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1. 发明申请

WO2007133735A2 YOKE WITH NOTCHED ARM ROOTS 审中-公开
标题翻译：与备注的ARM ROOTS
公开(公告)号：WO2007133735A2
公开(公告)日：2007-11-22
申请号：PCT/US2007/011532
申请日：2007-05-14
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , RAUBER, Richard, E. , POPELKA, David, A. , CAMPBELL, Thomas, C. , DONOVAN, Tom , TISDALE, Patrick, R.
发明人： STAMPS, Frank, B. , RAUBER, Richard, E. , POPELKA, David, A. , CAMPBELL, Thomas, C. , DONOVAN, Tom , TISDALE, Patrick, R.
IPC分类号： A63B21/02 , A63B21/04
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。

2. 发明申请

WO2008073073A3 STEP-OVER BLADE-PITCH CONTROL SYSTEM 审中-公开
公开(公告)号：WO2008073073A3
公开(公告)日：2008-06-19
申请号：PCT/US2006/046099
申请日：2006-12-08
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , RAUBER, Richard, E. , POPELKA, David, A. , TISDALE, Patrick, R. , CAMPBELL, Thomas, C. , BRASWELL, James, L., Jr. , STANNEY, Keith , WASIKOWSKI, Mark , DONOVAN, Tom , BASKIN, Bryan , SMITH, Ryan , CORRIGAN, John, J., III.
发明人： STAMPS, Frank, B. , RAUBER, Richard, E. , POPELKA, David, A. , TISDALE, Patrick, R. , CAMPBELL, Thomas, C. , BRASWELL, James, L., Jr. , STANNEY, Keith , WASIKOWSKI, Mark , DONOVAN, Tom , BASKIN, Bryan , SMITH, Ryan , CORRIGAN, John, J., III.
IPC分类号： B64C27/54 , F03B3/14
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.

3. 发明申请

WO2007081337A3 STIFF-IN-PLANE GIMBALED TILTROTOR HUB 审中-公开
公开(公告)号：WO2007081337A3
公开(公告)日：2007-07-19
申请号：PCT/US2006/001082
申请日：2006-01-13
申请人： BELL HELICOPTER TEXTRON INC. , RAUBER, Richard, E. , BRASWELL, James, L., Jr. , CAMPBELL, Thomas, C. , POPELKA, David, A. , SOUTHERLAND, Michael, J. , STAMPS, Frank, B. , STANNEY, Keith , TISDALE, Patrick, R. , WASIKOWSKI, Mark
发明人： RAUBER, Richard, E. , BRASWELL, James, L., Jr. , CAMPBELL, Thomas, C. , POPELKA, David, A. , SOUTHERLAND, Michael, J. , STAMPS, Frank, B. , STANNEY, Keith , TISDALE, Patrick, R. , WASIKOWSKI, Mark
IPC分类号： B64C27/48
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.

4. 发明申请

WO2010082935A1 YOKE AND BEARING FITTING ASSEMBLY FOR ROTORS 审中-公开
标题翻译：转子和轴承配件组装
公开(公告)号：WO2010082935A1
公开(公告)日：2010-07-22
申请号：PCT/US2009/031378
申请日：2009-01-19
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , TISDALE, Patrick, R. , CAMPBELL, Thomas, C. , RAUBER, Richard, E. , BRASWELL, James, L., Jr.
发明人： STAMPS, Frank, B. , TISDALE, Patrick, R. , CAMPBELL, Thomas, C. , RAUBER, Richard, E. , BRASWELL, James, L., Jr.
IPC分类号： B64C27/04
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并具有从主体的周边突出的两个轮缘的主体，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。

5. 发明申请

WO2010082936A1 STIFF-IN-PLANE ROTOR CONFIGURATION 审中-公开
标题翻译：棘轮式转子配置
公开(公告)号：WO2010082936A1
公开(公告)日：2010-07-22
申请号：PCT/US2009/031381
申请日：2009-01-19
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , TISDALE, Patrick, R. , DONOVAN, Tom , RAUBER, Richard, E.
发明人： STAMPS, Frank, B. , TISDALE, Patrick, R. , DONOVAN, Tom , RAUBER, Richard, E.
IPC分类号： B64C27/48
CPC分类号： B64C27/35 , B64C27/32 , B64C27/33 , B64C27/39 , B64C27/48
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。

6. 发明申请

WO2006132636A1 IMPROVED CONSTANT-VELOCITY JOINT FOR TILTROTOR HUBS 审中-公开
标题翻译：改进的恒定速度接头用于TILTROTOR HUBS
公开(公告)号：WO2006132636A1
公开(公告)日：2006-12-14
申请号：PCT/US2005/019979
申请日：2005-06-07
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , BRASWELL, James, L., Jr. , BASKIN, Charles, L. , ZIERER, Joe, J. , HAYNIE, David, A. , RAUBER, Richard, E. , CAMPBELL, Thomas , TISDALE, Patrick, R.
发明人： STAMPS, Frank, B. , BRASWELL, James, L., Jr. , BASKIN, Charles, L. , ZIERER, Joe, J. , HAYNIE, David, A. , RAUBER, Richard, E. , CAMPBELL, Thomas , TISDALE, Patrick, R.
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 link couple the yoke to the driver, each ling 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。多个直立连接器将轭架耦合到驱动器，每个引线可相对于轭，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。

7. 发明申请

WO2006081181A2 ASSEMBLY FOR PROVIDING FLEXURE TO BLADE SYSTEM 审中-公开
标题翻译：用于向刀片系统提供弯曲的组件
公开(公告)号：WO2006081181A2
公开(公告)日：2006-08-03
申请号：PCT/US2006/002284
申请日：2006-01-24
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , TISDALE, Patrick, R. , SHERRILL, Paul , RAUBER, Richard , CAMPBELL, Thomas, C. , BRASWELL, James, Lee, Jr. , MEASOM, Ron , HIROS, Tricia , POPELKA, David , SOUTHERLAND, Michael, J. , STANNEY, Keith , WASIKOWSKI, Mark , LEDBETTER, Tim
发明人： STAMPS, Frank, B. , TISDALE, Patrick, R. , SHERRILL, Paul , RAUBER, Richard , CAMPBELL, Thomas, C. , BRASWELL, James, Lee, Jr. , MEASOM, Ron , HIROS, Tricia , POPELKA, David , SOUTHERLAND, Michael, J. , STANNEY, Keith , WASIKOWSKI, Mark , LEDBETTER, Tim
IPC分类号： B64C27/50
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。

8. 发明申请

WO2009088495A1 CONSTANT-VELOCITY JOINT WITH TORQUE-COMBINING DIFFERENTIAL 审中-公开
标题翻译：恒定速度联合扭矩组合差异
公开(公告)号：WO2009088495A1
公开(公告)日：2009-07-16
申请号：PCT/US2008/050213
申请日：2008-01-04
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Frank, B. , TISDALE, Patrick, R.
发明人： STAMPS, Frank, B. , TISDALE, Patrick, R.
IPC分类号： B64C27/00
CPC分类号： B64C29/0033 , B64C27/32 , B64C27/41 , B64C2027/125 , F16D3/33 , Y10S464/904
摘要： A constant-velocity drive system for an aircraft rotor has a gimbal mechanism and a differential torque-combining mechanism. The gimbal mechanism has gimbals driven in rotation by a rotor mast about a mast axis, the gimbals providing for gimballing relative to the mast about gimbal axes generally perpendicular to the mast axis. The differential torque-combining mechanism is connected to the gimbal mechanism and configured to be driven in rotation about the mast axis by the gimbal mechanism. The differential mechanism is capable of gimballing relative to the mast about the gimbal axes, the differential torque-combining mechanism having an output component attached to a yoke of the rotor for driving the yoke in rotation with the differential torque- combining mechanism.
摘要翻译：用于飞行器转子的恒速驱动系统具有万向节机构和差动转矩组合机构。万向节机构具有围绕桅杆轴线的转子桅杆旋转驱动的万向节，所述万向架相对于桅杆提供关于通常垂直于桅杆轴线的万向轴线的槌球。差速转矩组合机构连接到万向节机构，并且构造成通过万向节机构围绕桅杆轴线旋转。该差速机构能够相对于桅杆围绕万向轴进行槌球，该差速扭矩组合机构具有附接到转子的轭的输出部件，用于通过差速转矩组合机构来旋转该轭。

9. 发明申请

WO2006086147A2 ASSEMBLY FOR PROVIDING FLEXURE TO BLADE SYSTEM 审中-公开
标题翻译：用于向刀片系统提供弯曲的组件
公开(公告)号：WO2006086147A2
公开(公告)日：2006-08-17
申请号：PCT/US2006/002413
申请日：2006-01-24
申请人： BELL HELICOPTER TEXTRON, INC. , STAMPS, Frank, B. , TISDALE, Patrick, R. , BRASWELL, James, L. , BASKIN, Charles, L., Jr. , CAMPBELL, Tom , LEDBETTER, Timothy, K. , ZIERER, Joseph, J. , REDDY, D., J. , WIINIKKA, Mark, A. , MARTIN, Ronnie, L. , HAYNIE, David, A. , SADLER, Stanley, Gene , MEASOM, Ron , OLDROYD, Paul , HIROS, Tricia , HARSE, Jim , MULLINS, Bob
发明人： STAMPS, Frank, B. , TISDALE, Patrick, R. , BRASWELL, James, L. , BASKIN, Charles, L., Jr. , CAMPBELL, Tom , LEDBETTER, Timothy, K. , ZIERER, Joseph, J. , REDDY, D., J. , WIINIKKA, Mark, A. , MARTIN, Ronnie, L. , HAYNIE, David, A. , SADLER, Stanley, Gene , MEASOM, Ron , OLDROYD, Paul , HIROS, Tricia , HARSE, Jim , MULLINS, Bob
IPC分类号： B64C27/33 , B64C27/51
CPC分类号： B64C27/48 , B64C27/33
摘要： An assembly for providing flexure to a blade of a rotary blade system, the assembly including 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 having a layer of cushioning material positioned thereon and secured thereto. The layer of cushioning material extending along and following the general contour of yoke surface, and the layer of cushioning material directly contacting a support plate. Another embodiment is 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.
摘要翻译：一种用于向旋转叶片系统的叶片提供挠曲的组件，该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。上和下磁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。缓冲材料层沿着轭铁表面的一般轮廓延伸并且沿着磁体表面的一般轮廓延伸，并且缓冲材料层直接接触支撑板。另一个实施例是用于向旋转刀片系统的刀片提供弯曲的组件，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板其中一个弯曲表面是不形成圆周的一部分的非圆弧。

10. 发明申请

WO2013002784A1 ROTOR HUB FOR USE WITH HIGH-INERTIA BLADES 审中-公开
标题翻译：用于高功率叶片的转子座
公开(公告)号：WO2013002784A1
公开(公告)日：2013-01-03
申请号：PCT/US2011/042350
申请日：2011-06-29
申请人： BELL HELICOPTER TEXTRON INC. , STAMPS, Franks, B. , TISDALE, Patrick, R. , YUCE, Mithal
发明人： STAMPS, Franks, B. , TISDALE, Patrick, R. , YUCE, Mithal
IPC分类号： B64C27/37
CPC分类号： B64C27/37 , B64C27/35
摘要： A rotor hub has a yoke with radial arms allowing flapping of connected blades about a flap axis. A grip is rigidly attached to each blade, and a lead-lag bearing connects each grip to one of the arms, the bearing defining a lead-lag axis outboard of the flap axis. Each arm has a pair of straps located on opposite sides of the rotor plane for transferring centrifugal force from the blades to the central portion of the yoke. A pair of lead-lag dampers is provided for each grip, the dampers of each pair being located on opposite sides of the rotor plane and connecting an inboard end portion of the grip to the adjacent strap. In-plane motion of a blade causes rotation of the attached grip about the lead-lag axis, causing opposite motion of an inboard end portion of the grip. The dampers act to oppose rotation of the grip.
摘要翻译：转子毂具有带有径向臂的轭，允许连接的叶片围绕翼片轴线振动。握把被刚性地附接到每个叶片，并且牵引延迟轴承将每个手柄连接到其中一个臂，所述轴承限定翼片轴线外侧的前后延伸轴线。每个臂具有位于转子平面的相对侧上的一对带，用于将离心力从叶片传递到轭的中心部分。为每个把手提供一对超前滞后阻尼器，每对的阻尼器位于转子平面的相对侧上，并将把手的内侧端部连接到相邻的带子上。刀片的平面内运动导致附接的把手围绕引线滞后轴线的旋转，引起把手的内侧端部部分的相反运动。阻尼器用于反对手柄的旋转。

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