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    Tilt-rotor vertical-lift aircraft
    4.
    发明授权
    Tilt-rotor vertical-lift aircraft 有权
    倾斜转子垂直升降机

    公开(公告)号：US09475585B2

    公开(公告)日：2016-10-25

    申请号：US14315109

    申请日：2014-06-25

    Applicant: The Boeing Company

    Inventor： Alicia Hong ,  Daniel I. Newman ,  Christopher R. Holtorf ,  John R. Chisholm ,  Stephen Dyess

    IPC: B64C15/12 ,  B64D35/00 ,  B64C29/00 ,  B64D35/08

    CPC classification number: B64D35/00 ,  B64C29/0033 ,  B64D35/08

    Abstract: Described herein is an aircraft that includes a fuselage with a higher portion and a lower portion. The aircraft also includes two fixed wings that are coupled to and extend from opposing sides of the lower portion of the fuselage. Additionally, the aircraft includes a tilt-rotor assembly that is coupled to each of the two fixed wings.

    Abstract translation: 这里描述的是包括具有较高部分和较低部分的机身的飞行器。 飞机还包括两个固定的翼片，它们耦合到机身的下部的相对侧并从机身的下部的相对侧延伸。 另外，飞机包括联接到两个固定翼中的每一个的倾斜转子组件。

    TILT-ROTOR VERTICAL-LIFT AIRCRAFT
    6.
    发明申请
    TILT-ROTOR VERTICAL-LIFT AIRCRAFT 有权
    TILT-ROTOR垂直升降飞机

    公开(公告)号：US20150375860A1

    公开(公告)日：2015-12-31

    申请号：US14315109

    申请日：2014-06-25

    Applicant: The Boeing Company

    Inventor： Alicia Hong ,  Daniel I. Newman ,  Christopher R. Holtorf ,  John R. Chisholm ,  Stephen Dyess

    IPC: B64C27/26 ,  B64D35/00

    CPC classification number: B64D35/00 ,  B64C29/0033 ,  B64D35/08

    Abstract: Described herein is an aircraft that includes a fuselage with a higher portion and a lower portion. The aircraft also includes two fixed wings that are coupled to and extend from opposing sides of the lower portion of the fuselage. Additionally, the aircraft includes a tilt-rotor assembly that is coupled to each of the two fixed wings.

    Abstract translation: 这里描述的是包括具有较高部分和较低部分的机身的飞行器。 飞机还包括两个固定的翼片，它们耦合到机身的下部的相对侧并从机身的下部的相对侧延伸。 另外，飞机包括联接到两个固定翼中的每一个的倾斜转子组件。

    FUSELAGE-MOUNTED LANDING GEAR ASSEMBLY FOR USE WITH A LOW WING AIRCRAFT
    7.
    发明申请
    FUSELAGE-MOUNTED LANDING GEAR ASSEMBLY FOR USE WITH A LOW WING AIRCRAFT 审中-公开
    用于低空飞机的FUSELAGE-MOUNTED LANDING GEAR ASSEMBLY FOR USE

    公开(公告)号：US20150069178A1

    公开(公告)日：2015-03-12

    申请号：US14021301

    申请日：2013-09-09

    Applicant: The Boeing Company

    Inventor： Stephen T. Brown ,  Michael Lane Drake ,  Christopher R. Holtorf ,  Justin Cottet

    IPC: B64C25/12

    CPC classification number: B64C25/12 ,  B64C2025/125

    Abstract: An aircraft comprises at least one wing comprising a trailing edge flap that is selectively moveable between a stowed position and an extended position. The aircraft also includes a fuselage comprising a first gear door on a side of the fuselage and a second gear door on a bottom of the fuselage. The first gear door is moveable in a gear door envelope between a closed position and an open position. The wing is coupled to the fuselage in a low-wing configuration. A landing gear assembly is coupled to the fuselage and is selectively moveable between a retracted position and a deployed position. The trailing edge flap may be extended simultaneously with, before, or after deployment of the landing gear assembly and opening of the first gear door.

    Abstract translation: 一种飞行器包括至少一个翼片，其包括可在收起位置和延伸位置之间选择性地移动的后缘翼片。 飞机还包括一个机身，其中包括在机身侧面的第一齿轮门和在机身底部的第二齿轮门。 第一个齿轮门可以在一个闭合位置和一个打开位置之间的一个齿轮门壳中移动。 机翼以低翼配置耦合到机身。 起落架组件联接到机身，并且可以在缩回位置和展开位置之间选择性地移动。 后缘襟翼可以与起落架组件展开同时延伸，也可以在第一档门打开后展开。

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