Patent · US Active

Dual cycle intercooled hydrogen engine architecture

US12037946B2 · kind B2 · utility

1Cited by
10References
16Claims
0Family size

Assignee

Inventor

Key dates

Filing dateDec 28, 2022
Grant dateJul 16, 2024
Priority date
Expiry dateDec 28, 2042

Classification

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

Abstract

In one aspect of the present disclosure, there is provided a gas turbine engine. The gas turbine engine includes a primary gas path having, in fluid series communication: an air inlet, a compressor fluidly connected to the air inlet, a combustor fluidly connected to an outlet of the compressor, and a turbine section fluidly connected to an outlet of the combustor section. In embodiments, a hydrogen expansion turbine is in fluid communication to receive hydrogen from the gaseous hydrogen outlet of the heat exchanger. In certain embodiments, the gas turbine engine includes a heat exchanger having a gas conduit fluidly connected to the primary gas path, and a fluid conduit in fluid isolation from the gas conduit and in thermal communication with the gas conduit.

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