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公开(公告)号：EP3403927A1
公开(公告)日：2018-11-21
申请号：EP18170148.3
申请日：2017-05-18
发明人： GROHMANN, Boris , ROHR, Thomas
摘要： The invention relates to a method of controlling an artificial force feel generating device (6) for generation of an artificial feeling of force on an inceptor (4a) of a vehicle control system (10) that comprises an automatic flight control system (7). The method comprises monitoring usage of the inceptor (4a) and of a mechanical connection (6a) during operation, determining a current accumulated fatigue (27a) on the basis of the monitored usage and determining a fatigue prediction (33a, 33b, 33c). Thus, steps of the method provide: re-configuring (7a) protections of the automatic flight control system (7) and re-configuring (21a) of force generating device (12) both on the basis of the current accumulated fatigue (27a), and determining an applicable overhaul interval of the inceptor (4a) and of the mechanical linkage (6a) on the basis of the determined fatigue prediction (33a, 33b, 33c).
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公开(公告)号：EP3403926A1
公开(公告)日：2018-11-21
申请号：EP17400028.1
申请日：2017-05-18
发明人： Grohmann, Boris , Rohr, Thomas
摘要： A method of controlling an artificial force feel generating device 6 for generation of an artificial feeling of force on an inceptor (4a) that is adapted for controlling a servo-assisted control unit (4) of a vehicle control system (10), wherein the artificial force feel generating device comprises at least one force generating device that is mechanically connected to the inceptor for generating a tactile cue force acting in operation on the inceptor, and wherein a safety device is provided for limiting authority of the at least one force generating device, the method comprising at least the steps of: monitoring usage of the safety device during operation of the artificial force feel generating device, determining a current accumulated fatigue of the safety device on the basis of the monitored usage, and re-configuring the at least one force generating device on the basis of the current accumulated fatigue.
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公开(公告)号：EP2479107A4
公开(公告)日：2017-03-01
申请号：EP10815491
申请日：2010-09-14
发明人： SHIROTA NEMU
CPC分类号： B64C13/46
摘要： A flight control system of an aircraft and a flight control method of the aircraft are provided in which the overrunning an operation limitation on a flight condition can be prevented even when a pilot operates a flight control device fast. The flight control system of the aircraft includes a flight control device; a sensor configured to detect a first parameter changed based on a flight condition of the aircraft; a limitation flight control position calculating section configured to calculate a limitation flight control position of the flight control device when the first parameter reaches a limitation value, based on the first parameter; a reaction force generating actuator configured to change a reaction force which the pilot receives when carrying out a flight control input to the flight control device, in response to a reaction force generating command generated based on the flight control position of the flight control device and the limitation flight control position; an inner loop command calculating section configured to generate an inner loop command based on the flight control position; and a control surface actuator configured to drive a control surface of the aircraft based on the flight control position and the inner loop command.
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4.发明公开Dispositif pour générer des efforts de rappel pour des manches tels que des manches d'aéronefs 有权设备技术用于产生反馈力量STICKS FOR EXAMPLE操纵杆飞机
公开(公告)号：EP2631170A1
公开(公告)日：2013-08-28
申请号：EP13154913.1
申请日：2013-02-12
CPC分类号： G05G17/00 , B64C13/04 , B64C13/46 , Y10T74/20201 , Y10T74/20666
摘要： Dispositif de génération d'effort de rappel (1) pour manche de commande (2) mobile depuis une position neutre selon une trajectoire (3) de déplacement, comprenant des moyens de liaison mécanique (5) du manche (2) à des moyens élastiques de rappel (4) du manche (2) vers la position neutre, caractérisé en ce que, les moyens de liaison mécanique (5) et les moyens élastiques de rappel (4) sont agencés pour produire, sur une première partie de la trajectoire (3a), une première intensité d'effort de rappel (F) et, sur une deuxième partie de la trajectoire (3b), une deuxième intensité d'effort de rappel (F), et en ce que les moyens de liaison mécanique (5) comportent une pièce de transmission (6) adaptée à être liée mécaniquement audit manche (2) de manière qu'à tout déplacement dudit manche (2) le long de la deuxième partie (3b) de la trajectoire corresponde une rotation de la pièce de transmission (6) et adaptée à transmettre l'effort de rappel (F) audit manche (2) au moins lorsque le manche (2) est positionné dans la deuxième partie de la trajectoire (3b).
摘要翻译： 所述装置（1）具有的机械连接单元（5）和弹性回位装置（4）也被布置成产生，在两个部分的移动轨迹的（3A，3B），返回工作的两个强度（F）。 所述连接单元包括：发送部（6）angepasst被机械地连接到一个手柄（2）的搜索没有把手的任何运动沿部分中的一个对应于旋转传动部件的运动，以及发送所述回复力到手柄 当手柄在部分被定位。
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公开(公告)号：EP1282554B1
公开(公告)日：2010-09-08
申请号：EP01970510.2
申请日：2001-05-16
CPC分类号： B64C13/10 , G05G9/047 , G05G2009/04774 , Y02T50/44
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公开(公告)号：EP1996459A2
公开(公告)日：2008-12-03
申请号：EP07867011.4
申请日：2007-03-07
申请人： THE BOEING COMPANY
CPC分类号： B64C39/024 , B64C13/22 , B64C13/46 , B64C13/50 , B64C2201/024 , B64C2201/146 , G05D1/0044
摘要： An apparatus for converting a manned aircraft for unmanned flight, the aircraft including at least one pilot control (1030) capable of manipulation to affect operation of the aircraft, the apparatus comprising a first actuator (1006) and a second actuator (1008) each configured to selectively provide movement or resistance to movement in a first manner including linear or rotational motion, a first clutch (1012) and a second clutch (1016) each configured to selectively couple movement of the associated actuator to the pilot control, and a vehicle controller capable of being selectively enabled to operate the pilot control actuators and clutches providing unmanned operation of the aircraft or disabled providing manned operation of the aircraft. The first actuator has a first scope describing a first amount of allowable movement (1062, 1042), while the second actuator has a second scope (1068, 1040) larger than the first scope.
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公开(公告)号：EP0067215B1
公开(公告)日：1986-11-05
申请号：EP82900457.1
申请日：1981-12-18
申请人： THE BOEING COMPANY
CPC分类号： B64C13/46 , G03G5/14791 , Y10T74/20207
摘要： Previous flight control systems summed the resistive forces which are overcome by the instant system. A bifurcated feel unit (60) for use in a dual path flight control system includes separate input levers (162, 164) for the pilot and copilot control paths. The input levers (162, 164) pivot about a common axis (166) but are capable of independent rotation upon override of the breakout pogos (44, 50) associated with the control system external to the feel unit (60). Each input lever (162, 164) is coupled to a source of resistive force (100), preferably a piston (86, 96) within a hydraulic chamber (88, 98). Normally the feel force supplied is the sum of the resistive forces applied to each input lever (162, 164). In the event of a jam in one path of the flight control system, the feel force supplied to the remaining operable path is reduced in proportion to the reduction in available control surface.
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公开(公告)号：EP2874874B1
公开(公告)日：2018-10-03
申请号：EP13844973.1
申请日：2013-07-17
申请人： Mason Electric Co.
发明人： SALAMAT, Bijan , SANGUINETTI, Jorge, J. , MYLES, Robert, J. , STEPANIAN, Avetis , GABLER, Andrew, K.
IPC分类号： B64C13/00 , B64C13/04 , G05G9/047 , B64C13/02 , B64C13/12 , B64C13/34 , B64C13/46 , F16H57/08 , G05G1/08
摘要： A complex-dynamic air and ground vehicle control inceptor assembly that provides active positional control with the capability of back drive (pilot over-ride) via a direct connection between the lever, a high gear-ratio gearbox, and the motor without the use of a clutch.
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10.发明授权AN ARTIFICIAL FORCE FEEL GENERATING DEVICE FOR A VEHICLE CONTROL SYSTEM OF A VEHICLE AND, IN PARTICULAR, OF AN AIRCRAFT 有权器具，用于产生人工能收购一种用于车辆的车辆控制系统，尤其是飞机
公开(公告)号：EP3069990B1
公开(公告)日：2017-01-11
申请号：EP15400013.7
申请日：2015-03-20
发明人： Grohmann, Boris , Rohr, Thomas , Klaubert, Jens
IPC分类号： B64C13/46
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