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. 28, 2024

Filed:

Feb. 14, 2022
Applicant:

Piasecki Aircraft Corporation, Essington, PA (US);

Inventor:

Frederick W. Piasecki, Haverford, PA (US);

Assignee:

Piasecki Aircraft Corporation, Essington, PA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 37/04 (2006.01); B64C 1/06 (2006.01); B64C 27/04 (2006.01); B64D 27/24 (2006.01); B64D 37/30 (2006.01); B64D 41/00 (2006.01);
U.S. Cl.
CPC ...
B64D 37/04 (2013.01); B64C 1/0685 (2020.01); B64C 27/04 (2013.01); B64D 27/24 (2013.01); B64D 37/30 (2013.01); B64D 2041/005 (2013.01);
Abstract

A fixed-wing or rotary-wing aircraft has a tail boom that contains a fuel tank. The fuel tank is configured to contain pressurized hydrogen. The pressurized hydrogen fuels a fuel cell stack to generate electricity to rotate one or more rotors or propellers. The fuel tank may define the structure of the tail boom and may support the empennage, tail rotor, propeller, convertible thruster, ducted fan or vectored thruster and associated drive systems with respect to the fuselage. The aircraft has adequate control authority for sustained coordinated flight when the fuel tank is filled with pressurized hydrogen and when the fuel tank is drained of pressurized hydrogen. The same aircraft may not have adequate control authority for coordinated flight if fuel tank was filled with a conventional liquid fuel.


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