|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/266; 062/087; 060/039.83; 060/772|
|우선권정보||FR-08 56459 (2008-09-25)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 9|
A system for managing heat fluxes of an aircraft is provided, including a fuel tank supplying a turbomachine with fuel via a fuel supply circuit; a cell cooling circuit connected to a thermal effluents source, which integrates a first heat exchanger ensuring heat transfer between a coolant circulating in the cell cooling circuit and air flow channeled into a cooling air channel extending from an air intake to an exhaust; and a second heat exchanger ensuring a heat transfer between the coolant circulating in the cell cooling circuit and the fuel. The air ...
1. A system for managing the heat fluxes of an aircraft that includes at least one propulsion system that integrates a turbomachine, and a cell, the system comprising: at least one fuel tank configured to supply the turbomachine with fuel via a fuel supply circuit;a cell cooling circuit connected to at least one source of thermal effluents, the cell cooling circuit integrating first means for ensuring a heat transfer between a coolant that circulates in the cell cooling circuit and an air flow that is channeled into at least one cooling air channel that ...