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Aircraft Energy Storage System Override Patent Granted

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Published March 24th, 2026
Detected March 25th, 2026
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Summary

The USPTO has granted a patent (US12583602B2) to Rolls-Royce Corporation for an aircraft energy storage system override. This system allows for controlled power reduction from the energy storage system to the aircraft engine supply bus, with configurable parameters for normal operation and a relaxed override state.

What changed

The United States Patent and Trademark Office (USPTO) has granted patent US12583602B2 to Rolls-Royce Corporation for an "Aircraft override for an energy storage system." The patent describes a power reduction system for aircraft energy storage systems. This system features a controller and an override switch. In its non-override state, the controller manages power reduction based on default parameters. When switched to the override state, the system operates under a relaxed configuration, potentially omitting or easing these parameters.

This patent grant is a notification of intellectual property protection for a specific technological innovation. It does not impose new regulatory obligations on the aviation industry. However, it signifies a development in aircraft power management systems that manufacturers and engineers in the sector should be aware of for competitive and technological landscape awareness. No immediate compliance actions are required based solely on this patent grant.

Source document (simplified)

← USPTO Patent Grants

Aircraft override for an energy storage system

Grant US12583602B2 Kind: B2 Mar 24, 2026

Assignee

Rolls-Royce Corporation

Inventors

Stephen Andrew Long, Michael Dougherty, Tomasz Marek Lubecki, Firman Sasongko, Chandana Gajanayake, Michael Adam Zagrodnik

Abstract

A power reduction system for an energy storage system of an aircraft includes a controller configured to control power reduction of power supplied from the energy storage system to an aircraft engine supply bus; and an override switch configurable in an override state and a non-override state. The override switch is configured to: in the non-override state, permit the controller to control the power reduction according to a default configuration comprising one or more parameters that trigger the power reduction; and in the override state, control the power reduction to be performed according to a relaxed configuration that at least one of relaxes and omits the one or more parameters in the default configuration.

CPC Classifications

B64D 31/00 B64D 27/24 B64D 27/026 B64D 2221/00 B60L 58/10 B60L 2200/10 H02J 3/322 H02J 7/0063 H02J 2310/44

Filing Date

2023-09-06

Application No.

18462210

Claims

15

View original document →

Named provisions

Aircraft override for an energy storage system

Source

Analysis generated by AI. Source diff and links are from the original.

Classification

Agency
USPTO
Published
March 24th, 2026
Instrument
Notice
Legal weight
Non-binding
Stage
Final
Change scope
Minor
Document ID
US12583602B2

Who this affects

Applies to
Manufacturers
Industry sector
3364 Aerospace & Defense
Activity scope
Aircraft Systems Engineering Power Management
Geographic scope
United States US

Taxonomy

Primary area
Aviation
Operational domain
Engineering
Topics
Energy Storage Aircraft Systems

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