Patent · US Active

Aircraft grid phase angle tracker based on nonlinear active disturbance rejection

US11802895B2 · kind B2 · utility

0Cited by
2References
1Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 22, 2021
Grant dateOct 31, 2023
Priority date
Expiry dateAug 18, 2041

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01R31/008
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

The present invention belongs to the technical field of aviation electrics and electric power, and provides an aircraft grid phase angle tracker based on nonlinear active disturbance rejection, which is used to estimate the grid phase angle on AC side of an aircraft grid. A embedded generator in the aircraft grid is arranged inside a compressor of an aviation gas turbine engine, and the embedded generator is directly coupled with the aviation gas turbine engine so that the AC frequency of the embedded generator varies with the speed of the aviation gas turbine engine. The present invention applies the nonlinear active disturbance rejection technology to the phase angle tracking of the more electric aircraft grid, is simple in operation and high in accuracy, and can realize high-accuracy tracking of the grid phase angle. The method has certain extensibility and can be extended to other fields.

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