发明名称 Flap valve for an aircraft.
摘要 <p>The invention relates mainly to a flap valve and a flap comprising a valve, as well as an aircraft comprising such a valve. …<??>The invention relates to a valve (1) comprising a flap (2) on its surface. The valve (1) is used for the (fine) regulation of pressure or flow, and the flap (2) permits a safety pressure balancing. The incorporation of the flap (2) into the valve (1), or of the valve (1) into the flap (2), makes it possible to form only a single orifice in the separating surface, and thus to reduce the weight and the price, and to increase safety. …<??>The device according to the present invention applies to any device for regulating pressure and/or flow between an enclosure and the outside, or between two enclosures comprising a safety balancing device. …<??>The invention applies, in particular, to aircraft construction, to the construction of oil refineries, of fluid-distribution devices and of chemical reactors. …<IMAGE>… </p>
申请公布号 EP0342069(A1) 申请公布日期 1989.11.15
申请号 EP19890400985 申请日期 1989.04.11
申请人 ABG-SEMCA 发明人 CARLA, FRANCIS;BAROUX, BRUNO;FRAISSE, JACQUES;SIGNORET, JACQUES
分类号 B64D13/02;B64D13/04;F16K17/04;F16K17/168 主分类号 B64D13/02
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