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Bret L.

Bret L. Lamoree, Woodinville, WA US

Patent application numberDescriptionPublished
20080239451Control System for Dimmable Windows - Electrically dimmable windows for aircraft are powered by energy harvesting devices on-board the aircraft. The harvested energy is stored and used to control the opacity of the windows based on individual window opacity settings selected either by passengers or a cabin attendant. Each window has an associated control circuit that controls the electrical power applied to the window based on the selected opacity setting. The control circuit includes a low energy usage processor that remains in a sleep mode until a change in the opacity setting is detected. Each control circuit may include a radio transceiver that receives control signals from a transmitter operated by the cabin attendant in order to simultaneously remotely control the opacity settings of multiple windows.10-02-2008
20100187080SYSTEM AND METHOD FOR AN ELECTRONIC INTERACTIVE SWITCH - An interactive switch system for a stowage compartment system for a mobile platform (for example, commercial aircraft) is provided. The switch system is mounted to a moveable structure, such as an overhead stowage bin, and is responsive to a local input from a user, as well as to a remote input from an external control/monitoring panel. The switch system has at least one indicator surface responsive to the local input and the remote input to display indicator data. The indicator surface has a portion that forms at least one user input device for enabling the local input. The switch system further comprises a control system disposed behind the indicator surface. The control system is responsive to the local input and the remote input to transmit the indicator data to the indicator surface.07-29-2010

Bret L. Lamoree, Snohomish, WA US

Patent application numberDescriptionPublished
20090242695SECURING EMERGENCY AND SAFETY EQUIPMENT ON AIRCRAFT - An emergency equipment system comprising an elongate member, an emergency equipment package, and a cutter. The elongate member may have a first end and an angled end. The emergency equipment package may have a sleeve on one side capable of receiving the elongate member from the angled end. The cutter may be attached to a side of the elongate member and may be capable of cutting the sleeve.10-01-2009
20090242699KNOWLEDGE BASED ACCESS AND ACCESS HIERARCHY IN AN AIRCRAFT - A method and apparatus for a hierarchical access system for a compartment. The hierarchical access system comprises a moveable barrier, a locking mechanism, and a control unit. The moveable barrier is capable of preventing access to at least one of a first space and a second space in the compartment in the lavatory when the moveable barrier is in a closed position. The locking mechanism is capable of securing the moveable barrier in the closed position. The control unit is capable of unlocking the locking mechanism in a manner that provides different levels of access to the first space and the second space in the compartment in response to receiving an access request.10-01-2009
20090243842METHODS AND SYSTEMS FOR SENSING ACTIVITY USING ENERGY HARVESTING DEVICES - A system for monitoring activities relating to movable and removable items within a vehicle is described. The system includes an electrical energy storage device, an energy harvesting device operable to store harvested energy in the electrical energy storage device, a sensor element configured to output signals corresponding to one or more of removal, installation, and a shift in position of a corresponding item within the vehicle, and a transmitter configured to receive the signals from the sensor element. The transmitter is also configured to transmit unique identification information and data corresponding to the signals received from the sensor element, where the unique identification information corresponds with a location of the item on the vehicle. The sensor element and the transmitter are configured to use energy from one or both of the energy harvesting device and the electrical energy storage device.10-01-2009
20090243868SEAT CUSHION RETENTION AND MONITORING IN AN AIRCRAFT - An aircraft seating system comprises a seat frame having a top side, a seat cushion having a bottom side, a plurality of conductive first sides of a hook-and-loop fastener system attached to the bottom side of the seat cushion in a first pattern, a plurality of conductive second sides of the hook-and-loop fastener system attached to the top side of the seat frame in a second pattern, and a sensor connector connected to the second pattern. The plurality of conductive first sides and the plurality of conductive second sides engage each other and create a closed circuit for the sensor connector when the bottom side of the seat cushion is placed on the top side of the seat frame.10-01-2009
20090243891INDICATING SYSTEM FOR SECURITY OF SPACES IN AN AIRCRAFT - A method and apparatus for managing security of areas in an aircraft. The method is provided for managing aircraft security. A set of sensors associated with a set of secured areas is monitored for an indication of a compromised space within a cabin of the aircraft. In response to receiving a signal from a sensor in the set of sensors identifying a breach, an area for the breach in the cabin is identified to form an identified area. A visual indication device associated with the identified area is identified to form an identified visual indication device. A presentation of an alert on the identified visual indication device is initiated.10-01-2009

Patent applications by Bret L. Lamoree, Snohomish, WA US

Bret L. Teusink, Dubuque, IA US

Patent application numberDescriptionPublished
20100232869BALL-AND-SOCKET JOINT FOR WORK VEHICLE - A ball-and-socket joint (09-16-2010