Patent · US Active

Hybrid gas turbine engine starter-generator

US7327048B2 · kind B2 · utility

6Cited by
32References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 30, 2006
Grant dateFeb 5, 2008
Priority date
Expiry dateMay 30, 2026

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH02P2101/30
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A rotating electrical machine, such as an aircraft starter-generator, that may be operated in either a DC motor mode or an AC generator mode. The machine includes a conventionally wound main stator that is selectively configurable as a multi-pole AC stator and a multi-pole DC stator. The machine also includes rotor windings that are configured to be selectively coupled to either an exciter or a plurality of commutator segments, and DC brushes that are selectively moveable into, and out of, electrical contact with the commutator segments, to thereby electrically couple and decouple a DC power source to and from, respectively, the rotor windings.

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