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    Waist-mounted parachute deployment and retracting system
    73.
    发明授权
    Waist-mounted parachute deployment and retracting system 有权
    腰式降落伞部署和收缩系统

    公开(公告)号：US08684891B1

    公开(公告)日：2014-04-01

    申请号：US13091368

    申请日：2011-04-21

    申请人： Archie Davidson

    发明人： Archie Davidson

    IPC分类号： A63B71/00 ,  A63B21/008 ,  B64D17/00 ,  B64D17/02

    CPC分类号： A63B69/0022 ,  A63B21/0088 ,  A63B21/4009 ,  A63B69/0028 ,  B64D17/30 ,  B64D17/343 ,  B64D17/42

    摘要： A waist-mounted parachute deployment and retracting system for training runners and other athletes that provides a user a method for selectively deploying and retracting the parachute during training without stopping or breaking stride. The parachute provides drag to increase resistance to improve performance by overloading the muscles. The user selectively deploys the parachute by pressing a button to release and open the parachute. Air flow created by the user's forward motion flows through a pair of ports on the side of a case holding the parachute. The air flow expands the parachute, causing the cords attaching the parachute to the case to extend and wind a recoil mechanism. The user selectively retracts the parachute by pressing a button to close the parachute and the recoil mechanism rewinds the cords, pulling the parachute into the case, ready to be deployed again when desired.

    摘要翻译： 一种用于训练跑步者和其他运动员的腰部安装的降落伞部署和收回系统，其为用户提供了一种在训练期间选择性地部署和缩回降落伞而不停止或断开步骤的方法。 降落伞提供阻力以增加阻力，以通过超载肌肉来提高性能。 用户通过按下按钮释放并打开降落伞来选择性地部署降落伞。 由使用者的前进运动产生的空气流动通过一个保持降落伞的壳体一侧的端口。 空气流扩张降落伞，导致将降落伞连接到壳体上的绳索延伸并卷绕反冲机构。 用户通过按压按钮来选择性地缩回降落伞以关闭降落伞，并且反冲机构回绕绳索，将降落伞拉到壳体中，以便在需要时重新部署。

    MECHANICALLY OPENING EMERGENCY PARACHUTE
    74.
    发明申请
    MECHANICALLY OPENING EMERGENCY PARACHUTE 审中-公开
    机械开启紧急停机

    公开(公告)号：US20110220764A1

    公开(公告)日：2011-09-15

    申请号：US13035593

    申请日：2011-02-25

    申请人： BONG H. SUH

    发明人： BONG H. SUH

    IPC分类号： B64D17/02 ,  B64D17/24 ,  B64D17/40 ,  B64D17/30

    CPC分类号： B64D17/70 ,  A62B1/02

    摘要： The mechanically opening emergency parachute is a parachute that may be opened quickly at low altitudes, such as during an emergency exit from an office building. The parachute includes a tube having opposed upper and lower ends, with an upper end of a suspension cord being secured to the lower end thereof. An upper annular runner is resiliently mounted on the tube. First ends of a plurality of ribs are pivotally attached to the upper end of the tube. An upper stretcher is mounted on the upper annular runner and includes a plurality of supports, with each support extending therefrom to one of the ribs. A lower stretcher is secured to the lower end of the suspension cord and includes a plurality of risers radially extending therefrom. A canopy is secured to the ribs, and a plurality of suspension lines extend between the risers and the canopy.

    摘要翻译： 机械开启的紧急降落伞是一种降落伞，可在低空下快速打开，例如在办公楼的紧急出口处。 降落伞包括具有相对的上端和下端的管，悬挂绳索的上端固定到其下端。 上环形流道弹性地安装在管上。 多个肋的第一端枢转地附接到管的上端。 上部担架安装在上部环形滑轮上并且包括多个支撑件，每个支撑件从该支撑件延伸到其中一个肋条。 下拉伸器固定到悬挂索的下端，并且包括从其径向延伸的多个立管。 顶篷固定在肋上，并且多个悬挂线在立管和顶盖之间延伸。

    Hybrid Parachute
    75.
    发明申请
    Hybrid Parachute 有权
    混合降落伞

    公开(公告)号：US20100163682A1

    公开(公告)日：2010-07-01

    申请号：US11914930

    申请日：2007-09-21

    申请人： Nicholas F. Jameson

    发明人： Nicholas F. Jameson

    IPC分类号： B64D17/02 ,  B64D17/62

    CPC分类号： B64D17/025 ,  B64D17/18 ,  B64D17/64

    摘要： A hybrid parachute, method of deploying a parachute and method of landing a payload. The hybrid parachute utilizes a reefing system that provides for the initial deployment of a deceleration stage that is configured to withstand the stresses of high-speed and/or high altitude openings. The deceleration stage has operating characteristics similar to known high-speed parachutes. After sufficient deceleration has been achieved with the deceleration stage, reefings are released deploying one or more low-speed high drag stages of the device. The high drag stage(s) provide the landing characteristics of a low-speed parachute, including the possibility of controlled descent and landing.

    摘要翻译： 混合降落伞，部署降落伞的方法和着陆有效载荷的方法。 混合降落伞利用了一种提供初始部署减速阶段的系统，该减速阶段被配置为承受高速和/或高空开口的应力。 减速阶段具有与已知的高速降落伞类似的操作特性。 在减速阶段实现了足够的减速后，释放部署一个或多个低速高阻力级的装置。 高拖曳阶段提供了低速降落伞的着陆特性，包括可控制的下降和着陆。

    Wing having a negative dihedron for towing a load
    76.
    发明授权
    Wing having a negative dihedron for towing a load 有权
    翼具有负二面体以牵引负载

    公开(公告)号：US07494093B2

    公开(公告)日：2009-02-24

    申请号：US11739936

    申请日：2007-04-25

    申请人： Dominique Legaignoux ,  Bruno Legaignoux

    发明人： Dominique Legaignoux ,  Bruno Legaignoux

    IPC分类号： B64D17/02

    CPC分类号： B63B35/7979 ,  B64C31/06 ,  B64C2031/065

    摘要： The wing (10) having a negative dihedron for towing a load comprises a flexible canopy (12) which is defined between two lateral ends (14A, 14B) which are connected to each other, at the front, by a leading edge and, at the rear, by a trailing. The wing (10) includes rear lines (40A, 40B) which are connected to the suspension members (30A, 30B) which are arranged at the lateral ends (14A, 14B) of the wing, and in that the auxiliary maintenance means of the propulsive central region (16) comprise at least a front line which is connected by one end to the propulsive central region adjacent to the leading edge and which is capable of being connected to the load at the other end. The front lines comprise an assembly of shroud lines (90A, 90B) which are applied to the propulsive central region (16) at locations which are distributed over the length of the leading edge, at least one sliding shroud line (90A, 90B) being engaged in a sliding manner in a guide (92A, 92B) which is fixedly joined to the leading edge, the end of the sliding shroud line (90A, 90B) being fixedly joined to a rear line (40A, 40B).

    摘要翻译： 具有用于牵引负载的负二面体的机翼（10）包括柔性罩（12），其限定在两个侧端（14A，14B）之间，两个侧端（14A，14B）在前部通过前缘彼此连接，并且在 后方，尾随。 机翼（10）包括连接到设置在机翼的侧端（14A，14B）处的悬挂构件（30A，30B）的后线（40A，40B），并且辅助维护装置 推进中心区域（16）包括至少一条前端线，其一端连接到与前缘相邻的推进中心区域，并且能够在另一端连接到负载。 前线包括在分配在前缘的长度上的位置处施加到推进中心区域（16）的护罩线（90A，90B）的组件，至少一个滑动护罩线（90A，90B） 在与前缘固定接合的引导件（92A，92B）中滑动地滑动，滑动护罩线（90A，90B）的端部固定地连接到后线（40A，40B）。

    Life parachute especially for ultra-lightweight aircrafts
    77.
    发明申请
    Life parachute especially for ultra-lightweight aircrafts 有权
    生命降落伞，特别适用于超轻型飞机

    公开(公告)号：US20080191098A1

    公开(公告)日：2008-08-14

    申请号：US12010479

    申请日：2008-01-25

    申请人： Milan Babovka

    发明人： Milan Babovka

    IPC分类号： B64D17/02

    CPC分类号： B64C31/0285 ,  B64D17/18

    摘要： The gift of the solution of the life parachute for ultra-lightweight aircrafts or for lightweight aircrafts consists in that the canopy (1) of the parachute is fitted with the pole opening (4) at least some wedge-shaped section (3) of the canopy (1) are in the top half of its height fitted with a discharge valve (5) of the air situated in the inside space of the canopy (1) and a slider (9) is installed at suspension parachute cords (2). The slider (9) is formed in a ring fitted with a central opening (10) surrounded with netting (11) comprising at least in peripheral edges (23) of a local stiffener (12), wherein through openings (13) are formed for the suspension parachute cords (2). The dischrarge valves (5) are in the width of the single wedge-shaped sections (3) overlapped with parachute material (6) with a bottom open end (7). The discharge valves (5) of the air are formed either with loose vents (8) or the open end (7) of the parachute material (6). The slider (9) is, to advantage, in the form of a regular polygon composed of single tetrahedral parts (17) of the netting (11) which are connected one another through the local stiffeners (12) wherein the through openings (13) are for the suspension parachute cords (2).

    摘要翻译： 超轻型飞机或轻型飞机的救生艇解决方案的优点在于，降落伞的顶盖（1）装有极开口（4）至少一些楔形截面（3）， 顶篷（1）位于其高度的上半部，其顶部装有位于顶篷（1）的内部空间中的空气的排放阀（5），并且滑块（9）安装在悬挂的降落伞帘线（2）上。 所述滑动件（9）形成为环形，所述环装配有由网状物（11）包围的中心开口（10），该网状物（11）至少包括在局部加强筋（12）的周边边缘（23）中，其中形成通孔（13） 悬挂降落伞绳（2）。 排放阀（5）的宽度与单个楔形部分（3）的宽度相重叠，具有与底部开口端（7）的降落伞材料（6）。 空气的排放阀（5）由降落伞材料（6）的松动排气口（8）或开口端（7）形成。 滑块（9）有利地是由网状物（11）的单个四面体部分（17）组成的正多边形的形式，其通过局部加强筋（12）彼此连接，其中通孔（13） 用于悬挂降落伞绳（2）。

    Flexible reefing loops for parachutes
    78.
    发明申请
    Flexible reefing loops for parachutes 审中-公开
    降落伞灵活的回弹环

    公开(公告)号：US20070267547A1

    公开(公告)日：2007-11-22

    申请号：US11443846

    申请日：2006-05-22

    申请人： Elsa Hennings

    发明人： Elsa Hennings

    IPC分类号： B64D17/02

    CPC分类号： B64D17/343

    摘要： A reefing loop assembly which is attached to the skirt of a parachute canopy to secure a reefing loop to a parachute. The reefing loop assembly is fabricated from a flexible fabric to allow a parachute to be packed without damaging the parachute during packing.

    摘要翻译： 一个连接到降落伞顶部的裙部上的固定环组件，用于将降落环固定在降落伞上。 救生圈组件由柔性织物制成，以在包装期间使降落伞被包装而不损坏降落伞。

    Air foil having valve
    79.
    发明授权
    Air foil having valve 失效
    气阀具有阀门

    公开(公告)号：US5967463A

    公开(公告)日：1999-10-19

    申请号：US961898

    申请日：1997-10-31

    申请人： Loyd D. Payne

    发明人： Loyd D. Payne

    IPC分类号： B64C31/036 ,  B64D17/02

    CPC分类号： B64C31/036 ,  B64D17/025

    摘要： A canopy-type parachute is provided which includes improved stability features and lends itself to relatively easy assembly. Integral valves promote stability of the airfoil by not allowing rapid deflation of the airfoil, and their location and orientation within the airfoil promote structural rigidly of the overall airfoil, even out to the front top edge of the airfoil. The valves in one configuration bias against a vertical, loaded rib which tends to provide a consistent taut and planar surface for the valves to bias and act against.

    摘要翻译： 提供了一种天篷式降落伞，其包括改进的稳定性特征并且使其相对容易地组装。 积分阀通过不允许翼型的快速放气来促进机翼的稳定性，并且它们在翼型内的位置和定向促进了整个翼型的刚性结构，甚至促进翼型的前顶边缘。 一个结构中的阀门偏压垂直装载的肋条，倾向于为阀门提供一致的拉紧和平坦的表面，以使阀门偏置和起作用。

    Gliding decelerator including an assembly for improving the lift to drag ratio associated therewith
    80.
    发明授权
    Gliding decelerator including an assembly for improving the lift to drag ratio associated therewith 失效
    滑动减速器包括用于改善与之相关联的提升阻力比的组件

    公开(公告)号：US5303883A

    公开(公告)日：1994-04-19

    申请号：US94671

    申请日：1993-07-16

    申请人： John C. Brewer ,  James E. Sadeck

    发明人： John C. Brewer ,  James E. Sadeck

    IPC分类号： B64D17/02

    CPC分类号： B64D17/025

    摘要： A gliding decelerator and an assembly for use therein for improving the l to drag ratio associated therewith. In a preferred embodiment, the gliding decelerator includes a ram-air canopy shaped to include a plurality of half-cells, each half-cell having an open leading end and a closed tailing end. Inflatable bladders are secured within the respective half-cells of the canopy, the inflatable bladders being appropriately dimensioned so that, when inflated soon after the canopy has been opened, each bladder fills its respective half-cell in such a way as to stiffen the half-cell both along its length and at its open leading end. The inflatable bladders may be inflated simultaneously or in stages, the inflation means comprising a gas source, a flexible manifold connecting the gas source to the half-cells and valve means for controlling the output of the gas source. Control of the valve means may be automatic, e.g., a timer, a remote control unit, or may be controlled by a parachutist, e.g., completion of an electric circuit. The inflation means may be mounted within the wing-shaped canopy or may be externally mounted.

    摘要翻译： 滑行减速器和用于其中用于改善与其相关联的提升阻力比的组件。 在优选实施例中，滑行减速器包括形成为包括多个半电池的冲压空气罩，每个半电池具有开放的前端和封闭的尾端。 充气囊被固定在冠层的相应的半单元内，充气囊被适当地设定尺寸，使得当盖子打开后不久膨胀时，每个膀胱以这样的方式填充其相应的半单元，以使半 在其长度和开放的领先端。 充气气囊可以同时或分阶段地充气，充气装置包括气体源，将气体源连接到半电池的柔性歧管以及用于控制气体源的输出的阀装置。 阀门装置的控制可以是自动的，例如定时器，遥控单元，或者可以由飞行员控制，例如完成电路。 充气装置可以安装在翼形罩中或者可以从外部安装。