Patent · US Active

Heat exchanger for a gas turbine engine propulsion system

US10677166B2 · kind B2 · utility

8Cited by
18References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 3, 2016
Grant dateJun 9, 2020
Priority date
Expiry dateApr 6, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A propulsion system including a gas turbine engine is disclosed herein. The propulsion system further includes a heat exchanger arranged outside the gas turbine engine and adapted to cool fluid from the gas turbine engine.

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