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1. 发明授权

US08287237B2 Step-over blade-pitch control system 有权
标题翻译：分步桨叶桨距控制系统
公开(公告)号：US08287237B2
公开(公告)日：2012-10-16
申请号：US12446597
申请日：2006-12-08
申请人： Frank B. Stamps , Richard E. Rauber , David A. Popelka , Patrick R. Tisdale , Thomas C. Campbell , Keith Stanney , James L. Braswell, Jr. , Mark Wasikowski , Tom Donovan , Bryan Baskin , John J. Corrigan, III , Ryan Smith
发明人： Frank B. Stamps , Richard E. Rauber , David A. Popelka , Patrick R. Tisdale , Thomas C. Campbell , Keith Stanney , James L. Braswell, Jr. , Mark Wasikowski , Tom Donovan , Bryan Baskin , John J. Corrigan, III , Ryan Smith
IPC分类号： B64C11/06
CPC分类号： B64C11/30 , B64C27/605 , B64C29/0033
摘要： A pitch control system for blades on a rotor of an aircraft has a gimballing rotor hub (31) and a plurality of step-over arms (61) connected to the hub and capable of pivoting relative to the hub about a pivot axis. Each of a plurality of pitch links (55) connects one of the step-over arms (61) to a flight control system for pivoting the connected step-over arm (61) about the pivot axis and relative to the hub in response to inputs from the control system. Each of a plurality of step-over links (69) connects one of the step-over arms (61) to one of the blades for rotating the associated blade about the pitch axis in response to pivoting of the associated step-over arm.
摘要翻译：用于飞行器转子上的叶片的俯仰控制系统具有连接到轮毂并且能够相对于轮毂围绕枢转轴线枢转的槌球转子轮毂（31）和多个步进臂（61）。多个节距连杆（55）中的每一个将步进臂（61）中的一个连接到飞行控制系统，用于响应于输入而围绕枢转轴线和相对于轮毂枢转连接的分离臂（61）从控制系统。多个翻转链节（69）中的每一个将分阶臂（61）中的一个连接到其中一个叶片，用于响应于相关联的分步臂的枢转而围绕俯仰轴旋转相关叶片。

2. 发明申请

US20100021301A1 Step-Over Blade-Pitch Control System 有权
标题翻译：叶片间距控制系统
公开(公告)号：US20100021301A1
公开(公告)日：2010-01-28
申请号：US12446597
申请日：2006-12-08
申请人： Frank B. Stamps , Rlohard E. Rauber , David A. Popelka , Patrick R. Tisdale , Thomas C. Campbell , James L. Braswell, JR. , Keith Stanney , Mark Wasikowski , Tom Donovan , Bryan Baskin , Ryan Smith
发明人： Frank B. Stamps , Rlohard E. Rauber , David A. Popelka , Patrick R. Tisdale , Thomas C. Campbell , James L. Braswell, JR. , Keith Stanney , Mark Wasikowski , Tom Donovan , Bryan Baskin , Ryan Smith
IPC分类号： B64C27/54
CPC分类号： B64C11/30 , B64C27/605 , B64C29/0033
摘要： A pitch control system for blades on a rotor of an aircraft has a gimballing rotor hub (31) and a plurality of step-over arms (61) connected to the hub and capable of pivoting relative to the hub about a pivot axis. Each of a plurality of pitch links (55) connects one of the step-over arms (61) to a flight control system for pivoting the connected step-over arm (61) about the pivot axis and relative to the hub in response to inputs from the control system. Each of a plurality of step-over links (69) connects one of the step-over arms (61) to one of the blades for rotating the associated blade about the pitch axis in response to pivoting of the associated step-over arm.
摘要翻译：用于飞行器转子上的叶片的俯仰控制系统具有连接到轮毂并且能够相对于轮毂围绕枢转轴线枢转的槌球转子轮毂（31）和多个步进臂（61）。多个节距连杆（55）中的每一个将步进臂（61）中的一个连接到飞行控制系统，用于响应于输入而围绕枢转轴线和相对于轮毂枢转连接的分离臂（61）从控制系统。多个翻转链节（69）中的每一个将分阶臂（61）中的一个连接到其中一个叶片，用于响应于相关联的分步臂的枢转而围绕俯仰轴旋转相关叶片。

3. 发明授权

US08360727B2 Yoke and bearing fitting assembly for rotors 有权
标题翻译：用于转子的轭和轴承配件组件
公开(公告)号：US08360727B2
公开(公告)日：2013-01-29
申请号：US13144510
申请日：2009-01-19
申请人： Frank B. Stamps , Patrick R. Tisdale , Thomas C. Campbell , Richard E. Rauber , James L. Braswell, Jr.
发明人： Frank B. Stamps , Patrick R. Tisdale , Thomas C. Campbell , Richard E. Rauber , James L. Braswell, Jr.
IPC分类号： B64C27/37
CPC分类号： B64C27/33 , B64C27/32
摘要： A yoke and bearing fitting assembly for a multi-blade aircraft rotor is disclosed. The assembly has a yoke having arms extending generally radially from a central portion of the yoke, the arms each having opposing surfaces. An aperture is formed in each arm and extends between the surfaces. A bearing fitting has a body configured for insertion into the aperture of the yoke and has two rims protruding from a periphery of the body, the body also having a bearing mount adapted for mounting a pitch change bearing assembly to the yoke. Each rim abuts one of the surfaces of the associated yoke arm when the bearing fitting is installed within the aperture, so as to create clamping forces between the rims and the arm and the arm. The bearing fitting transmits forces from the pitch bearing assembly into the yoke.
摘要翻译：公开了一种用于多叶片飞行器转子的轭和轴承配件组件。组件具有轭，其具有从轭的中心部分大致径向延伸的臂，每个臂具有相对的表面。在每个臂中形成一个孔，并在表面之间延伸。轴承配件具有构造成用于插入轭的孔中的主体，并且具有从主体的周边突出的两个轮缘，该主体还具有适于将变桨轴承组件安装到轭的轴承座。当轴承配件安装在孔内时，每个轮辋邻接相关联的轭臂的一个表面，以便在轮辋与臂和臂之间产生夹紧力。轴承配件将变桨轴承组件的力传递到轭架中。

4. 发明授权

US07867096B2 Joint for tiltrotor hubs 有权
标题翻译：接头用于倾斜旋转轮毂
公开(公告)号：US07867096B2
公开(公告)日：2011-01-11
申请号：US11916009
申请日：2005-06-07
申请人： Frank B. Stamps , James L. Braswell, Jr. , Charles L. Baskin , Joe J. Zierer , David A. Haynie , Richard E. Rauber , Thomas C. Campbell , Patrick R. Tisdale
发明人： Frank B. Stamps , James L. Braswell, Jr. , Charles L. Baskin , Joe J. Zierer , David A. Haynie , Richard E. Rauber , Thomas C. Campbell , Patrick R. Tisdale
IPC分类号： F16D3/08
CPC分类号： F16D3/48 , B64C27/14 , F16D3/28 , F16D3/78
摘要： A joint is configured for use with a rotary-wing aircraft having at least one engine. A driver is coupled to an output shaft of the engine, the driver being rotatable about an axis. A yoke is at least partially rotatable relative to the driver about a first center of rotation, the center of rotation being located on the axis. A plurality of upright links couple the yoke to the driver, each link being translatable relative to the yoke, the driver, or both. Each link is also rotatable relative to the yoke, the driver, or both, about a second center of rotation.
摘要翻译：接头构造成与具有至少一个发动机的旋翼飞机一起使用。驾驶员联接到发动机的输出轴，驾驶员可绕轴线旋转。轭围绕第一旋转中心相对于驾驶员至少部分可旋转，旋转中心位于轴上。多个直立连杆将轭轭联接到驱动器，每个连杆可相对于轭，驱动器或两者平移。每个连杆也可相对于轭，驱动器或两者围绕第二旋转中心旋转。

5. 发明申请

US20090325718A1 Constant Velocity Joint for Tiltrotor Hubs 有权
标题翻译：恒转轮毂恒速接头
公开(公告)号：US20090325718A1
公开(公告)日：2009-12-31
申请号：US11916009
申请日：2005-06-07
申请人： Frank B. Stamps , James L. Braswell, JR. , Charles L. Baskin , Joe J. Zierer , David A. Haynie , Richard E. Rauber , Thomas C. Campbell , Patrick R. Tisdale
发明人： Frank B. Stamps , James L. Braswell, JR. , Charles L. Baskin , Joe J. Zierer , David A. Haynie , Richard E. Rauber , Thomas C. Campbell , Patrick R. Tisdale
IPC分类号： F16D3/48
CPC分类号： F16D3/48 , B64C27/14 , F16D3/28 , F16D3/78
摘要： A constant-velocity joint is configured for use with a rotary-wing aircraft having at least one engine. A driver is coupled to an output shaft of the engine, the driver being rotatable about an axis. A yoke is at least partially rotatable relative to the driver about a first center of rotation, the center of rotation being located on the axis. A plurality of upright links couple the yoke to the driver, each link being translatable relative to the yoke, the driver, or both. Each link is also rotatable relative to the yoke, the driver, or both, about a second center of rotation.
摘要翻译：等速万向节被构造成与具有至少一个发动机的旋翼飞行器一起使用。驾驶员联接到发动机的输出轴，驾驶员可绕轴线旋转。轭围绕第一旋转中心相对于驾驶员至少部分可旋转，旋转中心位于轴上。多个直立连杆将轭轭联接到驱动器，每个连杆可相对于轭，驱动器或两者平移。每个连杆也可相对于轭，驱动器或两者围绕第二旋转中心旋转。

6. 发明申请

US20130287576A1 Aircraft Rotor with Discrete Flap Hinge 有权
标题翻译：飞机转子与离散瓣铰链
公开(公告)号：US20130287576A1
公开(公告)日：2013-10-31
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： B64C27/54
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。

7. 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。

8. 发明授权

US07845909B2 Assembly for providing flexure to blade system 有权
标题翻译：用于向刀片系统提供弯曲的组件
公开(公告)号：US07845909B2
公开(公告)日：2010-12-07
申请号：US11794850
申请日：2006-01-24
申请人： Frank B. Stamps , Patrick R. Tisdale , Paul Sherrill , Richard Rauber , Thomas C. Campbell , James Lee Braswell, Jr. , Ron Measom , Tricia Hiros , David Popelka , Michael J. Southerland , Keith Stanney , Mark Wasikowski , Tim Ledbetter
发明人： Frank B. Stamps , Patrick R. Tisdale , Paul Sherrill , Richard Rauber , Thomas C. Campbell , James Lee Braswell, Jr. , Ron Measom , Tricia Hiros , David Popelka , Michael J. Southerland , Keith Stanney , Mark Wasikowski , Tim Ledbetter
IPC分类号： B63H1/06
CPC分类号： B64C27/48 , B64C27/33
摘要： An assembly for providing flexure to a blade of a rotary blade system includes an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween. At least one of the upper and lower yoke surfaces has a layer of cushioning material positioned thereon and secured thereto. An alternate embodiment includes an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween and directly contacting the support plates wherein one of the curved surfaces is a non-circular arc that does not form part of the circumference of a circle. Another alternate embodiment includes a similar assembly having a twist-shank type of yoke for providing rotation of attached blades about their respective pitch axes.
摘要翻译：用于向旋转刀片系统的刀片提供挠曲的组件包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的轭。上和下轭表面中的至少一个具有定位在其上并固定到其上的缓冲材料层。替代实施例包括用于向旋转刀片系统的刀片提供挠曲的组件，包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的直接接触支撑件其中一个弯曲表面是不形成圆周的一部分的非圆弧。另一替代实施例包括具有扭转柄类型的轭的类似组件，用于提供附接刀片围绕它们各自的俯仰轴的旋转。

9. 发明申请

US20080101934A1 Assembly for Providing Flexure to Blade System 有权
标题翻译：为刀片系统提供弯曲的组装
公开(公告)号：US20080101934A1
公开(公告)日：2008-05-01
申请号：US11794850
申请日：2006-01-24
申请人： Frank B. Stamps , Patrick R. Tisdale , Paul Sherrill , Richard Rauber , Thomas C. Campbell , James Lee Braswell Jr. , Ron Measom , Tricia Hiros , David Popelka , Michael J. Southerland , Keith Stanney , Mark Wasikowski , Tim Ledbetter
发明人： Frank B. Stamps , Patrick R. Tisdale , Paul Sherrill , Richard Rauber , Thomas C. Campbell , James Lee Braswell Jr. , Ron Measom , Tricia Hiros , David Popelka , Michael J. Southerland , Keith Stanney , Mark Wasikowski , Tim Ledbetter
IPC分类号： B64C11/12 , B64C27/48
CPC分类号： B64C27/48 , B64C27/33
摘要： An assembly for providing flexure to a blade of a rotary blade system includes an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween. At least one of the upper and lower yoke surfaces has a layer of cushioning material positioned thereon and secured thereto. An alternate embodiment includes an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween and directly contacting the support plates wherein one of the curved surfaces is a non-circular arc that does not form part of the circumference of a circle. Another alternate embodiment includes a similar assembly having a twist-shank type of yoke for providing rotation of attached blades about their respective pitch axes.
摘要翻译：用于向旋转刀片系统的刀片提供挠曲的组件包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的轭。上和下轭表面中的至少一个具有定位在其上并固定到其上的缓冲材料层。替代实施例包括用于向旋转刀片系统的刀片提供挠曲的组件，包括具有上曲面的上支撑板，具有下弯曲表面的下支撑板和位于其间的直接接触支撑件其中一个弯曲表面是不形成圆周的一部分的非圆弧。另一替代实施例包括具有扭转柄类型的轭的类似组件，用于提供附接刀片围绕它们各自的俯仰轴的旋转。

10. 发明申请

US20090179107A1 Yoke with Notched Arm Roots 有权
标题翻译：具有缺口臂根的轭
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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