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公开(公告)号：US12038178B2
公开(公告)日：2024-07-16
申请号：US18163361
申请日：2023-02-02
发明人： Young Jun Shin , Han Jin Jeong , Eun Seong Cho
摘要： A micro-mixer includes a plurality of fuel tubes through which air and fuel flow, a casing accommodating the plurality of fuel tubes therein, an injection part formed as a pyramidal protrusion on one side of the casing and connected to a front end of the fuel tube to inject the air and the fuel, and a fuel supply divided into a plurality of fuel supply parts to supply the fuel to the fuel tubes.
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公开(公告)号：US20230250959A1
公开(公告)日：2023-08-10
申请号：US18163361
申请日：2023-02-02
发明人： Young Jun SHIN , Han Jin Jeong , Eun Seong Cho
摘要： A micro-mixer includes a plurality of fuel tubes through which air and fuel flow, a casing accommodating the plurality of fuel tubes therein, an injection part formed as a pyramidal protrusion on one side of the casing and connected to a front end of the fuel tube to inject the air and the fuel, and a fuel supply divided into a plurality of fuel supply parts to supply the fuel to the fuel tubes.
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公开(公告)号：US11959642B2
公开(公告)日：2024-04-16
申请号：US18163799
申请日：2023-02-02
发明人： Young Jun Shin , Han Jin Jeong , Eun Seong Cho
摘要： A micro-mixer includes a plurality of fuel tubes through which air and fuel flow, a casing accommodating the plurality of fuel tubes therein, and a plurality of injection parts each formed as a pyramidal protrusion on one side of the casing and connected to a front end of the fuel tube to inject the air and the fuel, wherein each of the plurality of injection parts has an inclined injection hole formed obliquely with respect to an extension direction of the plurality of fuel tubes on at least one side of the pyramidal protrusion.
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公开(公告)号：US20230250960A1
公开(公告)日：2023-08-10
申请号：US18163799
申请日：2023-02-02
发明人： Young Jun SHIN , Han Jin Jeong , Eun Seong Cho
摘要： A micro-mixer includes a plurality of fuel tubes through which air and fuel flow, a casing accommodating the plurality of fuel tubes therein, and a plurality of injection parts each formed as a pyramidal protrusion on one side of the casing and connected to a front end of the fuel tube to inject the air and the fuel, wherein each of the plurality of injection parts has an inclined injection hole formed obliquely with respect to an extension direction of the plurality of fuel tubes on at least one side of the pyramidal protrusion.
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公开(公告)号：US11543131B2
公开(公告)日：2023-01-03
申请号：US17548498
申请日：2021-12-11
发明人： Han Jin Jeong
摘要： A nozzle assembly for injecting fuel and compressed air into a combustion chamber of a gas turbine combustor is provided. The nozzle assembly includes a nozzle body disposed in the combustor and having a coolant outlet on one end of which an inside of the nozzle body communicates with the combustion chamber, a spray nozzle disposed in the nozzle body and including a plurality of first nozzle tubes each having a first flow path formed therein to allow combustion air to flow into the combustion chamber and a fuel hole formed to supply fuel, and a second nozzle tube having through-holes to allow the first nozzle tubes to pass therethrough and a second flow path formed to supply fuel, and a diaphragm disposed inside of the nozzle body and including a plurality of coolant flow holes through which a coolant supplied to the nozzle body is supplied towards one end of the nozzle body and a plurality of tube holes through which the first nozzle tubes pass.
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