公开(公告)号：US20250026484A1

公开(公告)日：2025-01-23

申请号：US18776574

申请日：2024-07-18

Applicant: Airbus Operations SAS

Inventor： Jérôme MILLIERE ,  Lionel CZAPLA ,  Romain JOUBERT

IPC: B64D37/32 ,  B64D37/16 ,  B64D37/30

Abstract: A module for an aircraft, the module comprising a sealed housing comprising walls delimiting an interior volume, a processing system to process dihydrogen and fixed on the inside of the housing, an inlet port connected to the interior volume and equipped with a first shut-off valve, an outlet port connected to the interior volume and equipped with a second shut-off valve and beads filling the interior volume.

公开(公告)号：US20240327024A1

公开(公告)日：2024-10-03

申请号：US18618261

申请日：2024-03-27

Applicant: Airbus Operations SAS

Inventor： Jérôme MILLIERE ,  Romain JOUBERT ,  Marc CASTERAN

IPC: B64D37/30

CPC classification number: B64D37/30

Abstract: An aircraft comprising a dihydrogen transport line, an embedded channel comprising a gutter in which the transport line is fixed and having a first end by which the transport line enters into the gutter and a second end by which the transport line leaves the gutter, and an evacuation system fluidically connected between the second end of the gutter and the outside of the aircraft for the evacuation of air and of water.

公开(公告)号：US20250026483A1

公开(公告)日：2025-01-23

申请号：US18776566

申请日：2024-07-18

Applicant: Airbus Operations SAS

Inventor： Jérôme MILLIERE ,  Lionel CZAPLA ,  Romain JOUBERT

IPC: B64D37/30

Abstract: A module for an aircraft, the module comprising a sealed housing comprising walls delimiting an interior volume, a processing system intended to process dihydrogen fixed on the inside of the sealed housing and filling elements filling at least in part the interior volume around the processing system. The filling elements may be foam or beads. Also an aircraft with such a module.

公开(公告)号：US20230086167A1

公开(公告)日：2023-03-23

申请号：US17948518

申请日：2022-09-20

Applicant: Airbus SAS ,  Airbus Operations SAS

Inventor： Jérôme MILLIERE ,  Romain JOUBERT ,  Lionel TEYSSEDRE ,  Alistair FORBES

IPC: B64D37/32 ,  B64F1/28

Abstract: An aircraft having at least one transport pipe in which dihydrogen flows and, for each transport pipe, an embedding channel in which the transport pipe is housed. The embedding channel has a gutter that has a bottom and an opening opposite the bottom and a cover that covers the opening of the gutter. The cover constitutes an outer wall of the aircraft in direct contact with external air surrounding the aircraft. The cover has ventilation windows passing through it that allow the passage of the dihydrogen towards the outside. With such an arrangement, even in the event of dihydrogen leaking into the embedding channel, the dihydrogen is automatically evacuated towards the outside of the aircraft.

公开(公告)号：US20240359811A1

公开(公告)日：2024-10-31

申请号：US18644785

申请日：2024-04-24

Applicant: Airbus Operations SAS

Inventor： Jérôme MILLIERE ,  Lionel CZAPLA ,  Romain JOUBERT

IPC: B64D37/30 ,  B64D37/00 ,  F17C7/00

CPC classification number: B64D37/30 ,  B64D37/005 ,  F17C7/00 ,  F17C2205/0332 ,  F17C2205/0335 ,  F17C2205/0355 ,  F17C2221/012 ,  F17C2227/0135 ,  F17C2227/0302 ,  F17C2265/066 ,  F17C2270/0189

Abstract: An aircraft comprising at least one secondary structure which separates an inner zone from an outer zone and at least one hydrogen supplying device connecting a hydrogen tank and a motor, and having at least one portion fitted with shut-off valves for isolating it in the event of a leak. The portion has at least one outer enclosure, at least one inner element that is located in the outer enclosure and carries the hydrogen, and at least one interior zone located between the inner element and the outer enclosure, the hydrogen supplying device comprising at least one ventilation system configured to vent gases present in the interior zone toward the outer zone of the secondary structure.

公开(公告)号：US20230406530A1

公开(公告)日：2023-12-21

申请号：US18335224

申请日：2023-06-15

Applicant: Airbus Operations SAS

Inventor： Romain JOUBERT ,  Lionel CZAPLA ,  Jérôme MILLIERE

IPC: B64D37/30 ,  B64D37/34

CPC classification number: B64D37/30 ,  B64D37/34

Abstract: A casing system mounted between an upstream solenoid valve of an upstream pipe and a downstream solenoid valve of a downstream pipe and which has a casing divided by a separation wall into a first volume which is placed under reduced pressure and a second volume, a heat exchanger which is fixed inside the casing with a first inlet which is arranged in the first volume and which is connected to the upstream pipe and a first outlet which is arranged in the second volume and which is connected to the downstream pipe, and a control unit which closes the solenoid valves if the deviation between two successive values of the pressure in the first volume or in the second volume is greater than a threshold.

公开(公告)号：US20230382551A1

公开(公告)日：2023-11-30

申请号：US18325217

申请日：2023-05-30

Applicant: Airbus Operations SAS

Inventor： Marc CASTERAN ,  Romain JOUBERT ,  Jérôme MILLIERE

IPC: B64D37/34 ,  B64D37/30

CPC classification number: B64D37/34 ,  B64D37/30 ,  B64D2041/005

Abstract: An aircraft having at least one dihydrogen transport pipe, an embedding channel with a lower gutter, an aeration aperture with an air inlet collecting external air and at least one supply pipe opening at the air inlet, a control unit, and, for one or more lower gutters, a bypass box having, for each lower gutter, an inlet connected to the supply pipe and an outlet connected to the lower gutter, between each associated inlet and outlet, a door able to move alternately between an open position and a closed position, and, for each door, a maneuvering system controlled by the control unit and moving the door.