| 摘要 |
<p>A cooling arrangement (10) suitable for use in an aircraft comprises a cooling energy consumer (14) having a housing (16) which is provided with a cooling fluid inlet (18) for supplying a cooling fluid to the housing (16) and a cooling fluid outlet (20) for discharging the cooling fluid from the housing (16). The cooling energy consumer (14) is received within a compartment (12). The compartment (12) is provided with a cooling air inlet (32) for supplying cooling air to the compartment (12) and a cooling air outlet (34) for discharging the cooling air from the compartment (12).</p> |
