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    • 1. 发明授权
    • Method for load limiting in drive systems for aircraft high lift systems
    • 用于飞机高升力系统的驱动系统中的负载限制方法
    • US08074937B2
    • 2011-12-13
    • US10579420
    • 2004-11-12
    • Udo CarlUwe NeumannBen Holert
    • Udo CarlUwe NeumannBen Holert
    • B64C13/16
    • B64D45/0005B64D2045/001
    • The invention relates to a device for load limitation in a aircraft high lift system, said system comprising individual segments of landing flap systems and slat flap systems, and a drive unit. The inventive device for load limitation comprises a control unit that is connected to position sensors and is embodied in such a way as to process signals from the position sensors and to generate a signal for limiting the supplied drive power. The invention also relates to a method for load limitation. According to said method, signals from at least two position sensors are measured; at least one reference variable is calculated form the measured signals; each reference variable is compared with a corresponding threshold value pre-determined from a maximum authorized load; and a control signal is generated for limiting the drive power, when at least one of the reference variables reaches or exceeds the threshold value.
    • 本发明涉及一种用于飞机高升降系统中的负载限制的装置,所述系统包括着陆挡板系统和板条翼片系统的单独部分以及驱动单元。 本发明的用于负载限制的装置包括连接到位置传感器的控制单元,并且以这样的方式实现,以便处理来自位置传感器的信号并产生用于限制所提供的驱动功率的信号。 本发明还涉及一种用于负载限制的方法。 根据所述方法,测量来自至少两个位置传感器的信号; 从测量信号计算出至少一个参考变量; 将每个参考变量与从最大授权负载预先确定的对应阈值进行比较; 并且当至少一个参考变量达到或超过阈值时,产生用于限制驱动功率的控制信号。
    • 2. 发明申请
    • Method for load limitation in drive systems for a high lift system for aeroplanes
    • 用于飞机高升力系统的驱动系统中的负载限制方法
    • US20070080261A1
    • 2007-04-12
    • US10579420
    • 2004-11-12
    • Uwe NeumannUdo CarlBen Holert
    • Uwe NeumannUdo CarlBen Holert
    • G05D1/00
    • B64D45/0005B64D2045/001
    • The invention relates to a device for load limitation in a aircraft high lift system, said system comprising individual segments of landing flap systems and slat flap systems, and a drive unit. The inventive device for load limitation comprises a control unit that is connected to position sensors and is embodied in such a way as to process signals from the position sensors and to generate a signal for limiting the supplied drive power. The invention also relates to a method for load limitation. According to said method, signals from at least two position sensors are measured; at least one reference variable is calculated form the measured signals; each reference variable is compared with a corresponding threshold value pre-determined from a maximum authorized load; and a control signal is generated for limiting the drive power, when at least one of the reference variables reaches or exceeds the threshold value.
    • 本发明涉及一种用于飞机高升降系统中的负载限制的装置,所述系统包括着陆挡板系统和板条翼片系统的单独部分以及驱动单元。 本发明的用于负载限制的装置包括连接到位置传感器的控制单元,并且以这样的方式实现,以便处理来自位置传感器的信号并产生用于限制所提供的驱动功率的信号。 本发明还涉及一种用于负载限制的方法。 根据所述方法,测量来自至少两个位置传感器的信号; 从测量信号计算出至少一个参考变量; 将每个参考变量与从最大授权负载预先确定的对应阈值进行比较; 并且当至少一个参考变量达到或超过阈值时,产生用于限制驱动功率的控制信号。