System and method for providing highly reactive fuels to a combustor
Номер патента: EP3325786A1
Опубликовано: 30-05-2018
Автор(ы): Douglas Frank Beadie, Ilya Alexandrovich Slobodyanskiy, Jeffrey Scott Goldmeer
Принадлежит: General Electric Co
Опубликовано: 30-05-2018
Автор(ы): Douglas Frank Beadie, Ilya Alexandrovich Slobodyanskiy, Jeffrey Scott Goldmeer
Принадлежит: General Electric Co
Реферат: A system and related method for providing a highly reactive fuel to a combustor of a gas turbine are disclosed herein. The system includes a fuel supply system that is in fluid communication with a fuel supply. The fuel supply system includes multiple fuel circuits. Each fuel circuit individually feeds fuel to a corresponding fuel distribution manifold. The system further includes a steam injection system. The steam injection system includes at least one flow control valve that is in fluid communication with at least one of the fuel circuits. The flow control valve provides for fluid communication between a superheated steam source and the fuel circuit during both fueled operation and during non-fueled operation of the corresponding fuel circuit.
Fuel supply system and fuel supply method for gas turbine cogeneration system
Номер патента: US20240240594A1. Автор: Kazuhiko Sato,Shohei Yoshida,Ryo Akiyama,Takashi Asao. Владелец: Mitsubishi Heavy Industries Ltd. Дата публикации: 2024-07-18.