Abstract: Provided are flush mountable bottle openers and methods of using such openers to remove bottle caps. These openers may be used in aircraft and other types of vehicles as well as any applications where protrusion away from supporting structures may be undesirable. A flush mountable bottle opener may include a base and a cap leverage plate pivotably coupled to the base. The base may protrude into a supporting structure such that the top edge of the base is substantially flush with the surface of the supporting structure. When the opener is not in use, the cap leverage plate may be closed and be substantially coplanar with the base edge. During operation, the cap leverage plate is brought into its open position directly by a user or using a bottle. The base and plate include engagement surfaces that support a bottle cap while the cap is removed.

Abstract: A method and an apparatus for forming an embedded light source in a composite panel. A first electrode and a second electrode are associated with a first layer of material. A light source is positioned in electrical communication with the first electrode and the second electrode. An assembly comprising the first layer of material, the first electrode, the second electrode, and the light source is processed to form a multilayer panel with an embedded light source.

Abstract: Methods for manufacturing composite panels for use in the interior of an aircraft are disclosed, specifically, methods of manufacturing joggled composite panels comprising metal inserts and the resulting composite panels and inserts.

Abstract: Aircraft passageway storage units are disclosed herein. An example apparatus includes a storage assembly to be supported on a floor of an interior of a fuselage of an aircraft. The storage assembly has a corner to be adjacent a passageway of the interior of the fuselage, and the passageway is to extend around the corner. The example apparatus also includes a door coupled to the storage assembly. The door extends from a first side of the storage assembly to a second side of the storage assembly and defines a portion of the corner. The door is to cover an opening of a compartment of the storage assembly when the door is in a closed position, and the opening is to extend from the first side to the second side.

Abstract: A method and apparatus for associating an edge of a first object with a second object using an insert. In one illustrative embodiment, an apparatus comprises a structure and a number of attachment features associated with the structure. The structure is configured to be inserted within a hollow portion of the first object at an edge of the first object. The structure is further configured to span an entire thickness of the first object at the edge of the first object. The number of attachment features is configured for use in attaching the second object to the structure to attach the second object to the edge of the first object.

Abstract: A method and apparatus for associating an edge of a first object with a second object. An insert comprising a structure holding a fastener element may be positioned within a hollow portion at the edge of the first object. The structure may be configured to span an entire thickness of the first object at the edge of the first object. The structure may be adhesively bonded to the first object. The second object may be attached to the edge of the first object using the fastener element.

Abstract: A structure comprises a door, a frame for the door, and a door snubber. One of the frame and the door has an overlapping edge trim, and the other carries the snubber such that the snubber engages the edge trim when the door is closed on the frame.

Abstract: A structure comprises a door, a frame for the door, and a door snubber. One of the frame and the door has an overlapping edge trim, and the other carries the snubber such that the snubber engages the edge trim when the door is closed on the frame.

Abstract: Aircraft passageway storage units are disclosed herein. An example apparatus includes a storage assembly to be supported on a floor of an interior of a fuselage of an aircraft. The storage assembly has a corner to be adjacent a passageway of the interior of the fuselage, and the passageway is to extend around the corner. The example apparatus also includes a door coupled to the storage assembly. The door extends from a first side of the storage assembly to a second side of the storage assembly and defines a portion of the corner. The door is to cover an opening of a compartment of the storage assembly when the door is in a closed position, and the opening is to extend from the first side to the second side.

Abstract: A method and apparatus for associating an edge of a first object with a second object using an insert. In one illustrative embodiment, an apparatus comprises a structure and a number of attachment features associated with the structure. The structure is configured to be inserted within a hollow portion of the first object at an edge of the first object. The structure is further configured to span an entire thickness of the first object at the edge of the first object. The number of attachment features is configured for use in attaching the second object to the structure to attach the second object to the edge of the first object.