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    ROTORCRAFT ROTOR BLADE ASSEMBLY
    21.
    发明申请
    ROTORCRAFT ROTOR BLADE ASSEMBLY 审中-公开
    滚子转子叶片组件

    公开(公告)号：US20170036759A1

    公开(公告)日：2017-02-09

    申请号：US14817442

    申请日：2015-08-04

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Drew Sutton ,  Paul K. Oldroyd ,  James Braswell, JR. ,  Scott Wolthuis ,  Paul Sherrill

    IPC: B64C27/473

    CPC classification number: B64C27/473 ,  B64C2027/4736

    Abstract: A rotorcraft rotor blade assembly includes an upper skin portion extending substantially a full span of the rotor blade assembly and a lower skin portion extending substantially the full span of the rotor blade assembly. Each of the upper skin portion and the lower skin portion is configured to carry at least substantially 30% of rotor blade assembly loads.

    Abstract translation: 旋翼航空器转子叶片组件包括基本上延伸的转子叶片组件的整个跨度的上部皮肤部分和基本上延伸的转子叶片组件的整个跨度的下部皮肤部分。 上皮肤部分和下皮肤部分中的每一个构造成承载至少基本上30％的转子叶片组件负载。

    System and method of constructing composite structures
    22.
    发明授权
    System and method of constructing composite structures 有权
    构造复合结构体系与方法

    公开(公告)号：US09090027B2

    公开(公告)日：2015-07-28

    申请号：US13658407

    申请日：2012-10-23

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Drew Sutton ,  Loan Thanh Vo ,  Frank Bradley Stamps ,  Nolan Phillips

    IPC: B21K3/04 ,  B29C70/30 ,  B29C70/54 ,  B29C37/02 ,  B29D99/00

    CPC classification number: B29C70/30 ,  B29C37/02 ,  B29C70/545 ,  B29D99/0025 ,  Y02T50/43 ,  Y10T29/37 ,  Y10T29/49337

    Abstract: A method of constructing a composite component includes at least one of laterally and longitudinally aligning a material strip relative to a concavity of a layup tool, at least one of laterally and longitudinally extending the material strip to a predetermined location relative to the layup tool, wherein the material strip is substantially rectangular, and vertically abutting the material strip to the concavity of the layup tool, wherein the longitudinally extending the material strip includes at least one of (1) measuring a longitudinal distance of the material strip and (2) aligning a longitudinal end of the material strip with a longitudinal distance indicium and wherein the laterally extending the material strip includes at least one of (1) measuring a lateral distance of the material strip and (4) aligning a lateral end of the material strip with a lateral distance indicium.

    Abstract translation: 构成复合部件的方法包括相对于叠层工具的凹部横向和纵向对准材料条中的至少一个，将材料条的横向和纵向延伸至相对于铺层工具的预定位置中的至少一个，其中 所述材料带基本上是矩形的，并且垂直地邻接所述材料带到所述铺层工具的凹部，其中所述纵向延伸的所述材料条包括以下中的至少一个：（1）测量所述材料条的纵向距离;和（2） 所述材料条的纵向端部具有纵向距离标记，并且其中所述横向延伸的所述材料条包括以下中的至少一个：（1）测量所述材料条的横向距离;以及（4）将所述材料条的侧向端与侧向 距离标记

    Flexing Clevis Arrangement Bolted Joint Attachment For Flexible Rotor Hub With High Offset And High Flapping
    23.
    发明申请
    Flexing Clevis Arrangement Bolted Joint Attachment For Flexible Rotor Hub With High Offset And High Flapping 有权
    弯曲夹具布置螺栓接头附件适用于具有高偏移和高颤动的柔性转子毂

    公开(公告)号：US20140271200A1

    公开(公告)日：2014-09-18

    申请号：US13801965

    申请日：2013-03-13

    Applicant: BELL HELICOPTER TEXTRON INC.

    Inventor： Drew Sutton ,  Frank B. Stamps ,  Patrick Ryan Tisdale ,  Paul Oldroyd

    IPC: F01D5/02

    CPC classification number: B64C27/33 ,  B64C11/02 ,  B64C27/32 ,  B64C27/48 ,  Y10T29/49316

    Abstract: A flexible joint assembly for providing flexure to a rotor blade comprising an upper hub plate and a lower hub plate configured to secure a rotor blade yoke via a bolted joint located radially outward of a mast; and an upper flexure assembly connected to the upper hub plate and a lower flexure assembly connected to the lower hub plate, wherein the upper flexure assembly and lower flexure assembly are configured to promote flapping of the rotor blade yoke about a flapping hinge located radially outward of the bolted joint.

    Abstract translation: 一种用于向转子叶片提供挠曲的柔性接头组件，包括上轮毂板和下轮毂板，所述上轮毂板和下轮毂板被构造成通过位于桅杆的径向外侧的螺栓接头固定转子叶片翼片; 以及连接到上轮毂板的上挠性组件和连接到下轮毂板的下挠曲组件，其中上弯曲组件和下挠曲组件构造成促使转子叶片轭绕着位于径向向外的振动铰链 螺栓接头。

    Constant Velocity Joint with Spring Rate Control Mechanism
    25.
    发明申请
    Constant Velocity Joint with Spring Rate Control Mechanism 有权
    具有弹簧速率控制机构的恒速接头

    公开(公告)号：US20140248150A1

    公开(公告)日：2014-09-04

    申请号：US14258187

    申请日：2014-04-22

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Drew Sutton ,  Frank B. Stamps ,  Christopher Foskey

    IPC: B64C27/41 ,  F16D3/16

    CPC classification number: B64C27/41 ,  B64C27/32 ,  F16D3/28 ,  F16D3/30 ,  F16D3/33

    Abstract: According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and three bearings. The first yoke is configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening. The second yoke is rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis. The first bearing is disposed about the first axis adjacent to the first yoke, the second bearing is disposed about the second axis adjacent to the first yoke or the second yoke, and the third bearing disposed about the third axis adjacent to the second yoke. The first and third bearings torsionally constrain movement the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device.

    Abstract translation: 根据一个实施例，等速（CV）接头包括第一磁轭，第二磁轭和三个轴承。 第一磁轭被配置成围绕第一轴线可旋转地联接到输入装置，并且被配置成通过第一开口接收输入装置。 第二轭被围绕第二轴可旋转地联接到第一轭，并且围绕第三轴可旋转地联接到输出装置。 所述第一轴承围绕所述第一轴线邻近所述第一磁轭设置，所述第二轴承围绕所述第二轴线邻近所述第一磁轭或所述第二磁轭设置，所述第三轴承围绕所述第三轴线邻近所述第二磁轭设置。 第一和第三轴承扭转约束运动第一轭和第二轭，以便在输入装置和输出装置之间实现基本的CV特性。

    Constant velocity joint with spring rate control mechanism
    28.
    发明授权
    Constant velocity joint with spring rate control mechanism 有权

    公开(公告)号：US09878783B2

    公开(公告)日：2018-01-30

    申请号：US14258187

    申请日：2014-04-22

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Drew Sutton ,  Frank B. Stamps ,  Christopher Foskey

    IPC: B64C27/41 ,  B64C27/32 ,  F16D3/33 ,  F16D3/28 ,  F16D3/30

    CPC classification number: B64C27/41 ,  B64C27/32 ,  F16D3/28 ,  F16D3/30 ,  F16D3/33

    Abstract: According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and three bearings. The first yoke is configured to be rotatably coupled to an input device about a first axis and configured to receive the input device through a first opening. The second yoke is rotatably coupled to the first yoke about a second axis and rotatably coupled to an output device about a third axis. The first bearing is disposed about the first axis adjacent to the first yoke, the second bearing is disposed about the second axis adjacent to the first yoke or the second yoke, and the third bearing disposed about the third axis adjacent to the second yoke. The first and third bearings torsionally constrain movement the first yoke and the second yoke so as to achieve a substantially CV characteristic between the input device and the output device.

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