发明名称 Flight simulator vibration system
摘要 The invention relates to a flight simulator vibration system, particularly to a crew seat (1), a flight control stick (20) and a panel (30) vibration system of a flight simulator with at least one plate of the crew seat (1), the flight control stick (20) and/or the panel (30) being equipped with predefined momentum weights (13, 16) and electric motors driving said respective momentum weights. Speed governors are controlling individually said electric motors (7, 8, 9, 21, 33, 34).
申请公布号 US9058750(B2) 申请公布日期 2015.06.16
申请号 US201113071300 申请日期 2011.03.24
申请人 Airbus Helicopters Deutschland GmbH 发明人 Bohlender Peter
分类号 G09B9/12;G09B9/08;G09B9/46;G09B9/16 主分类号 G09B9/12
代理机构 Brooks Kushman P.C. 代理人 Brooks Kushman P.C.
主权项 1. A flight simulator vibration system for an aircraft, the system defining three coordinate axes, the system comprising: a crew seat with a first predefined momentum weight driven by a first electric motor, a second predefined momentum weight driven by a second electric motor, and a third predefined momentum weight driven by a third electric motor, each respective electric motor being disposed within a respective motor casing removably retained by a respective flexible stripe, a flight control stick with a fourth momentum weight driven by a fourth electric motor, a panel vibration system with a fifth momentum weight driven by a fifth electric motor, and at least one electronic control circuit configured to individually control the electric motors to provide vibrations about all three coordinate axes, wherein when the respective flexible stripes are removed the respective motors may be rotated for tuning and the respective momentum weights may be adjusted or replaced for tuning.
地址 Donauworth DE