AIR GUIDING MEANS FOR A DISPENSER
    81.
    发明申请
    AIR GUIDING MEANS FOR A DISPENSER 有权
    空气导向装置

    公开(公告)号:US20120091278A1

    公开(公告)日:2012-04-19

    申请号:US13377299

    申请日:2009-06-11

    CPC classification number: F42B5/155 F42B4/26 F42B10/38 F42B12/62 F42B12/70

    Abstract: An air guide for a dispenser. At least one air scoop is configured to guide an air stream to a feeding out opening for chaffs on the dispenser in order to facilitate packages of chaffs to be released from the dispenser. A control unit is configured to control the air stream through the at least one air scoop.

    Abstract translation: 一个分配器的导航器。 至少一个空气铲斗构造成将空气流引导到分配器上的谷壳的送出开口,以便于将包装盒从分配器中释放出来。 控制单元构造成通过至少一个空气勺来控制空气流。

    Recoil dampening mechanism
    82.
    发明授权
    Recoil dampening mechanism 有权
    回油阻尼机构

    公开(公告)号:US08099892B1

    公开(公告)日:2012-01-24

    申请号:US12470575

    申请日:2009-05-22

    CPC classification number: F41A1/08 F41A25/14 F41F3/042

    Abstract: The invention concerns a recoilless weapon (1) comprising a launch tube (3) for launching a projectile and a recoil dampener (2) for dampening recoil forces from the projectile, characterized in that the recoil dampener (2) comprises at least two recoil dampening mechanisms (8) comprising dampening means (11, 13, 14, 15) and that the recoil dampener (2) is adjustable in regard to a gunner and/or to projectile.

    Abstract translation: 本发明涉及一种无后坐力武器(1),其包括用于发射射弹的发射管(3)和用于衰减来自射弹的反冲力的反冲阻尼器(2),其特征在于,反冲阻尼器(2)包括至少两个反冲阻尼 机构(8)包括阻尼装置(11,13,14,15),并且反冲阻尼器(2)可针对枪手和/或射弹进行调节。

    CABLE CONNECTION SYSTEM FOR UNDERWATER VEHICLE
    83.
    发明申请
    CABLE CONNECTION SYSTEM FOR UNDERWATER VEHICLE 有权
    用于水下车辆的电缆连接系统

    公开(公告)号:US20120006245A1

    公开(公告)日:2012-01-12

    申请号:US13145818

    申请日:2009-01-22

    Applicant: Lars Lundberg

    Inventor: Lars Lundberg

    CPC classification number: B63G8/001 B63B27/36 B63G2008/007

    Abstract: A system for interconnecting a mother ship with a submersible vehicle using a cable towed by the mother ship. The cable has a first cable end connected to the mother ship and a second cable end to be connected to the submersible vehicle. The second cable end is provided with a first connector. A capturing mast is arranged at the submersible vehicle for capturing the cable towed by the mother ship. A connector holder is arranged at the submersible vehicle for holding the first connector when it is to be connected to a second connector. The second connector is connected to the submersible vehicle. A first guide is arranged at the submersible vehicle for guiding the first connector towards the connector holder of the submersible vehicle. A second guide turns the connector to a well defined position into the connector holder.

    Abstract translation: 使用由母舰牵引的电缆将母舰与潜水车辆互连的系统。 电缆具有连接到母船的第一电缆端和要连接到潜水车辆的第二电缆端。 第二电缆端设置有第一连接器。 在潜水车辆处设置有捕获桅杆,用于捕获由母舰拖曳的缆索。 连接器支架设置在潜水车辆处,用于在要连接到第二连接器时保持第一连接器。 第二连接器连接到潜水车辆。 第一引导件布置在潜水车辆处,用于将第一连接器引向潜水车辆的连接器保持器。 第二个引导件将连接器转换成连接器固定器的良好定位位置。

    Cooling of avionics using a fuel tank and refrigerant source
    84.
    发明授权
    Cooling of avionics using a fuel tank and refrigerant source 有权
    使用燃料箱和制冷剂源冷却航空电子设备

    公开(公告)号:US08042343B2

    公开(公告)日:2011-10-25

    申请号:US11902729

    申请日:2007-09-25

    Abstract: An avionics cooling system including an avionics cooling circuit operating with a liquid coolant; a fuel circuit; and a vapor cooling cycle operating with a refrigerant. The avionics cooling circuit transfers heat withdrawn from avionics to the fuel circuit, whereby the heat is dumped into fuel, and the vapor cooling cycle transfers heat that cannot be dumped into the fuel from the fuel circuit to ram air.

    Abstract translation: 一种航空电子冷却系统,包括用液体冷却剂操作的航空电子冷却回路; 燃料电路; 以及用制冷剂操作的蒸气冷却循环。 航空电子设备冷却回路将从航空电子设备引出的热量转移到燃料回路,从而将热量转移到燃料中,并且蒸气冷却循环将不能从燃料回路转移到燃料中的热量传递给冲压空气。

    CARTRIDGE CASE AND A ROUND COMPRISING SUCH A CARTRIDGE CASE
    85.
    发明申请
    CARTRIDGE CASE AND A ROUND COMPRISING SUCH A CARTRIDGE CASE 有权
    盒子盒和包围这样的盒子的圆环

    公开(公告)号:US20110192313A1

    公开(公告)日:2011-08-11

    申请号:US13123264

    申请日:2008-10-10

    CPC classification number: F42B39/20 F42B5/285 F42B5/307

    Abstract: A cartridge case intended for explosive materials. A releasable base plate is provided in a bottom section of the cartridge case. A base plate locking device includes a temperature dependent shape memory material. The shape memory material of the base plate locking device is provided to exert a crushing force on the cartridge case at a temperature increase passing a temperature such that the shape memory material in question struggles to resume a former shape in order to break up the connection between the base plate and the bottom section of the cartridge case and release the base plate from the bottom section of the cartridge case. A round of ammunition includes the cartridge case.

    Abstract translation: 用于爆炸性材料的墨盒盒。 在盒壳体的底部设置有可释放的基板。 基板锁定装置包括温度依赖形状记忆材料。 基板锁定装置的形状记忆材料被设置成在通过温度的温度升高的情况下在盒壳体上施加破碎力,使得所讨论的形状记忆材料难以恢复前一形状,以便破坏 底座和盒壳体的底部部分,并将底板从盒壳体的底部部分释放。 一轮弹药包括墨盒盒。

    Support Structure for a Screen
    86.
    发明申请
    Support Structure for a Screen 审中-公开
    支持屏幕的结构

    公开(公告)号:US20110155983A1

    公开(公告)日:2011-06-30

    申请号:US11663916

    申请日:2005-09-27

    Applicant: Tom Westcott

    Inventor: Tom Westcott

    CPC classification number: E01F13/028

    Abstract: An elongate support member for use in a support structure for a screen made from flexible screen material. The support member is adapted to receive one or more elongate rolls of the screen material. The support member is a visually impenetrable beam whose sectional configuration defines an open W-shaped or M-shaped profile.

    Abstract translation: 一种用于由柔性筛网材料制成的筛网的支撑结构的细长支撑构件。 支撑构件适于接收屏幕材料的一个或多个细长辊。 支撑构件是视觉上不可穿透的梁,其横截面形状限定开放的W形或M形轮廓。

    Method, computer program and device for determining the risk of midair collision
    87.
    发明授权
    Method, computer program and device for determining the risk of midair collision 有权
    用于确定空中碰撞风险的方法,计算机程序和装置

    公开(公告)号:US07969289B2

    公开(公告)日:2011-06-28

    申请号:US12210806

    申请日:2008-09-15

    Abstract: A method for determining the probability of a vehicle colliding with a detected object. The object is detected. A stochastic process is determined representing a relative distance between the vehicle and the detected object. The stochastic process has a direction and a velocity relative the vehicle. A safety zone of the vehicle is defined in relation to the detected object as a straight line perpendicular to a line of sight of the detected object. The probability of colliding with the detected object over a period of time is determined as the probability of the stochastic process crossing the straight line with the direction and velocity of the stochastic process.

    Abstract translation: 一种用于确定车辆与检测到的物体碰撞的概率的方法。 检测到物体。 确定代表车辆和检测到的物体之间的相对距离的随机过程。 随机过程相对于车辆具有方向和速度。 车辆的安全区域相对于检测对象被定义为垂直于被检测物体的视线的直线。 随着随机过程与随机过程的方向和速度相交的直线的概率被确定为在一段时间内与被检测物体碰撞的概率。

    VALIDITY CHECK OF VEHICLE POSITION INFORMATION TRANSMITTED OVER A TIME-SYNCHRONIZED DATA LINK
    88.
    发明申请
    VALIDITY CHECK OF VEHICLE POSITION INFORMATION TRANSMITTED OVER A TIME-SYNCHRONIZED DATA LINK 审中-公开
    通过时间同步数据链路传输的车辆位置信息的有效性检查

    公开(公告)号:US20110140950A1

    公开(公告)日:2011-06-16

    申请号:US13000077

    申请日:2009-06-08

    Inventor: Svante Andersson

    CPC classification number: G01S13/765 G01S5/0072 G01S13/9303 G01S2205/003

    Abstract: A method for validating positional data in vehicle surveillance applications wherein vehicles transmit positional data indicating their own position to surrounding vehicles using a data link over which a transmission is initiated at a given transmission point in time that is known by all users of the data link. A signal transmitted from a radio source over the data link is received at a receiving unit. The signal carries positional data indicating an alleged position of a vehicle. The distance between the receiving unit and the radio source is estimated based on the time of flight and the propagation velocity of the received signal. The time of flight is determined based on the time elapsed from the transmission point in time of the signal to the time of reception of at least a first part of the signal. A deviation value is determined. The deviation value indicates the difference between the distance to the position of a vehicle according to the received positional data and the estimated distance to the radio source.

    Abstract translation: 一种用于验证车辆监视应用中的位置数据的方法,其中车辆使用在数据链路的所有用户已知的给定传输点发起传输的数据链路向周围车辆发送指示他们自己的位置的位置数据。 在接收单元处接收通过数据链路从无线电源发送的信号。 该信号携带指示车辆所指位置的位置数据。 基于飞行时间和接收信号的传播速度来估计接收单元和无线电源之间的距离。 基于从信号的发送点到接收信号的至少第一部分所经过的时间来确定飞行时间。 确定偏差值。 偏差值表示根据接收到的位置数据与车辆位置的距离与到无线电源的估计距离之间的差。

    Launch tube protective cover
    89.
    发明授权
    Launch tube protective cover 有权
    发射管保护罩

    公开(公告)号:US07954412B2

    公开(公告)日:2011-06-07

    申请号:US12271419

    申请日:2008-11-14

    Applicant: Åke Jansson

    Inventor: Åke Jansson

    CPC classification number: F41F3/077

    Abstract: A launch tube protective cover for mounting to a launch tube including a projectile. The launch tube protective cover is arranged for protecting the interior of the launch tube from external environment. The launch tube protective cover includes a flexible rippable vapor barrier faced towards the projectile and circumferentially attached to the launch tube.

    Abstract translation: 发射管保护盖,用于安装到包括射弹的发射管。 发射管保护盖布置用于保护发射管的内部免受外部环境的影响。 发射管保护盖包括面向射弹的柔性可撕开的蒸气屏障,并且周向地附接到发射管。

    Termination secured route planning
    90.
    发明授权
    Termination secured route planning 有权
    终止安全路线规划

    公开(公告)号:US07937191B2

    公开(公告)日:2011-05-03

    申请号:US11822037

    申请日:2007-07-02

    CPC classification number: G05D1/105

    Abstract: A method of forming a safe termination operation volume, and an aircraft provided with a system using such a volume to plan a flight route and/or an emergency route. The volume indicates the lowest allowable flight altitude to achieve a glide path of a vehicle to a termination point of an area of interest, wherein non allowable fly zones are taken into consideration by adding flight altitude to come around the non allowable fly zones when calculating the lowest allowable flight altitude.

    Abstract translation: 一种形成安全终端操作体积的方法,以及设置有使用这种体积的系统来规划飞行路线和/或紧急路线的飞机。 体积表示实现车辆到感兴趣区域的终点的滑行路径的最低允许飞行高度,其中通过在计算不允许飞行高度时加上飞行高度来考虑非允许飞行区域 最低允许飞行高度。

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