A seal assembly is positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine. The cavity includes a cavity wall. The seal assembly includes a seal and a seal protector. The seal extends circumferentially within the cavity. The seal protector extends
A seal assembly is positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine. The cavity includes a cavity wall. The seal assembly includes a seal and a seal protector. The seal extends circumferentially within the cavity. The seal protector extends circumferentially within the cavity. The seal protector is positioned between the seal and the cavity wall. The seal protector includes a locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal.
대표청구항▼
1. A seal assembly positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine, which cavity includes a cavity wall, which seal assembly comprises: a seal that extends circumferentially within the cavity; anda seal protector that extends circumferentia
1. A seal assembly positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine, which cavity includes a cavity wall, which seal assembly comprises: a seal that extends circumferentially within the cavity; anda seal protector that extends circumferentially within the cavity, which seal protector is positioned between the seal and the cavity wall, and which seal protector includes a radially-extending locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal;wherein the cavity includes a forward cavity wall, an aft cavity wall, a radially inner cavity wall, and a radially outer cavity wall, and wherein the seal protector is positioned between a positioning contact surface of the seal and the radially inner cavity wall; andwherein the locating feature is positioned between an aft sealing contact surface of the seal and the aft cavity wall. 2. The seal assembly of claim 1, wherein the seal is at least substantially annularly-shaped, and wherein the seal protector is at least substantially annularly-shaped. 3. The seal assembly of claim 2, wherein the seal forms a split ring, and wherein the seal protector forms a split ring. 4. The seal assembly of claim 1, wherein the seal protector includes a first body portion that extends between a first end of the seal protector and a bent portion of the seal protector, and a second body portion that extends between a second end and the bent portion of the seal protector, wherein the locating feature is formed by the first body portion of the seal protector. 5. The seal assembly of claim 1, wherein the seal is made from a material selected from the group consisting of: a cobalt alloy; a nickel alloy. 6. The seal assembly of claim 1, wherein the seal protector is made from a material selected from the group consisting of: a cobalt alloy; a nickel alloy; a ceramic. 7. A seal assembly positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine, which cavity includes a cavity wall, which seal assembly comprises: a seal that extends circumferentially within the cavity; anda seal protector that extends circumferentially within the cavity, which seal protector is positioned between the seal and the cavity wall, and which seal protector includes a radially-extending locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal;wherein the seal forms a radially extending recess, wherein the locating feature of the seal protector is positioned at least partially within the recess; andwherein the seal includes a first bellow and a second bellow, wherein the recess is formed between the first and second bellows. 8. The seal assembly of claim 7, wherein the seal comprises a cobalt alloy or a nickel alloy. 9. The seal assembly of claim 7, wherein the seal protector comprises a cobalt alloy, a nickel alloy or a ceramic. 10. A seal assembly positioned within a cavity that extends circumferentially about an axial centerline of a gas turbine engine, which cavity includes a cavity wall, which seal assembly comprises: a seal that extends circumferentially within the cavity; anda seal protector that extends circumferentially within the cavity, which seal protector is positioned between the seal and the cavity wall, and which seal protector includes a radially-extending locating feature that is operative to contact the seal to aid in axially positioning the seal protector relative to the seal;wherein the seal forms a radially extending recess, wherein the locating feature of the seal protector is positioned at least partially within the recess; andwherein the seal protector includes a bellow, and wherein the locating feature of the seal protector is formed by the bellow. 11. The seal assembly of claim 10, wherein the seal comprises a cobalt alloy or a nickel alloy. 12. The seal assembly of claim 10, wherein the seal protector comprises a cobalt alloy, a nickel alloy or a ceramic.
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이 특허에 인용된 특허 (8)
Durand, Didier Noel; Gehan, Dominique; Gros, Valerie Annie; Sotto-Lamy, Didier, Device for attaching ring sectors around a turbine rotor of a turbomachine.
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