Patent classifications
Y10S292/15
Modular aircraft galley systems, apparatus and methods for configuration
In a preferred embodiment, a modular galley monument for an aircraft cabin includes a first side panel, a second side panel, and an upper surface connecting the first side panel and the second side panel. The modular galley monument may include dividers partitioning the monument into a number of compartments. The monument may include an upper monument portion and a lower monument portion connected at a periphery via a seal allowing for vertical deflection between the first monument portion and the second monument portion of at least one inch while maintaining contact with both. The monument may include an integrated heating appliance for a compartment, including an insulation shell, a heated compartment positioned within the insulation shell, an electrical heating unit disposed within the insulation shell and configured to provide heat energy to the heated compartment. And a door assembly rotatably connected about an opening of the heated compartment.
Upper mounting apparatus for retaining aircraft monuments
In an illustrative embodiment, an upper monument attachment system is provided for retaining aircraft monuments, the system including a first support, a second support, and a joiner connecting a first end of the first support and a first end of the second support, a stay having a first end pivotably connected to the joiner, a tie rod configured to connect the joiner to an attachment point of the aircraft, a first rail having a first base configured to connect to an upper surface of the monument and a first facing configured to connect to the first support and the second support, and a second rail having a second base configured to connect to the upper surface of the monument and a second facing configured to connect to a second end of the stay.
Aircraft monument floor mounting system
A system for mounting an aircraft monument partition to an aircraft cabin surface such as a floor may include a mounting structure fitted within and attached to a floor-abutting edge of the monument partition, the mounting structure including a mounting opening. A securement apparatus for securing the monument partition to cabin surface via the mounting structure may include a threaded fastener for extending through the mounting opening of the mounting structure and through a corresponding opening in a track mounted to the cabin surface, and a bridging washer for mating with the mounting opening; where, to secure the monument partition to the floor of the cabin area, the threaded fastener is provided through the mounting opening of the mounting structure and threaded to a mating fixture on a bottom side of the track.
Automatic lock-unlock door safety control
An electromechanical door supporting system for temporarily maintaining a door in an open position having: a) a housing with an electric motor in communication with a power source; b) a base plate sized to pass underneath a swinging door; c) the base plate extending away from the housing; d) the electric motor causing rotational movement in a rod extending from inside the housing, to outside the housing and over a surface of the base plate; e) a door supporting element extending perpendicular to the extended rod; and f) the door supporting element being attached to the extended rod at a proximal location and extending over the surface of the base plate to a distal end so that rotation of the extended rod causes the distal end of the door supporting element to elevate above the base plate to secure an opened door.
Portable Door Securement Device
A portable door securement device is provided having a member extending from a first end engaged to a doorknob of a swinging door or endwall of a sliding door. A second end of the securement device is configured to be engaged with a support surface adjacent the door, to prevent opening of the door in a direction toward the engaged member.
Intermediate stowage retainer for aircraft monument storage bay
In an illustrative embodiment, an intermediate retaining assembly secures a rearmost equipment item of at least two horizontally-stacked equipment items within an aircraft galley compartment. The intermediate retaining assembly may include a manual control coupled to a first end of a rod where rotation of the manual control causes rotation of the rod. A retaining lever may engage a second end of the rod upon moving the rod to an axially extended position such that rotation of the rod causes the retaining lever to rotate between a position for securing the rearmost equipment item and a position for removing the rearmost equipment item from or inserting into the compartment. A mounting plate may be secured to an interior surface of the compartment and may have a recess for receiving the retaining lever, preventing the retaining lever from interfering with the equipment item during insertion into or release from the compartment.
DOOR SECURITY DEVICE
A door lock has a bottom surface, a bottom surface, a wedge portion extending upward from the bottom surface, and a projection member secured to the bottom surface. The projection member has a plurality of spikes defined therein that extend from a first side of the projection member in a direction away from the bottom surface.
Safety door lock using door handle
A safety door lock may include the door handle configured to be rotatable about a rotational axis and to slidably reciprocate in a horizontal direction and having a sliding groove on the side surface thereof adjacent to a door. The safety door lock may include a body combined with an inside of the sliding groove to form a rotating shaft with another door handle provided at the other side of the door and supporting sliding of the door handle so as to protrude the door handle from the front end of the door. The safety door lock may include an elastic unit fixed to the body, and elastically relaxing the door handle and the body. Other embodiments may also be provided.