Patent · US Active

UAV hybrid power systems and methods

US10501195B2 · kind B2 · utility

7Cited by
5References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 31, 2017
Grant dateDec 10, 2019
Priority date
Expiry dateJan 13, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U10/14
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Systems, methods, and devices are provided herein for improving the power performance of vehicle. A hybrid power system may comprise a power controller adapted to be in communication with a first power source, a second power source, and a load. The power controller may be configured to detect whether a current drawn by the load exceeds a predetermined threshold, control discharging of the first power source without permitting discharging of the second power source to power the load when the current drawn by the load is less than the predetermined threshold current, and control discharging of the first power source and the second power source to power the load when the current drawn by the load is greater than the predetermined threshold current.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.