Patent · US Active

Turboshaft load control using feedforward and feedback control

US11920521B2 · kind B2 · utility

0Cited by
72References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 7, 2022
Grant dateMar 5, 2024
Priority date
Expiry dateFeb 7, 2042

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/309
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

Control schemes for controlling a gas turbine engine in response to disturbances associated with a load mechanically coupled with the gas turbine engine are provided. In one aspect, a gas turbine engine mechanically coupled with a load has a controller that includes executable control logic. The control logic includes a feedforward module, an aggressive control module, and a power turbine governor module. By executing the modules, the controller seeks to maintain a constant power turbine speed stably and subtly in response to small disturbances associated with the load and aggressively in response to large disturbances associated with the load, as well as smooth transitions between the responses.

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