发明名称 DISPOSITIVO COMPENSADOR DE PRESIONES EN AERONAVE.
摘要 Pressure compensation device (100) deployed in an element that contains a flammable substance that compensates pressures between interior (101) of the element and exterior atmosphere (102) in which said element is deployed, by means of a continuous primary circulation (300) of air through primary channel (103) in said device (110) that communicates interior (100) and exterior (102) of the element, further comprising a secondary channel (104) integrated in the device (100) itself, communicating interior (102) and exterior (102) of the element, comprising said secondary channel (104) in the interior zone of the element a sheet (105) such that, in the event primary continuous circulation (300) of air through primary channel (103) is interrupted, said continuous circulation continues through secondary circulation (400) of air to interior (101) of the element, this secondary circulation (400) of air being capable of breaking sheet (105) of secondary channel (104).
申请公布号 ES2402613(B1) 申请公布日期 2014.03.13
申请号 ES20110031710 申请日期 2011.10.24
申请人 AIRBUS OPERATIONS S.L. 发明人 ZUNIGA SAGREDO, JUAN;FERNANDEZ ALONSO, CARLOS;OUTON HERNANDEZ, IGNACIO
分类号 B64D37/10 主分类号 B64D37/10
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