606results about "Toilet fittings" patented technology

The invention provides an improved automatic faucet for a lavatory unit of an aircraft. A body 110 of an automatic faucet 100 has on its lower left side (seen from the front) a liquid soap dispenser outlet 200, and the dispenser outlet 200 is connected to a liquid soap dispenser tank via a valve not shown. A reflective infrared sensor 210 for the liquid soap dispenser outlet and an LED light 230 for the liquid soap dispenser outlet are provided adjacent to the liquid soap dispenser outlet 200. When a user's hand is placed within the area of infrared waves 220, a predetermined amount of liquid soap is supplied over the user's hand. The LED light 230 is turned on to illuminate the user's hand. A water supply outlet 300 is provided at the lower right side of the body 110, which is connected to a water tank via a valve not shown. A reflective infrared sensor 310 for the water supply outlet and an LED light 330 for the water supply outlet are provided adjacent to the water supply outlet 300. When the user's hand is placed within the area of infrared waves 320, a predetermined amount of water is supplied over the user's hand. The LED light 330 is turned on to illuminate the user's hand.

The invention relates to a rest compartment arrangement in an aircraft, comprising a rest compartment and at least one monument, wherein the rest compartment is arranged above a cabin floor and comprises a passage that extends from a rest compartment floor in the direction of the cabin floor. When compared to the state of the art, the invention is characterised in that the at least one monument comprises at least one wall which above a seat region situated therein forms a recess to accommodate the passage. As a result of this, monuments can be positioned in a space-saving manner underneath the passage in the cabin without this resulting in reduced comfort, because the recess above the seat region is not perceived to be distracting by the passenger.

An interior structure for a mobile platform is provided. The interior structure is constructed of a lightweight collapsible frame that can be reconfigured from a compact, substantially flat collapsed state to a non-compact, substantially sprawling expanded state. In the expanded state, the collapsible frame provides at least a portion of a structural load bearing frame for the interior structure. The interior structure additionally includes a plurality of interchangeable panels that attach to the collapsible frame to form interior surfaces of the structure. The panels form such things as the interior wall, ceiling and floor surfaces and can also include amenities such as shelves, lights, beds, closets, electrical outlets, Internet connections and entertainment equipment. The interior structure can be carried though the typical man-door of a mobile platform. Thus, the interior structure can be installed after the outer structure of the mobile platform has been assembled and just as easily be removed at a later time by merely removing the interchangeable panels, collapsing the collapsible frame and carrying the panels and frame out though the man-door.

A space efficient lavatory module for commercial aircraft includes an aft facing concave wall recess that provides a greater distance from an upper, forward facing portion of a cabin structure, such as an aircraft passenger seat to avoid having a passenger's head impact the aft facing lavatory or enclosure wall in a sudden aircraft deceleration. The aft facing concave wall recess also provides space for mounting of a protective cushion, in order to reduce a passenger's risk of head trauma in a sudden deceleration, as well as other items, such as a video monitor, a bassinet or infant bed, without inhibiting passenger movement.

A vortex separator for drawing a substantially moisture-free airstream from a waste stream having an annular channel defining a first vortex flow path for separating liquid and solid waste from this waste stream and preferably a filter unit with an inverted conical cavity between nested inverted cones defining a second vortex flow path that is isolated from the first vortex flow path for separating additional liquid and solid waste from the waste stream before it exits the vortex separator. In preferred embodiments, the separator includes a removable filter unit cartridge positioned within the outer cone and a helix isolator to respectively make use of the separator more convenient to use and more efficient.

A handicapped-accessible aircraft lavatory includes a wheelchair region, a toilet assembly adjacent to and oriented at a non-zero angle with respect to the wheelchair region, and a sink assembly adjacent to the toilet assembly. The sink assembly includes a basin positioned at a predetermined height and a predetermined lateral distance with respect to the toilet seat, wherein the predetermined height and the predetermined distance are selected such that the sink assembly is within arms-reach of a passenger (e.g., a 95th percentile male passenger) sitting on the toilet seat. Additional amenities such as mirrors, toilet paper, tissues, and the like may also be similarly positioned.