The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 05, 2023

Filed:

Aug. 12, 2022
Applicant:

Zeroavia, Inc., Hollister, CA (US);

Inventor:

Valery Miftakhov, San Carlos, CA (US);

Assignee:

ZeroAvia, Inc., Hollister, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H01M 8/04 (2016.01); H01M 8/04111 (2016.01); F02C 1/02 (2006.01); H01M 8/04082 (2016.01); F02C 6/18 (2006.01); F02C 7/36 (2006.01); B64D 33/02 (2006.01); B64D 31/00 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
H01M 8/04111 (2013.01); B64D 33/02 (2013.01); F02C 1/02 (2013.01); F02C 6/18 (2013.01); F02C 7/36 (2013.01); H01M 8/04201 (2013.01); B64D 31/00 (2013.01); B64D 2033/024 (2013.01); B64D 2033/0266 (2013.01); B64D 2041/005 (2013.01); F05D 2220/323 (2013.01); F05D 2220/60 (2013.01); F05D 2260/211 (2013.01); H01M 2250/20 (2013.01);
Abstract

An aircraft power plant for a fuel cell including a turbo assembly, a compressor assembly, a turbo assembly, a compressor assembly controller, a first stage turbo assembly and compressor assembly operation configured to generate a first stage compressed fluid generated from ambient air and excess oxygen exhausted from a fuel cell of an aircraft power plant. A second stage turbo assembly and compressor assembly operation configured to receive the first stage compressed fluid, and a controller bleed valve coupled with the first stage turbo assembly and compressor assembly and the second stage turbo assembly and compressor assembly. An oxygen supply system, the oxygen supply system fluidically coupled with the first stage turbo assembly and compressor assembly wherein a first compressed oxygen is generated by the first stage turbo assembly is combined with a second compressed oxygen generated by the second stage turbo assembly to generate a combined oxygen controlled by the controller bleed valve. A third stage turbo assembly and compressor assembly operation configured to receive the combined oxygen, and a hydrogen supply system configured to provide hydrogen fluidically coupled with the third stage turbo assembly and compressor assembly.


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