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1. 发明授权

EP2018516B1 GYRO POWER STARTER 有权
标题翻译：性能STARTER一种旋转
公开(公告)号：EP2018516B1
公开(公告)日：2016-05-18
申请号：EP07755471.5
申请日：2007-04-16
申请人： Floyd, Tom Smith
发明人： DWORZAN, Bill
IPC分类号： A63B21/012 , A63B21/22 , G01C19/04 , G01C19/08 , A63B21/015
CPC分类号： G01C19/04 , A63B21/012 , A63B21/015 , A63B21/22 , A63B21/222 , G01C19/08 , Y10T74/1246 , Y10T74/1254 , Y10T74/1282

2. 发明授权

EP2265843B1 GEAR DEVICE AND METHOD FOR PROVIDING A ROTARY MOTION 有权转让
标题翻译：传输装置及方法，用于产生旋转运动
公开(公告)号：EP2265843B1
公开(公告)日：2013-04-17
申请号：EP08735274.6
申请日：2008-04-17
申请人： Erke Erke Arastirmalari Ve Mühendislik A.S.
发明人： OZTÜRK, Mustafa, Naci
IPC分类号： F16H33/10
CPC分类号： F16H33/10 , Y10T74/1254

3. 发明公开

EP2080701A1 Control moment gyroscope 有权
标题翻译：控制力矩陀螺仪
公开(公告)号：EP2080701A1
公开(公告)日：2009-07-22
申请号：EP09150569.3
申请日：2009-01-14
申请人： Honeywell International Inc.
发明人： Stevens, Carlos J. , Fiske, Stephen E.
IPC分类号： B64G1/28 , G05D1/08
CPC分类号： B64G1/286 , Y10T74/1229 , Y10T74/1254 , Y10T74/1282
摘要： A control moment gyroscope (CMG (50,120)) is provided for deployment on a spacecraft. The CMG includes a stator housing (52,122), an inner gimbal assembly (54,124) disposed in the stator housing, and a torque motor (94,138) coupled to the stator housing and at least partially disposed around an intermediate portion (78) of the inner gimbal assembly. The torque motor is configured to rotate the inner gimbal assembly about a gimbal axis (56,140).
摘要翻译：控制力矩陀螺仪（CMG（50,120））用于在航天器上部署。 CMG包括定子壳体（52,122），布置在定子壳体中的内万向节组件（54,124）以及联接到定子壳体并且至少部分地围绕内部的内部中间部分（78）设置的转矩马达（94,138）万向节组装。扭矩马达构造成围绕万向节轴线（56,140）旋转内部万向节组件。

4. 发明授权

EP1485292B1 ACTIONNEUR GYROSCOPIQUE DE PILOTAGE DE L'ATTITUDE D'UN VEHICULE SPATIAL 有权转让
标题翻译：控制力矩陀螺用于航天位置控制
公开(公告)号：EP1485292B1
公开(公告)日：2008-07-23
申请号：EP03727593.0
申请日：2003-03-18
申请人： EADS ASTRIUM SAS
发明人： DEFENDINI, Ange , GUAY, Pascal , FAUCHEUX, Philippe
IPC分类号： B64G1/28 , G05D1/08 , G01C19/02
CPC分类号： B64G1/286 , Y10T74/12 , Y10T74/1254 , Y10T74/138
摘要： The invention relates to a control moment gyro comprising a wheel support structure (12) which is mounted on a base (10) by means of a motor, which is used to rotate the support structure around a first axis (z), and bearing a wheel (14) which is equipped with means of driving the wheel spinner at a high speed around a second axis (x) perpendicular to the first. The aforementioned support structure or gimbal comprises a tubular part which rotates on the base and a flange which is disposed on only one side of the wheel and which is fixed to (i) said wheel and (ii) the tubular part. The diameter of the wheel and the point at which the wheel is fixed to the flange are proportioned such that the wheel penetrates the tubular part.

5. 发明公开

EP1639314A1 GYROSCOPIC ROLL STABILIZER FOR BOATS 审中-公开
标题翻译：船用陀螺仪滚动稳定器
公开(公告)号：EP1639314A1
公开(公告)日：2006-03-29
申请号：EP04785693.5
申请日：2004-05-11
申请人： Gearloose Engineering, LLC
发明人： ADAMS, John, D. , McKenney, Shepard W.
IPC分类号： G01C19/30
CPC分类号： B63B39/04 , Y10T74/1218 , Y10T74/1229 , Y10T74/1254
摘要： A gyroscopic roll stabilizer for a boat. The stabilizer includes a flywheel, a flywheel drive motor configured to spin the flywheel about a spin axis, an enclosure surrounding a portion or all of the flywheel and maintaining a below-ambient pressure or containing a below-ambient density gas, a gimbal structure configured to permit flywheel precession about a gimbal axis, and a device for applying a torque to the flywheel about the gimbal axis. The flywheel, enclosure, and gimbal structure are configured so that when installed in the boat the stabilizer damps roll motion of the boat. Preferably, the flywheel drive motor spins the flywheel at high tip speeds.
摘要翻译：船上的陀螺卷稳定器。稳定器包括飞轮，构造成使飞轮绕旋转轴线旋转的飞轮驱动马达，围绕飞轮的一部分或全部并且保持低于环境压力或包含低于环境密度的气体的外壳，配置为万向节结构的万向节结构以允许围绕万向轴的飞轮进动，以及用于围绕万向轴向飞轮施加转矩的装置。飞轮，外壳和万向架结构的配置使得当安装在船上时，稳定器可以阻止船的滚动。优选地，飞轮驱动马达以高尖端速度旋转飞轮。

6. 发明公开

EP1490654A1 INERTIAL CONTROL AND MEASUREMENT SYSTEM 审中-公开
标题翻译：惯性控制和测量系统
公开(公告)号：EP1490654A1
公开(公告)日：2004-12-29
申请号：EP03716885.3
申请日：2003-03-31
申请人： Honeywell International Inc.
发明人： HYDE, Tristram, T. , DAVIS, Lawrence, P.
IPC分类号： G01C19/30 , B64G1/28 , B64C17/06
CPC分类号： B64G1/288 , B64G1/286 , G01C19/30 , Y10T74/1246 , Y10T74/1254
摘要： An inertial control and measurement system is provided for applying inertial control to a vehicle and measuring angular rate of the vehicle. The system includes a control moment gyroscope having a spinning rotor, a gimbal, a gimbal support assembly attached to a spacecraft for allowing rotation of the gimbal about a gimbal axis, and a gimbal motor for rotating the gimbal about the gimbal axis to induce torque. A controller controls the gimbal motor to generate a control torque. The controller further determines an angular rate of the vehicle as a function of a determined torque and a gimbal angle acceleration.

7. 发明授权

EP0007378B1 GYROSCOPIC METHOD AND APPARATUS FOR DETERMINING MAGNETIC HEADING AND ATTITUDE 失效
标题翻译：用于确定磁头和姿态的陀螺仪方法和装置
公开(公告)号：EP0007378B1
公开(公告)日：1984-01-25
申请号：EP78900274.8
申请日：1978-10-30
申请人： CESSNA AIRCRAFT COMPANY
发明人： MOORE, Nathaniel, Newton
IPC分类号： G01C19/36 , G01C17/28 , G05D1/08
CPC分类号： G01C19/44 , G01C17/28 , G01C19/28 , G01C19/36 , Y10T74/1254
摘要： A gyroscopic device of the type having a short-circuited rotor winding or conductor (10) so shaped so as to produce axial and radial flux components when rotated in the earth's magnetic field is coupled to a coaxial sensing coil (15) coaxial which gyroscopically stabilized thereby, signals induced in the sensing coil due to the axial flux component of the rotor is used to derive magnetic heading information and there is provided at least one further coil (41) on the supporting body and inductively linked to the sensing coil and rotor such that when the sensing coil is gyroscopically stabilized by the rotor, the coil supported on the supporting body in relation to the gyroscopically stabilized sensing coil is such that any changes in angular orientation of the supporting body relative to the gyroscopically stabilized sensing coil introduces changes in the signal voltages induced in the coils. The further coil on the supporting body may be excited with one or more excitation signals of a frequency different than the angular speed of the rotor (10) and constituted by pairs of orthogonally related coils on all three axes namely, the roll (41, 42), pitch (43, 44) and yaw (45, 46) axes. The coil located on the yaw axis is coaxial with the gyroscopically stabilized sensing coil in the rest position and is used for eliminating ambiguities.

8. 发明公开

EP0016807A1 MOLDED INERTIAL SENSOR. 失效
标题翻译： GEFORMTER惯性传感器。
公开(公告)号：EP0016807A1
公开(公告)日：1980-10-15
申请号：EP79900965
申请日：1980-03-11
申请人： DRAPER LAB CHARLES S
发明人： SCHLUNTZ ROY A , STEMNISKI JOHN R
IPC分类号： G01C19/02 , G01C19/04 , G01C19/42 , G01C25/00
CPC分类号： G01C19/04 , G01C25/00 , Y10T74/12 , Y10T74/1254 , Y10T74/1275 , Y10T74/1282
摘要： Des elements de structure (13, 16, 18) d'un senseur d'inertie (10) sont fabriques a partir de materiau plastique moule. Les elements de structure (13, 16, 18) se caracterisent par des sections relativement petites, et comprennent en outre des cles et des passages de cle ainsi que des fentes de guidage et d'alignement (40, 42), amenagees par moulage dans les elements (13, 16, 18) pour accoupler plusieurs elements de structure.
摘要翻译：惯性传感器（10）的结构元件（13,16,18）由模制塑料材料制成。结构元件（13,16,18）的特征在于相对较小的横截面，并且还包括键和键槽以及导向和对准槽（40,42），其模制在元件（13,16,18）用于连接多个结构元件。

9. 发明公开

EP2103519A1 Signal torque module assembly for use in control moment gyroscope 有权
标题翻译： einem Steuermoment-Gyroskop的Signaldrehmomentmodulanordnung zur Verwendung
公开(公告)号：EP2103519A1
公开(公告)日：2009-09-23
申请号：EP09153465.1
申请日：2009-02-23
申请人： Honeywell International Inc.
发明人： Buchele, Paul , Davis, Torey
IPC分类号： B64G1/28
CPC分类号： B64G1/286 , F16H1/46 , Y10T74/1254 , Y10T74/1282
摘要： A signal torque module assembly (STMA (22)) is provided for use within a control moment gyroscope (20) of the type that includes a rotor assembly (29). In one embodiment, the STMA comprises a torque module assembly (TMA (60)), which includes: (i) a TMA housing (68), (ii) a torque motor (80) coupled to the TMA housing, and (iii) a gear train (72) coupled to the TMA housing and mechanically coupling the torque motor to the rotor assembly. A signal module assembly (62) is coupled to the TMA housing, and an elongated connector (102) electrically couples the signal module assembly and the rotor assembly. The elongated connector extends through the gear train.
摘要翻译：提供信号扭矩模块组件（STMA（22）），用于在包括转子组件（29）的类型的控制力矩陀螺仪（20）内使用。在一个实施例中，STMA包括扭矩模块组件（TMA（60）），其包括：（i）TMA壳体（68），（ii）联接到TMA壳体的扭矩马达（80），以及（iii）齿轮系（72），其联接到所述TMA壳体并且将所述扭矩马达机械地联接到所述转子组件。信号模块组件（62）联接到TMA壳体，并且细长连接器（102）电耦合信号模块组件和转子组件。细长连接器延伸穿过齿轮系。

10. 发明公开

EP1979189A2 STABILITY-ENHANCED TRACTION AND YAW CONTROL USING ELECTRONICALLY CONTROLLED LIMITED-SLIP DIFFERENTIAL 有权转让
标题翻译：电子控制的限滑差速器，稳定性USED牵引控制和贪婪
公开(公告)号：EP1979189A2
公开(公告)日：2008-10-15
申请号：EP07705516.8
申请日：2007-02-02
申请人： Eaton Corporation
发明人： PIYABONGKARN, Damrongrit , LEW, Jae, Y. , GROGG, John, A. , KYLE, Robert, J.
IPC分类号： B60K23/04
CPC分类号： B60K17/16 , B60K17/34 , B60K23/04 , B60T2201/14 , B60W2520/10 , B60W2520/14 , B60W2520/26 , B60W2720/14 , F16H48/08 , F16H48/22 , F16H48/30 , F16H48/32 , F16H48/34 , F16H2048/204 , F16H2200/2071 , Y10T74/1254 , Y10T74/1435 , Y10T74/19274 , Y10T74/2188
摘要： A control system (50) for a vehicle having first and second wheels (28, 30) is provided that includes a differential apparatus (22) adapted to distribute torque between the first and second wheels (28, 30) and a traction controller (52) for controlling operation of the differential apparatus (22) from vehicle launch up to a predetermined vehicle speed. The traction controller (52) is configured to engage the differential apparatus (22) in a first operating state according to at least one vehicle operating parameter indicative of a low traction operating condition and to further control engagement of the differential apparatus (22) in a second vehicle operating state during the low traction operating condition according to a difference between an actual vehicle yaw rate and a predetermined target vehicle yaw rate. The control system (50) also includes a stability controller (54) for controlling engagement of the differential apparatus (22) at or above the predetermined vehicle speed.

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