CABIN WINDOW WITH PLANNED DEFORMATION, METHOD OF MANUFACTURING SUCH A WINDOW AND AIRCRAFT COMPRISING SUCH A WINDOW
    1.
    发明申请
    CABIN WINDOW WITH PLANNED DEFORMATION, METHOD OF MANUFACTURING SUCH A WINDOW AND AIRCRAFT COMPRISING SUCH A WINDOW 有权
    具有计划变形的窗户窗口,制造这样一个窗口的方法和包含这样一个窗口的飞机

    公开(公告)号:US20130320143A1

    公开(公告)日:2013-12-05

    申请号:US13896754

    申请日:2013-05-17

    CPC classification number: B64C1/1484

    Abstract: The present invention relates to an aircraft window, of the type including a holding frame for securing the window to the fuselage of an aircraft and at least one pane mounted in the holding frame by a sealing system, the at least one pane having an inner surface and an outer surface, characterized in that: the pane includes, in a first state called the rest state, at least one concavity in its outer surface when there is no pressure difference between the outer surface and the inner surface of the pane, and the at least one concavity of the pane is at least partially eradicated in a second state in which there is a pressure difference between the outer surface and the inner surface of the pane.

    Abstract translation: 本发明涉及一种飞机窗,其类型包括用于将窗口固定到飞行器的机身上的保持框架和通过密封系统安装在保持框架中的至少一个窗格,所述至少一个窗格具有内表面 和外表面,其特征在于,当所述外表面和所述窗格的内表面之间没有压力差时,所述窗格在处于静止状态的第一状态中包括在其外表面中的至少一个凹部,并且 在第二状态下至少部分根除窗格的至少一个凹面,其中在窗格的外表面和内表面之间存在压力差。

    METHOD FOR MODULAR CONSTRUCTION OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND FLEET OF AIRCRAFT OBTAINED

    公开(公告)号:US20200094936A1

    公开(公告)日:2020-03-26

    申请号:US16139806

    申请日:2018-09-24

    Abstract: A method for constructing at least two fleets of aircraft of different families for which each aircraft has a front part comprising windows, a framing of the windows and a windshield front fairing, comprising, for each aircraft, constructing a module composed of the framing of all of the windows allowing outward visibility from the cockpit and of the windshield front fairing whose form is identical and constant for all the aircraft of the fleets and independent of a form of the fuselages thereof, and constructing a section of fuselage of which at least a part of an edge of the fuselage is of a form identical to an edge of the module, such that the module can be assembled directly with the contiguous fuselage section, whatever the aircraft of the fleets.

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