基本信息:
- 专利标题： A FLIGHT CONTROL DEVICE FOR AN AIRCRAFT
- 专利标题（中）：FLUGSTEUERUNGSVORRICHTUNGFÜREIN FLUGZEUG
- 申请号：EP15703959.5 申请日：2015-02-04
- 公开(公告)号：EP3110691A1 公开(公告)日：2017-01-04
- 发明人： TILLY, Bruno , RAVOUX, Nicolas
- 申请人： Safran Electronics & Defense
- 申请人地址： 18/20 Quai du Point du Jour 92100 Boulogne-Billancourt FR
- 专利权人： Safran Electronics & Defense
- 当前专利权人： Safran Electronics & Defense
- 当前专利权人地址： 18/20 Quai du Point du Jour 92100 Boulogne-Billancourt FR
- 优先权： US201461946015P 20140228
- 国际公布： WO2015128162 20150903
- 主分类号： B64C13/46
- IPC分类号： B64C13/46
摘要：
The invention relates to a flight control device for an aircraft, the device comprising a mount, a lever pivotally mounted on the mount, and mechanical means for generating a return force for the lever, said means including a spring and a first motor member that are arranged so that a first end of the spring is constrained to move in rotation with the lever and a second end of the spring is constrained to move in rotation with an outlet shaft of the first motor member. According to the invention, the flight control device includes an electrical assistance system for assisting said mechanical means for generating a return force.
摘要（中）：
本发明涉及一种用于飞行器的飞行控制装置，该装置包括安装件，可枢转地安装在安装件上的杆和用于产生用于杆的返回力的机械装置，所述装置包括弹簧和第一马达构件， 布置成使得弹簧的第一端被限制为随着杠杆旋转移动，并且弹簧的第二端被限制为随着第一马达构件的出口轴旋转运动。 根据本发明，飞行控制装置包括用于辅助所述机械装置产生返回力的电气辅助系统。
公开/授权文献:
- EP3110691B1 A FLIGHT CONTROL DEVICE FOR AN AIRCRAFT 公开/授权日：2019-05-29