Alakai Technologies Corporation

Raytheon Company

Other

Parker-hannifin Corporation

Cbl Acquisition LLC

Cbi Systems Corporation

Brian D Morrison

Peter F Falt

Andre H De Salis

Adil M Ali

Martti J Lampela

Michael N Robillard

Fazzio Youn

Martin R Batten

Creig E Wienke

Paul A Connolly

Ronald E Wilkinson

Jack J Rosenberg

David R Blake

Stephan A Hanvey

Randolph W Holtgrefe

William Spellane

An integrated multifunction dynamic display system and method for an air vehicle that provides an interactive user experience. The system is based around an array of multifunction display nodes that are disposed throughout the air vehicle. The multifunction display nodes are connected through a databus or network such that the display nodes can operate individually or in combination to create a desired interactive experience. The nodes can include interior lighting, exterior lighting, interior displays, exterior displays, and windows. The multifunction dynamic display system can be used to control or otherwise provide interior lighting or displays, loading/unloading instruction, inflight entertainment or information, emergency notification and instruction, augmented reality, external lighting and displays. In addition, the multifunction dynamic display can be configured for each passenger.

Multifunction dynamic visual display for interactive user experience

A lightweight, high power density, fault-tolerant fuel cell system, method, and apparatus for full-scale clean fuel electric-powered aircraft having a fuel cell module including a plurality of fuel cells working together to process gaseous oxygen from air compressed by turbochargers, superchargers, blowers or local oxygen supply and gaseous hydrogen from liquid hydrogen transformed by heat exchangers, with an electrical circuit configured to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to motor controllers commanded by autopilot control units configured to select and control an amount and distribution of electrical voltage and torque or current for each of the plurality of motor and propeller assemblies, wherein electrons returning from the electrical circuit combine with oxygen in the compressed air to form oxygen ions, then the protons combine with oxygen ions to form HO molecules and heat.

Lightweight high power density fault-tolerant fuel cell system and apparatus for clean fuel electric aircraft

An improved efficiency cooling plate apparatus for full-scale clean fuel electric-powered aircraft having a cooling body including a plurality of bores, apertures and interior chambers working together to process and circulate fluid coolant and function as a heat sink device, interconnecting with the cooling system of an electric motor and cooperatively functioning to transfer thermal energy away from the electric motor using conduction, convection and radiation, while transporting heated fluid coolant away from heated motor components and to other components of a vehicle for further processing, then returning cooled fluid coolant into the cooling system of an electric motor, effectively partitioning heated fluid coolant, cooled fluid coolant, and electrical circuitry in a space saving design formed from a single part or minimal number of parts to reduce modes of failure and reduce required fasteners or connections to improve robustness and reliability while maintaining suitable aerodynamic characteristics.

Cooling plate system, method and apparatus for clean fuel electric vehicles

Method of operating a lightweight high power density fault-tolerant fuel cell system for clean fuel electric aircraft

A fuel cell oxygen delivery system, method, and apparatus for full-scale clean fuel electric-powered vehicle having a fuel cell module including a plurality of fuel cells working together that augments gaseous oxygen from ambient air and gaseous hydrogen extracted from liquid hydrogen by pressure change or heat exchangers, with fuel cells containing electrical circuits configured to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to motor controllers commanded by control units configured to control an amount and distribution of electrical voltage and torque or current for each of one or more motor and propeller or rotor assembly, wherein electrons returning from the electrical circuits combine with both oxygen derived from air and onboard oxygen from the delivery system to form oxygen ions, then protons combine with oxygen ions to form HO molecules and heat.

Fuel cell oxygen delivery system, method and apparatus for clean fuel electric aircraft

Hybrid wire-fiber data networks that include wire-fiber transceivers protected against environmental interferences. In some embodiments, a hybrid-wire-fiber data network of this disclosure provides a fiber-optic link between portions of one or more wired networks. In some embodiments, a hybrid wire-fiber data network of this disclosure includes a fiber-optic link that relies only on message-priority arbitration performed on wired portions of one or more wired networks. In some embodiments, a wire-fiber transceiver of this disclosure includes electromagnetic environment (EME) protective circuitry for one or both of input power and input signals. In some embodiments, a wire-fiber transceiver of this disclosure is configured for use with a controlled area network media-access protocol (CAN) and/or a derivative of CAN. Various data communication and other methods are also disclosed in addition to hybrid wire-fiber data networks and components thereof.

Hybrid wire-fiber data networks for electromagnetic and/or ground-noise environments, components thereof, and systems incorporating same

An integrated multimode thermal energy transfer system, method and apparatus for full-scale clean fuel electric-powered multirotor aircraft with automatic on-board-capability to provide sensor-based temperature awareness and adjustment to critical components and zones of the aircraft. Automatic computer monitoring, including by a programmed triple-redundant digital autopilot computer, controls each motor-controller and motor to produce pitch, bank, yaw and elevation, while simultaneously measuring, calculating, and adjusting temperature and heat transfer of aircraft components and zones, to protect critical components from exceeding operating parameters and to provide a safe, comfortable environment for occupants during flight. By using the results of the measurements to inform computer monitoring, the methods and systems can use byproducts including thermal energy disparities and differentials related to both fuel supply systems and power generating systems to both add and remove heat from different aircraft zones to improve aircraft function, comfort, and efficiency.

Integrated multimode thermal energy transfer system, method and apparatus for clean fuel electric multirotor aircraft

Aircraft windshield

Aircraft airframe

Aircraft seating configuration

Lightweight high power density fault-tolerant fuel cell system, method and apparatus for clean fuel electric aircraft

Methods and systems for a clean fuel, manned or unmanned aircraft, having an electric, low-emission or zero-emission lift and propulsion system, an integrated 'highway in the sky' avionics system for navigation and guidance, a tablet-based motion command, or mission planning system to provide the operator with drive-by-wire style direction control, and automatic on-board-capability to provide traffic awareness, weather display and collision avoidance. Automatic computer monitoring by a programmed multiple-redundant autopilot control units control each motor-controller and motor to produce pitch, bank, yaw and elevation, while simultaneously restricting the flight regime that the pilot can command, to protect the pilot from inadvertent potentially harmful acts that might lead to loss of control or loss of vehicle stability. By using the results of the state measurements to inform motor control commands, the methods and systems contribute to the operational simplicity, reliability and safety of the vehicle.

Clean fuel electric aircraft for personal air transportation and manned or unmanned operation

Set of aircraft canards

Aircraft avionics console

Aircraft moon roof

Growing community of inventors

Hopkinton, MA, United States of America

Brian D Morrison