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US 2026/0194008 A1Published application
Bead protrusions heat transfer surface structure of fluid conduits and manifolds
AssigneeRtx Corporation
InventorsOrin G. Avidane, Tyler G. Vincent, Subhadeep Gan, Jorn A. Glahn
Life of this patent
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Abstract
A turbine engine including one or more conduits is disclosed herein. At least one conduit of the turbine engine includes a first end coupled to the turbine engine, a second end, and a body extending from the first end to the second end, the body including an interior surface and an exterior surface, wherein at least one of the interior surface or the exterior surface includes a protrusion configuration.
Claims20
A conduit of a turbine engine, comprising:
- a first end coupled to the turbine engine;
- a second end;
- and
- a body extending from the first end to the second end, the body including an interior surface and an exterior surface, wherein at least one of the interior surface or the exterior surface includes a protrusion configuration.
1 more element
A gas turbine engine, comprising:
- a fan section;
- a turbine section;
- and
- a conduit coupled to the fan section and the turbine section, the conduit including:
- an inlet coupled to the turbine section;
- an outlet coupled to the fan section;
- and
- a body extending between the inlet and the outlet, the body including a protrusion configuration along one of an exterior surface of the body or an interior surface of the body.
5 more elements
A gas turbine engine, comprising:
- a first section;
- a second section adjacent the first section;
- and
- a conduit fluidly coupled to the first section and the second section, the conduit including:
- an inlet fluidly coupled to the first section;
- an outlet fluidly coupled to the second section;
- and
- a body fluidly coupled to the inlet and the outlet, the body including a protrusion configuration along at least one of an interior surface of the body or an exterior surface of the body.
5 more elements
Dependencies are inferred from the claim text.