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    STORAGE MODES FOR TILTROTOR AIRCRAFT
    1.
    发明授权
    STORAGE MODES FOR TILTROTOR AIRCRAFT 有权

    公开(公告)号：EP3296201B1

    公开(公告)日：2018-08-08

    申请号：EP16201821.2

    申请日：2016-12-01

    Applicant: Bell Helicopter Textron Inc.

    Inventor： FOSKEY, Christopher Edward

    IPC: B64C29/00 ,  B64C3/56 ,  B64C11/28 ,  B64C5/02

    CPC classification number: B64C29/0033 ,  B64C3/56 ,  B64C5/02 ,  B64C11/28

    Abstract: A tiltrotor aircraft (10) having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage (12) having a wing (18) rotatably mounted thereto. The wing (18) has an orientation generally perpendicular to the fuselage (12), in the flight modes, and an orientation generally parallel to the fuselage (12), in the storage mode. First and second pylon assemblies (22a, 22b) are positioned proximate outboard ends of the wing (18). First and second mast assemblies (24a, 24b) are respectively rotatable relative to the first and second pylon assemblies (22a, 22b) and have generally vertical orientations in the VTOL flight mode, and generally horizontal orientations in the forward flight mode and the storage mode. First and second proprotor assemblies (26a, 26b) are respectively rotatable relative to the first and second mast assemblies (24a, 24b). Each proprotor assembly includes a plurality of rotor blades (52a-f) and has a radially extended orientation, in the flight modes, and a stowed orientation, in the storage mode.

    STORAGE MODES FOR TILTROTOR AIRCRAFT
    2.
    发明公开
    STORAGE MODES FOR TILTROTOR AIRCRAFT 有权
    TILTROTOR AIRCRAFT的存储模式

    公开(公告)号：EP3296201A1

    公开(公告)日：2018-03-21

    申请号：EP16201821.2

    申请日：2016-12-01

    Applicant: Bell Helicopter Textron Inc.

    Inventor： FOSKEY, Christopher Edward

    IPC: B64C29/00 ,  B64C3/56 ,  B64C11/28 ,  B64C5/02

    CPC classification number: B64C29/0033 ,  B64C3/56 ,  B64C5/02 ,  B64C11/28

    Abstract: A tiltrotor aircraft (10) having a VTOL flight mode, a forward flight mode and a storage mode includes a fuselage (12) having a wing (18) rotatably mounted thereto. The wing (18) has an orientation generally perpendicular to the fuselage (12), in the flight modes, and an orientation generally parallel to the fuselage (12), in the storage mode. First and second pylon assemblies (22a, 22b) are positioned proximate outboard ends of the wing (18). First and second mast assemblies (24a, 24b) are respectively rotatable relative to the first and second pylon assemblies (22a, 22b) and have generally vertical orientations in the VTOL flight mode, and generally horizontal orientations in the forward flight mode and the storage mode. First and second proprotor assemblies (26a, 26b) are respectively rotatable relative to the first and second mast assemblies (24a, 24b). Each proprotor assembly includes a plurality of rotor blades (52a-f) and has a radially extended orientation, in the flight modes, and a stowed orientation, in the storage mode.

    Abstract translation: 具有垂直起降飞行模式，前进飞行模式和存储模式的倾转旋翼飞机（10）包括机身（12），机身（12）具有可旋转地安装到其上的机翼（18）。 在存储模式下，机翼（18）在飞行模式中具有大致垂直于机身（12）的取向以及大致平行于机身（12）的取向。 第一和第二挂架组件（22a，22b）位于机翼（18）的外侧端附近。 第一和第二桅杆组件（24a，24b）分别相对于第一和第二吊挂组件（22a，22b）可旋转并且在垂直起降飞行模式下具有大致垂直的方位，并且在前方飞行模式和存储模式下具有大致水平的方位 。 第一和第二旋翼组件（26a，26b）分别相对于第一和第二桅杆组件（24a，24b）可旋转。 每个旋翼飞行器组件包括多个转子叶片（52a-f）并且在存储模式下具有在飞行模式中的径向延伸取向和收起取向。

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