专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP2935000A1 INCEPTOR APPARATUS 有权
标题翻译：控制设备的设备
公开(公告)号：EP2935000A1
公开(公告)日：2015-10-28
申请号：EP13799666.6
申请日：2013-12-02
申请人： BAE Systems PLC
发明人： TAYLOR, Adam , DESALVO, Keith, Michael
IPC分类号： B64C13/04
CPC分类号： G05G1/04 , B64C13/04 , B64C13/0421 , G05G5/03 , G05G9/047 , G05G25/00 , G05G2009/04718 , G05G2009/04766
摘要： An inceptor apparatus and method for operating a machine, the operation of the machine providing an output from at least one inertial sensor. The apparatus comprises a stick member having a base portion, and a grip portion extending from the base portion in only one direction. The apparatus further comprises at least one sensor for generating actual stick member position data, and a control unit configured to receive an inertial force signal from the or each inertial sensor and the actual stick member position data. The control unit is operable generate a first stick member position compensation signal in dependence upon the inertial force signal and actual stick member position data.

2. 发明公开

EP3860910A1 OSCILATION SYSTEM 审中-公开
公开(公告)号：EP3860910A1
公开(公告)日：2021-08-11
申请号：EP19772811.6
申请日：2019-09-16
申请人： BAE SYSTEMS plc
发明人： TAYLOR, Adam
IPC分类号： B64C13/04 , B64C13/50

3. 发明公开

EP3728026A1 AIRCRAFT CONTROL SYSTEMS 有权
公开(公告)号：EP3728026A1
公开(公告)日：2020-10-28
申请号：EP18811338.5
申请日：2018-11-29
申请人： BAE SYSTEMS plc
发明人： TAYLOR, Adam , DRAPER, Jonathan David
IPC分类号： B64C13/04 , B64C25/50 , G05G9/00

4. 发明授权

EP2490936B1 TACTILE CUEING APPARATUS 有权
标题翻译：触觉SIGNALISIERUNGSVORRICHTUNG
公开(公告)号：EP2490936B1
公开(公告)日：2015-06-10
申请号：EP10765486.5
申请日：2010-10-08
申请人： BAE Systems PLC
发明人： TAYLOR, Adam
IPC分类号： B64C13/46
摘要： A tactile cueing apparatus for incorporation in an aircraft flight control system comprising a flight control surface, and a pilots inceptor (12) for moving the surface via a servo-assisted mechanical linkage (28) connecting the inceptor to the control surface, the apparatus comprising a force sensor for sensing a force applied to the inceptor by the pilot to move the control surface, an electromechanical actuator (34) configured to be installed with the mechanical linkage between the inceptor and means in the system providing said servo-assistance, and control means programmed to cause the actuator (i) to move so that the linkage moves to a position determined by said force according to a predetermined relationship, (ii) to apply to the inceptor a resisting force according to a predetermined relationship and which when the linkage has moved to its commanded position is equal and opposite to the force sensed by the force sensor.

5. 发明授权

EP2935000B1 INCEPTOR APPARATUS 有权
公开(公告)号：EP2935000B1
公开(公告)日：2019-06-26
申请号：EP13799666.6
申请日：2013-12-02
申请人： BAE Systems PLC
发明人： TAYLOR, Adam , DESALVO, Keith, Michael
IPC分类号： B64C13/04

6. 发明公开

EP3442862A1 AN AIRCRAFT 审中-公开
公开(公告)号：EP3442862A1
公开(公告)日：2019-02-20
申请号：EP17715971.2
申请日：2017-03-28
申请人： BAE Systems PLC
发明人： TAYLOR, Adam
IPC分类号： B64C13/12

7. 发明公开

EP3148877A2 INCEPTOR APPARATUS 审中-公开
标题翻译： STEUERORGANVORRICHTUNG
公开(公告)号：EP3148877A2
公开(公告)日：2017-04-05
申请号：EP15724011.0
申请日：2015-05-19
申请人： BAE Systems PLC
发明人： TAYLOR, Adam , BEAN, Jason, Howard
IPC分类号： B64C13/04 , G05D1/00 , G05G9/047
CPC分类号： G05D1/0077 , B64C13/04 , B64C13/14 , B64C13/46 , B64C13/503 , G05G1/04 , G05G5/12 , G05G9/047 , G05G2009/04718 , G05G2009/04748 , G05G2009/04751 , G05G2009/04762 , G05G2009/04777 , G05G2505/00 , G05G2700/02
摘要： An active inceptor apparatus and method for operating a machine. The apparatus comprises a stick member having a grip portion, the stick member being pivotably mounted relative to a housing. It further comprises a position sensor responsive to, and for generating signals indicative of, stick member position. A force sensor is provided on the stick member responsive to, and for generating signals indicative of, force applied to the stick by a user. The apparatus also includes a control unit operable to receive the position and force signals from the position and force sensors respectively. The control unit is operable to process the signals according to a predetermined relationship to determine a value FD indicative of force applied to the stick member relative to displacement of the stick member. The control unit is also operable to generate machine control signals as a function of position signals and force signals in dependence upon the value FD, for communication to the machine.
摘要翻译：公开了一种用于控制诸如飞行器的机器的操纵杆或接收器。操纵杆12被设计成在卡住或卡在一个位置时操作，或变得通常不能操作。为此，它连接到力28和位置传感器32，其同时检测用户施加到操纵杆的力量和移动方向。然后将这些信号发送到控制单元40，控制单元40使用它们来根据预定关系确定值。用于控制机器48,50和52的各个部件的机器控制信号是根据取决于该确定值的位置和力信号的函数产生的。在控制器发生故障的情况下，可以仅使用力或位置传感器中的一个产生控制信号。棒状构件12可以联接到致动器，致动器可以在发生故障的情况下移动棒或将其锁定。

8. 发明授权

EP2021895B1 IMPROVEMENTS IN OR RELATING TO AN ACTIVE STICK APPARATUS 有权
标题翻译：与之相关的改进到活动STICK DEVICE
公开(公告)号：EP2021895B1
公开(公告)日：2011-03-09
申请号：EP07733677.4
申请日：2007-05-11
申请人： BAE Systems PLC
发明人： TAYLOR, Adam , WELLS, Daniel, John , INGLETON, Martyn
IPC分类号： G05G9/047 , G05G1/04
CPC分类号： G05G9/047 , B64C13/04 , B64C13/10 , G05G1/04 , G05G2009/04707 , G05G2009/04718 , G05G2009/04748 , G05G2009/04762 , G05G2009/04766 , Y10T74/20201
摘要： An active stick apparatus (40) includes a stick housing (41) and a stick control member (42) pivotally mounted to the stick housing (41) at a pivot point (43). The pivot point (43) acts to divide the stick control member (42) into a first member section (44) and a second member section (45). The pivot point (43) allows the stick control member (42) to pivot with respect to the stick housing (41), as indicated by directional arrows (46) and (47). An actuator (50) is attached to the first member section (44) at an end distal from the pivot point (43). The actuator (50) is arranged to act as a counterbalance to movement of the stick control member (42) about the pivot point (43) under acceleration forces asserted on the stick control member (42). The output axle drive (52) of the actuator (50) is fixedly coupled to a first section (53) of a drive link (54) and a second section (55) of the drive link (54) is pivotally coupled to a first section (56) of a mounting linkage (57). A second section (58) of the mounting linkage (57) is pivotally coupled to the stick housing (41). Coupling of the actuator (50) to the first member section mitigates the requirement for a conventional lump mass.

9. 发明授权

EP2490936B2 TACTILE CUEING APPARATUS 有权
公开(公告)号：EP2490936B2
公开(公告)日：2020-07-22
申请号：EP10765486.5
申请日：2010-10-08
申请人： BAE Systems PLC
发明人： TAYLOR, Adam
IPC分类号： B64C13/46

10. 发明公开

EP2490936A1 TACTILE CUEING APPARATUS 有权
标题翻译：触觉信号装置
公开(公告)号：EP2490936A1
公开(公告)日：2012-08-29
申请号：EP10765486.5
申请日：2010-10-08
申请人： BAE Systems Plc.
发明人： TAYLOR, Adam
IPC分类号： B64C13/46
CPC分类号： B64C13/10 , B64C13/46
摘要： A tactile cueing apparatus for incorporation in an aircraft flight control system comprising a flight control surface, and a pilots inceptor (12) for moving the surface via a servo-assisted mechanical linkage (28) connecting the inceptor to the control surface, the apparatus comprising a force sensor for sensing a force applied to the inceptor by the pilot to move the control surface, an electromechanical actuator (34) configured to be installed with the mechanical linkage between the inceptor and means in the system providing said servo-assistance, and control means programmed to cause the actuator (i) to move so that the linkage moves to a position determined by said force according to a predetermined relationship, (ii) to apply to the inceptor a resisting force according to a predetermined relationship and which when the linkage has moved to its commanded position is equal and opposite to the force sensed by the force sensor.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式