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기록

GAS TURBINE ENGINE WITH HEAT EXCHANGER

발명심사 중
1조회수
20청구항 · 2 독립항
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개요

발명자

Hojjat Nasr; Ashish Sharma; Michael Vadnais; Kevin Edward Hinderliter; Jonathan Russell Ratzlaff

IPC 분류

F2C 7/14F28D 15/4

CPC 분류

F2C7/14F28D15/43F5D2260/208

A heat exchanger for a gas turbine engine includes an inlet manifold, an outlet manifold, a plate extending from the inlet manifold to the outlet manifold, and a heat pipe in thermal communication with the plate. The heat pipe includes a pipe defining a cavity and a fluid disposed in the cavity.

원문 (중국어)

A heat exchanger for a gas turbine engine includes an inlet manifold, an outlet manifold, a plate extending from the inlet manifold to the outlet manifold, and a heat pipe in thermal communication with the plate. The heat pipe includes a pipe defining a cavity and a fluid disposed in the cavity.