Ducted fan air vehicle with deployable wings
    1.
    发明授权
    Ducted fan air vehicle with deployable wings 失效
    带有可展翅膀的风扇飞机

    公开(公告)号:US07681832B2

    公开(公告)日:2010-03-23

    申请号:US11947585

    申请日:2007-11-29

    Abstract: A ducted fan air vehicle and method of operation is disclosed for obtaining aerodynamic lift and efficiency in forward flight operation without significantly impacting hover stability. One or more retractable wings are included on the ducted fan air vehicle and are deployed during forward flight to provide aerodynamic lift. The wing or wings are retracted when the vehicle hovers to reduce the impact the wings have on stability in a wind. Each wing may conform to the curvature or profile of the vehicle when retracted, and may be constructed in one or more wing sections. The wing or wings may be deployed and retracted automatically or at the command of an operator. Each wing and related components may be integrated into the vehicle or may be detachable.

    Abstract translation: 公开了一种管道风扇空气动力车辆和操作方法,用于在前进飞行操作中获得空气动力学提升和效率,而不会显着影响悬停稳定性。 一个或多个伸缩翼包括在管道式风扇飞行器上,并且在向前飞行期间部署以提供空气动力学提升。 当车辆悬停时,翼或翼缩回,以减少翼对风中的稳定性的影响。 每个翼可以在缩回时符合车辆的曲率或轮廓,并且可以构造在一个或多个翼部中。 机翼或机翼可以自动部署和撤回,或者在操作员的指令下进行。 每个翼和相关部件可以集成到车辆中或者可以是可拆卸的。

    SYNTHETIC INSTRUMENT LANDING SYSTEM
    2.
    发明申请
    SYNTHETIC INSTRUMENT LANDING SYSTEM 有权
    合成仪器着陆系统

    公开(公告)号:US20080319592A1

    公开(公告)日:2008-12-25

    申请号:US11765783

    申请日:2007-06-20

    CPC classification number: G05D1/0684

    Abstract: Systems and methods for generating approach information for a first vehicle approaching a second dynamic vehicle. An example method determines motion information of the second vehicle and generates approach information based on the determined motion information and the approach centerline. The method generates at least one of an approach path or a plurality of approach path reference points based on at least one of a center of motion of the second vehicle or a touchdown point on the second vehicle and generates at least one of a synthetic path or a plurality of synthetic path reference points by filtering the generated at least one approach path or plurality of approach path reference points.

    Abstract translation: 用于生成接近第二动态车辆的第一车辆的方法信息的系统和方法。 示例性方法确定第二车辆的运动信息,并且基于所确定的运动信息和接近中心线来生成方法信息。 该方法基于第二车辆的运动中心或第二车辆上的着陆点中的至少一个产生进场路径或多个进场路径参考点中的至少一个,并且生成合成路径或 多个合成路径参考点,通过对生成的至少一个进场路径或多个进场路径参考点进行过滤。

    Synthetic instrument landing system
    3.
    发明授权
    Synthetic instrument landing system 有权
    合成仪器着陆系统

    公开(公告)号:US08234021B2

    公开(公告)日:2012-07-31

    申请号:US11765783

    申请日:2007-06-20

    CPC classification number: G05D1/0684

    Abstract: Systems and methods for generating approach information for a first vehicle approaching a second dynamic vehicle. An example method determines motion information of the second vehicle and generates approach information based on the determined motion information and the approach centerline. The method generates at least one of an approach path or a plurality of approach path reference points based on at least one of a center of motion of the second vehicle or a touchdown point on the second vehicle and generates at least one of a synthetic path or a plurality of synthetic path reference points by filtering the generated at least one approach path or plurality of approach path reference points.

    Abstract translation: 用于生成接近第二动态车辆的第一车辆的方法信息的系统和方法。 示例性方法确定第二车辆的运动信息,并且基于所确定的运动信息和接近中心线来生成方法信息。 该方法基于第二车辆的运动中心或第二车辆上的着陆点中的至少一个产生进场路径或多个进场路径参考点中的至少一个,并且生成合成路径或 多个合成路径参考点,通过对生成的至少一个进场路径或多个进场路径参考点进行过滤。

    Recursive structure for diagnostic model
    4.
    发明授权
    Recursive structure for diagnostic model 有权
    诊断模型的递归结构

    公开(公告)号:US08170968B2

    公开(公告)日:2012-05-01

    申请号:US12192700

    申请日:2008-08-15

    CPC classification number: G06N5/02 G05B23/0251

    Abstract: A recursive mapping structure for diagnostic models is provided. A parent diagnostic model includes a first input module, a first output module, a first monitor module coupled to the first input and first output modules, and a first propagation module coupled between the first input and first output modules. A child diagnostic model includes a second input module, a second output module, a second monitor module coupled to the second input and second output modules, and a second propagation module coupled between the second input and second output modules, wherein the second monitor module is coupled to the first monitor module.

    Abstract translation: 提供了诊断模型的递归映射结构。 父诊断模型包括耦合到第一输入和第一输出模块的第一输入模块,第一输出模块,第一监控模块以及耦合在第一输入模块和第一输出模块之间的第一传播模块。 儿童诊断模型包括第二输入模块,第二输出模块,耦合到第二输入和第二输出模块的第二监测模块,以及耦合在第二输入模块和第二输出模块之间的第二传播模块,其中第二监测模块是 耦合到第一监视器模块。

    RECURSIVE STRUCTURE FOR DIAGNOSTIC MODEL
    5.
    发明申请
    RECURSIVE STRUCTURE FOR DIAGNOSTIC MODEL 有权
    诊断模型的回归结构

    公开(公告)号:US20100042872A1

    公开(公告)日:2010-02-18

    申请号:US12192700

    申请日:2008-08-15

    CPC classification number: G06N5/02 G05B23/0251

    Abstract: A recursive mapping structure for diagnostic models is provided. A parent diagnostic model includes a first input module, a first output module, a first monitor module coupled to the first input and first output modules, and a first propagation module coupled between the first input and first output modules. A child diagnostic model includes a second input module, a second output module, a second monitor module coupled to the second input and second output modules, and a second propagation module coupled between the second input and second output modules, wherein the second monitor module is coupled to the first monitor module.

    Abstract translation: 提供了诊断模型的递归映射结构。 父诊断模型包括耦合到第一输入和第一输出模块的第一输入模块,第一输出模块,第一监控模块以及耦合在第一输入模块和第一输出模块之间的第一传播模块。 儿童诊断模型包括第二输入模块,第二输出模块,耦合到第二输入和第二输出模块的第二监测模块,以及耦合在第二输入模块和第二输出模块之间的第二传播模块,其中第二监测模块是 耦合到第一监视器模块。

    DISTRIBUTED DECISION MAKING ARCHITECTURE FOR EMBEDDED PROGNOSTICS
    6.
    发明申请
    DISTRIBUTED DECISION MAKING ARCHITECTURE FOR EMBEDDED PROGNOSTICS 审中-公开
    嵌入式预防措施的分布式决策制定

    公开(公告)号:US20100042366A1

    公开(公告)日:2010-02-18

    申请号:US12192665

    申请日:2008-08-15

    CPC classification number: G06F11/008 G05B23/0283 G06F11/3013 G06F11/3072

    Abstract: A distributed decision making architecture for embedded prognostics in a platform is provided. An estimation system determines at least one performance characteristic of at least one device in the platform. A supervisory system is in communication with, and superior to, the estimation system. The supervisory system calculates a prediction of remaining useful life (RUL) of the at least one device in the platform. The supervisory system is adapted for collecting the at least one performance characteristic from the estimation system to generate a performance estimate, and implementing at least one data-driven equation to match the at least one performance estimate against of at least one known degradation condition to generate the prediction of remaining useful life of the at least one device.

    Abstract translation: 提供了平台中嵌入式预测的分布式决策架构。 估计系统确定平台中的至少一个设备的至少一个性能特征。 监督系统与评估系统通信并优于估计系统。 监控系统计算平台中至少一个设备的剩余使用寿命(RUL)的预测。 所述监控系统适于从所述估计系统收集所述至少一个性能特征以产生性能估计,以及实施至少一个数据驱动方程以将所述至少一个性能估计与至少一个已知的降级条件相匹配以产生 预测所述至少一个设备的剩余使用寿命。

    Ducted Fan Air Vehicle with Deployable Wings
    7.
    发明申请
    Ducted Fan Air Vehicle with Deployable Wings 失效
    具有可部署翅膀的风扇飞机

    公开(公告)号:US20080272226A1

    公开(公告)日:2008-11-06

    申请号:US11947585

    申请日:2007-11-29

    Abstract: A ducted fan air vehicle and method of operation is disclosed for obtaining aerodynamic lift and efficiency in forward flight operation without significantly impacting hover stability. One or more retractable wings are included on the ducted fan air vehicle and are deployed during forward flight to provide aerodynamic lift. The wing or wings are retracted when the vehicle hovers to reduce the impact the wings have on stability in a wind. Each wing may conform to the curvature or profile of the vehicle when retracted, and may be constructed in one or more wing sections. The wing or wings may be deployed and retracted automatically or at the command of an operator. Each wing and related components may be integrated into the vehicle or may be detachable.

    Abstract translation: 公开了一种管道风扇空气动力车辆和操作方法,用于在前进飞行操作中获得空气动力学提升和效率,而不会显着影响悬停稳定性。 一个或多个伸缩翼包括在管道式风扇飞行器上,并且在向前飞行期间部署以提供空气动力学提升。 当车辆悬停时,翼或翼缩回,以减少翼对风中的稳定性的影响。 每个翼可以在缩回时符合车辆的曲率或轮廓,并且可以构造在一个或多个翼部中。 机翼或机翼可以自动部署和撤回,或者在操作员的指令下进行。 每个翼和相关部件可以集成到车辆中或者可以是可拆卸的。

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