Patent · US Active

Aircraft comprising a hydrogen supply device incorporating a hydrogen heating system positioned in the fuselage of the aircraft

US11840962B2 · kind B2 · utility

0Cited by
0References
11Claims
0Family size

Assignees

Inventors

Key dates

Filing dateAug 1, 2022
Grant dateDec 12, 2023
Priority date
Expiry dateAug 1, 2042

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T90/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft including a fuselage, a wing structure, at least one turbomachine running on hydrogen and generating thrust at a propulsion unit distant from the fuselage, at least one fuel tank positioned in the fuselage and configured to store hydrogen in the cryogenic state, at least one hydrogen supply device connecting the fuel tank and the turbomachine and including at least one pump positioned in the fuselage in the vicinity of the fuel tank, at least one hydrogen heating system positioned in the fuselage in the vicinity of the pump. This solution makes it possible to reduce a length of the complex double-walled pipes configured for carrying the hydrogen in the cryogenic state between the fuel tank and the hydrogen heating system.

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