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US 10,294,816 B2Granted
High durability turbine exhaust case
AssigneesUnited Technologies Corporation, GKN Aerospace Sweden AB
InventorsDaryl B. Mountz, Theodore W. Kapustka, Glenn Levasseur, Marcus Borg, Joakim Berglund, Anders Svahn, Johan Ockborn, Bengt Pettersson
Life of this patent
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Abstract
A turbine exhaust case has an outer housing to be secured within a gas turbine engine and a central hub. Struts extend between the outer housing and the central hub. The struts are formed at least in part of a first material. The central hub is formed at least in part of a second material.
Claims4
A gas turbine engine comprising:
- a fan delivering air into a core engine, and into a bypass duct as bypass air, said core engine including a compressor fluidly connected to a combustor, said combustor fluidly connected to a turbine section, with a turbine exhaust case downstream of said turbine section, said turbine exhaust case including:
- a central hub including a support surface;
- and
- an outer housing secured within the gas turbine engine;
- said turbine section including at least one turbine rotor, with the turbine rotor including a shaft supported at least, in part, by the support surface in the turbine exhaust case;
- wherein the turbine exhaust case is constructed of at least a first material and a second material;
- and
- said central hub having a plurality of radially outwardly extending stubs and struts extending between the outer housing and said central hub, and said plurality of radially outwardly extending stubs being welded to said struts, such that radially inner portions of an airfoil are formed by the stubs of the second material, and radially outward portions of said airfoil are formed by the struts of the first material.
5 more elements
A gas turbine engine comprising:
- a fan delivering air into a core engine, and into a bypass duct as bypass air, said core engine including a compressor fluidly connected to a combustor, said combustor fluidly connected to a turbine section, with a turbine exhaust case downstream of said turbine section;
- the turbine exhaust case downstream of and in fluid communication with the core engine, the turbine exhaust case having:
- a central hub including a support surface;
- and
- an outer housing secured within the gas turbine engine;
- a turbine section including at least a turbine rotor, with the turbine rotor including a shaft supported at least, in part, by the support surface in the turbine exhaust case;
- wherein the turbine exhaust case is constructed of at least a first material and a second;
- material;
- and
- said central hub having a plurality of radially outwardly extending stubs and struts extending between the outer housing and said central hub, and said plurality of radially outwardly extending stubs being welded to said struts, such that radially inner portions of an airfoil are formed by the stubs of the second material, and radially outward portions are formed by the struts of the first material.
7 more elements
Dependencies are inferred from the claim text.