Abstract: A method of operating a lighting fixture comprising a plurality of discrete illumination sources of distinguishably different color coordinates comprises determining target color coordinates and luminous flux at which to operate the lighting fixture, determining input electrical power values for each of the plurality of discrete illumination sources that substantially produce the target color coordinates and luminous flux by referencing a calibration data lookup table having calibration data based on measurements of the plurality of discrete illumination sources, determining a color mixing zone defined by three distinguishably different color coordinates of the plurality of discrete illumination sources within which the target color coordinates lie according to the calibration data, determining luminous flux ratios for each of the plurality of discrete illumination sources having one of the three distinguishably different color coordinates defining the color mixing zone that substantially produces the target

Abstract: A premium class passenger suite that includes a main seat positioned in the suite together with separate bed. The bed has a flexible mattress of predetermined dimensions and is movable between a stowed position to one side of the main seat and a deployed position above and separate from the main seat. A drive apparatus is provided for driving the bed between the stowed and deployed positions. The main seat is configured to be movable between a seating position when the bed is stowed, and a stowed position with a lowered seat back when the bed is deployed for use.

Abstract: An aircraft passenger seat swivel assembly for an aircraft seating unit that includes a pair of transversely spaced-apart base rails, each including fore and aft fittings for connecting the base rails to an aircraft deck. The base rails define a transversely-extending horizontal plane extending between the pair of base rails. A swivel assembly is mounted between the pair of base rails in the laterally-extending horizontal plane. The swivel assembly provides a low profile seat with a spar that forms a part of the swivel assembly and transfers loads from the seat efficiently to the aircraft deck. A slide assembly enables the seat occupant to slide the seat fore-and-aft and side-to-side independent of the rotation of the seat on the swivel.

Abstract: A disclosed power supply includes a power factor correction circuit including a switch, an inductor having a first terminal connected to an input voltage, and a second terminal connected to the switch, a storage capacitor and a load, a value of the inductor selected to operate the power factor correction circuit in discontinuous conduction mode, and a controller programmed to operate the switch to increase a power factor of the power supply. The switching frequency of the switch is periodically adjusted to reduce electromagnetic interference.

Abstract: A three dimensional lattice panel structure having a multitude of mutually offset holes formed in a respective top and bottom of the panel and intersecting to form voids with interspersed support posts interconnecting the top and bottom of the panel in areas not encompassed by the mutually offset holes.

Abstract: In one embodiment of an aircraft emergency oxygen delivery system, power can be generated by the flow of gas over a transducer disposed inside an oxygen delivery tube. A pressure differential gives rise to a temperature difference across the transducer, and the temperature difference can be converted to a voltage. The voltage can be quadratically dependent upon the Mach number M (e.g. flow velocities from 1 to 140 m/s) and proportional to a Seebeck coefficient of the transducer. The power thus generated may be used to operate LED indicators visible from the exterior of the tube, a variety of sensors, and wireless communication with a central control system. Oxygen flow to a mask may be adjusted based on ambient oxygen content and data collected from a passenger wearing the mask, including a blood oxygen saturation level, pulse or respiration rate.

Abstract: A reconfigurable vent system in fluid communication with an air chiller to deliver chill air to one or more galley food and beverage storage compartments in parallel is reconfigurable to operate in either of an air-through or an air-over orientation. The reconfigurable vent system comprises a vent in fluid communication with the air chiller via a duct and configured to provide the chill air to the one or more galley food and beverage storage compartments. The vent directs the chill air substantially toward the interior of the one or more galley food and beverage storage compartments in the air-through orientation at a first angle, and the vent directs the chill air substantially around the one or more galley food and beverage storage compartments in the air-over orientation at a second angle different from the first angle.

Abstract: A multi-purpose beverage pod holder for a beverage brewing apparatus is disclosed comprising a flange adapted to be received in a slot in the brewing apparatus, a screen disposed orthogonal with the flange for allowing fluid to pass therein through, a first cylindrical wall encircling the screen on a first surface of the pod holder, the first cylindrical wall having a first diameter and defining a first packet retainer, and a second cylindrical wall encircling the screen on an opposite surface of the pod holder, the second cylindrical wall having a second diameter that is larger than the first diameter and defining a second packet retainer. The pod holder can be used to brew both espresso and coffee in the same machine depending upon the orientation of the pod holder.

Abstract: A modular floor track adapter system including a plurality of adapter plates laterally sized to span existing aircraft floor beams, each of the plurality of adapter plates shaped to interlock with an adjacent adapter plate in a side-by-side arrangement and including a series of holes for attaching seat track crown sections and panel attachment tabs for securing an aircraft floor panel thereto.

Abstract: A location and support system for installation of an aircraft galley insert case for location and attachment of an aircraft galley insert in an aircraft galley monument includes a floating stabilizer connector fixedly mounted to an upper surface of the aircraft galley insert case, and a floating receiver shelf engagement insert fixedly mounted to an attachment slot in an upper portion of a compartment in the aircraft galley monument for receiving the aircraft galley insert case. The floating receiver shelf engagement insert includes a slotted portion configured to removably receive the floating stabilizer connector. The aircraft galley insert may also include a plurality of ceramic spacers embedded in formed insulation.

Abstract: A system and method for delivering oxygen to a passenger of an aircraft including a supply of oxygen, an oral-nasal mask, a controller for adjusting a flow of oxygen from the supply of oxygen to the oral-nasal mask, and a sensor for determining a user's blood oxygen saturation level, wherein the controller adjusts the flow of oxygen based on the sensor's determination of the user's blood oxygen saturation level.

Abstract: A passenger suite seating arrangement including a first passenger suite including a first seat and a first video monitor fixed in position directly forward of the first seat, and a second passenger suite including a second seat facing the first seat and laterally offset relative thereto, the second suite including a second video monitor configured to move parallel to a viewing angle of a passenger seated in the second seat to selectively connect and divide the first and second suites.

Abstract: A check valve for an aircraft galley plumbing system having a valve body including an inlet for a potable water supply line, and first and second outlet ports leading to a distribution manifold. In a preferred embodiment, quick disconnects that include reverse flow inhibitors seal the valve's output ports. A vertical channel extends through the valve body for draining water through the valve, which is coupled to a pressure line connection port that exerts pressure from the aircraft's pressure system. A piston reciprocating across the vertical channel and biased by a spring is in fluid communication with the pressure line connection port, such that when water pressure is introduced from a pressure line to the connection port of sufficient pressure to collapse said spring, the piston blocks said channel, and when the water pressure is insufficient to collapse said spring then the piston retracts to open said channel.

Abstract: A lavatory for an aircraft cabin includes a wall having a forward wall portion disposed immediately aft of and substantially conforming to an exterior aft surface of an aircraft cabin structure, such as a passenger seat, that is substantially not flat in a vertical plane. The forward wall portion includes a forward projection over an aft portion of the adjacent passenger seat. The forward wall portion can define a secondary space in the interior lavatory space, which can provide an amenity stowage space, and can include design elements providing visual space.

Abstract: A door assembly including a swinging door, a sealing member pivotally to the door configured to pivot between a first position into contact with the floor and a second position out of contact with the floor, a lever arranged to actuate pivoting movement of the sealing member in response to opening and closing of the door, a biasing member arranged to bias the lever toward a non-actuating position, and a separate deployment stop arranged to actuate the lever.

Abstract: A seat pan assembly including a fixed seat pan frame defining a substantially horizontal forward portion and a rear portion at an angle to horizontal, and a seat pan pivotally supported on the fixed seat pan frame, the seat pan having a pivot axis established through a width of the seat pan such that the seat pan is free to pivot relative to the fixed seat pan frame between substantially horizontal and an angle to horizontal. An aircraft passenger seat including a seat pan assembly adapted to adjust independent of seatback recline motion.

Abstract: A lavatory for an aircraft cabin includes a wall having a forward wall portion disposed immediately aft of and substantially conforming to an exterior aft surface of an aircraft cabin structure, such as a passenger seat, that is substantially not flat in a vertical plane. The forward wall portion includes a forward projection over an aft portion of the adjacent passenger seat. The forward wall portion can define a secondary space in the interior lavatory space, which can provide an amenity stowage space, and can include design elements providing visual space.

Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.

Abstract: A vacuum powered system for moving a movable component, such as for raising and lowering a stowage container, includes a vacuum actuator connected between a fixed structure and a movable component. The vacuum actuator includes one or more intake ports that are configured to connect with a source of vacuum for moving the movable component in a first direction to a first position, and one or more bleed valve ports for venting the vacuum actuator to move the movable component in a second direction to a second position. The vacuum actuator may be an air bellows, a single acting linear vacuum actuator, or a dual acting linear vacuum actuator. A guiding system is further provided that includes elongated tracks in a stationary stowage container housing that houses the movable component, and corresponding guide elements on the movable component that slidably engage with the elongated tracks for moving the movable component.