公开(公告)号：US20240026813A1

公开(公告)日：2024-01-25

申请号：US18356662

申请日：2023-07-21

Applicant: Airbus Operations SAS

Inventor： Pierre-Olivier MARTIN ,  Lionel CZAPLA ,  Mathieu BELLEVILLE

IPC: F02C3/22 ,  F02C7/224 ,  F02C7/232

CPC classification number: F02C3/22 ,  F02C7/224 ,  F02C7/232

Abstract: A supply system for an aircraft arranged between two dihydrogen tanks and an engine. The supply system includes a supply module that assures the flow of dihydrogen between the tanks and an outlet pipe and two heaters mounted in series on a main pipe connected to the engine. The supply system also includes a network of pipes and solenoid valves that, in the event of a problem in one of the components of the supply system, enable dihydrogen to be redirected so as to reach the engine. Also an aircraft with such a supply system.

公开(公告)号：US20240150033A1

公开(公告)日：2024-05-09

申请号：US18356655

申请日：2023-07-21

Applicant: Airbus Operations SAS

Inventor： Pierre-Olivier MARTIN ,  Lionel CZAPLA ,  Mathieu BELLEVILLE

IPC: B64D37/30 ,  B64D37/00 ,  F02C7/232

CPC classification number: B64D37/30 ,  B64D37/005 ,  F02C7/232

Abstract: A supply system for an aircraft, wherein the supply system has a supply module with outlet pipes, feed pipes connected to dihydrogen tanks, and means for channeling the dihydrogen in the feed pipes towards the outlet pipes, a distribution module having introduction pipes connected to the outlet pipes via heaters, distribution pipes connected to an engine, and means for channeling the dihydrogen in the introduction pipes towards the distribution pipes, and a control unit which commands the means of the supply module and of the distribution module depending on the information provided by the detection means. Also an aircraft with such a supply system.