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公开(公告)号：US08181755B2
公开(公告)日：2012-05-22
申请号：US10568170
申请日：2004-08-27
申请人： Frank B. Stamps , David A. Popelka , Michael R. Smith , Christopher M. Bothwell , Lawrence M. Corso , James L. Braswell, Jr. , Ernst C. Schellhase , Charles L. Hollimon , Thomas J. Newman , Bryan Baskin , Thomas C. Campbell , Daniel B. Robertson
发明人： Frank B. Stamps , David A. Popelka , Michael R. Smith , Christopher M. Bothwell , Lawrence M. Corso , James L. Braswell, Jr. , Ernst C. Schellhase , Charles L. Hollimon , Thomas J. Newman , Bryan Baskin , Thomas C. Campbell , Daniel B. Robertson
摘要： A damper has a piston having an axis, an outer surface, and opposing ends. Elastomeric seals are in sealing contact with the outer surface of the piston, the seals being coaxial with the piston and limiting movement of the piston to a path along the axis of the piston. The seals also define fluid chambers adjacent the ends of the piston. A primary passage communicates the fluid chambers, and a selectively switchable valve for controls a flow of fluid from one of the chambers to another of the chambers through the primary passage. When the flow of fluid through the primary passage is permitted, movement of the piston is resisted by a first spring rate due to a shear force required to cause shear deflection of the seals. When the flow of fluid through the primary passage is restricted, movement of the piston is resisted by a second spring rate due to a fluid force required to cause bulging deflection of the seals.
摘要翻译： 阻尼器具有具有轴线，外表面和相对端的活塞。 弹性密封件与活塞的外表面密封接触，密封件与活塞同轴并且限制活塞沿着活塞轴线的路径运动。 密封件还限定了邻近活塞端部的流体室。 主要通道连通流体室，以及可选择地可切换的阀，用于控制通过主通道从一个室到另一个腔的流体流。 当允许通过主通道的流体流动时，活塞的运动由于需要剪切力而引起密封件的剪切偏转而抵抗第一弹簧刚度。 当通过主通道的流体流被限制时，活塞的运动由于需要使密封件凸起偏转所需的流体力而受到第二弹簧刚度的抵抗。
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公开(公告)号：US20100090055A1
公开(公告)日：2010-04-15
申请号：US12443950
申请日：2006-10-12
申请人： Michael R. Smith , Frank B. Stamps
发明人： Michael R. Smith , Frank B. Stamps
CPC分类号： B64C27/12 , B64C2027/002 , F16F7/10 , F16F15/02 , F16F2230/16
摘要： A preferred embodiment of a pylon has six pylon mounting links for mounting the pylon to an airframe. Each link is considered “near-rigid” and has a spherical-bearing rod-end on both ends such that the link can only transmit axial loads. At least one of the links has a mass carried within the link and selectively moveable by an actuating means along the axis of the link in an oscillatory manner for attenuating vibrations traveling axially through the link. The actuating means may be an electromechanical, hydraulic, pneumatic, or piezoelectric system. By mounting each link in a selected orientation relative to the other links, the actuating means may be operated in a manner that attenuates axial vibration that would otherwise be transmitted through the link and into the airframe.
摘要翻译： 塔的优选实施例具有用于将吊架安装到机身上的六个安装链。 每个连杆被认为是“接近刚性”的，并且在两端具有球形轴承杆端，使得连杆只能传递轴向载荷。 链节中的至少一个具有在链节内承载的质量，并且可以通过致动装置沿着连杆的轴线以振荡方式选择性地移动，以便衰减轴向穿过连杆的振动。 致动装置可以是机电，液压，气动或压电系统。 通过将每个链节相对于其它连杆安装在选定的方向上，致动装置可以以衰减轴向振动的方式操作，否则轴向振动将通过连杆传递到机身中。
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公开(公告)号：US20100009764A1
公开(公告)日：2010-01-14
申请号：US12376979
申请日：2006-08-17
申请人： Frank B. Stamps , Richard Rauber , David Popelka , Pat Tisdale , Tom Campbell , James Lee Braswell, JR.
发明人： Frank B. Stamps , Richard Rauber , David Popelka , Pat Tisdale , Tom Campbell , James Lee Braswell, JR.
IPC分类号： F16D3/18
摘要： A torque coupling for a rotor head of a rotary-wing aircraft is configured for rotation with a mast and for causing rotation of an attached yoke. The coupling has trunnions that rotate with the mast and extend generally radially. Pad-bearing assemblies each have a central member coupled to one of the trunnions with a laminated spherical bearing and have laminated pad bearings affixed to opposing sides of the central member. The laminated bearings have alternating rigid and elastomeric layers. A bearing mount is affixed to each pad bearing and is connected to a yoke for rotating the yoke with the mast. The pad-bearing assemblies allow for relative motion between each central member and the associated trunnion and between each central member and the bearing mounts through elastic shear deformation, and this allows for gimballing of the attached yoke relative to the mast.
摘要翻译： 用于旋转翼飞行器的转子头的扭矩联接器构造成用桅杆旋转并且用于使附接的轭的旋转。 联轴器具有与桅杆一起旋转并且径向延伸的耳轴。 垫轴承组件各自具有与层叠的球面轴承联接到其中一个耳轴的中心构件，并且具有固定到中心构件的相对侧的层压垫轴承。 层压轴承具有交替的刚性和弹性层。 轴承座固定到每个垫轴承上，并连接到轭架上，用于使桅杆旋转。 垫片轴承组件允许在每个中心构件和相关联的耳轴之间以及通过弹性剪切变形在每个中心构件和轴承座之间进行相对运动，并且这允许相对于桅杆对附接的轭进行槌球。
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公开(公告)号：US20090179107A1
公开(公告)日：2009-07-16
申请号：US12300065
申请日：2007-05-14
申请人： Frank B. Stamps , Richard E. Rauber , Thomas C. Campbell , Tom Donovan , Patrick R. Tisdale , James Lee Braswell Jr.
发明人： Frank B. Stamps , Richard E. Rauber , Thomas C. Campbell , Tom Donovan , Patrick R. Tisdale , James Lee Braswell Jr.
IPC分类号： B64C27/52
CPC分类号： B64C27/33 , B64C27/32 , B64C29/0033
摘要： A yoke for a rotary wing aircraft rotor system has a plurality of arms, each arm having a root. Each root has a notched portion configured to allow passage of a portion of a blade-pitch control system through the notched portion.
摘要翻译： 用于旋翼飞机转子系统的轭具有多个臂，每个臂具有根部。 每个根部具有被配置为允许叶片间距控制系统的一部分通过切口部分的切口部分。
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公开(公告)号：US20080292468A1
公开(公告)日：2008-11-27
申请号：US12159007
申请日：2006-01-13
申请人： Frank B. Stamps , Richard E. Rauber
发明人： Frank B. Stamps , Richard E. Rauber
IPC分类号： B64C27/32
CPC分类号： B64C29/0033 , B64C27/32 , B64C27/82
摘要： A rotor-hub for a rotary-wing aircraft is disclosed. The rotor-hub comprises a yoke comprising a plurality of yoke arms and a plurality of yoke straps, wherein the yoke arms are joined together by the yoke straps, and wherein a plurality of inner walls of the yoke define a central void space. A pitch horn is movably connected to the yoke and a portion of the pitch horn is located within the central void space. A connecting shell is fixedly attached to the yoke.
摘要翻译： 公开了一种用于旋翼飞机的转子毂。 转子毂包括包括多个轭臂和多个轭带的轭，其中轭臂通过轭带连接在一起，并且其中轭的多个内壁限定中心空隙空间。 节距角可移动地连接到轭，并且节距角的一部分位于中心空隙内。 连接外壳固定在轭上。
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公开(公告)号：US6009983A
公开(公告)日：2000-01-04
申请号：US866603
申请日：1997-05-30
申请人： Frank B. Stamps , Michael R. Smith
发明人： Frank B. Stamps , Michael R. Smith
摘要： A vibration-isolatator utilizes a relatively small-diameter tuning port or passage and associated reduction in component size. In the illustrative embodiment described herein, a passive isolator is provided which includes a tuning passage or port which has a diameter which is approximately one-half the diameter of the prior-art isolators. The reduced radial dimension of the tuning passage of the isolator results in a remarkable decrease in its size and weight, thus increasing the efficiency of operation of the aircraft.
摘要翻译： 振动隔离器利用相对较小直径的调谐端口或通道以及相关的部件尺寸减小。 在本文所述的说明性实施例中，提供了一种无源隔离器，其包括调谐通道或端口，该调谐通道或端口的直径约为现有技术隔离器的直径的一半。 隔离器的调谐通道的减小的径向尺寸导致其尺寸和重量的显着减小，从而提高飞行器的操作效率。
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公开(公告)号：US09896198B2
公开(公告)日：2018-02-20
申请号：US14805159
申请日：2015-07-21
申请人： Hunter Davis , Frank B. Stamps
发明人： Hunter Davis , Frank B. Stamps
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.
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公开(公告)号：US09765641B2
公开(公告)日：2017-09-19
申请号：US13593113
申请日：2012-08-23
CPC分类号： F01D25/06 , B64C27/001 , F16F13/08 , Y10T29/49321
摘要： In accordance with one embodiment of the present disclosure, a system includes a first housing, a second housing, a seal, and a spring system. The first housing includes a first volume of fluid. The first housing is capable of connecting to a first element and to a second element, and is also capable of reducing an amount of movement transferred from the first element to the second element. The second housing is connected to the first housing. The second housing includes a second volume of fluid and a volume of gas. The first volume of fluid is in fluid communication with the second volume of fluid. The seal is capable of separating the second volume of fluid from the volume of gas. The spring system is capable of applying pressure to the first volume of fluid and the second volume of fluid.
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公开(公告)号：US09382933B2
公开(公告)日：2016-07-05
申请号：US13430117
申请日：2012-03-26
CPC分类号： F16B11/008 , B64D27/26 , C09J5/00 , Y10T403/343 , Y10T403/473 , Y10T403/52
摘要： A tube form assembly includes an inner member and an outer member. Each of the inner and outer members has an offset which creates a cavity therebetween. During assembly of the tube form assembly, an adhesive is located in the cavity and squeezed out and through the adjacent bond lines between the inner member and outer member. The pressurization and flow of adhesive outward from the cavity facilitates removal of air bubbles, as well as prevents the introduction of air bubbles into the bond line.
摘要翻译： 管形组件包括内部构件和外部构件。 内部和外部构件中的每一个具有在其之间形成空腔的偏移。 在组装管形组件期间，粘合剂位于空腔中并挤出并穿过内部构件和外部构件之间的相邻接合线。 从空腔向外的粘合剂的加压和流动有助于除去气泡，同时防止气泡进入粘合线。
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公开(公告)号：US20160152328A1
公开(公告)日：2016-06-02
申请号：US14805159
申请日：2015-07-21
申请人： Hunter Davis , Frank B. Stamps
发明人： Hunter Davis , Frank B. Stamps
IPC分类号： B64C27/32
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.
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