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    • 1. 发明申请
    • RECIRCULATING-FLOW WIND TUNNEL, IN PARTICULAR FOR FREE-FALLING OR PARACHUTING SIMULATIONS
    • 回流流风隧道,特别是免费下落或附加模拟
    • WO2017006251A1
    • 2017-01-12
    • PCT/IB2016/054036
    • 2016-07-06
    • EXTREME FLIGHT FZEMENGA, Gianni
    • MENGA, GianniEURIBE, Carlos
    • G01M9/02
    • G01M9/02A63G31/00A63G2031/005B64D23/00
    • A recirculating-flow wind tunnel, in particular for free-falling or parachuting simulations, comprising: a substantially vertical duct including a substantially vertical flight chamber (10), for housing a person who will fluctuate when hit by an air flow; a recirculation apparatus (16, 26, 28, 18, 32, 34, 36) in fluidic communication with the flight chamber (10), defining a substantially closed path for the air flow; and a blower device (14) for producing the air flow that will circulate between the flight chamber (10) and the recirculation apparatus (16, 26, 28, 18, 32, 34, 36). The substantially vertical duct includes: a cylindrical portion (11) having a circular cross-section; and a truncated cone portion (12), connected at the top to the cylindrical portion (11), having the shape of an upward-diverging truncated cone.
    • 特别是用于自由落体或跳伞模拟的再循环风洞,包括:基本上垂直的管道,其包括基本上垂直的飞行室(10),用于容纳当被空气流击打时波动的人; 与所述飞行室(10)流体连通的再循环设备(16,26,28,18,32,34,36),其限定用于空气流的基本封闭的路径; 以及用于产生将在所述飞行室(10)和所述再循环装置(16,26,28,18,32,34,36)之间循环的空气流的鼓风装置(14)。 所述基本垂直的管道包括:具有圆形横截面的圆柱形部分(11); 以及在顶部连接到圆柱形部分(11)的截头圆锥形部分(12),具有向上发散的截锥体的形状。
    • 4. 发明申请
    • FLYING CHAMBER FOR WIND TUNNEL AND ASSOCIATED WIND TUNNEL
    • 风洞和相关风洞的飞行室
    • WO2017103768A1
    • 2017-06-22
    • PCT/IB2016/057553
    • 2016-12-13
    • EXTREME FLIGHT FZEMENGA, Gianni
    • MENGA, GianniEURIBE, Carlos
    • G01M9/04A63G31/00B64D23/00
    • G01M9/04A63G31/00A63G2031/005B64D23/00
    • Flying chamber (2) for wind tunnels (1), preferably non- recirculating wind tunnels. The flying chamber (2) comprising a support structure (20) defining an inlet opening (21) and an outlet opening (22), which allow an air flow (F) to flow between them, said inlet opening (21) and outlet opening (22) being substantially aligned along a longitudinal axis (K) of the support structure (20) itself; said support structure (20) having an inner volume that is such as to house a person or user (U), who is going to be hit by the air flow (F). The flying chamber (2) comprising at least one moving device (3), for moving at least one portion of said support structure (20); Said at least one moving device (3) having at least one degree of freedom, moving said at least one portion of said support structure (20) at least around a rotation axis (X). Said rotation axis (X) being perpendicular to said longitudinal axis (K) of the support structure (20).
    • 用于风洞(1)的飞行室(2),优选非循环风洞。 所述飞行室(2)包括限定允许气流(F)在它们之间流动的入口开口(21)和出口开口(22)的支撑结构(20),所述入口开口(21)和出口开口 (22)沿着所述支撑结构(20)自身的纵向轴线(K)基本对齐; 所述支撑结构(20)具有内部容积,以便容纳将要被气流(F)击中的人或使用者(U)。 所述飞行室(2)包括至少一个移动装置(3),用于移动所述支撑结构(20)的至少一部分; 所述至少一个移动装置(3)具有至少一个自由度,从而使所述支撑结构(20)的所述至少一部分至少围绕旋转轴线(X)移动。 所述旋转轴线(X)垂直于支撑结构(20)的所述纵向轴线(K)。