Patent · US Active

Gas turbine engine thermal management system

US10352241B2 · kind B2 · utility

9Cited by
1References
9Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 3, 2018
Grant dateJul 16, 2019
Priority date
Expiry dateMay 3, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/213
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The present disclosure provides systems and methods related to thermal management systems for gas turbine engines. For example, a thermal management system comprises a thermally neutral heat transfer fluid circuit, a first heat exchanger disposed on the fluid circuit, and a second heat exchanger disposed on the fluid circuit.

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