Combustor assembly for a turbine engine
US-2017059160-A1 · Mar 2, 2017 · US
US11149646B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11149646-B2 |
| Application number | US-201514842954-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 2, 2015 |
| Priority date | Sep 2, 2015 |
| Publication date | Oct 19, 2021 |
| Grant date | Oct 19, 2021 |
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A gas turbine engine is provided having a combustion section with a liner extending between a forward end and an aft end. A structural member is positioned in or around at least a portion of the combustion section. Additionally, a piston ring holder is provided attached to the structural member at a first end and positioned proximate to the aft end of the liner at a second end. The piston ring holder is a bimetallic member including a first portion formed of a first material and a second portion formed of a second material. A coefficient of thermal expansion of the first material is different than a coefficient of thermal expansion of the second material.
Opening claim text (preview).
What is claimed is: 1. A piston ring assembly for a gas turbine engine including a structural member positioned in or around at least a portion of a combustion section, the combustion section having an inner liner extending between a forward end and an aft end, the piston ring assembly comprising: a piston ring configured to extend around the aft end of the inner liner; and an inner piston ring holder including a flange for attachment to the structural member of the gas turbine engine at a first end and a slot for receiving the piston ring at a second end, the inner piston ring holder further including a first portion having a U-shaped configuration and comprised of a first metallic material, the first metallic material having a first coefficient of thermal expansion, αH1, and a second portion comprised of a second metallic material, the second metallic material having a second coefficient of thermal expansion, αH2, the first coefficient of thermal expansion, αH1, being different than the second coefficient of thermal expansion, αH2; and, wherein the inner piston ring holder further includes an arm extending from the flange positioned at the first end to the slot positioned at the second end, wherein the first portion of the inner piston ring holder includes the flange and at least a portion of the arm, wherein the second portion of the inner piston ring holder includes the slot and at least a portion of the arm, and wherein at least about sixty percent of the arm comprises the first metallic material and comprises part of the first portion. 2. The piston ring assembly of claim 1 , wherein the first coefficient of thermal expansion, αH1, is greater than the second coefficient of thermal expansion, αH2. 3. The piston ring assembly of claim 1 , wherein the piston ring is a bimetallic piston ring comprised of a first material having a first coefficient of thermal expansion, αPR1, and a second material having a second coefficient of thermal expansion, αPR2, the first coefficient of thermal expansion, αPR1, being different than the second coefficient of thermal expansion, αPR2. 4. The piston ring assembly of claim 3 , wherein the second material of the piston ring is configured to be positioned closer to the inner liner of the combustion section than the first material of the piston ring, and wherein the first coefficient of thermal expansion, αPR1, of the first material of the piston ring is higher than the second coefficient of thermal expansion, αPR2, of the second material of the piston ring. 5. The piston ring assembly of claim 1 , further comprising a spring element positioned in the slot of the inner piston ring holder configured to press the piston ring towards the aft end of the inner liner.
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