초록 ▼

An air return grille for an aircraft mounted below the passenger cabin sidewall comprises openings to allow return airflow from the air conditioning system. In a preferred embodiment, the grille openings are covered by a single thin baffle 32 with cutouts within its periphery that slip over and are

An air return grille for an aircraft mounted below the passenger cabin sidewall comprises openings to allow return airflow from the air conditioning system. In a preferred embodiment, the grille openings are covered by a single thin baffle 32 with cutouts within its periphery that slip over and are held in place by fasteners on the molded grille 28. The thin baffle 32 is affixed to the molded grille 28 along one or more edges on the grille. All other thin baffle 32 attachments allow for the baffle to be disengaged upon the onset of a rapid decompression. During normal operation, the thin baffle 32 restricts flow through a small opening in the grille. During a sudden/rapid decompression of the cargo compartment/lower lobe, the baffle is dislodged from the fasteners and forced into a position parallel to the airstream. This allows the airflow to pass through all of the molded grille 28 openings in order to achieve rapid pressure equalization.

대표청구항 ▼

[ What is claimed is:] [1.] A combination aircraft return air vent/decompression panel assembly comprising a molded grille covering a return air vent in an aircraft and a flexible baffle releaseably attached to the downstream side of the grille and covering a portion thereof,wherein the baffle has a

[ What is claimed is:] [1.] A combination aircraft return air vent/decompression panel assembly comprising a molded grille covering a return air vent in an aircraft and a flexible baffle releaseably attached to the downstream side of the grille and covering a portion thereof,wherein the baffle has a plurality of holes therein and four slits extending outward from each hole;the grille has a plurality of headed fasteners attached to the downstream side thereof; andthe position and size of the holes, slits, and fastener heads are adapted so that the fastener heads protrude through the holes in the baffle during normal flight operations, and the baffle at least partially releases from the grille upon a rapid decompression event.