US 12,358,632 B2
Aircraft electrical system
Jonathan Mark Roadley-Battin, Birmingham (GB)
Assigned to HAMILTON SUNDSTRAND CORPORATION, Charlotte, NC (US)
Filed by Hamilton Sundstrand Corporation, Charlotte, NC (US)
Filed on Sep. 8, 2023, as Appl. No. 18/463,808.
Claims priority of application No. 22194702 (EP), filed on Sep. 8, 2022.
Prior Publication US 2024/0083589 A1, Mar. 14, 2024
Int. Cl. B64D 27/24 (2024.01); B60L 50/00 (2019.01); B64D 27/02 (2006.01); B64D 31/00 (2024.01); H02J 1/00 (2006.01)
CPC B64D 27/24 (2013.01) [B60L 50/00 (2019.02); B64D 31/00 (2013.01); H02J 1/00 (2013.01); B60L 2200/10 (2013.01); B60L 2210/30 (2013.01); B64D 27/026 (2024.01); B64D 2221/00 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A voltage converter for an aircraft electrical system, comprising:
an input power line configured to receive input electrical power;
an output power line configured to supply output electrical power to aircraft loads;
conversion circuitry; and
a controller;
wherein the conversion circuitry is configured to convert the input electrical power to supply the output electrical power based on one or more control parameters;
wherein the controller is configured to receive data relating to the aircraft loads and modify at least one control parameter based on the data;
wherein the controller is configured to receive the data relating to the aircraft loads from a central computer of the aircraft electrical system.