Patents Assigned to B E Aerospace, Inc.
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Patent number: 11769657Abstract: A system for powering an excimer bulb includes a first inductor configured to be coupled to a first terminal of the excimer bulb. The system further includes a first transistor coupled to the first inductor and having an on state configured to allow current to flow through the first inductor and an off state. The system further includes a second transistor configured to be coupled to the first terminal of the excimer bulb and having an on state configured to allow current to flow through the excimer bulb and an off state. The system further includes a controller coupled to the first transistor and the second transistor, and to control operation of the first transistor and the second transistor to power the excimer bulb.Type: GrantFiled: July 9, 2021Date of Patent: September 26, 2023Assignee: B/E AEROSPACE, INC.Inventors: Eric Johannessen, Jeremy Fredrich
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Patent number: 11766856Abstract: In a preferred embodiment, a composite panel with a smooth outer surface, ready for painting with or without addition of primer, may be created by constructing a panel layup assembly upon a mold, the panel layup assembly including a composite panel having a core and a resin formulation, and a release film between the mold and the composite panel, where a smooth release surface of the release film is in contact with the composite panel upon construction; initiating curing of the composite panel at a first temperature within a lowermost ten percent of a curing temperature range of the resin formulation; continuing curing of the composite panel at a second temperature above the lowermost ten percent of the curing temperature range; and completing curing of the composite panel at a third temperature below the second temperature.Type: GrantFiled: January 5, 2022Date of Patent: September 26, 2023Assignee: B/E Aerospace, Inc.Inventors: George T. Franck, III, Alvin S. Bartolome, Patrick G. Jarvis-Shean
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Patent number: 11760487Abstract: A ceiling-mounted delivery assembly for a cabin of a vehicle includes a conveyance system that has a pair of guide rails, and a trolley operatively connected to the conveyance system for movement relative thereto. The trolley includes a control box having a pair of wheels. Each wheel is operatively connected to a respective one of the pair of guide rails. The control box includes a plurality of pulley drums extending from the control box. The trolley includes cable connection system having a plurality of cables. Each cable attached to a respective one of the pulley drums of the control box. The trolley includes a tray operatively connected to the cables of the cable connection system to be moved up and down relative to the control box.Type: GrantFiled: February 1, 2022Date of Patent: September 19, 2023Assignee: B/E Aerospace, Inc.Inventors: Biplav Bijoy Goswami, Girish Channakeshavrao Hirekerur
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Patent number: 11760619Abstract: An beverage mixing device is may comprise a controller in electronic communication with a sensor, the controller configured to: determine a drink type based on receiving sensor data from the sensor, and mix a pre-mixed composition with a carbonated water or a non-carbonated water based on the drink type.Type: GrantFiled: August 26, 2021Date of Patent: September 19, 2023Assignee: B/E AEROSPACE, INC.Inventors: Brian P. Mills, Bryan Rogers, Mudar Abu-Saymeh
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Patent number: 11753170Abstract: An aircraft seat may include a seat pan cushion coupled to a seat base. The aircraft seat may include a seat back cushion. The aircraft seat may include an auxiliary rear section. The auxiliary rear section may be configured to transition between an extended position and a retracted position. The seat pan cushion and the seat back cushion may be configured to transition between a first position and a second position. The auxiliary rear section may be configured to be in the extended position when the seat pan cushion and the seat back cushion are in the first position. The auxiliary rear section may be configured to be in the retracted position when the seat pan cushion and the seat back cushion are in the second position.Type: GrantFiled: March 29, 2021Date of Patent: September 12, 2023Assignee: B/E Aerospace, Inc.Inventors: Tracy Pence, Aaron D. LaPrade, Twinkle V. Jacob, Catalin Bunea, Horng Lin
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Publication number: 20230279963Abstract: A control system for a motorized valve. The control system comprises a backup circuit comprising energy storage means and a discharge gate through which the energy storage means can be selectively discharged to provide a discharge actuation pulse to the valve to cause the valve to move to a safe (e.g. closed) position. The backup circuit further includes an energy harvesting circuit for harvesting power from the power supply lines. The energy harvesting circuit is able to harvest sufficient energy within the duration for a single actuation pulse provided by the motor controller to charge the energy storage means from zero to a sufficient level to allow the backup circuit to generate at least one corresponding discharge actuation pulse for causing the valve to move to the safe position.Type: ApplicationFiled: February 24, 2023Publication date: September 7, 2023Applicant: B/E Aerospace, Inc.Inventors: Dariusz Celestyn Sapija, Filip Andrzej Sobolewski, Iwona Herbik
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Patent number: 11747024Abstract: An oven comprises an interior electronics cavity defined within electronics cavity walls. The oven includes an air inlet for receiving ambient air from an ambient space outside the electronics cavity into the interior electronics cavity and a first air outlet for returning steam laden air from a cooking space to the ambient space outside the cooking space. The oven also includes a second air outlet positioned to separate flow going into the air inlet from flow from the first air outlet. An air plenum can be defined outside of the cooking space, and the air inlet can be defined in a first portion of an exterior interface of the air plenum. The second air outlet can be defined in a second portion of the exterior interface.Type: GrantFiled: December 30, 2020Date of Patent: September 5, 2023Assignee: B/E Aerospace, Inc.Inventor: Manuel Perez Camacho
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Patent number: 11738216Abstract: In a preferred embodiment, methods and systems for the control of the breathing gas supply from a pressure-leading supply conduit to one or more breathing masks of an oxygen emergency supply device in a passenger aircraft include an on/off valve arranged between the supply conduit and the one or more breathing masks. The valve can be blocked or released to control air supply based upon monitoring mass flow to the breathing masks. The valve, for example, is actuated to an open position until the error between the actual mass flow and a desired mass flow exceeds a maximal error value, whereupon the valve is actuated to a closed position until the error between the actual mass flow and the desired mass flow exceeds a minimal error value whereupon the valve is actuated to the open position and the mass flow monitoring cycle is repeated.Type: GrantFiled: July 9, 2020Date of Patent: August 29, 2023Assignee: B/E Aerospace, Inc.Inventors: Heiko Marz, Thomas Sauerbaum
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Patent number: 11738870Abstract: An in-flight entertainment system is disclosed. In various embodiments, the in-flight entertainment system includes a display having a viewing surface and a back surface opposite the viewing surface; and a projector connected to the display and configured to illuminate the viewing surface.Type: GrantFiled: December 29, 2020Date of Patent: August 29, 2023Assignee: B/E AEROSPACE, INC.Inventors: Tippanna Shetgar, Rajesh Mohanam, Aravinda Mahabaleshwara, Sivakumar Dwaraganathan
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Patent number: 11731766Abstract: A device for securing passenger seat frame structures (e.g., seat spreaders, legs) to a lateral crossbeam includes a wedged clamping device insertable into a pocket directly adjacent to a passage allowing the crossbeam to pass through the seat frame structure. The wedged clamping device has an upper face providing a locking taper angle and a lower arcuate face opposite the upper face and in contact with the crossbeam. When inserted into the pocket, the wedged clamping device provides a clamping force securing the seat frame structure to the crossbeam without driving a bolt through, deforming, or otherwise compromising the integrity of the crossbeam. The wedged clamping device accepts a tuning bolt through a lateral face; tightening the tuning bolt can more precisely control the amount of clamping force provided on the crossbeam.Type: GrantFiled: March 29, 2022Date of Patent: August 22, 2023Assignee: B/E Aerospace, Inc.Inventors: Neil M. Ralph, Ryan J. Suhre, Stephen A. Puglisi, Eric M. McKee
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Patent number: 11732898Abstract: A device can include an enclosure defining an interior having an enclosure volume and configured to hold one or more items, a heat system configured to heat the interior of the enclosure, a fluid system configured to input a known amount of a fluid (e.g., water, steam, air) into the enclosure, and a pressure sensor configured to sense a pressure within the enclosure. The device can include an item volume deduction module operatively connected to the pressure sensor and the fluid system. The item volume deduction module can be configured to correlate a pressure increase caused by injection of a known amount of the fluid (e.g., water, steam, air) in the enclosure to a total item volume of the one or more items within the enclosure.Type: GrantFiled: December 21, 2020Date of Patent: August 22, 2023Assignee: B/E AEROSPACE, INC.Inventors: Arnau Castillo Gonzalez, Hans Huijsing
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Patent number: 11725744Abstract: A self closing tap (102) comprising a cartridge (12) and a tap handle interface is disclosed. The cartridge (12) comprises a piston (122), and a plunger (32). The piston (122) is comprised of a piston head (124), and a piston shaft (126), the piston shaft (126) has a longitudinal axis (A) and is fixed to the piston head (124) at a first end, and the second end of the piston shaft (126) is an engagement end (182). The plunger (32) is movably fixed to a first portion of the piston shaft (126) and adapted to move longitudinally along the first portion of the piston shaft (126).Type: GrantFiled: February 8, 2022Date of Patent: August 15, 2023Assignee: B/E Aerospace, Inc.Inventors: Piotr Kostanski, Modest Adam Reszewicz, Pawel Swirniak
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Patent number: 11717086Abstract: A rotary recline mechanism for allowing reclining movement of a first part relative to a second part, the mechanism comprising: a plurality of friction pads arranged to be compressed together, the plurality of friction pads comprising alternating first friction pads connected to the first part and second friction pads connected to the second part; biasing means to bias the friction pads into compressed frictional engagement; actuator means to which force is applied by a user; and a force transmission means that translates a first force applied by the user in a first direction to act against the force of the biasing means to release the frictional pads from the compressed frictional engagement to allow the first friction pads to rotate relative to the second friction pads.Type: GrantFiled: November 2, 2021Date of Patent: August 8, 2023Assignee: B/E Aerospace, Inc.Inventors: Adrian Tarnowski, Tomasz Wanski, Lukasz Turek, Tomasz Kupczyk
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Publication number: 20230246875Abstract: An electronic device may comprise: a token input circuit comprising a token input electrical line, a pull up resistor, and a power source; a token output circuit comprising a token output electrical line and an electrical switch; a communication input electrical line; a communication output electrical line; a processor in electrical communication with the token input electrical line, the token output electrical line, the communication input electrical line, and the communication output electrical line; and a tangible, non-transitory computer-readable storage medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations comprising: receive, via the processor, a token from an adjacent electronic device via the token input electrical line, and determine, based on the token, a location of the electronic device in a string of electronic devices.Type: ApplicationFiled: January 21, 2022Publication date: August 3, 2023Applicant: B/E AEROSPACE, INC.Inventor: ERIC JOHANNESSEN
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Patent number: 11713125Abstract: An adjustable armrest assembly provides for quick and easy height and tilt adjustments to the armrest. Generally, the armrest assembly disclosed herein includes a base, an armrest, and one or more shafts extending from the base and being pivotably coupled to the armrest. By moving the one or more shafts relative to the base, the height and/or tilt of the armrest relative to the base can be adjusted.Type: GrantFiled: March 28, 2022Date of Patent: August 1, 2023Assignee: B/E AEROSPACE, INC.Inventors: Sreekanth Koti Ananda Rao, Pavan Kumar Krishna Kumar, Pradeep Acharya
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Patent number: 11708163Abstract: A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.Type: GrantFiled: October 2, 2020Date of Patent: July 25, 2023Assignee: B/E Aerospace, Inc.Inventors: Glenn A. Johnson, Mark B. Dowty, Jefferey M. McKee, Tracy Pence, Michael M. Princip
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Patent number: 11708164Abstract: A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.Type: GrantFiled: April 20, 2021Date of Patent: July 25, 2023Assignee: B/E Aerospace, Inc.Inventor: Glenn A. Johnson
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Publication number: 20230228073Abstract: An automatic drain system may comprise a drain including a neck defining a drain orifice and a flange extending from the neck. A liquid detection sensor is located on at least one of the neck or the flange. A sink assembly may comprise a sink basin and the drain located in a sink opening formed in the sink basin.Type: ApplicationFiled: January 14, 2022Publication date: July 20, 2023Applicant: B/E AEROSPACE, INC.Inventors: Jon Shearer, Eric Kaufman, Alexander V. Drum
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Patent number: 11701527Abstract: A pulse modulated oxygen dispensing and pressurization system provides a variable range of controlled oxygen bolus to an enclosed breathing environment supporting and maintaining required pressure conditions in accordance with desired flow demand. As oxygen is consumed by the user from within the enclosed breathing environment, the exhaled gases and moisture are conditioned or vented to acceptable levels by additional systems associated with the environment. These additional systems cause an ongoing need to replenish the oxygen within the environment and maintain the required partial pressure of oxygen. Specific to one of a plurality of modes of operation, the system responds to changes in regulated output pressure by delivering a precisely metered periodic bolus volume of oxygen to support a requirement of the environment volume. The bolus is variable based on a plurality of factors to increase and decrease changes in rates of flow required to maintain regulated pressure.Type: GrantFiled: August 31, 2020Date of Patent: July 18, 2023Assignee: B/E Aerospace, Inc.Inventors: John T. Barker, Bryce Baker
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Patent number: 11702209Abstract: An aircraft passenger seat construction capable of in-flight rocking motion and berthing, wherein rocking motion and berthing are mutually exclusive features. The seat construction includes a fixed frame including spaced frame members each having a support surface to be rocked on, a rocking frame including a seat pan and spaced rockers, the spaced rockers positioned to rock on the support surfaces, guides carried on the spaced rockers engaged to travel within guide slots of the spaced frame members, a backrest pivotally attached to the rocking frame, and a leg rest pivotally attached to the rocking frame. The rocking frame may rock back-and-forth in-flight or may be locked at any given position based on passenger preference. The seat construction is compatible with or without other seat adjustment mechanisms such as tracking, swivel, lie-flat and recline adjustment mechanisms.Type: GrantFiled: June 25, 2019Date of Patent: July 18, 2023Assignee: B/E Aerospace, Inc.Inventors: Arjun Koustubhan, Arvind Mahabaleshwara, Rajesh Mohanam