Patent ID: 11878806
Assignee: AIRBUS OPERATIONS S.L.
Field: Transport (Mechanical engineering)
Classification: CPC B  H  Y | IPC B

Claim 8:
9. The aircraft according to claim 7,
wherein the cooling system has a first heat exchanger, a second heat exchanger, an exchange duct in which a heat-transfer fluid circulates, the reservoir and the conveying duct,
wherein the exchange duct forms a loop that is arranged to:
successively pass through the first heat exchanger,
ensure an exchange of heat successively between each linear electric motor and the heat-transfer fluid,
pass through the second heat exchanger and re-join the first heat exchanger,

wherein the first heat exchanger is arranged to ensure an exchange of heat between the dihydrogen circulating in the conveying duct between the reservoir and the fuel cell and the heat-transfer fluid circulating in the exchange duct,
wherein the second heat exchanger is arranged to ensure an exchange of heat between the heat-transfer fluid circulating in the exchange duct and an additional fluid, and
wherein the first heat exchanger is disposed upstream of the linear electric motors and the second heat exchanger is disposed downstream of the linear electric motors with respect to a direction of flow of the heat-transfer fluid in the exchange duct.