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:
Jan. 31, 2023

Filed:

Jul. 29, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Zubair Ahmed Baig, Glastonbury, CT (US);

Neil Terwilliger, Meriden, CT (US);

Sorin Bengea, Glastonbury, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/02 (2006.01); H02J 7/14 (2006.01); B60L 15/20 (2006.01); B60L 50/61 (2019.01); H02J 7/34 (2006.01);
U.S. Cl.
CPC ...
B64D 27/02 (2013.01); B60L 15/20 (2013.01); B60L 50/61 (2019.02); H02J 7/1423 (2013.01); B60L 2200/10 (2013.01); B60L 2260/50 (2013.01); B64D 2027/026 (2013.01); H02J 7/143 (2020.01); H02J 7/345 (2013.01);
Abstract

A power system of an aircraft includes a hybrid energy storage system with at least two energy storage subsystems each having a different power-energy density. The power system also includes one or more electric motors operably coupled to the hybrid energy storage system and to an aircraft engine. The power system further includes a means for controlling one or more electric power flows of the hybrid energy storage system to/from the one or more electric motors based on a modeled electric power demand associated with an engine load of one or more spools of the aircraft engine.


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