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1. 发明授权

US09702402B2 Increased capacity spherical lined bearings 有权
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
IPC分类号： F01D25/16 , F16C23/04 , B64C27/48 , B64C27/82
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.

2. 发明申请

US20130108447A1 Increased Capacity Spherical Lined Bearings 有权
标题翻译：增加容量球面轴承
公开(公告)号：US20130108447A1
公开(公告)日：2013-05-02
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
IPC分类号： B64C27/32 , B23P15/00 , B64C27/45
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.
摘要翻译：一种用于控制转子叶片的羽化运动的旋转系统和方法。该系统具有构造成使转子叶片旋转的轭臂。第一轴承和第二轴承用于将转子叶片固定到轭臂上，并且构造成限制纵向和横向运动，同时允许转子叶片相对于轭臂的羽化运动。

3. 发明申请

US20130216384A1 Compact Rotorcraft Dual-Element Spherical Elastomeric Centrifugal-Force Bearing Assembly 有权
标题翻译：紧凑型Rotorcraft双元件球形弹性离心力轴承组件
公开(公告)号：US20130216384A1
公开(公告)日：2013-08-22
申请号：US13401203
申请日：2012-02-21
申请人： Frank B. Stamps , Bryan W. Marshall , Terry K. Thompson , Orion Braziel , David Popelka , Patrick Tisdale
发明人： Frank B. Stamps , Bryan W. Marshall , Terry K. Thompson , Orion Braziel , David Popelka , Patrick Tisdale
IPC分类号： B64C27/00
CPC分类号： B64C27/35
摘要： A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.
摘要翻译：旋转系统包括保持构件和具有形成桥的开口的柔性轭。旋转系统还设置有两个轴承组件，第一轴承组件延伸穿过轭的开口并且构造成将转子叶片固定到保持构件，以及延伸穿过柔性轭的开口的第二轴承组件，转子叶片到桥。第二轴承元件包括具有形成球形轮廓的第一表面和形成锥形轮廓的相对的整体第二表面的轴承元件。

4. 发明授权

US09487290B2 Composite rotor blade having weighted material for mass balancing 有权
标题翻译：复合转子叶片具有用于质量平衡的加权材料
公开(公告)号：US09487290B2
公开(公告)日：2016-11-08
申请号：US13578975
申请日：2010-11-12
申请人： Paul B. Sherrill , Frank B. Stamps , Ronald J. Measom
发明人： Paul B. Sherrill , Frank B. Stamps , Ronald J. Measom
IPC分类号： B64C27/473 , B64C27/00 , B29C70/30 , B29L31/08
CPC分类号： B64C27/473 , B29C70/30 , B29L2031/085 , B64C27/008 , B64C2027/4736 , Y02E10/721 , Y02P70/523 , Y10T428/24992
摘要： A rotor blade for an aircraft includes a composite portion having fiber-reinforced resin material, the composite portion having an outside surface that forms at least a partial airfoil shape. The weighted portion includes a plurality of weighted material layers and a plurality of fiber-reinforced resin material layers. Weighted material is configured to be compatible with and integrated into composite manufacturing processes used to fabricate the rotor blade. The weighted portion has a higher density than the composite portion and positioned to produce desired mass balance characteristics of the rotor blade.
摘要翻译：用于飞行器的转子叶片包括具有纤维增强树脂材料的复合部分，所述复合部分具有形成至少部分翼型形状的外表面。加权部分包括多个加权材料层和多个纤维增强树脂材料层。加权材料被配置为与用于制造转子叶片的复合制造工艺兼容并被集成。加权部分具有比复合部分更高的密度，并且定位成产生转子叶片的期望的质量平衡特性。

5. 发明授权

US09352830B2 Aircraft rotor with discrete flap hinge 有权
标题翻译：具有离散翼片铰链的飞机转子
公开(公告)号：US09352830B2
公开(公告)日：2016-05-31
申请号：US13455814
申请日：2012-04-25
申请人： Frank B. Stamps , David A. Popelka , Tom Donovan , Patrick R. Tisdale , Richard E. Rauber
发明人： Frank B. Stamps , David A. Popelka , Tom Donovan , Patrick R. Tisdale , Richard E. Rauber
IPC分类号： B64C27/39 , B64C27/48
CPC分类号： B64C27/39 , B64C27/48
摘要： An aircraft rotor assembly has upper and lower hub plates adapted to be mounted to a central rotor mast for rotation therewith. A plurality of radial arms is connected to at least two flap bearings mounted between the hub plates and forming a discrete flap hinge, each flap hinge defining a flap axis and allowing rotation of the associated arm relative to the hub plates and about the corresponding flap axis. Each of a plurality of blade grips is rotatably connected to one of the arms for rotation about a pitch axis and adapted for mounting of a blade to each blade grip, such that each blade is capable of rotation with the grip about the pitch axis and capable of rotation together with the corresponding arm relative to the hub plates and about the corresponding flap axis.
摘要翻译：飞机转子组件具有适于安装到中心转子桅杆上的上和下毂板，以与其一起旋转。多个径向臂连接到安装在轮毂板之间并形成离散的翼片铰链的至少两个翼片轴承，每个翼片铰链限定翼片轴线并允许相关联的臂相对于轮毂板和相应翼片轴线的旋转。多个叶片夹具中的每一个可旋转地连接到一个臂上，用于围绕俯仰轴线旋转，并适于将叶片安装到每个叶片手柄上，使得每个叶片能够围绕俯仰轴线旋转，并且能够与相应的臂相对于轮毂板和围绕相应的翼片轴线旋转。

6. 发明申请

US20130274961A1 Self Tuning Vibration Isolation System 有权
标题翻译：自调谐隔振系统
公开(公告)号：US20130274961A1
公开(公告)日：2013-10-17
申请号：US13444469
申请日：2012-04-11
申请人： Michael Seifert , Frank B. Stamps , Michael R. Smith , David E. Heverly
发明人： Michael Seifert , Frank B. Stamps , Michael R. Smith , David E. Heverly
IPC分类号： F16F9/50 , G05B13/02 , B64C27/51 , B64C19/00 , B64C1/06
CPC分类号： B64C27/001 , B64C2027/002 , B64C2027/004 , F16F13/06 , F16F13/24 , F16F15/002 , F16F15/027
摘要： A system and method to isolate vibrations from a vibrating structure. The system includes an adjustable vibration isolator that creates a reacting force matching the vibratory force of the vibrating structure. The method includes continuously monitoring the reacting force and vibratory force with a sensor system operably associated with a control unit having an algorithm to determine if adjustment of the vibration isolator is required. If required, the control unit commands a driver to selectively adjust the vibration isolator.
摘要翻译：将振动与振动结构隔离的系统和方法。该系统包括可调节隔振器，其产生与振动结构的振动力相匹配的反作用力。该方法包括使用与具有确定是否需要调节隔振器的算法的控制单元可操作地相关联的传感器系统连续地监测反作用力和振动力。如果需要，控制单元命令驾驶员选择性地调节隔振器。

7. 发明申请

US20130224025A1 Offset Stacked Yoke Hub for Tiltrotor Aircraft 有权
标题翻译：用于倾斜机的偏移堆叠式轭架
公开(公告)号：US20130224025A1
公开(公告)日：2013-08-29
申请号：US13405030
申请日：2012-02-24
申请人： Christopher Foskey , Frank B. Stamps
发明人： Christopher Foskey , Frank B. Stamps
IPC分类号： F01D7/00
CPC分类号： B64C27/33 , B64C27/35
摘要： A tiltrotor rotor hub comprises first and second configurations of yokes arranged in two parallel and axially offset planes, each having an equal number of two or more yokes substantially equally spaced about a mast, wherein a portion of each yoke overlaps with a portion of each azimuthally adjacent yoke. Another tiltrotor rotor hub is selectively positionable for operation in helicopter/airplane/transition modes and comprises substantially parallel and axially offset first and second planes, each containing a plurality of blade yokes arranged about a central axis and a portion of each yoke overlaps with a portion of each azimuthally adjacent yoke. Another tiltrotor rotor hub is coupled to a tiltrotor mast and comprises a stacked arrangement of blade yokes wherein a portion of each yoke overlaps with a portion of each azimuthally adjacent yoke, and a plurality of mounting components coupling each yoke to the overlapping azimuthally adjacent yoke.
摘要翻译：倾斜转子转子毂包括布置在两个平行和轴向偏移平面中的轭的第一和第二构造，每个具有相等数量的两个或更多个围绕桅杆等间隔的轭，其中每个轭的一部分与每个方位角的一部分重叠相邻的轭。另一个倾斜转子转子毂可选择定位以在直升机/飞机/转换模式中操作，并且包括基本上平行和轴向偏移的第一和第二平面，每个平面包含围绕中心轴布置的多个叶片轭，并且每个轭的一部分与一部分每个方位角相邻的轭。另一个倾斜旋转器转子毂联接到倾斜旋转桅杆并且包括叶片轭的堆叠布置，其中每个轭的一部分与每个方位角相邻的轭的一部分重叠，并且多个安装部件将每个轭耦合到重叠的方位角相邻的轭。

8. 发明申请

US20130216382A1 Hub Assembly with Centrifugal and Radial Bearings 有权
标题翻译：带离心轴承和径向轴承的轴毂组件
公开(公告)号：US20130216382A1
公开(公告)日：2013-08-22
申请号：US13400837
申请日：2012-02-21
申请人： Mark Wiinikka , Frank B. Stamps , Daniel P. Sottiaux , Zach Dailey
发明人： Mark Wiinikka , Frank B. Stamps , Daniel P. Sottiaux , Zach Dailey
IPC分类号： F01D7/00 , F01D5/02
CPC分类号： B64C27/35 , B64C27/605
摘要： A rotary system including a yoke having an opening forming a bridge for receiving a spoke extending therethrough. A rotor blade couples to the spoke and a pitch horn positioned outside the opening pitches the rotor blade during flight. A bearing assembly attaches the spoke and the pitch horn to the bridge and control blade forces exerted against the hub assembly during flight.
摘要翻译：一种旋转系统，包括具有开口的轭，所述开口形成用于容纳从其延伸穿过的辐条的桥。转子叶片耦合到轮辐，并且位于开口外侧的桨距角在飞行期间对转子叶片进行间距。轴承组件将辐条和桨距喇叭连接到桥上，并且在飞行期间控制施加在轮毂组件上的叶片力。

9. 发明申请

US20130175384A1 Bearing Restraint for Rotor Systems 有权
标题翻译：转子系统的轴承约束
公开(公告)号：US20130175384A1
公开(公告)日：2013-07-11
申请号：US13346912
申请日：2012-01-10
申请人： Chad L. Jarrett , Frank B. Stamps , Mark Wiinikka , Scott Hemmen
发明人： Chad L. Jarrett , Frank B. Stamps , Mark Wiinikka , Scott Hemmen
IPC分类号： B64C27/04 , B23P11/00 , B64D35/00 , B64C27/48
CPC分类号： B64C27/322 , B64C27/35
摘要： According to one embodiment, a rotor system comprises a yoke, a grip, an elastomeric bearing, and a bearing restraint. The grip is positioned around a portion of the yoke and has both a closed end and an open end. The elastomeric bearing is coupled to the closed end of the grip and located between the closed end and the yoke. The bearing restraint is coupled to the grip between the yoke and the open end at a distance from the closed end such that the yoke contacts the bearing restraint when the rotor system is subject to a first centrifugal force but does not contact the bearing restraint when the rotor system is subject to a second centrifugal force greater than the first centrifugal force
摘要翻译：根据一个实施例，转子系统包括轭，手柄，弹性体轴承和轴承约束件。把手位于轭的一部分周围，并且具有闭合端和开口端。弹性轴承联接到手柄的封闭端并且位于封闭端和轭之间。轴承约束件在轭和开口端之间的距离闭合端的距离处被联接，使得当转子系统受到第一离心力而不接触轴承约束时，轭与轴承约束接触转子系统经受大于第一离心力的第二离心力

10. 发明申请

US20130121827A1 Dual Mode Rotor Hub Assembly 有权
标题翻译：双模转子毂总成
公开(公告)号：US20130121827A1
公开(公告)日：2013-05-16
申请号：US13298033
申请日：2011-11-16
申请人： Frank B. Stamps , Patrick Tisdale , John Corrigan
发明人： Frank B. Stamps , Patrick Tisdale , John Corrigan
IPC分类号： B64C27/51 , B21D53/78 , B64C11/04
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运动。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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