Equipment fastening device to enhance the crash safety of an...

Aeronautics and astronautics – Aircraft structure – Load accommodation

Reexamination Certificate

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Reexamination Certificate

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07823829

ABSTRACT:
An equipment-fastening device EFD to enhance the crash safety of aircraft, for fastening a piece of equipment to a support structure of an airframe, includes a load-limiting release mechanism and a load-peak transformer connected to the release mechanism and having a load-limiting, impact-energy-absorbing deformation element. Load peaks that occur in case of a crash and that stem from equipment fastened to the support structure by means of the equipment-fastening device are first reduced to a residual load peak by the EFD after the release, thereby relieving the stress on the support structure. Only then is any residual load peak that might still remain introduced via a first fastening section of the EFD into the support structure with a time delay vis-à-vis the load peaks that occurred originally.

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Translation of German Office Action received in corresponding German Patent Application 10 2005 042 400.7-22.
W.G. Hienstorfer, “Crashstimuiationsrechnungen und Bauteilidealislerung für einen Luftfahrzeugunterboden” [Crash-simulation computations and component idealization for the subfloor of aircraft] published in the Zeitschrift for Flugwissenschaft und Weltraumforschung [magazine for aviation science and space research], vol. 11, 1987.

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