| 摘要 |
<p>The method involves maintaining fluid e.g. fuel and oil, circulation in fluid circulation circuits (19, 21) of fluidic and mechanical type equipment of an aircraft until temperature decreases to a predetermined value after stopping of a turbojet engine. The circulation of the fluids is made in respective fluid circulation circuits. A fan (7) is maintained to circulate air in the turbojet engine in a rotating manner. Oil in one of the fluid circulation circuits is passed in a heat exchanger. An independent claim is also included for a device for cooling an equipment of an aircraft comprising a turbojet engine.</p> |
