Patent · US Active

Ignition device and gas turbine combustor

US10578024B2 · kind B2 · utility

0Cited by
4References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 1, 2017
Grant dateMar 3, 2020
Priority date
Expiry dateJul 16, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R3/28
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An ignition device of an embodiment is provided to a gas turbine combustor to which supercritical-pressure CO2 is introduced. The ignition device includes: a shutoff valve provided on an outer side face of a casing of the combustor to make the inside of the casing and the outside of the casing communicate with each other or shut off from each other; an ignition rod formed of a long rod including a spark discharge portion at a leading end, and capable of advancing to and retreating from the inside of a combustor liner provided in the casing from/to the outside of the casing through the shutoff valve; and a driving part which makes the ignition rod advance and retreat.

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