Abstract: Described are aircraft cabin arrangements (12) with at least one lavatory unit (14) with a first side wall (1402) and at least one seat unit (16) positioned adjacent the first side wall. A separate wall is not positioned between the first side wall and the at least one seat unit. The first side wall includes a recessed portion, and the at least one seat unit includes a foot support surface (1606) incorporated into the recessed portion of the first side wall.

Abstract: An aircraft cabin arrangement includes at least one cabin attendant seat, called a high-comfort seat, which can assume a stowed position, a sitting position and at least one rest position, and at least one furniture unit. The high-comfort seat is installed in a space provided in the furniture unit, or can extend at least partially into a space arranged in the furniture unit when said high-comfort seat is in the rest position.

Abstract: A safety belt is intended to be installed on an aircraft seat and includes a first part and a second part which are able to be joined together by means of a buckle to hold the passenger on the seat. The safety belt may also include a status detection system able to transmit information relating to the fastening status of the safety belt, a presence detection system able to transmit information relating to the presence of a passenger wearing the safety belt, and/or a communications module, notably wireless, able to transmit information relating to the fastening of the safety belt and/or to the presence of a passenger wearing the safety belt.

Abstract: Described are commercial aircraft cabin arrangement comprising a plurality of seat units (14), each seat unit including a primary seat (16) and a secondary seat (18) arranged facing one another. The primary seat (16) and the secondary seat (18) are configured to combine into a single bed position for the seat unit. The plurality of seat units (14) are arranged in two columns separated by a wide central aisle (72).

Abstract: The invention relates mainly to an aircraft cabin (10) arrangement comprising: at least one cabin attendant seat, called a high-comfort seat (11), which can assume a stowed position, a sitting position and at least one rest position, and at least one furniture unit (18), characterized in that said high-comfort seat (11) is installed in a space (21) provided in the furniture unit (18), or can extend at least partially into a space (21) arranged in the furniture unit (18) when said high-comfort seat (11) is in the rest position.

Abstract: A safety belt is intended to be installed on an aircraft seat and includes a first part and a second part which are able to be joined together by means of a buckle to hold the passenger on the seat. The safety belt may also include a status detection system able to transmit information relating to the fastening status of the safety belt, a presence detection system able to transmit information relating to the presence of a passenger wearing the safety belt, and/or a communications module, notably wireless, able to transmit information relating to the fastening of the safety belt and/or to the presence of a passenger wearing the safety belt.

Abstract: Described are aircraft cabin arrangements (12) with at least one lavatory unit (14) with a first side wall (1402) and at least one seat unit (16) positioned adjacent the first side wall. A separate wall is not positioned between the first side wall and the at least one seat unit. The first side wall includes a recessed portion, and the at least one seat unit includes a foot support surface (1606) incorporated into the recessed portion of the first side wall.

Abstract: Embodiments of the present invention provide systems and methods for allowing use of what has traditionally been a cargo area of a passenger aircraft to be used as a lower deck passenger cabin. Various modifications to the aircraft are described, as well as various features to be added in order to enhance the passenger experience. For example, there may be provided a lowered technical floor (32), stairs or other passageways (50) provided at both ends of the lower deck cabin, a window replacement technique, an alternative way of storing cabin luggage, or any combination thereof.

Abstract: A monitoring system to be installed in a cabin (100a-100c) of an aircraft (100) or spacecraft for passenger transportation comprises at least one imaging device and at least one output device. Information displayed by the output device comprises indication of whether a passenger seat (110) in the cabin is occupied or empty. For more reliable information, several types of imaging devices may be used within the system, in particular selected among a visible light camera, a near-infrared lighting source combined with a near-infrared camera, a thermal camera, and a range imaging device.

Abstract: Described are commercial aircraft cabin arrangement comprising a plurality of seat units (14), each seat unit including a primary seat (16) and a secondary seat (18) arranged facing one another. The primary seat (16) and the secondary seat (18) are configured to combine into a single bed position for the seat unit. The plurality of seat units (14) are arranged in two columns separated by a wide central aisle (72).