Patent ID: 11909079
Assignee: ALAKAI TECHNOLOGIES CORPORATION
Field: Electrical machinery, apparatus, energy (Electrical engineering)
Classification: CPC H  B  Y | IPC B  H

Claim 10:
11. The oxygen delivery system of claim 1, wherein the system augments a fuel cell system for a clean fuel aircraft, the system comprising:
a power generation subsystem comprising one or more fuel cell modules comprising:
a plurality of hydrogen fuel cells configured to supply electrical voltage and current to one or more motor and propeller or rotor assembly controlled by one or more motor controller;
a fuel supply subsystem comprising a fuel tank in fluid communication with the one fuel or more cell modules and configured to store and transport a fuel;
a thermal energy interface subsystem comprising a heat exchanger in fluid communication with the fuel tank, the oxygen delivery storage comprising an onboard oxidizer, and the one or more fuel cell modules including each hydrogen fuel cell of the one or more fuel cells, a plurality of fluid conduits, and at least one radiator in fluid communication with the one or more fuel cell modules, configured to store and transport a coolant;
an external interface subsystem comprising intake components comprising one or more of turbochargers, superchargers, blowers, compressors, or combinations thereof, configured to compress ambient air and in fluid communication with at least one air intake, the oxygen delivery system and the one or more fuel cell modules; and
a power distribution monitoring and control subsystem for monitoring and controlling distribution of supplied electrical voltage and current to the one or more motor controller and an avionics subsystem, comprising:
one or more sensing devices configured to measure operating conditions; and
an electrical circuit configured to collect electrons from each hydrogen fuel cell of the plurality of hydrogen fuel cells and supply voltage and current to the one or more motor controller and aircraft components, wherein electrons returning from the electrical circuit combine with oxygen in the compressed air to form oxygen ions, then protons combine with oxygen ions to form H2O molecules, wherein the one or more motor controller is commanded by one or more autopilot control unit or computer unit comprising a computer processor configured to compute algorithms based on measured operating conditions, and configured to select and control an amount and distribution of electrical voltage and torque or current for each of the one or more motor and propeller or rotor assembly.