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:
May. 12, 2026

Filed:

Oct. 17, 2023
Applicant:

Hs Elektronik Systeme Gmbh, Noerdlingen, DE;

Inventors:

Thomas Gietzold, Unterwilflingen, DE;

Gerd Kluger, Ederheim, DE;

Peter Brantl, Fremdingen, DE;

Stefan Schreitmueller, Auhausen, DE;

Assignee:

HS Elektronik Systeme GmbH, Nordlingen, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02H 3/28 (2006.01); H02J 1/00 (2006.01); H02J 105/30 (2026.01);
U.S. Cl.
CPC ...
H02H 3/28 (2013.01); H02J 1/00 (2013.01); H02J 2310/44 (2020.01);
Abstract

An aircraft solid state power controller comprises a feed node to be electrically connected to a primary electric power supply; a load node to be electrically connected to at least one electric load; and at least one electric switching device, in particular a solid state switching device, which is arranged between the feed node and the load node. The at least one electric switching device is switchable between an on-state, in which the at least one electric switching device provides a low-resistive electric connection between the feed node and the load node; and an off-state, in which the at least one electric switching device electrically isolates the load node from the feed node. The aircraft solid state power controller further comprises a secondary electric power supply, which is independent from the primary electric power supply, and which is configured for applying a test voltage between the feed node and the load node of the aircraft solid state power controller in order to allow determining the switching state of the at least one electric switching device by detecting a voltage drop between the feed node and the load node of the aircraft solid state power controller.


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