Patent · US Active

Controlling soot

US12241629B2 · kind B2 · utility

0Cited by
20References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 26, 2022
Grant dateMar 4, 2025
Priority date
Expiry dateOct 2, 2042

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R2900/03041
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine comprising a variable geometry combustor having fuel injectors, a rich-burn zone, a quick-quench zone, and a lean-burn zone, and further comprising quench ports for admitting quench air to the quick-quench zone; a variable geometry airflow arrangement for the variable geometry combustor, which is configured to vary an airflow through the fuel injectors and/or the quench ports; and a control system configured to control the variable geometry airflow arrangement in dependence upon an airflow delivered to the combustor, a fuel flow to the fuel injectors, and a target index of soot emissions to control the quantity of soot produced by combustion.

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