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公开(公告)号：US12012210B2
公开(公告)日：2024-06-18
申请号：US17512148
申请日：2021-10-27
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison , Peter F. Falt
CPC classification number: B64D11/00 , G05D1/0669 , H04L12/40 , H04L2012/40215 , H04L2012/4028
Abstract: 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.
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2.发明公开公开(公告)号：US20230278715A1
公开(公告)日：2023-09-07
申请号：US18197398
申请日：2023-05-15
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
IPC: B64D27/24 , H01M8/04082 , H02K9/19 , H01M10/613 , B64D33/08 , H02K5/20 , H01M8/04029 , B64D45/00 , B64D13/06 , B64C29/00
CPC classification number: B64D27/24 , H01M8/04201 , H02K9/19 , H01M10/613 , B64D33/08 , H02K5/203 , H01M8/04029 , B64D2045/0085 , B64D2013/0607 , B64C29/0025 , B64D2013/0611
Abstract: 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 battery systems and power generating systems to both add and remove heat from different aircraft zones to improve aircraft function, comfort, and efficiency.
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公开(公告)号：US20220289379A1
公开(公告)日：2022-09-15
申请号：US17690652
申请日：2022-03-09
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
IPC: B64C39/02 , B64D27/24 , B64C29/00 , B60L50/70 , B60L58/30 , B60L55/00 , H04L12/40 , H01M8/04082 , H01M8/04858 , H01M8/0432
Abstract: A mobile emergency power generation and vehicle propulsion power system, method, and apparatus for full-scale, clean fuel, electric-powered vehicles having a fuel cell module including a plurality of fuel cells working together to process oxidizers including gaseous oxygen from the atmosphere or local oxygen supply and fuels including gaseous hydrogen or gaseous hydrogen from liquid hydrogen, to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to and control an amount and distribution of electrical voltage and torque or current for use with power inverters and power outlets for exterior use, and for propulsion systems of the vehicle itself.
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公开(公告)号：US20210104935A1
公开(公告)日：2021-04-08
申请号：US17063578
申请日：2020-10-05
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
Abstract: 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.
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公开(公告)号：US11923748B2
公开(公告)日：2024-03-05
申请号：US17063578
申请日：2020-10-05
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
Abstract: 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.
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Patent Agency Ranking
公开(公告)号：US11649059B2
公开(公告)日：2023-05-16
申请号：US16880732
申请日：2020-05-21
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
IPC: H02K5/20 , H02K9/19 , B64D27/24 , B64D33/08 , H01M10/613 , H01M8/04029 , H01M8/04082 , B64D13/06 , B64D45/00 , B64C29/00
CPC classification number: B64D27/24 , B64D33/08 , H01M8/04029 , H01M8/04201 , H01M10/613 , H02K5/203 , H02K9/19 , B64C29/0025 , B64D2013/0607 , B64D2013/0611 , B64D2045/0085
Abstract: 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.
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公开(公告)号：USD984335S1
公开(公告)日：2023-04-25
申请号：US29692504
申请日：2019-05-24
Applicant: Alakai Technologies Corporation
Designer： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt
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公开(公告)号：US11560234B2
公开(公告)日：2023-01-24
申请号：US16906739
申请日：2020-06-19
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
IPC: H01M8/00 , B64D27/24 , H01M8/04029 , H01M8/04007 , H01M8/2457 , B60L58/32 , H01M8/04858
Abstract: 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 H2O molecules and heat.
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公开(公告)号：USD912601S1
公开(公告)日：2021-03-09
申请号：US29692489
申请日：2019-05-24
Applicant: Alakai Technologies Corporation
Designer： Brian D. Morrison , Andre H. De Salis , Martti J. Lampela , Adil M. Ali , Peter F. Falt
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10.发明申请公开(公告)号：US20180001994A1
公开(公告)日：2018-01-04
申请号：US15686625
申请日：2017-08-25
Applicant: Alakai Technologies Corporation
Inventor： Brian D. Morrison
CPC classification number: B64C13/18 , B64C27/08 , B64D27/24 , B64D2027/026 , B64D2041/005 , G01C23/00 , G05D1/0077 , Y02T50/44 , Y02T50/54 , Y02T50/64 , Y02T90/36
Abstract: Methods and systems for a full-scale vertical takeoff and landing manned or unmanned aircraft, having an all-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 triple-redundant digital autopilot computer controls 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.
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