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1.发明申请公开(公告)号：US20120234985A1
公开(公告)日：2012-09-20
申请号：US13411950
申请日：2012-03-05
申请人： Romuald Biest , Robert Convers
发明人： Romuald Biest , Robert Convers
IPC分类号： B64C13/14
摘要： The invention provides a control mechanism for controlling flight of an aircraft, the control mechanism comprising a cyclic control stick (1) that is mounted to tilt (B1, B2) on a carrier structure (4) and that is in engagement with remote mechanical transmission members (2, 3). The stick (1) is arranged as a telescopic member provided with locking means (20) for locking it in a normal-use retracted position, and is equipped with deployment means (21). Unlocking of the locking means (20) and use of the deployment means (21) depend on an assistance device (17) associated with the stick (1) being in a defective state. In the event of such a defective state being detected, the stick (1) is suitable for being deployed so as to increase the comfort of the pilot while manipulating it.
摘要翻译： 本发明提供了一种用于控制飞行器飞行的控制机构，该控制机构包括一个循环控制杆（1），该循环控制杆安装成在载体结构（4）上倾斜（B1，B2）并与远程机械传动 会员（2,3）。 杆（1）被布置为具有用于将其锁定在正常使用的缩回位置的锁定装置（20）的伸缩构件，并且配备有展开装置（21）。 锁定装置（20）的解锁和展开装置（21）的使用取决于与棒（1）相关联的辅助装置（17）处于缺陷状态。 在检测到这样的缺陷状态的情况下，棒（1）适于被部署，以便在操纵该飞行员的同时增加飞行员的舒适性。
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2.发明授权Cyclic stick for mechanically transmitting commands for controlling a rotorcraft, the stick having a lever arm that is amplified selectively in the event of an emergency 有权用于机械传送用于控制旋翼航空器的命令的循环杆，该杆具有在紧急情况下被选择性放大的杆臂公开(公告)号：US08590843B2
公开(公告)日：2013-11-26
申请号：US13411950
申请日：2012-03-05
申请人： Romuald Biest , Robert Convers
发明人： Romuald Biest , Robert Convers
IPC分类号： B64C13/04
摘要： The invention provides a control mechanism for controlling flight of an aircraft, the control mechanism comprising a cyclic control stick (1) that is mounted to tilt (B1, B2) on a carrier structure (4) and that is in engagement with remote mechanical transmission members (2, 3). The stick (1) is arranged as a telescopic member provided with locking means (20) for locking it in a normal-use retracted position, and is equipped with deployment means (21). Unlocking of the locking means (20) and use of the deployment means (21) depend on an assistance device (17) associated with the stick (1) being in a defective state. In the event of such a defective state being detected, the stick (1) is suitable for being deployed so as to increase the comfort of the pilot while manipulating it.
摘要翻译： 本发明提供了一种用于控制飞行器飞行的控制机构，该控制机构包括一个循环控制杆（1），该循环控制杆安装成在载体结构（4）上倾斜（B1，B2）并与远程机械传动 会员（2,3）。 杆（1）被布置为具有用于将其锁定在正常使用的缩回位置的锁定装置（20）的伸缩构件，并且配备有展开装置（21）。 锁定装置（20）的解锁和展开装置（21）的使用取决于与棒（1）相关联的辅助装置（17）处于缺陷状态。 在检测到这样的缺陷状态的情况下，棒（1）适于被部署，以便在操纵该飞行员的同时增加飞行员的舒适性。
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