SYSTEM AND METHOD FOR NETWORK SECURITY INCLUDING DETECTION OF MAN-IN-THE-BROWSER ATTACKS
    2.
    发明申请
    SYSTEM AND METHOD FOR NETWORK SECURITY INCLUDING DETECTION OF MAN-IN-THE-BROWSER ATTACKS 有权
    用于网络安全的系统和方法,包括检测人员在浏览器中的攻击

    公开(公告)号:US20110185421A1

    公开(公告)日:2011-07-28

    申请号:US13014668

    申请日:2011-01-26

    CPC classification number: H04L63/1425 G06F21/552 G06F21/554 H04L63/1416

    Abstract: A method is performed in a network security system implemented in a computer or electronic device that is coupled to secured online resources for detecting unauthorized accesses of those secured online resources. The method includes monitoring a user activity session. It is determined whether the user activity session is indicative of a hidden session by an attacker, where the determination includes comparing the user activity session to an average user activity session.

    Abstract translation: 在计算机或电子设备中实现的网络安全系统中执行一种方法,所述计算机或电子设备耦合到安全的在线资源,用于检测对这些安全的在线资源的未经授权的访问。 该方法包括监视用户活动会话。 确定用户活动会话是否指示攻击者的隐藏会话,其中确定包括将用户活动会话与一般用户活动会话进行比较。

    METHOD AND SYSTEM TO MONITOR A DIVERSE HETEROGENEOUS APPLICATION ENVIRONMENT
    3.
    发明申请
    METHOD AND SYSTEM TO MONITOR A DIVERSE HETEROGENEOUS APPLICATION ENVIRONMENT 有权
    监测多元异构应用环境的方法和系统

    公开(公告)号:US20110099430A1

    公开(公告)日:2011-04-28

    申请号:US12986877

    申请日:2011-01-07

    CPC classification number: G06F11/3495 G06F11/3447 G06F11/3476 G06F2201/87

    Abstract: A method to detect potential problems within a heterogeneous and diverse application environment. Operations data is received from a plurality of application servers within the application environment. The operations data pertains to operations performed at the plurality of application servers over a predetermined time interval. The operations data is aggregated. The aggregated data is compared to reference data, and a potential problem within the application environment is detected if the aggregated data deviates from the reference data in a predetermined manner.

    Abstract translation: 一种检测异构和多样化应用环境中的潜在问题的方法。 从应用环境中的多个应用服务器接收操作数据。 操作数据涉及在多个应用服务器上在预定时间间隔内执行的操作。 操作数据被聚合。 将聚合数据与参考数据进行比较,如果聚合数据以预定方式偏离参考数据,则检测应用环境内的潜在问题。

    Ferry Flight Engine Fairing Kit
    4.
    发明申请
    Ferry Flight Engine Fairing Kit 审中-公开
    渡轮飞行发动机整流套件

    公开(公告)号:US20100047077A1

    公开(公告)日:2010-02-25

    申请号:US11966165

    申请日:2007-12-28

    Abstract: A fairing kit for a gas turbine engine, where the engine has a core gas turbine engine, a fan rotor, and a plurality of external fan blades attached to the fan rotor and powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The fairing kit comprises: a) a fairing; b) a plurality of fasteners for securing the fairing to the core gas turbine engine; and c) a conformable seal for sealing mating surfaces of the fairing and the core gas turbine engine.

    Abstract translation: 一种用于燃气涡轮发动机的整流罩,其中发动机具有核心燃气涡轮发动机,风扇转子和附接到风扇转子并由核心燃气涡轮发动机供电的多个外部风扇叶片。 核心燃气涡轮发动机具有用于将一部分进入的气流引导到核心燃气涡轮发动机中的环形分配器。 整流罩包括:a)整流罩; b)用于将整流罩固定到核心燃气涡轮发动机的多个紧固件; 以及c)用于密封整流罩和核心燃气涡轮发动机的配合表面的适形密封件。

    Method of Preparing an Engine for Ferry Flight
    5.
    发明申请
    Method of Preparing an Engine for Ferry Flight 审中-公开
    准备飞机发动机的方法

    公开(公告)号:US20100043228A1

    公开(公告)日:2010-02-25

    申请号:US11966180

    申请日:2007-12-28

    Abstract: A method for preparing a gas turbine engine for a ferry flight, where the engine has a core gas turbine engine, a spinner, and a plurality of external fan blades powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The method comprises the steps of: a) removing the spinner; b) removing the fan blades; and c) securing a fairing in sealing engagement with the core gas turbine engine.

    Abstract translation: 一种制备用于渡轮飞行的燃气涡轮发动机的方法,其中发动机具有核心燃气涡轮发动机,旋转器和由核心燃气涡轮发动机供电的多个外部风扇叶片。 核心燃气涡轮发动机具有用于将一部分进入的气流引导到核心燃气涡轮发动机中的环形分配器。 该方法包括以下步骤:a)去除旋转器; b)拆下风扇叶片; 以及c)确保整流罩与所述核心燃气涡轮发动机的密封接合。

    LIQUID, EYE-INSTILLABLE PREPARATIONS COMPRISING SODIUM HYALURONATE
    6.
    发明申请
    LIQUID, EYE-INSTILLABLE PREPARATIONS COMPRISING SODIUM HYALURONATE 审中-公开
    液体,包含高锰酸钠的眼科制剂

    公开(公告)号:US20100022472A1

    公开(公告)日:2010-01-28

    申请号:US12573536

    申请日:2009-10-05

    CPC classification number: A61K9/0048 A61K31/728 A61K31/737

    Abstract: A liquid, eye-instillable preparation comprises a viscosity-enhancing agent comprised of one or both of sodium hyaluronate and chondroitin sulphate, a preservative comprised of polyhexanide, and one or more carriers in which the agent and the preservative are dispersed.

    Abstract translation: 液体,滴眼液制剂包括由透明质酸钠和硫酸软骨素之一或两者组成的粘度增强剂,由聚己酰胺组成的防腐剂和其中分散有试剂和防腐剂的一种或多种载体。

    METHOD AND SYSTEM TO MONITOR A DIVERSE HETEROGENEOUS APPLICATION ENVIRONMENT
    7.
    发明申请
    METHOD AND SYSTEM TO MONITOR A DIVERSE HETEROGENEOUS APPLICATION ENVIRONMENT 有权
    监测多元异构应用环境的方法和系统

    公开(公告)号:US20090228741A1

    公开(公告)日:2009-09-10

    申请号:US12414543

    申请日:2009-03-30

    CPC classification number: G06F11/3495 G06F11/3447 G06F11/3476 G06F2201/87

    Abstract: A method to detect potential problems within a heterogeneous and diverse application environment. Operations data is received from a plurality of application servers within the application environment. The operations data pertains to operations performed at the plurality of application servers over a predetermined time interval. The operations data is aggregated. The aggregated data is compared to reference data, and a potential problem within the application environment is detected if the aggregated data deviates from the reference data in a predetermined manner.

    Abstract translation: 一种检测异构和多样化应用环境中的潜在问题的方法。 从应用环境中的多个应用服务器接收操作数据。 操作数据涉及在多个应用服务器上在预定时间间隔内执行的操作。 操作数据被聚合。 将聚合数据与参考数据进行比较,如果聚合数据以预定方式偏离参考数据,则检测应用环境内的潜在问题。

    Athletic hammock
    8.
    发明授权
    Athletic hammock 失效
    运动吊床

    公开(公告)号:US07578009B1

    公开(公告)日:2009-08-25

    申请号:US11904818

    申请日:2007-09-28

    CPC classification number: A41D1/08 A41B9/023

    Abstract: A pair of men s shorts, including under shorts, has a typical chassis with an abdomen opening, a right pant leg and a left pant leg. The user's genitals pass through an opening on the front of the chassis whenever the shorts are being worn. A hammock overlies the opening and is anchored to the chassis at two points on the right out seam, one point below the other, and two points on the left out seam, symmetrical with the right out seam attachment. The hammock is also attached to the chassis at the waist band and at the lower edge of the opening just above the left and right inseam joinder area. The hammock by being anchored at the out seams and being non-stretching in a transverse direction, acts as a sling in supporting the genitals of the user.

    Abstract translation: 一双男子短裤,包括短裤,有一个典型的底盘,腹部开口,右裤腿和左裤腿。 当短裤穿着时,用户的生殖器通过底盘前面的开口。 吊床位于开口处,并在右侧出口处的两个点上锚固到底盘,另一个点在另一个位置,左侧两个接缝处的两个点与右侧接缝附件对称。 吊床也附着在腰带的底盘上,并且位于开口的下边缘,正好在左侧和右侧的接合区域中。 吊床通过锚定在接缝处并且在横向上不拉伸,起到支撑使用者生殖器的吊带的作用。

    Trim panel including integrally formed members
    9.
    发明授权
    Trim panel including integrally formed members 有权
    修剪面板包括一体形成的构件

    公开(公告)号:US07559598B2

    公开(公告)日:2009-07-14

    申请号:US11189674

    申请日:2005-07-26

    Abstract: A trim panel (10) includes at least one integrally-formed first member (12) and at least one integrally-formed second member (14) extend from an outboard surface (16) of the trim panel (10). The at least one integrally-formed first member (12) engages an inboard surface (42) of a barrier (36) to push the barrier (36) in an outboard direction. The at least one integrally-formed second member (14) extends through an opening or perforation (40) of the barrier (36) to retain the barrier (36) to the trim panel (10). The barrier (36) may be a water/acoustic ingression barrier (36). The at least one integrally-formed first member (12) causes an adhesive bead (44) arranged on an outboard surface (46) of the barrier (36) to positively engage an inboard surface (48) of an inner door panel (38). The at least one integrally-formed second member (14) extends through an opening or perforation (40) of the barrier (36) to retain the barrier (36) with the interior door trim panel (10).

    Abstract translation: 装饰板(10)包括至少一个整体形成的第一构件(12),并且至少一个整体形成的第二构件(14)从装饰板(10)的外侧表面(16)延伸。 所述至少一个整体形成的第一构件(12)接合屏障(36)的内侧表面(42),以沿外侧方向推动所述屏障(36)。 至少一个整体形成的第二构件(14)延伸穿过阻挡件(36)的开口或穿孔(40),以将阻挡件(36)保持到修剪面板(10)。 屏障(36)可以是水/声入侵屏障(36)。 所述至少一个整体形成的第一构件(12)使得布置在所述屏障(36)的外侧表面(46)上的粘合剂珠(44)能够与内门板(38)的内侧表面(48) 。 所述至少一个整体形成的第二构件(14)延伸穿过所述屏障(36)的开口或穿孔(40),以将所述屏障(36)与所述内门装饰板(10)保持在一起。

    AIRCRAFT COMPONENT
    10.
    发明申请
    AIRCRAFT COMPONENT 有权
    飞机组件

    公开(公告)号:US20080087768A1

    公开(公告)日:2008-04-17

    申请号:US11762342

    申请日:2007-06-13

    Applicant: James LLOYD

    Inventor: James LLOYD

    CPC classification number: B64C1/064 B64C1/065

    Abstract: This invention relates to improving the tolerance of composite laminate structures to damage and/or delamination, resulting in weakening of the structure and/or to reducing the possibility of such damage and/or delamination. In particular, but not exclusively the invention relates to protecting the end surfaces of composite laminate structures present on aircraft from impact damage. The invention provides aircraft component comprising a composite laminate structure, the composite laminate structure including an end surface at which a multiplicity of the layers of the laminate structure terminate, wherein the aircraft component further comprises a deflecting surface mounted to the composite laminate structure for protecting the end surface from direct impacts. In one embodiment, the end surface of the composite laminate structure has a convex cross-section and the deflecting surface comprises laminate material laid over the end surface. In a further embodiment, the deflecting surface comprises an inert strip.

    Abstract translation: 本发明涉及改善复合层压结构损坏和/或分层的公差,导致结构变薄和/或降低这种损坏和/或分层的可能性。 特别地但并非排他性地,本发明涉及保护飞机上存在的复合层压结构的端面免受冲击损坏。 本发明提供了包括复合层压结构的飞行器部件,复合层压结构包括端面,层叠结构的多个层终止于该端面,其中飞行器部件还包括安装到复合层压结构的偏转表面,用于保护 端面受到直接冲击。 在一个实施例中,复合层压结构的端面具有凸的横截面,并且偏转表面包括铺设在端表面上的层压材料。 在另一实施例中,偏转表面包括惰性条带。

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