가스 터빈 시스템

• Main Authors: UCHIDA MASAHIRO, ITO SHINTARO, FUJIMORI TOSHIRO, CHOI WONYOUNG
• Format: Patent
• Language: Korean
• Published: 28.11.2023
• Subjects: AIR INTAKES FOR JET-PROPULSION PLANTS; BLASTING; CHEMISTRY; COMBUSTION ENGINES; COMPOUNDS THEREOF; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS; GAS-TURBINE PLANTS; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; INORGANIC CHEMISTRY; LIGHTING; MECHANICAL ENGINEERING; METALLURGY; NON-METALLIC ELEMENTS; WEAPONS

흡기 유로(101)와, 연소기(13)와 접속되는 배기 유로(102)와, 흡기 유로(101)에 설치되는 압축기(11a)와, 배기 유로(102)에 설치되는 터빈(11b)과, 암모니아 탱크(14)와, 암모니아 탱크(14)와 접속되는 암모니아 공급구(16a)와, 연소기(13)와 접속되는 수소 배출구(16b)를 가지고, 배기 유로(102) 중 터빈(11b)보다 하류측, 또는, 흡기 유로(101) 중 압축기(11a)보다 하류측에 배치되고, 암모니아 분해 촉매 및 수소 분리막을 가지는 수소 발생 분리 장치(16)를 구비한다. A gas turbine system (1) includes: a combustor (13); an intake flow passage (101) connected to the combustor (13); an exhaust flow passage (102) connected to the combustor (13); a compressor (11a) provided in the intake flow passage (101); a turbine (11b) provided in the exhaust flow passage (102); an ammonia tank (14); and a hydrogen generator-separator (16) having an ammonia supply port (16a) connected to the ammonia tank (14) and a hydrogen discharge port (16b) connected to the combustor (13), the hydrogen generator-separator (16) being arranged on a downstream side of the turbine (11b) in the exhaust flow passage (102) or on a downstream side of the compressor (11a) in the intake flow passage (101), the hydrogen generator-separator (16) including an ammonia cracking catalyst and a hydrogen separation membrane.