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公开(公告)号：US09499262B2
公开(公告)日：2016-11-22
申请号：US13958192
申请日：2013-08-02
Applicant: Bell Helicopter Textron Inc.
Inventor： Christopher Foskey , Frank B. Stamps , Joel McIntyre , Gary Miller
CPC classification number: B64C27/33 , B64C27/48 , B64C29/0033
Abstract: A composite flexure that secures a rotor blade to a gimbaled yoke in a tiltrotor rotor system. The composite flexure includes a composite flexure member, a first end, and a second end. The first end of the composite flexure couples the composite flexure to the gimbaled yoke, and the second end of the composite flexure couples the composite flexure to the rotor blade. The composite flexure is twisted when the composite flexure is not subject to torsional loads in order to accommodate various forces imparted on the rotor system.
Abstract translation: 复合弯曲，其将转子叶片固定在倾斜旋转器转子系统中的万向轭。 复合挠曲件包括复合挠曲构件，第一端和第二端。 复合挠曲件的第一端将复合挠曲件联接到万向架轭架上，并且复合挠曲件的第二端将复合挠曲件联接到转子叶片。 当复合挠曲件不受扭转载荷的影响时，复合挠曲是扭转的，以适应转子系统上施加的各种力。
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公开(公告)号：US09399513B2
公开(公告)日：2016-07-26
申请号：US13673475
申请日：2012-11-09
Applicant: Bell Helicopter Textron Inc.
Inventor： Drew A. Sutton , Christopher Foskey , Dudley Smith , Frank B. Stamps
Abstract: According to one embodiment, a constant velocity (CV) joint includes a first yoke, a second yoke, and a control mechanism. 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 control mechanism is adapted to constrain 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，第二磁轭和控制机构。 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。 控制机构适于约束第一磁轭和第二磁轭，以便在输入装置和输出装置之间实现基本的CV特性。
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公开(公告)号：US20160083087A1
公开(公告)日：2016-03-24
申请号：US14954694
申请日：2015-11-30
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Troy Schank , Frank B. Stamps
IPC: B64C27/41 , B64C27/615
CPC classification number: B64C27/30 , B64C11/28 , B64C27/32 , B64C27/41 , B64C27/50 , B64C27/52 , B64C27/605 , B64C27/615 , B64C29/0033
Abstract: A method of selectively preventing flapping of a rotor hub includes providing a flapping lock proximate to a rotor hub and shaft assembly and moving the flapping lock from an unlocked position to a locked position, the flapping lock operable in the locked position to prevent at least some flapping movement of the rotor hub relative to the shaft, the flapping lock operable in the unlocked position to allow the at least some flapping movement of the rotor hub relative to the shaft.
Abstract translation: 选择性地防止转子毂振动的方法包括提供靠近转子轮毂和轴组件的摇动锁，并将摇动锁从解锁位置移动到锁定位置，所述摇动锁可在锁定位置操作以防止至少一些 转子毂相对于轴振动运动，所述摇动锁在可解锁位置中可操作以允许转子毂相对于轴的至少一些拍动运动。
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公开(公告)号：US20160075430A1
公开(公告)日：2016-03-17
申请号：US14485967
申请日：2014-09-15
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Christopher Foskey , Frank B. Stamps
IPC: B64C27/46 , B64C27/473
CPC classification number: B64C27/463 , B64C27/473
Abstract: A rotor blade system includes a rotor blade having an outboard section and an inboard section, a hinge joint rigidly attached to the outboard section, and an adhedral tip engaged with the hinge joint. A method includes pivotally attaching an adhedral tip to the rotor blade and pivoting the adhedral tip during flight to change the flight performance characteristics of the blade during flight.
Abstract translation: 转子叶片系统包括具有外侧部分和内侧部分的转子叶片，刚性地附接到外侧部分的铰链接头以及与铰链接合部相接合的内接尖端。 一种方法包括将飞散的顶端枢转地连接到转子叶片上，并且在飞行期间枢转该内向尖端以改变飞行中叶片的飞行性能特征。
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公开(公告)号：US09199730B2
公开(公告)日：2015-12-01
申请号：US13949766
申请日：2013-07-24
Applicant: Bell Helicopter Textron Inc.
Inventor： Troy Schank , Frank B. Stamps
IPC: B64C27/50 , B64C27/32 , B64C27/30 , B64C27/615
Abstract: According to one embodiment, a flapping lock for a rotor system includes a downstop, a flapping stop, and an actuator. The downstop is in mechanical communication with a shaft. The flapping stop is in mechanical communication with a rotor hub. The actuator is operable to move the downstop towards the flapping stop.
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Patent Agency Ranking
公开(公告)号：US20150298804A1
公开(公告)日：2015-10-22
申请号：US13949766
申请日：2013-07-24
Applicant: Bell Helicopter Textron Inc.
Inventor： Troy Schank , Frank B. Stamps
IPC: B64C27/615 , B64C27/32
CPC classification number: B64C27/30 , B64C11/28 , B64C27/32 , B64C27/41 , B64C27/50 , B64C27/52 , B64C27/605 , B64C27/615 , B64C29/0033
Abstract: According to one embodiment, a flapping lock for a rotor system includes a downstop, a flapping stop, and an actuator. The downstop is in mechanical communication with a shaft. The flapping stop is in mechanical communication with a rotor hub. The actuator is operable to move the downstop towards the flapping stop.
Abstract translation: 根据一个实施例，用于转子系统的扑动锁包括下降挡块，挡板挡块和致动器。 下停止与轴的机械通信。 挡板与转子毂机械连通。 致动器可操作以将下降挡块移向扑动挡块。
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公开(公告)号：US20150274290A1
公开(公告)日：2015-10-01
申请号：US13949698
申请日：2013-07-24
Applicant: Bell Helicopter Textron Inc.
Inventor： Carlos A. Fenny , Troy Schank , Frank B. Stamps
CPC classification number: B64C27/30 , B64C11/28 , B64C27/32 , B64C27/41 , B64C27/50 , B64C27/52 , B64C27/605 , B64C27/615 , B64C29/0033
Abstract: According to one embodiment, a rotor blade rotation system includes a hub, a rotor blade in mechanical communication with the hub and pivotable about an axis of rotation, a swashplate, a pitch link, and an actuator. The swashplate includes a rotating portion and a non-rotating portion. The pitch link is coupled to the rotating portion of the swashplate and in mechanical communication with the rotor blade. The actuator is coupled to the non-rotating portion of the swashplate and operable to reposition the swashplate from a first position to a second position such that the pitch links pivot the rotor blade from a deployed position to a folded position.
Abstract translation: 根据一个实施例，转子叶片旋转系统包括轮毂，转子叶片，其与轮毂机械连通并可围绕旋转轴线旋转，斜盘，俯仰杆和致动器。 旋转斜盘包括旋转部分和非旋转部分。 节距连杆联接到旋转斜盘的旋转部分并且与转子叶片机械连通。 致动器联接到旋转斜盘的非旋转部分并且可操作以将斜盘从第一位置重新定位到第二位置，使得俯仰杆将转子叶片从展开位置枢转到折叠位置。
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公开(公告)号：US20150136901A1
公开(公告)日：2015-05-21
申请号：US14598961
申请日：2015-01-16
Applicant: Bell Helicopter Textron Inc.
Inventor： Emily Schofield , Chad Jarrett , Dan Sottiaux , Frank B. Stamps
CPC classification number: B64C27/35 , B23P19/04 , B64C27/41 , F16C7/04 , F16C11/083 , F16C27/063 , F16C2326/43 , F16D3/62 , F16F1/3863 , Y10T29/49643 , Y10T29/4984
Abstract: An apparatus comprising a drivelink comprising a housing including a socket, wherein the socket comprises a cross-sectional area, and a bearing cartridge disposed within the socket, wherein a cross-sectional area of the cartridge is less than the cross-sectional area of the socket. An apparatus comprising a drivelink comprising a housing having a socket, and a bearing cartridge positioned within the socket and comprising a first portion and a second portion, wherein the first portion is configured to undergo compression when a load is applied to the drivelink, and wherein the second portion is configured to not be in tension when the load is applied to the drivelink.
Abstract translation: 一种包括驱动装置的装置，包括壳体，该壳体包括插座，其中所述插座包括横截面区域，以及设置在所述插座内的轴承盒，其中所述盒的横截面积小于所述插座的横截面积 插座。 一种包括驱动装置的装置，包括具有插座的壳体和定位在所述插座内并包括第一部分和第二部分的轴承盒，其中所述第一部分被配置为当负载施加到所述传动装置时经受压缩，并且其中 第二部分被配置为当负载施加到驱动器时不处于张力。
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公开(公告)号：US20150125300A1
公开(公告)日：2015-05-07
申请号：US14072511
申请日：2013-11-05
Applicant: Bell Helicopter Textron Inc.
Inventor： Frank B. Stamps , Richard Rauber , Hunter Jay Davis
Abstract: A drive mechanism for a rotary aircraft includes an outer drive member having a plurality of drive trunnions extending therefrom; a middle drive member resiliently coupled to the outer drive member; and an inner drive member resiliently coupled to the middle drive member.
Abstract translation: 用于旋转飞行器的驱动机构包括具有从其延伸的多个驱动轴颈的外部驱动构件; 弹性地联接到所述外部驱动构件的中间驱动构件; 以及弹性地联接到所述中间驱动构件的内部驱动构件。
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公开(公告)号：US20150060597A1
公开(公告)日：2015-03-05
申请号：US14533869
申请日：2014-11-05
Applicant: Bell Helicopter Textron Inc.
Inventor： Drew Sutton , Frank B. Stamps
CPC classification number: B64C27/605 , B23P15/003 , B23P2700/01 , B64C27/54 , F16C11/0614 , F16C11/083 , F16C17/10 , F16C27/063 , F16C33/20 , F16C2208/32 , F16C2326/43 , F16F1/393 , Y10T29/49636 , Y10T29/49643 , Y10T29/4971
Abstract: According to one embodiment, a bearing is situated between a pitch link and a swashplate or a hub. The bearing comprises an outer housing having a first opening therethrough, an intermediate housing adjacent the housing inside the first opening and having a second opening therethrough, and an inner housing adjacent the intermediate housing inside the second opening and having a third opening therethrough. The inner housing comprising a first inner surface and a second inner surface defining the third opening. A first member is adjacent the first inner surface inside the third opening having a fourth opening therethrough. A second member is adjacent the second inner surface inside the third opening having a fifth opening therethrough coaxial with the fourth opening.
Abstract translation: 根据一个实施例，轴承位于节距连杆和斜盘或轮毂之间。 轴承包括具有穿过其中的第一开口的外壳体，与第一开口内部的壳体相邻并且具有穿过其的第二开口的中间壳体，以及与第二开口内部的中间壳体相邻并且具有穿过其的第三开口的内壳体。 内壳体包括限定第三开口的第一内表面和第二内表面。 第一构件邻近第三开口内的第一内表面，具有穿过其的第四开口。 第二构件与第三开口内的第二内表面相邻，具有与第四开口同轴的第五开口。
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