustable in a plane parallel to the support plate.

17. The adjustable mounting system of claim 10 , wherein the support plate is welded to the inlet ring of the transition duct.

18. The adjustable mounting system of claim 10 , wherein each of the second holes is threaded for coupling to the plurality of fasteners.

19. The adjustable mounting system of claim 10 , wherein one or more backing plates are positioned on opposing side of the leg portion of the H-block plate.

20. The adjustable mounting system of claim 19 , further comprising a means for retaining the plurality of fasteners in the adjustable mounting system.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded Mar 27, 2024
From: HPS INVESTMENT PARTNERS, LLC
To: CHROMALLOY GAS TURBINE LLC
Reel/Frame 066923/0229 →
SECURITY INTEREST Recorded Mar 27, 2024
From: CHROMALLOY GAS TURBINE LLC
To: ROYAL BANK OF CANADA
Reel/Frame 066926/0565 →
SECURITY INTEREST Recorded Nov 23, 2022
From: CHROMALLOY GAS TURBINE LLC
To: HPS INVESTMENT PARTNERS, LLC
Reel/Frame 061869/0287 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 10, 2020
From: FOLKERS, DANIEL L.; ELLIS, CHARLES A.; RIVERO, PEDRO E.
To: CHROMALLOY GAS TURBINE LLC
Reel/Frame 053734/0775 →