Stromversorgung für Flugzeugsysteme
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3849068
- Aktenzeichen
- EP20215998
- Anmeldetag
- 21. Dezember 2020
- Veröffentlichung
- 10. Juli 2024
- Erteilung
- 10. Juli 2024
- Rechtsraum
- EP
- IPC
- H02M1/00H02M3/156
Abstract
Disclosed is a direct current power supply. The direct current power supply includes a voltage output (150) defining a voltage rail (154) and a ground (152). The direct current power supply includes a holdup capacitor (106) operable to conduct with the voltage output. The direct current power supply includes a redundant power supply (108) connected in series with the holdup capacitor (106) between the voltage rail (154) and the ground (152) of the voltage output (150) to provide the voltage output. The direct current power supply includes a first switch (112) disposed between the holdup capacitor (106) and the redundant power supply (108) operable to create a conductive path between the holdup capacitor (106) and the redundant power supply (108).
Anmelder
- Firma
- Hamilton Sundstrand Corporation
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.
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