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:
May. 06, 2025

Filed:

Apr. 21, 2022
Applicant:

Dr. Ing. H.c. F. Porsche Aktiengesellschaft, Stuttgart, DE;

Inventor:

Mikel Fauri, Ludwigsburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/26 (2005.12); B60L 3/00 (2018.12); B64C 29/00 (2005.12); B64D 27/24 (2005.12); B64D 37/02 (2005.12); B64D 41/00 (2005.12); H01M 8/04082 (2015.12); H01M 8/04089 (2015.12); H01M 8/04746 (2015.12); H01M 8/22 (2005.12);
U.S. Cl.
CPC ...
B64C 13/26 (2012.12); B60L 3/0053 (2012.12); B64C 29/0008 (2012.12); B64D 27/24 (2012.12); B64D 37/02 (2012.12); B64D 41/00 (2012.12); H01M 8/04089 (2012.12); H01M 8/04201 (2012.12); H01M 8/04753 (2012.12); H01M 8/22 (2012.12); B60L 2200/10 (2012.12); B64D 2041/005 (2012.12); H01M 2250/20 (2012.12);
Abstract

A drive system of an aircraft, including a fuel cell, which can be supplied with hydrogen from a hydrogen tank and with air from a blower, the fuel cell being configured to provide drive power for operational flight after takeoff and before landing dependent on a hydrogen mass flow supplied by the hydrogen tank and dependent on an air mass flow supplied by the blower, and an electrical energy store, which is configured to provide additional drive power for takeoff and landing, wherein an additional hydrogen tank and an air or oxygen tank are configured to interact with the fuel cell such that the fuel cell can be supplied with an additional hydrogen mass flow and with an additional air or oxygen mass flow, thereby compensating at least partially for a loss of the additional drive power provided by the electrical energy store for landing.


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