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:
Oct. 27, 2026

Filed:

Apr. 04, 2024
Applicant:

Hs Elektronik Systeme Gmbh, Nördlingen, DE;

Inventor:

Markus Greither, Augsburg, DE;

Assignee:

HS Elektronik Systeme GmbH, Nordlingen, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H03K 17/00 (2006.01); H02H 3/08 (2006.01); H03K 17/082 (2006.01); H03K 17/12 (2006.01); H03K 17/567 (2006.01);
U.S. Cl.
CPC ...
H03K 17/567 (2013.01); H02H 3/08 (2013.01); H03K 17/0822 (2013.01); H03K 17/122 (2013.01);
Abstract

An aircraft solid state power controller (SSPC) includes a first input terminal, first output terminal, and first electric power switching device switchable between (i) an on-state that electrically couples the first output terminal with the first input terminal and (ii) an off-state that electrically isolates the first output terminal from the first input terminal. The SSPC also includes a second input terminal, second output terminal, and second electric power switching device switchable between (i) an on-state that electrically couples the second output terminal with the second input terminal and (ii) an off-state that electrically isolates the second output terminal from the second input terminal. The SSPC further includes a switch controller configured to synchronously switch the electric power switching devices from their respective on-states into respective off-states. In addition, the SSPC includes an energy dumping circuit configured to dissipate inductive energy generated when the electric power switching devices are switched.


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Greither, Markus. (2026). Aircraft solid state power controller, aircraft power supply system, and method of switching an aircraft solid state power controller (U.S. Patent No. 12776771). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12776771

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