公开(公告)号：US20240217357A1

公开(公告)日：2024-07-04

申请号：US18520186

申请日：2023-11-27

Applicant: Airbus Operations S.L.U.

Inventor： Carlos CASADO MONTERO

IPC: B60L53/18 ,  B60L53/30 ,  B60L53/60

CPC classification number: B60L53/18 ,  B60L53/30 ,  B60L53/60 ,  B60L2200/10 ,  B64U2101/00

Abstract: An in-flight electrical charging system and method for a battery-powered aircraft located in a charging aircraft and including an electrical generation module including a turbine, an electric generator in electrical connection to the turbine for generating electricity, a turbine control unit in connection with the turbine and controlling it, and an electric generator control unit in connection with the electric generator and controlling it, a deployable power supply module, in electrical connection to the electrical generation module and including at least a cable configured for the electrical connection of the electrical generation module to the battery-powered aircraft to be charged, a pod configured to be applied to the charging aircraft, wherein the electrical generation module and the deployable power supply module are located within the pod.

公开(公告)号：US20250026485A1

公开(公告)日：2025-01-23

申请号：US18772614

申请日：2024-07-15

Applicant: Airbus Operations S.L.U.

Inventor： Carlos CASADO MONTERO ,  Pablo Manuel CALDERÓN GÓMEZ

IPC: B64D37/34 ,  F02C7/224

Abstract: A conditioning system for an aircraft having a pressure accumulator connected to the heat recovery circuit and to the fuel conduct. A fluid of the fuel conduct is hydrogen (H2), or the working fluid of the heat recovery circuit comprises Nitrogen (N2), Helium (He), ethylene glycol water (EGW), and mixtures thereof, or both. Also an aircraft comprising such a conditioning system.

公开(公告)号：US20240218832A1

公开(公告)日：2024-07-04

申请号：US18525143

申请日：2023-11-30

Applicant: AIRBUS OPERATIONS, S.L.U.

Inventor： Carlos CASADO MONTERO ,  Pablo Manuel CALDERÓN GÓMEZ ,  María Cruz ZAMARRO MARTÍN ,  Agustín GÓMEZ FERNÁNDEZ ,  David CASTAÑO DE LA MOTA

IPC: F02C7/224 ,  B64D41/00

CPC classification number: F02C7/224 ,  B64D41/00 ,  F05D2260/20

Abstract: A conditioning system for an aircraft including a fuel conduit which receives a liquid fuel, an evaporator and a heater which heat the liquid fuel to convert the fuel to a gas fuel supplied to an engine on the aircraft, the evaporator transfers heat from a hot working fluid to the liquid fuel and the heater converts energy into heat applied to the liquid fuel, and a heat recovery circuit which circulates the working fluid through the evaporator and a heat exchanger in a hot exhaust gas stream generated by the engine.

公开(公告)号：US20240271576A1

公开(公告)日：2024-08-15

申请号：US18529072

申请日：2023-12-05

Applicant: Airbus Operations S.L.U.

Inventor： Carlos CASADO MONTERO ,  Pablo Manuel CALDERÓN GÓMEZ

IPC: F02C9/28 ,  B64D41/00 ,  F02C7/224 ,  F23R3/28

CPC classification number: F02C9/28 ,  B64D41/00 ,  F02C7/224 ,  F23R3/28 ,  F05D2270/301 ,  F05D2270/303

Abstract: An aircraft conditioning system including a fuel tank, including an outlet connected to an Auxiliary Power Unit (APU) fuel inlet, configured to maintain a pressurized gas fuel, a pressure regulator, downstream of the fuel tank, configured to regulate a pressure of the pressurized gas fuel injected to the APU inlet, a first temperature sensor downstream of the pressure regulator and a second temperature sensor upstream of an engine, a first pressure sensor inside the fuel tank, a second pressure sensor downstream of the pressure regulator and a third pressure sensor at an engine inlet, and a controller connected to the pressure sensors and the temperature sensors, the controller receiving temperature and pressure values from the pressure sensors and from the temperature sensors and actuating on at least one of the pressure regulator or the injection position of the pressurized gas fuel inside a plurality of engine combustion chambers.

公开(公告)号：US20240190581A1

公开(公告)日：2024-06-13

申请号：US18523042

申请日：2023-11-29

Applicant: AIRBUS OPERATIONS, S.L.U.

Inventor： Benjamin DAVID ,  Marcos Javier CHIABRANDO ,  María Cruz ZAMARRO MARTÍN ,  Francisco Manuel ANDREU FERNÁNDEZ ,  Carlos CASADO MONTERO

IPC: B64D41/00 ,  B60L3/00 ,  B60L50/00 ,  F02C7/26 ,  H02J3/00

CPC classification number: B64D41/00 ,  B60L3/0092 ,  B60L50/00 ,  F02C7/26 ,  H02J3/0073 ,  B60L2200/10 ,  F05D2220/76 ,  F05D2260/85

Abstract: An auxiliary power generator system for an aircraft including an auxiliary power unit (APU) with dual and fully redundant starter and electrical power generation systems that connects independently to a normal electric network or an emergency electric network of an aircraft. A method for supplying electric power to an aircraft by means of the system.

公开(公告)号：US20250027723A1

公开(公告)日：2025-01-23

申请号：US18779212

申请日：2024-07-22

Applicant: AIRBUS OPERATIONS, S.L.U.

Inventor： Carlos CASADO MONTERO ,  Pablo Manuel CALDERÓN GÓMEZ ,  Ignacio ENEBRAL TRIGO ,  Agustín GÓMEZ FERNÁNDEZ ,  Jorge BERROCOSO REDONDO ,  Domingo Jose SANTANA SANTANA ,  Pedro Ángel GONZÁLEZ GÓMEZ ,  Antonio ACOSTA IBORRA ,  Marta LAPORTE AZCUE

IPC: F28D9/00 ,  B64D41/00

Abstract: A heat exchanger configured to be positioned in a tail cone section of a fuselage of an aircraft and including a liner through which passes hot gases from an auxiliary power unit (APU) and plates within the liner, wherein the plates are hollow and receive a second fluid from a first collector and discharge the second fluid from the plates to a second collector.