Hamilton Sundstrand Corporation

Matthew Ryan Hasseman

Dwight D Schmitt

Jeffrey D Myroth

Kamaraj Thangavelu

Vlatko Miskovic

Shawn J Young

Ryan Thomas Carter

A system comprises a generator control unit (GCU) configured to control a generator. The system includes a first sensor connected to provide feedback to the GCU for generator control. The first sensor is configured to connect to sense at least one of voltage and/or current in a feeder connecting between the generator and a load. The system also includes a second sensor connected to provide feedback to the GCU for generator control. The second sensor is configured to sense at least one of voltage and/or current in a feeder connecting between the generator and the load. The first and second sensors are configured to connect to the feeder apart from one another with feeder impedance therebetween.

Fast POR trim correction

In accordance with at least one aspect of this disclosure, a controller for an aircraft electrical system includes, a software safe module. In embodiments, the software safe module can be configured to determine whether there was a sudden power failure upon controller initialization, and cause operation of the controller in a software safe mode if there was a sudden power failure such that manual intervention is required to leave the software safe mode to prevent repetitive power failure of the controller.

Systems and methods for circuit failure protection

Growing community of inventors

Poplar Grove, IL, United States of America

Matthew Ryan Hasseman