Patents Assigned to Europcopter
  • Patent number: 8532845
    Abstract: The present invention relates to a method of monitoring the effectiveness of a damper system, wherein the method consists in measuring the relative movements of two strength members, in filtering the measurements in order to isolate those that relate to the lead-lag resonant frequency of the blade, in rectifying the signal, in recording the signal, in comparing the rectified signal (S) with a threshold value (SL), in determining an initial time interval (T0) as soon as the rectified signal exceeds the threshold value (SL), in calculating the integrals of the signal from T0 to T0+? and from T0 to T0+p?, in calculating the ratio R of the integrals, and in comparing the ratio R with a limit value RL, and in activating and delivering an alert signal (V1) if the ratio R is greater than or equal to the limit value RL.
    Type: Grant
    Filed: June 9, 2011
    Date of Patent: September 10, 2013
    Assignee: Europcopter
    Inventor: Alain Eberhard
  • Patent number: 8532329
    Abstract: The invention relates to a device and a method for testing systems or devices with visual output and at least one mechanical input element. The device comprises an input unit for the automated mechanical actuation of the at least one input element of the device, an image analysis unit, which acquires and analyzes the visual output of the device, and a control unit, which controls the input unit and image analysis unit, and automatically determines a test result based on predetermined desired outputs and the findings of the image analysis unit.
    Type: Grant
    Filed: August 6, 2009
    Date of Patent: September 10, 2013
    Assignees: Europcopter Deutschland GmbH, ESG Elektroniksystem Und Logistik GmbH
    Inventors: Hartmut Braun, Bernd Gumpel, Jürgen Müller
  • Patent number: 5462408
    Abstract: The blade has its lower-surface and upper-surface skins of its shell, its front and rear filling bodies and its spar made of a composite material having the same thermoplastic matrix, preferably made of PEEK, reinforced preferably with carbon fibres. The spar is extended outside the shell by an integrated rooting part with linkage attachment, in a loop or laminate, in the same thermoplastic composite. The method consists in assembling, by melting, under pressure, all the thermoplastic composite components of the blade, in a single step after manufacturing these components in the form of prefabricated elementary pieces.
    Type: Grant
    Filed: December 14, 1993
    Date of Patent: October 31, 1995
    Assignee: Europcopter France
    Inventor: Rene L. Coffy