公开(公告)号：US20240353186A1

公开(公告)日：2024-10-24

申请号：US18304771

申请日：2023-04-21

Applicant: RAYTHEON TECHNOLOGIES CORPORATION

Inventor： ORIN G. AVIDANE ,  TYLER G. VINCENT ,  SUBHADEEP GAN

IPC: F02C7/12 ,  F28D9/00 ,  F28F3/04

CPC classification number: F28F9/02 ,  F02C7/12 ,  F05D2260/20 ,  F05D2260/22141 ,  F28F2009/0292 ,  F28F2215/00

Abstract: A heat exchanger can comprise: a housing; a heat transfer region disposed within the housing; and an inlet manifold or an inlet conduit defined at least partially by an interior surface extending axially from a first end of the heat exchanger to an inlet defined by the heat transfer region, the inlet manifold or the inlet conduit comprising a protrusion configuration disposed in the interior surface. The heat exchanger can further comprise an outlet manifold or an outlet conduit including a protrusion configuration disposed on an interior surface of the outlet manifold or outlet conduit.

公开(公告)号：US20250020080A1

公开(公告)日：2025-01-16

申请号：US18352878

申请日：2023-07-14

Applicant: Raytheon Technologies Corporation

Inventor： ORIN G. AVIDANE ,  Tyler G. VINCENT ,  SUBHADEEP GAN ,  JORN A. GLAHN

IPC: F02C7/143

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.