COMPRESSION MOUNTED WINDOW ASSEMBLY
    1.
    发明公开

    公开(公告)号:EP3611098A2

    公开(公告)日:2020-02-19

    申请号:EP19173139.7

    申请日:2011-08-26

    Abstract: A compression mounted window assembly (100) is disclosed that includes a circular window having opposed front and rear planar surfaces and an outer periphery having forward and rearward chamfered edge surfaces (116,118), a compressible gasket circumscribing the outer periphery of the window, a housing with a portal having an annular seat for accommodating the window circumscribed by the gasket (125), wherein the annular seat has a first chamfered abutment surface corresponding to the forward chamfered edge surface of the window, an annular bezel (130) operatively associated with the housing for compressively retaining the window assembly (100) within the annular seat of the portal (14), and structure for securing the bezel to the housing, wherein the bezel (130) has a second chamfered abutment surface corresponding to the rearward chamfered edge surface of the window.

    TOOL-LESS LOW PROFILE ROTATION MOUNT
    2.
    发明公开
    TOOL-LESS LOW PROFILE ROTATION MOUNT 有权
    WERKZEUGLOSES DREHLAGER MIT NIEDRIGEM PROFIL

    公开(公告)号:EP3115674A1

    公开(公告)日:2017-01-11

    申请号:EP16175266.2

    申请日:2016-06-20

    Abstract: A mount includes a keyed insert and a key receiver (32). The keyed insert includes a key base (34) and a keyed plate (36) mounted to the key base (34) and having one or more key features (56a-56c) extending from a periphery of the keyed plate (36). The key receiver (32) accepts the keyed insert and includes a receiver base (50), a retaining ring (40), a key set ring (44), a key entrance ring (42), and a spring plate (46). The retaining ring (40) is connected to the receiver base (50). The key set ring (44) is disposed between the retaining ring (40) and the receiver base (50) and includes one or more receiving notches (62a-62c) and one or more locking notches (64a-64c). The one or more receiving notches (62a-62c) is configured to receive the one or more key features (56a-56c) the one or more locking notch (64a-64c) is spaced away from the one or more receiving notch (62a-62c) and is configured to lockingly engage the one or more key features (56a-56c).

    Abstract translation: 安装座包括一个带键的插入件和一个钥匙接收器(32)。 所述带键插入件包括安装到所述键座(34)上并具有从所述键盘(36)的周边延伸的一个或多个键特征(56a-56c)的键座(34)和键盘(36)。 钥匙接收器(32)接受带键的插入件并包括接收器底座(50),保持环(40),钥匙圈(44),钥匙入口环(42)和弹簧板(46)。 保持环(40)连接到接收器基座(50)。 钥匙圈(44)设置在保持环(40)和接收器基座(50)之间,并且包括一个或多个接收槽口(62a-62c)和一个或多个锁定槽口(64a-64c)。 一个或多个接收凹口(62a-62c)被配置为接收一个或多个锁定凹口(64a-64c)与一个或多个接收凹口(62a-64c)间隔开的一个或多个键特征(56a-56c) 62c)并且被配置成锁定地接合所述一个或多个键特征(56a-56c)。

    COMPRESSION MOUNTED WINDOW ASSEMBLY
    3.
    发明公开

    公开(公告)号:EP3611098A3

    公开(公告)日:2020-08-12

    申请号:EP19173139.7

    申请日:2011-08-26

    Abstract: A compression mounted window assembly (100) is disclosed that includes a circular window having opposed front and rear planar surfaces and an outer periphery having forward and rearward chamfered edge surfaces (116,118), a compressible gasket circumscribing the outer periphery of the window, a housing with a portal having an annular seat for accommodating the window circumscribed by the gasket (125), wherein the annular seat has a first chamfered abutment surface corresponding to the forward chamfered edge surface of the window, an annular bezel (130) operatively associated with the housing for compressively retaining the window assembly (100) within the annular seat of the portal (14), and structure for securing the bezel to the housing, wherein the bezel (130) has a second chamfered abutment surface corresponding to the rearward chamfered edge surface of the window.

    SYSTEM AND METHOD FOR AIRCRAFT CAMERA IMAGE ALIGNMENT
    5.
    发明公开
    SYSTEM AND METHOD FOR AIRCRAFT CAMERA IMAGE ALIGNMENT 审中-公开
    用于飞机相机图像对准的系统和方法

    公开(公告)号:EP3312823A1

    公开(公告)日:2018-04-25

    申请号:EP17197560.0

    申请日:2017-10-20

    Abstract: An alignment system for images produced by cameras externally mounted on an aircraft (10) includes a visual display (56) positioned at a first location in the aircraft (10) (such as a flight deck) and an alignment device (54) positioned at a second location in the aircraft (10) (such as an electronics bay). The visual display (56) displays images provided by the cameras (46, 48, 50, 52). The alignment device (54) includes a user interface, which includes user inputs for selecting one of the cameras and for aligning an image from the camera selected on the visual display (56), a depiction of an aircraft (10), and indicators (82, 84, 86, 88) positioned adjacent the depiction. Each of the indicators (82, 84, 86, 88) represents selection of one of the cameras for aligning the image from that camera on the visual display.

    Abstract translation: 由外部安装在飞机(10)上的摄像机产生的图像的对准系统包括定位在飞机(10)中的第一位置(例如驾驶舱)上的视觉显示器(56)和定位在 飞机(10)中的第二个位置(例如电子设备舱)。 视觉显示器(56)显示由照相机(46,48,50,52)提供的图像。 对准装置(54)包括用户界面,该用户界面包括用于选择照相机中的一个并且用于对准在视觉显示器(56)上选择的来自照相机的图像的用户输入,飞机(10)的描绘以及指示器 82,84,86,88)定位在描绘附近。 每个指示器(82,84,86,88)表示选择用于在视觉显示器上对准来自该照相机的图像的一个照相机。

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