Patent · US Active

Thermal management system

US12259194B2 · kind B2 · utility

0Cited by
84References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 10, 2023
Grant dateMar 25, 2025
Priority date
Expiry dateJul 10, 2043

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF28D2021/0026
  • WIPO fieldThermal processes and apparatus
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine is provided. The gas turbine engine includes: a thermal management system having a thermal fluid member having a flow of thermal fluid therethrough during operation of the gas turbine engine and a heat exchanger assembly, the heat exchanger assembly including: a core section comprising a plurality of heat exchange members; and a heat exchange manifold including a first direction pressure vessel in fluid communication with the thermal fluid member and a second direction pressure vessel extending from the first direction pressure vessel, the first and second direction pressure vessels each extending in a reference plane, the second direction pressure vessel in fluid communication with the first direction pressure vessel and with at least one of the plurality of heat exchange members.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.