Zeroavia, Inc.

Numerical Technologies, Inc.

Ilya Henry Grishashvili

Valery Miftakhov

Vadim Belogorodsky

Shao-Po Wu

Seonghun Cho

Alexandre Arkhipov

In one or more embodiments of the novel aircraft fuel cell system without the use of a buffer battery, the fuel cell and compressor would be sized sufficiently larger for the intended application, allowing the compressor to change speeds much faster. This in turn would allow power outputs to change much quicker. If power outputs can change as quickly as the application dictates, then a buffer battery is not necessary. In one or more embodiments, because the system is mostly electronically controlled, software can be written to protect the fuel cell from instantaneous power spikes. If a large power output is suddenly requested of the fuel cell, the software can smooth out the demand curve to provide an easier load profile to follow.

Aircraft fuel cell system without the use of a buffer battery

A power generating system comprised of a hydrogen fuel cell and rechargeable battery connected together in series to be used as a load following system without the use of a DC-DC converter. The hydrogen fuel cell's cathode air compressor is driven off of the output of this power generation system. This is made possible by the following innovations: A novel way to wire the systems in series with the use of switches and bypass diodes, a method to limit the system output voltage so that we do not exceed the maximum voltage of downstream components, and an isolated DC-DC converter to charge the rechargeable battery with the hydrogen fuel cell.

Fuel cell—battery hybrid system for transportation use

An air compression system for a fuel cell system, the air compression system has a main air compressor with a maximum air flow output approximately equal to a continuous mode air flow requirement of the fuel cell system. The main air compressor weighs less than an air compressor having a maximum air flow output approximately equal to a peak air flow requirement of the fuel cell system such that the weight of the air compression system is reduced compared to a conventional air compression system. The air compression system also includes a supplemental oxygen supply system which is fluidically coupled with the fuel cell system.

On-board oxygen booster for peak power in fuel cell systems

One embodiment of the invention provides a system that automatically resolves conflicts between phase shifters during creation of a phase shifting mask to be used in an optical lithography process for manufacturing an integrated circuit. Upon receiving a specification of a layout on the integrated circuit, the system identifies critical-dimension features within the layout. Next, the system places phase shifters comprised of phase shifting geometries on the phase shifting mask to precisely define the critical-dimension features. In doing so, the system identifies junctions within and/or between the critical-dimension features, and removes phase shifting geometries associated with the junctions to obviate coloring conflicts between phase shifters on the phase shifting mask. In one embodiment of the invention, the junctions include T-junctions and/or L-junctions.

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San Jose, CA, United States of America

Ilya Henry Grishashvili