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公开(公告)号：US20080267778A1
公开(公告)日：2008-10-30
申请号：US11629027
申请日：2006-04-19
申请人： Frank B. Stamps , Richard Rauber
发明人： Frank B. Stamps , Richard Rauber
IPC分类号： F01D7/00
CPC分类号： B64C27/32
摘要： A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent drive links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the drive links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-link configuration, a pad-bearing configuration, or another type of articulating assembly.
摘要翻译： 用于转翼飞行器的转子头（11）的扭矩联接器（13）具有被配置为与转子桅杆（19）一起旋转的上板和下板（29,31）。 枢转地连接到上板和下板（29,31）的驱动连杆（33）围绕大致平行于板的旋转轴线并径向偏移的枢转轴线枢转。 每个连杆（33）与相邻的驱动连杆（33）接合以形成连续的环形环，使得一个连杆（33）围绕其枢转轴线的运动引起每个相邻连杆（33）围绕其枢轴的相反方向的运动 枢轴。 驱动元件（25）将驱动连杆（33）连接到被配置为接收转子叶片的组件。 驱动元件（25）可以是万向接头，多拖尾构造，衬垫承载构型或另一类型的铰接组件的组件。
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公开(公告)号：US5868351A
公开(公告)日：1999-02-09
申请号：US653731
申请日：1996-05-23
CPC分类号： B64C29/0033 , B64C27/50
摘要： Rotor blade stowing system for stowing rotor blades that conserves storage space without adding significant weight or cost to the aircraft. The system includes a rotary actuator disposed on a blade grip member. A rotor blade is pivotally connected to the blade grip member. The rotary actuator is operably coupled to a blade pivoting cam and a locking cam. The system includes a cam follower linkage which has a first end which includes a blade pivoting cam follower and a locking cam follower and a second end. The blade pivoting cam follower follows the blade pivoting cam. The locking cam follower follows the locking cam. The second end of the cam follower linkage is coupled to the blade grip member. The system includes a shaft rotatably coupled to the blade grip member, a locking linkage bell crank operably coupled to the shaft, a delay cam coupled to the blade grip member, and a locking linkage idler operably coupled to the locking linkage bell crank. The locking linkage idler includes a delay cam follower that follows the delay cam. The system includes a locking linkage which has a first end coupled to the locking cam and a second end coupled to the locking linkage idler.
摘要翻译： 用于收起转子叶片的转子叶片收集系统，可节省存储空间，而不会对飞机造成重大的负担或成本。 该系统包括设置在刀片夹持构件上的旋转致动器。 转子叶片枢转地连接到叶片夹持构件。 旋转致动器可操作地联接到刀片枢转凸轮和锁定凸轮。 该系统包括凸轮从动件联动装置，其具有第一端，该第一端包括刀片枢转凸轮从动件和锁定凸轮从动件以及第二端。 刀片枢转凸轮从动件跟随刀片枢转凸轮。 锁定凸轮从动件跟随锁定凸轮。 凸轮从动联动装置的第二端联接到叶片把手构件。 该系统包括可旋转地联接到刀片夹持构件的轴，可操作地联接到轴的锁定联动钟形曲柄，联接到刀片抓握构件的延迟凸轮以及可操作地联接到锁定连杆机构的曲柄的锁定联动惰轮。 锁定连接惰轮包括跟随延迟凸轮的延迟凸轮从动件。 该系统包括锁定连杆机构，其具有联接到锁定凸轮的第一端和联接到锁定联动惰轮的第二端。
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公开(公告)号：US09702402B2
公开(公告)日：2017-07-11
申请号：US13283973
申请日：2011-10-28
申请人： Frank B. Stamps , Bryan W. Marshall
发明人： Frank B. Stamps , Bryan W. Marshall
CPC分类号： F16C23/043 , B64C27/48 , B64C27/82 , F16C2326/43 , Y10T29/49332
摘要： A rotary system and method to control feathering movement of a rotor blade. The system having a yoke arm configured to rotate a rotor blade. A first bearing and a second bearing are utilized to secure the rotor blade to the yoke arm and are configured to restrict longitudinal and transverse movement, while allowing feathering movement of the rotor blade relative to yoke arm.
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公开(公告)号：US09327832B2
公开(公告)日：2016-05-03
申请号：US13597433
申请日：2012-08-29
摘要： The centrifugal force bearing includes a plurality of tapered metal shims such that the thicker end of each tapered metal shim near the inner portion of bearing. The bearing can include a plurality of tapered elastomeric members that are consequently tapered so that the inner portions are narrower than the outer portions. The tapered metal shims can increase the axial stiffness in the direction of the centrifugal force, thereby reducing the axial deflection under loading, as compared to non-tapered shims. Further, reducing axial deflection reduces clearance issues that may arise when the rotor blade is allowed to axial deflect significant distances. As such, the tapered metal shims can increase the capacity of the bearing. Tapering the metal shims can decrease the compression induced shear strain near the outer portions of the elastomeric member, where loads are typically higher.
摘要翻译： 离心力轴承包括多个锥形金属垫片，使得每个锥形金属的较厚端部在轴承的内部附近垫紧。 轴承可以包括多个锥形弹性体构件，因此锥形的内部部分比外部部分窄。 与非锥形垫片相比，锥形金属垫片可以增加离心力方向上的轴向刚度，从而减少加载时的轴向挠度。 此外，减小轴向偏转减小了当转子叶片被允许轴向偏转显着距离时可能出现的间隙问题。 因此，锥形金属垫片可以增加轴承的容量。 锥形金属垫片可以减小弹性体构件的外部部分附近的压缩诱导剪切应变，其中负载通常较高。
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公开(公告)号：US09126680B2
公开(公告)日：2015-09-08
申请号：US13298033
申请日：2011-11-16
IPC分类号： B64C27/51 , B64C27/635 , B64C29/00
CPC分类号： B64C27/51 , B64C27/635 , B64C29/0033 , Y10T29/49332
摘要： A rotor hub assembly and method for controlling movement of a rotor blade relative to a swashplate. The hub assembly having an attachment device operably associated with the rotor blade and the swashplate. The attachment device provides pivot and rotational blade movement relative to the swashplate. A dual spring-rate damper is operably associated with the attachment device. The damper switches between a first spring rate and a second spring rate during flight to control movement of the rotor blade. The method includes the process of switching the damper between the first spring rate and the second spring rate during flight.
摘要翻译： 用于控制转子叶片相对于斜盘的运动的转子轮毂组件和方法。 轮毂组件具有可操作地与转子叶片和旋转斜盘相关联的附接装置。 附接装置提供相对于斜盘的枢转和旋转刀片移动。 双弹簧阻尼器与附接装置可操作地相关联。 减速器在飞行期间在第一弹簧速率和第二弹簧刚度之间切换以控制转子叶片的运动。 该方法包括在飞行期间在第一弹簧刚度和第二弹簧刚度之间切换阻尼器的过程。
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公开(公告)号：US09085357B2
公开(公告)日：2015-07-21
申请号：US13296974
申请日：2011-11-15
申请人： Hunter Davis , Frank B. Stamps
发明人： Hunter Davis , Frank B. Stamps
IPC分类号： B64C27/35
摘要： The bearing system is configured for treating and reacting dynamic loading within a rotor hub of rotorcraft. The bearing system includes an outer member having a plurality of alternating outer elastomeric layers and shim layers. The outer member has an inboard surface configured for bonding to an inboard bearing support, and the outer member has an outboard surface configured for bonding to an outboard bearing support. The bearing system has an inner member bonded to an interior surface of the outer member. The inner member can include a rigid inner core, as well as a plurality of elastomeric layers and shim layers configured to react torsional movements of the rotor blade.
摘要翻译： 轴承系统被配置用于在旋翼航空器的转子轮毂内处理和反应动载荷。 轴承系统包括具有多个交替的外部弹性体层和垫片层的外部构件。 外部构件具有被构造成用于结合到内侧轴承支撑件的内侧表面，并且外部构件具有被配置为用于结合到外侧轴承支撑件的外侧表面。 轴承系统具有结合到外部构件的内表面的内部构件。 内部构件可以包括刚性内芯，以及被配置成反作用于转子叶片的扭转运动的多个弹性体层和垫片层。
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公开(公告)号：US09010679B2
公开(公告)日：2015-04-21
申请号：US13532910
申请日：2012-06-26
申请人： Drew Sutton , Frank B. Stamps
发明人： Drew Sutton , Frank B. Stamps
IPC分类号： B64C27/52 , F16C25/00 , B64C27/54 , B64C27/605 , F16C11/06 , F16C11/08 , F16C17/10 , F16C27/06 , F16F1/393
CPC分类号： F16C27/063 , B64C27/54 , B64C27/605 , F16C11/0614 , F16C11/083 , F16C17/10 , F16C33/201 , F16C33/74 , F16C2326/43 , F16F1/393 , Y10T29/4971
摘要： 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 elastomeric bearing adjacent the housing inside the first opening and having a second opening therethrough, and an inner housing adjacent the elastomeric bearing 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.
摘要翻译： 根据一个实施例，轴承位于节距连杆和斜盘或轮毂之间。 所述轴承包括具有穿过其中的第一开口的外壳体，在所述第一开口内部邻近所述壳体并且具有穿过其的第二开口的弹性体轴承，以及邻近所述第二开口内的所述弹性轴承并具有通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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公开(公告)号：US08956117B2
公开(公告)日：2015-02-17
申请号：US13144448
申请日：2009-01-19
摘要： A rotor assembly for a rotary-wing aircraft, the rotor having a central hub assembly with a flexure-type, twist-shank yoke with multiple arms, each arm being adapted for a rotor blade to be mounted thereto. The arms provide for pitch changes of blades attached to the yoke through twisting of portions of the arms about a corresponding pitch axis. An inboard pitch bearing associated with each arm is attached to the hub assembly and allows for rotation of the attached blade about the pitch axis, the inboard pitch bearing also allowing for out-of-plane motion of the arm relative to the hub assembly about a flapping axis. An outboard pitch bearing associated with each arm is attached to the associated arm a selected distance from the inboard pitch bearing and allows for rotation of the attached blade about the pitch axis.
摘要翻译： 一种用于旋转翼飞行器的转子组件，该转子具有中心轮毂组件，其具有带有多个臂的挠曲型扭转柄轭，每个臂适于安装在其上的转子叶片。 臂通过扭转相应的俯仰轴线的臂的部分来提供附接到轭的叶片的桨距变化。 与每个臂相关联的内侧变桨轴承附接到轮毂组件并且允许所附接的叶片围绕俯仰轴线旋转，内侧变桨轴承还允许臂相对于轮毂组件的平面外运动绕一个 拍动轴。 与每个臂相关联的外侧变桨轴承从相对于内侧变桨轴承的选定距离附接到相关联的臂，并且允许所附接的叶片围绕桨距轴线旋转。
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公开(公告)号：US08936436B2
公开(公告)日：2015-01-20
申请号：US13144433
申请日：2009-01-19
申请人： Frank B. Stamps , Richard E. Rauber
发明人： Frank B. Stamps , Richard E. Rauber
IPC分类号： B64C11/06 , B64C27/605 , B64C27/32
CPC分类号： B64C27/32 , B64C27/605
摘要： A blade-pitch control system has a swashplate configured for continuous rotation with an associated rotor and mast, and at least one link connects the swashplate to each blade of the rotor. The swashplate provides for collective control of the pitch angle of the blades through selective rotation of the swashplate about a swashplate axis while the swashplate is rotating with the rotor and mast. The system can be configured to provide for cyclic control of the pitch angle of the blades through planar translation of the swashplate or through tilting of the swashplate about axes generally perpendicular to the swashplate axis.
摘要翻译： 桨叶桨距控制系统具有配置成与相关联的转子和桅杆连续旋转的斜盘，并且至少一个连杆将旋转斜盘连接到转子的每个叶片。 旋转斜盘通过旋转斜盘围绕斜盘轴线的选择性旋转而提供叶片桨距角的集中控制，同时斜盘与转子和桅杆一起旋转。 该系统可以被配置成通过斜盘的平面平移或者通常围绕通常垂直于斜盘轴线的轴线倾斜旋转斜盘来提供叶片的桨距角的循环控制。
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公开(公告)号：US20140248011A1
公开(公告)日：2014-09-04
申请号：US13596588
申请日：2012-08-28
IPC分类号： F16C17/22
CPC分类号： F16C17/22 , F03G7/065 , F16C27/06 , F16C2202/28 , F16F1/3842
摘要： The bearing assembly includes one or more elastomeric members loaded in a precompression by a shim that includes a shape memory alloy. The shape memory alloy is configured to generate the precompression in the elastomeric members upon a temperature change.
摘要翻译： 轴承组件包括一个或多个由包括形状记忆合金的垫片预先压缩的弹性部件。 形状记忆合金被配置为在温度变化时在弹性体构件中产生预压缩。
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