Patent ID: 9058750
Filing Date: 2015-06-16
Classification: G09B

Abstract:
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.