公开(公告)号：US20220119117A1

公开(公告)日：2022-04-21

申请号：US17500028

申请日：2021-10-13

Applicant: DASSAULT AVIATION

Inventor： Quentin DUGAS ,  Jean-Rémi BILLON

IPC: B64D11/06

Abstract: An interior layout of an aircraft cabin extends along a longitudinal axis on a floor and comprises a table having at least one leg, at least one base for each leg and at least one flat tabletop. Each base is intended to be fixed to the floor, each leg is mounted on a base, and each flat tabletop is mounted on at least one leg. The table defines at least one main aisle accessible to a passenger of the aircraft. The main aisle extends in the longitudinal axis along a longitudinal edge of the flat tabletop. The interior layout comprises at least one seat arranged opposite the table. The seat has a seating direction oriented transversely to the longitudinal axis.

公开(公告)号：US20200269982A1

公开(公告)日：2020-08-27

申请号：US16792488

申请日：2020-02-17

Applicant: DASSAULT AVIATION

Inventor： Christophe HARROIS ,  Jean-Rémi BILLON ,  Séverine ASFAUX

IPC: B64D11/00 ,  B64D11/04 ,  B64C1/14

Abstract: An aircraft (10) includes a fuselage (12) delimiting a cockpit (14), a passenger entry area (18) and a passenger cabin (16) configured to accommodate passengers during a flight phase. The entry area (18) is interposed longitudinally between the cockpit (14) and the cabin. The cockpit and the entry area are delimited by a front separating element (24) and the entry area and the cabin are delimited by a rear separating element (26). The fuselage delimits a side boarding door (20). A transverse median plane (66) of the boarding door is placed at a distance from the front separating element, considered along the longitudinal axis, greater than 39% of the length between the front separating element and the rear separating element, considered along the longitudinal axis.

公开(公告)号：US20250100692A1

公开(公告)日：2025-03-27

申请号：US18890220

申请日：2024-09-19

Applicant: DASSAULT AVIATION

Inventor： Jean-Rémi BILLON ,  Matthieu HAUTEM ,  Quentin FOOS ,  Maxime NICOT

IPC: B64D11/06

Abstract: A reclining aircraft seat structure, and associated aircraft cabin, the structure includes a base, a carriage, supported by the base, the carriage including a front edge and a rear edge, a seat pan support, articulated on the carriage about a transverse front axis, located between the front edge and the rear edge and a backrest support, articulated with respect to the seat pan support, about a transverse rear axis, located to the rear of the front axis. The structure also includes an actuator including a deployable rod between a retracted position and a deployed position, the deployable rod being articulated on a lower arm of the backrest support in a rear articulation point. The rear articulation point is located behind the front articulation axis over at least part of the travel of the deployable rod between the retracted position and the deployed position.

公开(公告)号：US20230373630A1

公开(公告)日：2023-11-23

申请号：US18201539

申请日：2023-05-24

Applicant: DASSAULT AVIATION

Inventor： Jean-Rémi BILLON ,  Olivier CAPISTRAN ,  Quentin FOOS ,  Grégory LEFLOCH

IPC: B64D11/00

CPC classification number: B64D11/00 ,  B64D2011/0046

Abstract: A support device for an aircraft cabin interior layout assembly comprises a fixed frame extending according to a longitudinal direction; and a table comprising a tray deployable relative to the frame between a retracted configuration and a deployed configuration. The tray extends horizontally in the retracted configuration and in the deployed configuration and is displaceable in rotation about a first axis of rotation, substantially parallel, while remaining horizontal between the retracted configuration and the deployed configuration. The tray is displaceable in translation relative to the frame in the longitudinal direction between a first position of use and a second position of use when the tray is in the deployed configuration, while being fixed in rotation about the first rotation axis.

公开(公告)号：US20230373629A1

公开(公告)日：2023-11-23

申请号：US18198263

申请日：2023-05-16

Applicant: DASSAULT AVIATION

Inventor： Jean-Rémi BILLON ,  Quentin DUGAS ,  Grégory LEFLOCH ,  Maxime NICOT

IPC: B64D11/00

CPC classification number: B64D11/00

Abstract: A device for holding objects in an aircraft cabin includes at least one interface, intended for being attached to a wall of the cabin, or for being formed in a wall of the cabin, the interface defining an attachment region for the object, the object being suitable for being placed in contact with the attachment region. The object can be rotated over the attachment region between a position for placing the object on the attachment region, wherein the object can be moved away from the attachment region, and an attachment position of the object on the attachment region, wherein the object is held on the attachment region.

公开(公告)号：US20190008335A1

公开(公告)日：2019-01-10

申请号：US16024405

申请日：2018-06-29

Applicant: DASSAULT AVIATION

Inventor： Denis PEUZIAT ,  Yann MAILLAUT ,  Jean-Rémi BILLON ,  Bruno MARCHESSOU

IPC: A47K10/42 ,  B64D11/02

Abstract: This towel dispenser (10) comprises a housing (12) partially closed by a façade (20) defining an opening (22). The dispenser (10) further comprises a holder (30) inserted in the housing (12), this holder (30) having a substantially planar base (32) and, protruding from the base (32), at least one wall (34, 36) substantially perpendicular to the base (32). The base (32) and the or each wall (34, 36) together defining a parallelepiped cavity (38), the cavity (38) emerging outside the holder (30) through a first window arranged in a first face (56) of the parallelepiped orthogonal to the base (32) and through a second window (62) arranged in a second face (58) of the parallelepiped opposite the base (32). The holder (30) can be positioned inside the housing (12) in a first position, in which the first window faces the opening (22), and in a second position, in which the second window (62) faces the opening (22).