US 11,851,183 B2
Aircraft cabin equipped with a safety device and associated process
Lionel Patrick Germe, Merignac (FR); Emmanuel Picut, Merignac (FR); Alain Levavasseur, Merignac (FR); Erwan Boulo, Merignac (FR); and Jérémie Guerard, Merignac (FR)
Assigned to DASSAULT AVIATION, Paris (FR)
Filed by DASSAULT AVIATION, Paris (FR)
Filed on Oct. 22, 2020, as Appl. No. 17/077,684.
Claims priority of application No. FR 19 11839 (FR), filed on Oct. 23, 2019.
Prior Publication US 2021/0122473 A1, Apr. 29, 2021
Int. Cl. B64D 11/06 (2006.01); B64D 41/00 (2006.01)
CPC B64D 11/0621 (2014.12) [B64D 11/0601 (2014.12); B64D 11/0605 (2014.12); B64D 11/0638 (2014.12); B64D 41/00 (2013.01); B64D 2201/00 (2013.01)] 19 Claims
OG exemplary drawing
 
1. An aircraft cabin comprising:
at least one seat configured to receive at least one passenger;
at least one table arranged opposite the seat; and
a safety device configured to be mounted on the table, below the table or received in the table, the safety device including:
at least one airbag, the at least one airbag being deployable from a retracted idle configuration to a deployed safety configuration of the at least one passenger seated on the seat, and
a controller configured to control the deployment of the at least one airbag, and to trigger the deployment of the at least one airbag beyond a threshold deceleration value of the aircraft,
the table being a dining table which comprises a tray, the tray comprising at least one base extending at all times in a plane parallel to a cabin floor,
wherein the at least one airbag is mounted on the tray or received in the tray,
wherein the tray comprises a base and at least one flap that is movable relative to the base between a stowed configuration in which the flap is folded on the base and a usage configuration in which the flap is deployed in the extension of the base.