초록 ▼

An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present

An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.

대표청구항 ▼

1. A system of introducing a recirculated exhaust stream into a turbomachine, the system comprising: the turbomachine comprising a gas turbine comprising: a compressor section, an external combustion system, and a turbine section; wherein the gas turbine operatively produces an exhaust stream;an inl

1. A system of introducing a recirculated exhaust stream into a turbomachine, the system comprising: the turbomachine comprising a gas turbine comprising: a compressor section, an external combustion system, and a turbine section; wherein the gas turbine operatively produces an exhaust stream;an inlet system located upstream of the compressor section, wherein the inlet system channels an inlet fluid towards the compressor section of the gas turbine, wherein the inlet fluid comprises an airstream and an exhaust stream,an exhaust gas recirculation (EGR) system comprising an EGR skid and an EGR duct integrated with a portion of the inlet system; wherein the EGR system operatively facilitates the sequestration and removal of concentrated CO2 and reduces the level of constituents within the exhaust stream; wherein the EGR system:receives the exhaust stream at a first temperature from an exhaust section of the gas turbine; wherein the exhaust stream comprises the constituents at a first level;allows the exhaust steam to enter the EGR skid, which reduces the constituents to a second level; andallows the exhaust stream to exit the EGR skid at a second temperature and flow through the EGR duct, wherein the exhaust stream enters the inlet system, wherein the inlet system comprises:a weather hood configured to reduce an amount of precipitation entering the inlet system, wherein the weather hood comprises an opening for receiving the airstream; andan inlet filter system configured to reduce an amount of foreign objects entering the compressor section, and the inlet system further comprises an inlet duct located downstream of the transition duct and upstream of an inlet plenum, wherein the inlet plenum is connected to an upstream portion of the compressor section, wherein the EGR duct is located on a portion of the inlet duct adjacent to the transition duct. 2. The system of claim 1, wherein the EGR duct is located on a portion of the inlet plenum located adjacent the compressor section. 3. The system of claim 1, wherein the EGR duct comprises a plurality of vanes for directing a flow path of the exhaust stream. 4. The system of claim 3, wherein the plurality of vanes are movable to change the direction of the flow path of the exhaust stream. 5. The system of claim 1, wherein the EGR duct nearly uniformly distributes the inlet fluid within the inlet system. 6. The system of claim 1, wherein the EGR duct comprises an inlet damper that opens to allow the exhaust stream to enter the inlet system and combine with the airstream.