FASTENING DEVICE FOR A MODULE ELEMENT IN AN AIRCRAFT
A fastening device (100) for attaching a module element to a support structure (300) in an airplane is provided. The fastening device (100) comprises a stud (110), having a broadened head (112) at a first end for engaging in a support recess (302) of the support structure (300) and a section (114) t...
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Format: | Patent |
Sprache: | eng ; fre |
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Zusammenfassung: | A fastening device (100) for attaching a module element to a support structure (300) in an airplane is provided. The fastening device (100) comprises a stud (110), having a broadened head (112) at a first end for engaging in a support recess (302) of the support structure (300) and a section (114) that connects to the head (112) and has a first lateral dimension (L1) and a second lateral dimension (L2), which is disposed at least substantially perpendicularly to the first lateral dimension (L1) and is larger than the first lateral dimension (L1). At an opposite second end, the stud (110) is provided with a lever (150), which is connected to the stud (110) for rotation and can be moved into an opening position and a closing position. A bushing (120), which is provided on the stud (110) so as to be moved longitudinally, is designed to support an outer wall (200) of the module element and supports an electrically conductive leaf spring (130) for contacting the outside of the outer wall (200) on the one side and the support structure (300) on the other side. An eccentric (158), which can be actuated by the lever (150), moves the bushing (120) along the stud (110) toward the head (112) during a movement of the lever (150) into the closing position thereof. |
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