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:
Feb. 27, 2024

Filed:

Feb. 19, 2019
Applicant:

Delorean Aerospace, Llc, Bloomfield Hills, MI (US);

Inventor:

Paul J. DeLorean, Bloomfield Hills, MI (US);

Assignee:

DELOREAN AEROSPACE, LLC, Bloomfield Hills, MI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64D 27/24 (2006.01); B64C 39/12 (2006.01); B64C 39/10 (2006.01); B64C 39/04 (2006.01); B64C 27/32 (2006.01); B64U 10/25 (2023.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 27/32 (2013.01); B64C 39/04 (2013.01); B64C 39/10 (2013.01); B64C 39/12 (2013.01); B64D 27/24 (2013.01); B64U 10/25 (2023.01); Y02T 50/10 (2013.01); Y02T 50/60 (2013.01);
Abstract

The disclosure generally pertains to a vertical take-off and landing (VTOL) aircraft comprising a fuselage and at least one fixed wing. The aircraft may include at least two powered rotors located generally along a longitudinal axis of the fuselage. The rotor units may be coupled to the fuselage via a rotating chassis, which allows the rotors to provide directed thrust by movement of the rotor units about at least one axis. The VTOL aircraft may include instructions to perform a degraded rotor landing protocol. The degraded rotor landing protocol may include adjusting a power to an operable rotor unit to control a rate of descent and/or slow a rate of acceleration toward a landing surface. The VTOL aircraft may be configured to impact the landing surface from a substantially vertical configuration, and adjust a thrust vector to cause the aircraft to come to rest in a generally upright configuration.


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