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:
Nov. 04, 2025

Filed:

Apr. 29, 2021
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Alexis Raquel Nunes, West Chester, OH (US);

Kurt David Murrow, Dayton, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64U 10/20 (2023.01); B64U 30/10 (2023.01); B64U 50/12 (2023.01); B64U 50/14 (2023.01); B64U 101/30 (2023.01); G05D 1/00 (2024.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64U 10/20 (2023.01); B64U 30/10 (2023.01); B64U 50/12 (2023.01); B64U 50/14 (2023.01); G05D 1/102 (2013.01); B64U 2101/30 (2023.01);
Abstract

An aircraft equipped with a multi-fan propulsion system for controlling flight orientation transitions is provided. In one example aspect, an aircraft includes a fuselage and a pair of wings. The aircraft includes a propulsion system having a first propulsor and a second propulsor each mounted to the fuselage. The first propulsor has a fan positioned primarily above and the second propulsor has a fan positioned primarily below the pair of wings. The aircraft also includes a computing system having one or more processors configured to cause, in response to a demand to change an orientation of the aircraft for a flight orientation transition, the fans of the first and second propulsors to produce different amounts of thrust with respect to one another so that the aircraft performs the flight orientation transition. The thrust differential causes the aircraft to transition between orientations.


Find Patent Forward Citations

Loading…