Wall installation system and method

A system (8) for attaching a wall panel (10) includes a wall panel 10) and a lock strip (58). The wall panel has a back (14) and a tab (38) extending from the back. The lock strip is moveably attached to a wall frame member (12), and has a three-position locking slot (60), including a receiving port...

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Bibliographische Detailangaben
Hauptverfasser:	Cloud, Mark, Cheung, W. Kwun-Wing, Schwitters, Christopher L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A system (8) for attaching a wall panel (10) includes a wall panel 10) and a lock strip (58). The wall panel has a back (14) and a tab (38) extending from the back. The lock strip is moveably attached to a wall frame member (12), and has a three-position locking slot (60), including a receiving portion (62) configured to receive the tab, a locking portion (64) configured to lock the tab with respect to the frame member, and a release portion (66) configured to release the tab. The wall panel is removably attachable to the frame member by inserting the tab into the receiving portion and linearly moving the lock strip to lock the tab in the locking portion. The system can be used for attaching interior sidewall panels in an aircraft.