Abstract: A seat frame fastening assembly for laterally fastening a seat frame in a vehicle, wherein the seat frame fastening assembly comprises a holding rail arranged in a longitudinal direction of the vehicle, and a lateral element laterally fastened to a seat frame and coupled to the holding rail. The holding rail comprises a first power- and/or data-transfer interface and the lateral holding element comprises a second power- and/or data-transfer interface. The second power- and/or data-transfer interface is furthermore arranged in the lateral holding element such that a position of the second power- and/or data-transfer interface corresponds to a position of the first power- and/or data-transfer interface when the lateral holding element is coupled to the holding rail. Furthermore, a seat frame has such a seat frame fastening assembly, a vehicle portion has a corresponding seat frame and a vehicle has such a vehicle portion.

Abstract: An aircraft region comprising an aisle section extending in a longitudinal direction of the aircraft region, a bench seat oriented transversely with respect to the longitudinal direction and having a first seat adjacent to the aisle section and a second seat arranged remote from the aisle section, and an aircraft stowage bin system having a first stowage bin arranged at least in part above the first seat and a second stowage bin arranged at least in part above the second seat. The first stowage bin has a first rear side facing away from the aisle section, and the second stowage bin has a second rear side facing away from the aisle section. The second stowage bin is arranged above the second seat such that it is accessible for a person sitting on the second seat or standing in the longitudinal direction in front of the second seat.

Abstract: An interior component carrier system comprises a first and second installation rail. Each rail includes at least one connecting portion connectable to an associated primary structure component to fasten the rail to the component, and a carrier portion extending from the connecting portion in a direction along a longitudinal axis of the system. The system further comprises a first carrier element having a first end connected to a first carrier rod extending in a direction along the longitudinal axis and a second end connectable to a first interior component, wherein the first carrier rod is fastened to the carrier portion of the first rail, and a second carrier element having a first end connected to a second carrier rod extending in the longitudinal axis direction and a second end connected to the first carrier element, wherein the second carrier rod is fastened to the second rail carrier portion.

Abstract: A seat frame fastening assembly for laterally fastening a seat frame in a vehicle, wherein the seat frame fastening assembly comprises a holding rail arranged in a longitudinal direction of the vehicle, and a lateral element laterally fastened to a seat frame and coupled to the holding rail. The holding rail comprises a first power- and/or data-transfer interface and the lateral holding element comprises a second power- and/or data-transfer interface. The second power- and/or data-transfer interface is furthermore arranged in the lateral holding element such that a position of the second power- and/or data-transfer interface corresponds to a position of the first power- and/or data-transfer interface when the lateral holding element is coupled to the holding rail. Furthermore, a seat frame has such a seat frame fastening assembly, a vehicle portion has a corresponding seat frame and a vehicle has such a vehicle portion.

Abstract: A system for installing modules on a fuselage structure has modules with holders arranged thereon for fastening on a fuselage structure, assembly stands, which can be moved on a floor level, and a flexible connecting element, extending via all the modules and coupling them together. Each assembly stand has a base for supporting the stand on the floor level and a holding device, designed to support the module. The assembly stands, the modules and the at least one connecting element are designed to form a chain of assembly stands, such that two successive groups of assembly stands enclose a pivot point at which the mutually facing modules have a larger spacing relative to one another than the modules within the respective groups. The connecting element allows the pivoting of the groups relative to one another at the pivot point through an angle of at least 90°.

Abstract: An aircraft region comprising an aisle section extending in a longitudinal direction of the aircraft region, a bench seat oriented transversely with respect to the longitudinal direction and having a first seat adjacent to the aisle section and a second seat arranged remote from the aisle section, and an aircraft stowage bin system having a first stowage bin arranged at least in part above the first seat and a second stowage bin arranged at least in part above the second seat. The first stowage bin has a first rear side facing away from the aisle section, and the second stowage bin has a second rear side facing away from the aisle section. The second stowage bin is arranged above the second seat such that it is accessible for a person sitting on the second seat or standing in the longitudinal direction in front of the second seat.

Abstract: The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.

Abstract: An interior component carrier system comprises a first and second installation rail. Each rail includes at least one connecting portion connectable to an associated primary structure component to fasten the rail to the component, and a carrier portion extending from the connecting portion in a direction along a longitudinal axis of the system. The system further comprises a first carrier element having a first end connected to a first carrier rod extending in a direction along the longitudinal axis and a second end connectable to a first interior component, wherein the first carrier rod is fastened to the carrier portion of the first rail, and a second carrier element having a first end connected to a second carrier rod extending in the longitudinal axis direction and a second end connected to the first carrier element, wherein the second carrier rod is fastened to the second rail carrier portion.

Abstract: An aircraft region comprising a main aisle extending along a longitudinal axis of an aircraft cabin, a door aisle extending along a transverse axis of the aircraft cabin substantially perpendicularly to the main aisle and an aircraft monument arranged in the door aisle and comprising at least one flight attendant seat facing a section of the main aisle adjoining the door aisle.

Abstract: The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.

Abstract: A shell structure of a fuselage at a door opening of the fuselage comprising a main door frame arranged on a cross-sectional plane of the fuselage. A wall portion of the main door frame extends into the fuselage and forms at least part of a first monument wall.

Abstract: An aircraft region comprising a main aisle extending along a longitudinal axis of an aircraft cabin, a door aisle extending along a transverse axis of the aircraft cabin substantially perpendicularly to the main aisle and an aircraft monument arranged in the door aisle and comprising at least one flight attendant seat facing a section of the main aisle adjoining the door aisle.