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    • 1. 发明授权
    • Aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft
    • 包括用于影响飞行器的方向稳定性的装置的飞行器以及影响飞行器的方向稳定性的方法
    • US09315255B2
    • 2016-04-19
    • US13255246
    • 2010-03-17
    • Carsten WeberMarkus FischerArnaud Namer
    • Carsten WeberMarkus FischerArnaud Namer
    • B64C5/06B64C9/32
    • B64C5/06B64C9/32Y02T50/32
    • An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
    • 提供了包括用于影响飞行器的方向稳定性的装置的飞机。 该装置包括控制输入装置; 飞行控制装置; 用于获取飞行器的转速的传感器装置,包括偏航率; 以及与副翼,扰流器,电梯和方向舵耦合的至少一个致动器。 飞行控制装置包括控制功能,该控制功能根据控制命令产生用于控制飞行器的致动器的调节命令。 飞机包括两个尾部安装的翼片,每个翼片包括与飞行控制装置连接的致动器,其彼此对称并且在机身的相对侧上对准,并且可在缩回位置和伸出位置之间移动。 控制功能被设计成使得基于所获取的旋转速度而基于控制命令生成的调节命令包括调整到尾部安装的翼片的致动器的命令。
    • 2. 发明申请
    • AIRCRAFT COMPRISING A DEVICE FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT, AND A METHOD FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT
    • 包含影响飞机方向稳定性的装置的飞机,以及影响飞机方向稳定性的方法
    • US20120104184A1
    • 2012-05-03
    • US13255246
    • 2010-03-17
    • Carsten WeberMarkus FischerArnaud Namer
    • Carsten WeberMarkus FischerArnaud Namer
    • B64C13/16B64C9/02B64C9/08B64C9/00
    • B64C5/06B64C9/32Y02T50/32
    • An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
    • 提供了包括用于影响飞行器的方向稳定性的装置的飞机。 该装置包括控制输入装置; 飞行控制装置; 用于获取飞行器的转速的传感器装置,包括偏航率; 以及与副翼,扰流器,电梯和方向舵耦合的至少一个致动器。 飞行控制装置包括控制功能,该控制功能根据控制命令产生用于控制飞行器的致动器的调节命令。 飞机包括两个尾部安装的翼片,每个翼片包括与飞行控制装置连接的致动器,其彼此对称并且在机身的相对侧上对准,并且可在缩回位置和伸出位置之间移动。 控制功能被设计成使得基于所获取的旋转速度而基于控制命令生成的调节命令包括调整到尾部安装的翼片的致动器的命令。