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    • 1. 发明申请
    • VALVE FOR CONTROLLING THE INTERNAL PRESSURE IN A CABIN OF AN AIRCRAFT
    • 用于控制飞机仓库内部压力的阀门
    • US20130210330A1
    • 2013-08-15
    • US13816203
    • 2011-05-17
    • Martin SteinertAxel Springer
    • Martin SteinertAxel Springer
    • B64D13/04G05D7/06
    • B64D13/04B64D13/02F16K1/223F16K39/028G05D7/0647Y02T50/44Y10T137/87917
    • The invention relates to a valve (10) for controlling the internal pressure p in a cabin of an aircraft, comprising a first flap (11) and a second flap (12), wherein the flaps (11, 12) control a pressure-changing fluid flow (L) between the surroundings and the cabin through an opening (15) of a limiting element (14) of the cabin. in order to increase the inflow volume of the fluid, according to the invention at least one of the flaps (11, 12) is adjustable in the inflow position in respect of the opening (15) in the direction of the surroundings, such that the flow surface of the flap (11, 12) is increased for the air flow (L). Furthermore according to the invention at least one of the flaps (11, 22) has a closure device (21) which reduces an outflow of the fluid that had previously flowed in during an inflow process. According to the invention, a closure-device (21) is furthermore arranged, wherein said closure device closes a region between the first flap (11) and the second flap(12) in the inflow position of the flaps (11, 12).
    • 本发明涉及一种用于控制飞行器舱室内部压力p的阀门(10),包括第一挡板(11)和第二挡板(12),其中挡板(11,12)控制压力变化 通过机舱的限制元件(14)的开口(15)在周围和车厢之间的流体流(L)。 为了增加流体的流入体积,根据本发明,至少一个翼片(11,12)可以相对于开口(15)沿着周围的方向在流入位置中是可调节的,使得 翼片(11,12)的流动表面对于空气流(L)而增加。 此外,根据本发明,至少一个翼片(11,22)具有闭合装置(21),其减少了在流入过程中预先流入的流体的流出。 根据本发明,还布置了闭合装置(21),其中所述闭合装置在所述翼片(11,12)的流入位置中封闭所述第一翼片(11)和所述第二翼片(12)之间的区域。