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1. 发明申请

WO1994014653A1 DIRECT TORQUE CONTROL MOMENT GYROSCOPE 审中-公开
标题翻译：直接扭矩控制旋转陀螺仪
公开(公告)号：WO1994014653A1
公开(公告)日：1994-07-07
申请号：PCT/US1993012132
申请日：1993-12-13
申请人： HONEYWELL INC.
发明人： HONEYWELL INC. , HAVENHILL, Douglas, D.
IPC分类号： B64G01/28
CPC分类号： F16C39/06 , B64G1/286 , F16C32/04 , F16C2326/47 , F16C2370/00 , G01C19/30 , H02K7/09 , Y10T74/1218 , Y10T74/125
摘要： A control moment gyroscope (10) for providing directional control in a spacecraft. The control moment gyroscope has a rotor (50) which is electrostatically or magnetically supported within a gimbal housing (24) so as not to touch any of the interior surfaces of the housing. The housing is mounted on a gimbal support (14) which in turn is mounted on the spacecraft. Connected to the gimbal housing is a torque motor (12) which rotates the housing around a gimbal axis. In order to induce a direction changing torque on the spacecraft, the rotor (50) is first spun about its rotor axis. A torque is then induced on the rotor (50) about the output axis. This induced torque will cause the rotor (50) to precess about the gimbal axis which the torque motor follows. The torque induced around the output axis is transferred directly to the spacecraft.
摘要翻译：一种用于在航天器中提供方向控制的控制力矩陀螺仪（10）。控制力矩陀螺仪具有静电或磁力支撑在万向架壳体（24）内的转子（50），以便不接触壳体的任何内表面。壳体安装在万向支架（14）上，后者又安装在航天器上。连接到万向节壳体的是扭矩马达（12），其使壳体围绕万向轴旋转。为了引起航天器上的方向改变扭矩，转子（50）首先围绕其转子轴线旋转。然后在转子（50）上围绕输出轴线产生转矩。该感应扭矩将导致转子（50）围绕扭矩电动机跟随的万向轴线进入。输出轴周围产生的转矩直接转移到航天器。

2. 发明申请

WO1995001279A1 TOUCHDOWN AND LAUNCH-LOCK APPARATUS FOR MAGNETICALLY SUSPENDED CONTROL MOMENT GYROSCOPE 审中-公开
标题翻译：用于磁悬浮控制器的陀飞轮和开启装置GYROSCOPE
公开(公告)号：WO1995001279A1
公开(公告)日：1995-01-12
申请号：PCT/US1994007422
申请日：1994-06-30
申请人： HONEYWELL INC.
发明人： HONEYWELL INC. , SMITH, Dennis, W.
IPC分类号： B64G01/28
CPC分类号： B64G1/32 , B64G1/286 , G01C19/26 , Y10T74/1204
摘要： A control moment gyroscope (10) including a rotor (16) extending along a rotor axis (18). The rotor includes a first and second rotor end. A gimbal housing (12) includes a magnetic suspension system for magnetically suspending the rotor (16) within the gimbal housing (12) to allow rotation of the rotor about the rotor axis. A first and second conical clutch (22, 24) positioned adjacent to the first and second rotor end, respectively, and connected to the gimbal housing couples the rotor to the gimbal housing if the magnetic suspension system is inoperative. The gyroscope (10) also includes an apparatus for forcing the first and second clutches (22, 24) to couple the rotor (16) to the gimbal housing (12).
摘要翻译：包括沿转子轴线（18）延伸的转子（16）的控制力矩陀螺仪（10）。转子包括第一和第二转子端。万向节壳体（12）包括用于将转子（16）磁悬浮在万向节壳体（12）内以允许转子围绕转子轴线旋转的磁悬浮系统。如果磁悬浮系统不起作用，第一和第二锥形离合器（22,24）分别定位成邻近第一和第二转子端并且连接到万向节壳体将转子耦合到万向节壳体。陀螺仪（10）还包括用于迫使第一和第二离合器（22,24）将转子（16）连接到万向节壳体（12）的装置。

3. 发明申请

WO1994010036A1 DEVICE WITH TWO GYROSCOPES FOR SWIVELLING A FLYING OBJECT 审中-公开
标题翻译： DEVICE一个航班身体有两个旋翼的SWING
公开(公告)号：WO1994010036A1
公开(公告)日：1994-05-11
申请号：PCT/DE1993000963
申请日：1993-10-12
申请人： TELDIX GMBH , ECKARDT, Thomas
发明人： TELDIX GMBH
IPC分类号： B64G01/28
CPC分类号： B64G1/24 , B64G1/28
摘要： The orientation of flying objects, in particular satellites, must be stabilised in space. For that purpose, gyroscope devices are used with swivellable gyroscopes in a cardan frame or with gyroscopes fixed in three different directions with adjustable speeds of rotation. These constructions are costly, heavy and prone to failure in certain circumstances. The disclosed device requires only two gyroscopes (1, 2) which may be suspended with a limited cardan mobility, whose axes of rotation coincide in the initial stage and which rotate in opposite directions. By tilting at least one gyroscope and modifying the speed of rotation, any desired resulting torque-vector (Hg) and any desired rotation of the satellite may be achieved.

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