B/E Intellectual Property, Inc. Patent applications |
Patent application number | Title | Published |
20140238046 | REFRIGERATOR-OVEN COMBINATION FOR AN AIRCRAFT GALLEY FOOD SERVICE SYSTEM - A refrigerator-oven combination for an aircraft galley food service system includes a housing with a thermally insulated compartment, a heating device for heating the compartment in a heating mode, and a refrigeration device for cooling the compartment in a refrigeration mode. | 08-28-2014 |
20140196719 | OXYGEN CONSERVATION SYSTEM FOR COMMERCIAL AIRCRAFT - An emergency oxygen supply system for use on aircraft in the event of a loss in cabin pressure is configured for delivering allotments of oxygen and timing the delivery such allotments to each passenger so as maximize the efficiency of the transfer of such oxygen into the passenger's bloodstream. The delivery of each allotment is selected so that the entire allotment is available for inhalation into the region of the lung most efficient at oxygen transfer while the volume of the allotment is selected to substantially coincide with the volume of such region of the lung. | 07-17-2014 |
20140152162 | ELECTRICALLY ACTIVATED LATCH FOR AIRCRAFT STOWAGE BINS - An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the movable stowage bin portion in a closed position and unlatches the movable stowage bin portion to an open position. An electrically operated stowage bin activation switch operates the stowage bin latch mechanism, allowing the aircraft stowage bins to be locked by independently controlling the overhead stowage bins through the aircraft cabin management system, or by control of the latch by the stowage bin activation switch. | 06-05-2014 |
20140109908 | SYSTEM FOR REGULATING THE DISPENSING OF COMMERCIAL AIRCRAFT PASSENGER OXYGEN SUPPLY - The aircraft emergency oxygen supply system includes one or more sources of supplemental breathable oxygen, one or more inlet valves for one or more breathing devices, connected to the inlet valves, and one or more cabin air pressure transducers. A pressure controller controls the inlet valves in response to the one or more cabin air pressure transducers. One or more second pressure transducers may connected to conduits downstream of inlet valves to be monitored, and the pressure controller may also control operation of the inlet valves in response to the one or more second pressure transducers. | 04-24-2014 |
20130019866 | LAVATORY CHEMICAL OXYGEN WITH REMOTELY LOCATED OXYGEN GENERATION - A lavatory chemical oxygen system for providing breathing gas to an aircraft lavatory includes a remotely located oxygen generation system for supplying oxygen to the aircraft lavatory. The lavatory chemical oxygen system includes an aircraft passenger main cabin, an aircraft lavatory, and a lavatory oxygen drop box housing with a lavatory oxygen mask in the aircraft lavatory. A chemical oxygen generator located remotely from the aircraft lavatory is connected to the lavatory oxygen mask to provide supplemental oxygen to an occupant of the lavatory. The chemical oxygen generator can be activated electronically or manually. | 01-24-2013 |
20120285942 | REFRIGERATOR-OVEN COMBINATION FOR AN AIRCRAFT GALLEY FOOD SERVICE SYSTEM - A refrigerator-oven combination for an aircraft galley food service system includes a housing with a thermally insulated compartment, a heating device for heating the compartment in a heating mode, and a refrigeration device for cooling the compartment in a refrigeration mode. | 11-15-2012 |
20120240785 | BREW CHAMBER PACKET EJECTOR - A brew basket for a brewing apparatus is disclosed having a housing adapted to couple the brew basket to a brewing apparatus and a platform extending from the housing, the platform including a brewing chamber defined by a continuous peripheral wall and a perforated floor. The perforated floor is coupled to a vertically reciprocating member at a first end for raising and lowering the perforated floor of the brew basket with respect to the continuous peripheral wall, the vertically reciprocating member extending below a lowermost surface of the platform so that it can be raised by lowering the platform onto a flat surface. | 09-27-2012 |
20120240776 | PRESSURE RELIEF SYSTEM FOR ESPRESSO MAKER - A brewing system for brewing a beverage is disclosed having an inlet for receiving fresh water for brewing, and a first solenoid for directing water to a water storage tank when a level in the water storage tank falls below a predetermined level. A pair of pumps direct water from the storage tank to a second solenoid. Two or more brew paths lead away from the second solenoid, each brew path including a heating element to heat the water flowing therethrough. The second prevents overpressurization in the brew paths by routing excess pressurized water from the respective brew path back through the second solenoid and out a drain line leading to a drain, where the path to the drain is not part of the brew path. | 09-27-2012 |
20120222676 | OXYGEN CONSERVATION SYSTEM FOR COMMERCIAL AIRCRAFT - An emergency oxygen supply system for use on aircraft in the event of a loss in cabin pressure is configured for delivering allotments of oxygen and timing the delivery such allotments to each passenger so as maximize the efficiency of the transfer of such oxygen into the passenger's bloodstream. The delivery of each allotment is selected so that the entire allotment is available for inhalation into the region of the lung most efficient at oxygen transfer while the volume of the allotment is selected to substantially coincide with the volume of such region of the lung. | 09-06-2012 |
20120222443 | LIQUID GALLEY REFRIGERATION SYSTEM FOR AIRCRAFT - The liquid galley refrigeration system for cooling food carts for aircraft employs an intermediate working fluid to transfer heat from one or more food carts to one or more remote chillers, allowing the carts and chillers to be advantageously distributed in the aircraft. While the chiller working fluid undergoes a phase change in order to transfer heat from the intermediate working fluid to the cooling air, the intermediate working fluid remains in its liquid phase throughout its circulation. A recirculation pump circulates the intermediate working fluid through a distribution system that may link a plurality of chillers to a plurality of food carts, and the temperature of the food carts is regulated by a combination of controls. | 09-06-2012 |
20120074258 | INTEGRATED AIRCRAFT INTERIOR - An integrated aircraft interior module includes one or more ceiling panels, sidewall linings, decompression ventilation provisions, and overhead stowage compartments including cabin air distribution ducting, personal service units. The sidewall linings, overhead stowage compartments and other interior structure integrated items attach to existing aircraft structural provisions. | 03-29-2012 |
20110256821 | USE OF AIRCRAFT CABIN SURFACES TO GUIDE AIRFLOW AND SOUND - An interior ceiling panel system includes a ceiling panel mounted in a ceiling area, a first airflow directing panel in a first side of the ceiling area defining an airflow passage, and a second airflow directing panel in a second side of the ceiling area, defining an eddy space. An airflow supply source introduces airflow into the ceiling area, and the second airflow directing panel provides an obstruction that creates an eddy in the eddy space that incoming airflow with air in the cabin. One or more speakers project sound energy upward toward the ceiling panel, which deflects sound energy to provide more uniform sound levels in the cabin. | 10-20-2011 |
20110255296 | AIRCRAFT CEILING MODULE WITH INTEGRATED LIGHTING, VALENCES AND WIRING - An aircraft ceiling module includes a ceiling panel with integrated lighting, valences and wiring. LED lighting units are mounted directly to the ceiling panel, and one or more valence panels are connected to the ceiling panel to shield the LED lighting units. The valence panels are integral to the ceiling panel, and provide structural stiffness to overall construction of the ceiling module. Wiring connected to the LED lighting units is integrated into the ceiling panel. | 10-20-2011 |
20110254705 | ELECTRICALLY ACTIVATED LATCH FOR AIRCRAFT STOWAGE BINS - An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the movable stowage bin portion in a closed position and unlatches the movable stowage bin portion to an open position. An electrically operated stowage bin activation switch operates the stowage bin latch mechanism, allowing the aircraft stowage bins to be locked by independently controlling the overhead stowage bins through the aircraft cabin management system, or by control of the latch by the stowage bin activation switch. | 10-20-2011 |
20110253836 | AIRCRAFT BIN MODULE WITH INTEGRATED AIR DUCTS AND LIGHTING - An aircraft overhead luggage bin module includes a stowage bin assembly, an integral light assembly providing structural stiffness to an upper portion of the stowage bin assembly. The stowage bin assembly includes an air distribution plenum that also transmits loads to mounting structures, an upper air diffuser connected to the air distribution plenum, and an optional lower sidewall diffuser connected to the air distribution plenum. | 10-20-2011 |
20110253835 | AIRCRAFT INTERIOR LAVATORY - 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. | 10-20-2011 |
20110253714 | LIFT ASSIST MECHANISM - A lift assist mechanism is provided for assisting lifting of a movable component that can move between lowered and raised positions relative to a fixed structure. The lift assist mechanism includes a lift assist spring connected to a spring shaft, and an elongated track in which an end of the lift assist spring or an end of the spring shaft are movably engaged. A spring lock restrains movement of the spring shaft when a lift assist is not required, and releases the spring shaft when a lift assist is required. | 10-20-2011 |
20110238742 | GAIN TO GAIN NETWORK FOR AIRCRAFT GALLEY SYSTEM - An aircraft galley system is configured with a GAIN to GAIN network that allows for data exchange and communication between each GAIN on the system. By omitting reliance on a galley network controller for acquisition of GAIN data, the present system is simpler, lighter, and more cost-effective. Each GAIN may be polled for data by any other GAIN, such as via a data port, dedicated bus, or wireless connection. The data acquisition between the GAIN and a data collection and display device may be wired in network, wired out of network, or through a wireless link such as a Wi-Fi network. | 09-29-2011 |
20110233333 | SMALL DIAMETER PRESSURE STRUCTURE COMMERCIAL AIRCRAFT CREW REST - An aircraft crew rest station includes an overhead crew rest portion including a central deck portion, forward and aft bunk portions, and a central entry vestibule connected between a passenger seating area and the central deck portion. The forward and aft bunk portions include a plurality of adjacent partitioned individual sleeping berths configured in interfitting alternating trapezoid shapes to optimize spatial accommodation of body proportions of crew members in the available aircraft space. The central deck portion includes an emergency escape hatch, a fold-down jump seat, and a fold-down entry door that removably covers a stairway of the central entry vestibule. | 09-29-2011 |
20110168182 | QUICK-DONNING FULL FACE OXYGEN MASK WITH INFLATABLE HARNESS AND SOFT FOLDABLE LENS - A mask and harness system for use in providing breathing oxygen and protection from pollutants for the eyes and respiratory system as might be encountered in high altitude aviation environments. In one preferred embodiment, the mask system has a face seal, a soft flexible lens, a pneumatically-actuated harness, and a regulator with microphone to control the flow of oxygen and to facilitate communications in aircraft flight decks and other aircraft compartments. The system is designed for required five-second donning with one hand and because of the flexible lens, is capable of storage in the relatively preferred on crowded flight decks. It is connected to an oxygen source and, optionally, with aircraft communications. The regulator controls the flow rate of oxygen to the wearer based on altitude and physiological requirements. The regulator includes a valve for purging the condensation-prone moist gases from the lens area and provides positive pressure in the mask. A second preferred embodiment molds the lens and mask seal of a single material having sufficient optical quality and flexibility to accomplish both purposes. | 07-14-2011 |
20110139931 | FIREPROOF BIDIRECTIONAL DECOMPRESSION PANEL - A fireproof, bi-directional decompression panel includes a frame member and a pressure relief panel member that is releasably retained to the frame member to removably cover a decompression vent opening of an aircraft partition, such as a sidewall of an aircraft cargo compartment. During a decompression event, the pressure relief panel member is released bi-directionally in either of two opposing directions from the frame member when a predetermined pressure differential exists across the partition. The decompression panel assembly is fire resistant, and has reduced weight and fewer parts than prior conventional decompression panel assemblies. | 06-16-2011 |
20110011177 | LIQUID LEVEL SENSOR FOR GALLEY INSERTS - The liquid level sensing device includes rotating electrically conductive probes and uses a self-cleaning rotary electrical connection system with a contact stylus on a rotating conductive barrel, for sensing a liquid level in a dispensing container of an aircraft galley insert. The probes, pivot arms of the probes, rotating drum and stylus may have an exterior surface formed of an electrically conductive, corrosion resistant material. | 01-20-2011 |
20100319698 | OXYGEN CONSERVATION SYSTEM FOR COMMERCIAL AIRCRAFT - An emergency oxygen supply system for use on aircraft in the event of a loss in cabin pressure is configured for delivering allotments of oxygen and timing the delivery such allotments to each passenger so as maximize the efficiency of the transfer of such oxygen into the passenger's bloodstream. The delivery of each allotment is selected so that the entire allotment is available for inhalation into the region of the lung most efficient at oxygen transfer while the volume of the allotment is selected to substantially coincide with the volume of such region of the lung. | 12-23-2010 |
20100200555 | REFRIGERATOR-OVEN COMBINATION FOR AN AIRCRAFT GALLEY FOOD SERVICE SYSTEM - A refrigerator-oven combination for an aircraft galley food service system includes a housing with a thermally insulated compartment, a heating device for heating the compartment in a heating mode, and a refrigeration device for cooling the compartment in a refrigeration mode. | 08-12-2010 |
20100186499 | ELECTRO-OPTIC LIQUID LEVEL SENSING SYSTEM FOR AIRCRAFT BEVERAGE BREWING - The electro-optic liquid level sensing system detects a level of liquid in a container having an upper opening, such as for a server container of a beverage maker for a transport system, such as for aircraft, trains, trucks, buses and the like. A support housing mates with the upper opening of the container, and a primary liquid level sensor is mounted in the support housing for non-intrusively measuring the liquid level. A secondary liquid level sensor may be mounted in the support housing to sense a predetermined liquid level to prevent accidental overflows. Protective lenses may be placed in front of the primary liquid level sensor. | 07-29-2010 |
20100102050 | PROXIMITY SENSOR - A proximity switch flow sensor detects movement of a faucet handle of a faucet of a hot water container in order to detect flow from the hot water container. The proximity switch flow sensor includes an emitter paired with a detector, which can be mounted in association with the faucet handle to detect open and closed positions of the faucet handle, to provide electronic logic information regarding the status of the faucet handle position, as an indication of a flow condition, to a control unit that controls heating of water in the hot water container. An electro-mechanical switch and a mechanism to transfer movement of the faucet handle to the switch may also be used to detect open and closed positions of the faucet handle as an indication of a flow condition. | 04-29-2010 |
20090314296 | SYSTEM FOR REGULATING THE DISPENSING OF COMMERCIAL AIRCRAFT PASSENGER OXYGEN SUPPLY - The aircraft emergency oxygen supply system includes one or more sources of supplemental breathable oxygen, one or more inlet valves for one or more breathing devices, connected to the inlet valves, and one or more cabin air pressure transducers. A pressure controller controls the inlet valves in response to the one or more cabin air pressure transducers. One or more second pressure transducers may connected to conduits downstream of inlet valves to be monitored, and the pressure controller may also control operation of the inlet valves in response to the one or more second pressure transducers. | 12-24-2009 |
20090114036 | Use of Reed Switch and Magnet to Detect Movement of Faucet Handle - A flow sensing apparatus detects movement of a faucet handle of a faucet of a hot water container in order to detect flow from the hot water container. A reed switch and an associated magnet can be mounted to detect open and closed positions of the faucet handle to provide electronic logic information regarding the status of the faucet handle position as an indication of a flow condition to a control unit that controls heating of water in the hot water container. | 05-07-2009 |
20080289800 | LIQUID GALLEY REFRIGERATION SYSTEM FOR AIRCRAFT - The liquid galley refrigeration system for cooling food carts for aircraft employs an intermediate working fluid to transfer heat from one or more food carts to one or more remote chillers, allowing the carts and chillers to be advantageously distributed in the aircraft. A plurality of heat exchanges effect a cooling of the carts wherein heat from the food cart is first transferred to a first airflow; heat from the first airflow is then transferred to an intermediate working fluid that is circulated between a location immediately adjacent the food carts and a remote chiller; heat from the intermediate working fluid is subsequently transferred to the chiller working fluid; and finally, heat from the chiller working fluid is expelled. While the chiller working fluid undergoes a phase change in order to transfer heat from the intermediate working fluid to the cooling air, the intermediate working fluid remains in its liquid phase throughout its circulation. A recirculation pump circulates the intermediate working fluid through a distribution system that may link a plurality of chillers to a plurality of food carts, and the temperature of the food carts is regulated by a combination of controls. | 11-27-2008 |
20080236586 | INFLATABLE HARNESS CREW MASK - The inflatable harness crew mask includes an inflatable harness with a compressed gas supply system connected to the inflatable harness independent of oxygen supplied to the mask from an oxygen regulator. The mask includes a valve connector with an exhalation and inhalation valve and an inflation valve connected to a pressurized gas inflation supply assembly including a container portion for a compressed gas cartridge, and a regulator portion connected to provide pressurized gas from the cartridge to an inflation gas supply tube connected to the inflation valve, which is manually operable by the user. | 10-02-2008 |