System and method for providing compressed air to a gas turbine combustor
Номер патента: EP3874129A1
Опубликовано: 08-09-2021
Автор(ы): Daniel L. Folkers, Vincent C. Martling, Zhenhua Xiao
Принадлежит: Chromalloy Gas Turbine Corp
Опубликовано: 08-09-2021
Автор(ы): Daniel L. Folkers, Vincent C. Martling, Zhenhua Xiao
Принадлежит: Chromalloy Gas Turbine Corp
Реферат: A system for directing cooling air into a gas turbine combustor is provided. The system comprises a transition duct coupled to a flow sleeve, where air to be used for combustor cooling and in the combustion process enters a bellmouth of the transition duct, passes through a plurality of struts within the bellmouth, and is distributed to a passage located between the combustion liner and flow sleeve.
System and method for performing an in situ repair of an internal component of a gas turbine engine
Номер патента: SG11201810589RA. Автор: Herbert Chidsey Roberts,Nicholas Edward Antolino. Владелец: Gen Electric. Дата публикации: 2018-12-28.