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    Breaking apart a platform upon pending collision
    12.
    发明授权
    Breaking apart a platform upon pending collision 有权

    公开(公告)号：US10207802B2

    公开(公告)日：2019-02-19

    申请号：US14757425

    申请日：2015-12-23

    Applicant: SPACE DATA CORPORATION

    Inventor： Gerald Mark Knoblach ,  Eric A Frische

    IPC: B64D1/02 ,  B64B1/40 ,  B64B1/42 ,  B64B1/50 ,  B64B1/70 ,  G08G5/04

    Abstract: A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

    BREAKING APART A PLATFORM UPON PENDING COLLISION
    16.
    发明申请
    BREAKING APART A PLATFORM UPON PENDING COLLISION 审中-公开
    打破一个平台在垂死的碰撞

    公开(公告)号：US20160214716A1

    公开(公告)日：2016-07-28

    申请号：US14757425

    申请日：2015-12-23

    Applicant: SPACE DATA CORPORATION

    Inventor： Gerald Mark KNOBLACH ,  Eric A. FRISCHE

    IPC: B64D1/02 ,  B64B1/50 ,  B64B1/70 ,  B64B1/42

    CPC classification number: B64D1/02 ,  B64B1/40 ,  B64B1/42 ,  B64B1/50 ,  B64B1/70 ,  G08G5/045

    Abstract: A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

    Abstract translation: 公开了一种用于分离和释放响应于高冲突概率的浮动平台的有效载荷的组成部分的方法和系统。 该方法包括：确定飞行中飞行器是否在至少与浮动平台相关联的安全区域内，其中所述浮动平台包括可释放地耦合的组件; 以及响应于确定所述飞行中飞行器至少在所述安全区域内的确定而启动释放机构，其中所述释放机构被配置为使所述组件部件脱离连接。

    Techniques for intelligent balloon/airship launch and recovery window location
    17.
    发明申请
    Techniques for intelligent balloon/airship launch and recovery window location 审中-公开
    智能气球/飞艇发射和恢复窗口位置的技术

    公开(公告)号：US20160196757A1

    公开(公告)日：2016-07-07

    申请号：US14757426

    申请日：2015-12-23

    Applicant: SPACE DATA CORPORATION

    Inventor： Gerald Mark Knoblach

    IPC: G08G5/04 ,  B64B1/40 ,  G08G5/00

    CPC classification number: G08G5/04 ,  B64B1/40 ,  G05D1/105 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/003 ,  G08G5/0034 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0082 ,  G08G5/045 ,  H04B7/18502

    Abstract: Devices, methods and systems for minimizing the probability of a collision between an aircraft and a floating platform are described. The device may include a processor in communication with a memory. The processor is configured to obtain a flight-path vector of an aircraft; determine a probability related to a plurality of flight-paths of a floating platform over a period of time based on operating parameters for the floating platform and weather data; and determine, based on the flight-path vector and the probability related to the plurality of flight-paths of the floating platform, a time and/or a location for launch or recovery of the floating platform that minimizes a probability of a collision between the aircraft and the floating platform while the floating platform is in flight.

    Abstract translation: 描述了用于最小化飞机和浮动平台之间的碰撞概率的装置，方法和系统。 该设备可以包括与存储器通信的处理器。 处理器被配置为获得飞机的飞行路径向量; 基于浮动平台和天气数据的操作参数，在一段时间内确定与浮动平台的多个飞行路径相关的概率; 并且基于飞行路线向量和与浮动平台的多个飞行路径相关的概率来确定用于启动或恢复浮动平台的时间和/或位置，其使得将所述浮动平台之间的碰撞概率最小化 飞机和浮动平台，而浮动平台正在飞行。

    MULTIFUNCTIONAL BALLOON MEMBRANE
    18.
    发明申请
    MULTIFUNCTIONAL BALLOON MEMBRANE 审中-公开
    多功能气球膜

    公开(公告)号：US20160185435A1

    公开(公告)日：2016-06-30

    申请号：US14983119

    申请日：2015-12-29

    Applicant: SPACE DATA CORPORATION

    Inventor： Gerald Mark KNOBLACH

    IPC: B64B1/58 ,  B64B1/40 ,  G01W1/08

    CPC classification number: B64B1/58 ,  B64B1/40 ,  B64B1/62 ,  G01W1/08

    Abstract: Disclosed herein is a lighter-than-air (LTA) device and method of making the same. In an embodiment, the LTA device may include a membrane having a flexible substrate and an active material disposed thereon, wherein the active material is configured to controllably change the surface area of at least a portion of the substrate when an electrical stimulus is applied to the active material.

    Abstract translation: 本文公开了一种轻型（LTA）装置及其制造方法。 在一个实施例中，LTA装置可以包括具有柔性基板和设置在其上的活性材料的膜，其中活性材料构造成当将电刺激施加到所述基板上时可控地改变至少一部分基板的表面积 活性物质

    BREAKING APART A PLATFORM UPON PENDING COLLISION
    19.
    发明申请
    BREAKING APART A PLATFORM UPON PENDING COLLISION 审中-公开

    公开(公告)号：US20200331609A1

    公开(公告)日：2020-10-22

    申请号：US16884799

    申请日：2020-05-27

    Applicant: SPACE DATA CORPORATION

    Inventor： Gerald M. Knoblach ,  Eric A. Frische

    IPC: B64D1/02 ,  B64B1/40 ,  B64B1/42 ,  B64B1/50 ,  B64B1/70

    Abstract: A method and system for separating and releasing component parts of a payload of a floating platform in response to a high collision probability is disclosed. The method includes, determining if an in-flight aircraft is within at least a safety zone associated with a floating platform, wherein the floating platform comprises releasably-coupled component parts; and activating, responsive to a determination that the in-flight aircraft is within at least the safety zone, a release mechanism, wherein the release mechanism is configured to uncouple the component parts.

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