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公开(公告)号：US08002251B2
公开(公告)日：2011-08-23
申请号：US11940032
申请日：2007-11-14
CPC分类号： F16F15/005 , B64G1/286 , F16C19/18 , F16C27/04 , F16C2326/47 , F16C2361/55 , Y10T74/1257 , Y10T74/1293
摘要： A vibration reduction system is provided for use in conjunction with a rotational device including a stationary body, a rotating body, and a first bearing assembly disposed between the stationary body and the rotating body. The vibration reduction system includes a first plurality of bearing mount actuators residing between the stationary body and the first bearing assembly. The first plurality of bearing mount actuators is configured to adjust the radial position of the first bearing assembly. The vibration reduction system further includes a vibration sensor, which is coupled to the stationary body, and a controller, which is coupled to the vibration sensor and to the first plurality of bearing mount actuators. The controller is configured to reduce vibrations sensed by the vibration sensor by selectively adjusting the radial position of the first bearing assembly utilizing the first plurality of bearing mount actuators.
摘要翻译： 提供一种与包括固定体，旋转体以及设置在固定体和旋转体之间的第一轴承组件的旋转装置结合使用的减振系统。 减振系统包括位于固定体和第一轴承组件之间的第一多个轴承安装致动器。 第一多个轴承安装致动器构造成调节第一轴承组件的径向位置。 减振系统还包括耦合到固定体的振动传感器和耦合到振动传感器和第一多个轴承安装致动器的控制器。 控制器被配置为通过利用第一多个轴承安装致动器选择性地调节第一轴承组件的径向位置来减少由振动传感器感测到的振动。
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公开(公告)号：US20090121399A1
公开(公告)日：2009-05-14
申请号：US11940032
申请日：2007-11-14
CPC分类号： F16F15/005 , B64G1/286 , F16C19/18 , F16C27/04 , F16C2326/47 , F16C2361/55 , Y10T74/1257 , Y10T74/1293
摘要： A vibration reduction system is provided for use in conjunction with a rotational device including a stationary body, a rotating body, and a first bearing assembly disposed between the stationary body and the rotating body. The vibration reduction system includes a first plurality of bearing mount actuators residing between the stationary body and the first bearing assembly. The first plurality of bearing mount actuators is configured to adjust the radial position of the first bearing assembly. The vibration reduction system further includes a vibration sensor, which is coupled to the stationary body, and a controller, which is coupled to the vibration sensor and to the first plurality of bearing mount actuators. The controller is configured to reduce vibrations sensed by the vibration sensor by selectively adjusting the radial position of the first bearing assembly utilizing the first plurality of bearing mount actuators.
摘要翻译： 提供一种与包括固定体，旋转体以及设置在固定体和旋转体之间的第一轴承组件的旋转装置结合使用的减振系统。 减振系统包括位于固定体和第一轴承组件之间的第一多个轴承安装致动器。 第一多个轴承安装致动器构造成调节第一轴承组件的径向位置。 减振系统还包括耦合到固定体的振动传感器和耦合到振动传感器和第一多个轴承安装致动器的控制器。 控制器被配置为通过利用第一多个轴承安装致动器选择性地调节第一轴承组件的径向位置来减少由振动传感器感测到的振动。
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公开(公告)号：US07690602B2
公开(公告)日：2010-04-06
申请号：US11394037
申请日：2006-03-29
IPC分类号： B64G1/28
CPC分类号： G05D1/0883 , B64G1/286 , B64G1/38
摘要： Methods and apparatus are provided for active motion damping of a spacecraft whose attitude control system (SACS) has experienced a partial failure. In a preferred embodiment, the apparatus comprises, an attitude control processor (ACP), a motion damping controller (MDC) coupled to the ACP, a control moment gyro (CMG) comprising a gimbal loop controller (GLC) coupled to the MDC and a gimbal motor with input coupled to the GLC and gyroscopic torque output coupled to the satellite. Normally, a gimbal rate command (GRC) from the ACP passes to the GLC for execution to rotate the CMG gimbal and the coupled satellite. If the ACP output becomes invalid, the MDC assumes control and can modify CMG operation in several ways to safely decelerate a moving satellite without hazardous mechanical stress. Following such active motion damping, the CMG remains quiescent until a RESET is received whereby further valid GRCs are then executable.
摘要翻译： 提供了用于姿态控制系统（SACS）经历部分故障的航天器的主动运动阻尼的方法和装置。 在优选实施例中，该装置包括姿态控制处理器（ACP），耦合到ACP的运动阻尼控制器（MDC），包括耦合到MDC的万向环控制器（GLC）的控制力矩陀螺仪（CMG）和 具有与GLC耦合的输入的万向电机和耦合到卫星的陀螺转矩输出。 通常，来自ACP的万向节速率命令（GRC）传递到GLC执行以旋转CMG万向节和耦合的卫星。 如果ACP输出无效，则MDC将采取控制，并可以通过多种方式修改CMG操作，以安全地减速运动的卫星，而不会产生有害的机械应力。 在这种主动运动阻尼之后，CMG保持静止，直到接收到RESET，从而可执行其它有效的GRC。
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公开(公告)号：US20080223990A1
公开(公告)日：2008-09-18
申请号：US11685931
申请日：2007-03-14
IPC分类号： B64G1/28
CPC分类号： B64G1/286
摘要： A system and method are provided for operating a control moment gyro (CMG) in a spacecraft. The CMG includes a spin motor, and a CMG rotor that is coupled to the spin motor and is configured to rotate about a spin axis. Electrical power from a power source is supplied to the spin motor to rotate the CMG rotor about the spin axis. A determination is made as to whether the power source can supply sufficient electrical power to the spin motor. If the power source cannot supply sufficient electrical power to the spin motor, the spin motor is rotated by the CMG rotor to generate and supply electrical power to the power source.
摘要翻译： 提供了一种用于操作航天器中的控制力矩陀螺（CMG）的系统和方法。 CMG包括旋转马达和耦合到旋转马达的CMG转子，并被配置为围绕旋转轴旋转。 来自电源的电力被提供给旋转电机以使CMG转子围绕旋转轴旋转。 确定电源是否能够向旋转电机提供足够的电力。 如果电源不能向旋转电机提供足够的电力，则旋转电机由CMG转子旋转以产生电源并向电源供电。
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公开(公告)号：US07325769B1
公开(公告)日：2008-02-05
申请号：US11067038
申请日：2005-02-25
申请人： Paul E. Harnisch , Robert E. Winkel
发明人： Paul E. Harnisch , Robert E. Winkel
IPC分类号： F42B10/64
CPC分类号： F42B10/64
摘要： Methods and apparatus are provided for a missile that includes a housing, a fin, and a first actuator. The housing has a slot formed therethrough. The fin is disposed within the housing proximate the slot. The first actuator is coupled to the fin and configured to selectively move the fin at least partially in and out of the housing through the slot.
摘要翻译： 为包括壳体，翅片和第一致动器的导弹提供了方法和装置。 壳体具有穿过其中形成的槽。 翅片设置在靠近狭槽的壳体内。 第一致动器联接到翅片并且构造成选择性地将鳍片至少部分地移入和移出壳体通过狭槽。
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公开(公告)号：US20080029642A1
公开(公告)日：2008-02-07
申请号：US11067038
申请日：2005-02-25
申请人： Paul E. Harnisch , Robert E. Winkel
发明人： Paul E. Harnisch , Robert E. Winkel
IPC分类号： F42B15/01
CPC分类号： F42B10/64
摘要： Methods and apparatus are provided for a missile that includes a housing, a fin, and a first actuator. The housing has a slot formed therethrough. The fin is disposed within the housing proximate the slot. The first actuator is coupled to the fin and configured to selectively move the fin at least partially in and out of the housing through the slot.
摘要翻译： 为包括壳体，翅片和第一致动器的导弹提供了方法和装置。 壳体具有穿过其中形成的槽。 翅片设置在靠近狭槽的壳体内。 第一致动器联接到翅片并且构造成选择性地将鳍片至少部分地移入和移出壳体通过狭槽。
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公开(公告)号：US07299817B2
公开(公告)日：2007-11-27
申请号：US10933093
申请日：2004-09-01
CPC分类号： B64G1/286 , F16K17/087 , Y10T137/1939 , Y10T137/2012 , Y10T137/7905
摘要： A valve is provided for use on a control moment gyroscope (CMG) having a housing separating an internal environment from an external environment. The valve includes a valve housing, a valve element, and bellows. The valve housing is configured to couple to the CMG housing and includes an inner surface defining a cavity, an outer surface, and an opening extending therebetween. The valve element is disposed within the valve housing cavity and is movable between a closed position, in which fluid is prevented from flowing through the valve housing opening, and an open position, in which fluid may flow through the valve housing opening. The bellows is disposed within the valve housing and coupled to the valve element and has an internal chamber. The bellows selectively moves the valve element closed and open in response to a differential pressure between the bellows internal chamber and the valve housing cavity.
摘要翻译： 提供一种用于在具有将内部环境与外部环境分离的壳体的控制力矩陀螺仪（CMG）上使用的阀。 阀包括阀壳体，阀元件和波纹管。 阀壳体构造成联接到CMG壳体并且包括限定空腔的内表面，外表面和在其间延伸的开口。 阀元件设置在阀壳体腔内，并且可在阻止流体流过阀壳体开口的关闭位置和流体可流过阀壳体开口的打开位置之间移动。 波纹管设置在阀壳体内并联接到阀元件并具有内部腔室。 波纹管响应于波纹管内部腔室和阀壳体空腔之间的压差而选择性地将阀门元件关闭并打开。
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公开(公告)号：US07721998B2
公开(公告)日：2010-05-25
申请号：US11685931
申请日：2007-03-14
IPC分类号： B64G1/28
CPC分类号： B64G1/286
摘要： A system and method are provided for operating a control moment gyro (CMG) in a spacecraft. The CMG includes a spin motor, and a CMG rotor that is coupled to the spin motor and is configured to rotate about a spin axis. Electrical power from a power source is supplied to the spin motor to rotate the CMG rotor about the spin axis. A determination is made as to whether the power source can supply sufficient electrical power to the spin motor. If the power source cannot supply sufficient electrical power to the spin motor, the spin motor is rotated by the CMG rotor to generate and supply electrical power to the power source.
摘要翻译： 提供了一种用于操作航天器中的控制力矩陀螺（CMG）的系统和方法。 CMG包括旋转马达和耦合到旋转马达的CMG转子，并被配置为围绕旋转轴旋转。 来自电源的电力被提供给旋转电机以使CMG转子围绕旋转轴旋转。 确定电源是否能够向旋转电机提供足够的电力。 如果电源不能向旋转电机提供足够的电力，则旋转电机由CMG转子旋转以产生电源并向电源供电。
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公开(公告)号：US20090100957A1
公开(公告)日：2009-04-23
申请号：US11877409
申请日：2007-10-23
IPC分类号： G01C19/06
CPC分类号： B64G1/283 , B64G1/286 , F16C19/08 , F16C19/54 , F16C33/581 , F16C2370/00 , G01C19/18 , Y10T74/12
摘要： A rotor assembly includes a rotor assembly housing, a shaft, a bearing assembly coupling the shaft to the rotor assembly housing, and a mass structure coupled to and rotatable with the shaft. The bearing assembly includes a bearing housing, a first raceway defined in the bearing housing, a second raceway defined in the shaft, and a plurality of ball bearings positioned within the first and second raceways to enable the shaft to rotate relative to the rotor assembly housing.
摘要翻译： 转子组件包括转子组件壳体，轴，将轴联接到转子组件壳体的轴承组件，以及联接到轴上并与轴可旋转的质量结构。 所述轴承组件包括轴承壳体，限定在所述轴承壳体中的第一滚道，限定在所述轴中的第二滚道以及定位在所述第一和第二滚道内的多个滚珠轴承，以使所述轴能够相对于所述转子组件壳体旋转 。
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公开(公告)号：US07000308B2
公开(公告)日：2006-02-21
申请号：US10062182
申请日：2002-01-31
申请人： Stephen E. Fiske , Robert E. Winkel
发明人： Stephen E. Fiske , Robert E. Winkel
IPC分类号： H02K15/02
CPC分类号： G01C19/06 , B64G1/283 , B64G1/286 , Y10T29/49009 , Y10T29/49012 , Y10T29/49988 , Y10T29/53143 , Y10T74/12
摘要： A method of constructing a rotor for a gyroscopic device is provided comprising fabricating a unitary assembly comprising a rim, a hollow shaft, a hub at each end of the shaft, a web that extends radially inward from the rim to one of the hubs at an angle to a spin axis of the rotor and machining the assembly. A second web may be welded between the rim and the second hub.
摘要翻译： 提供了一种构造用于陀螺装置的转子的方法，包括制造整体组件，其包括边缘，中空轴，在轴的每一端的轮毂，沿着轮缘径向向内延伸到其中一个轮毂的腹板 与转子的旋转轴线成角度并加工组件。 第二腹板可以焊接在轮辋和第二轮毂之间。
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