发明名称 GAS TURBINE EXHAUST SYSTEM
摘要 A power generation system (10). Stationary and rotatable blades (34, 37) are positioned about a rotor (8) to receive exhaust gas (46) from a combustor (6) and to impart an axial velocity component. A section of ductwork (48) is positioned to receive the exhaust gas and has a central transition portion (80t) into which the rotor extends. A spiral portion (80s) of the ductwork comprises a helically shaped flow section (80) extending outwardly from the central portion to provide a helical section of the flow path to carry the exhaust gas away from the central portion. A portion of the flow path along the helically shaped flow section may have an area in cross section which increases as a function of position along the flow path. The spiral portion is positioned to redirect the exhaust in a direction orthogonal to the rotor.
申请公布号 EP3129608(A1) 申请公布日期 2017.02.15
申请号 EP20140722501 申请日期 2014.04.10
申请人 Siemens Aktiengesellschaft 发明人 RODRIGUEZ, Jose L.
分类号 F01D25/30 主分类号 F01D25/30
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