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:
Apr. 21, 2025

Filed:

Jul. 13, 2023
Applicant:

Bae Systems Controls Inc., Endicott, NY (US);

Inventors:

Matthew S. Boecke, Endicott, NY (US);

Arthur P. Lyons, Maine, NY (US);

Assignee:

BAE Systems Controls Inc., Endicott, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2023.12); B64D 31/06 (2023.12); B64D 27/02 (2005.12);
U.S. Cl.
CPC ...
B64D 27/24 (2012.12); B64D 31/06 (2012.12); B64D 27/026 (2023.12);
Abstract

An energy management system (EMS) for an aircraft is provided. The aircraft may have one of a plurality of propulsion systems such as a parallel hybrid electric propulsion system, a parallel turbo electric propulsion system, an electric propulsion system, a turbo electric propulsion system and a turbo hybrid electric propulsion system. The EMS comprises redundant control paths for controlling safety critical operation. Each redundant control path is configured to independently determine whether to electrically isolate a line replaceable unit (LRU) from a high voltage DC link (HVDC link) based on status information from the LRU. The isolation is based on the independent determination. The HVDC link is used for propulsion. The number of the redundant control paths and components may be depending on the type of the propulsion system.


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