发明名称 Cogen heat load matching through reheat and capacity match
摘要 One example of a gas turbine engine may include a gas generator, a reheat combustor that is disposed downstream of the gas generator, and a power turbine that is disposed downstream of the reheat combustor and includes a plurality of nozzle guide vanes. The reheat combustor is configured to increase a fuel flow so as to increase a temperature of the reheat combustor and match a required exhaust temperature. The nozzle guide vanes are configured to increase a real capacity at a power turbine inlet in proportion with the required exhaust temperature. A constant apparent capacity at a gas generator exit upstream of the reheat combustor remains constant, in response to proportionately increasing the temperature and the real capacity with respect to one another.
申请公布号 US9624829(B2) 申请公布日期 2017.04.18
申请号 US201314135532 申请日期 2013.12.19
申请人 INDUSTRIAL TURBINE COMPANY (UK) LIMITED 发明人 Lebel Jean-Francois;Carson Carl
分类号 F02C3/10;F02C6/00;F02C9/54;F02C6/18 主分类号 F02C3/10
代理机构 Beusse Wolter Sanks & Maire 代理人 Beusse Wolter Sanks & Maire
主权项 1. A gas turbine engine, comprising: a gas generator; a reheat combustor downstream of the gas generator; a power turbine downstream of the reheat combustor and having a plurality of variable area nozzle guide vanes; and a controller configured to operate the gas turbine engine such that: the reheat combustor is configured to increase a fuel flow so as to increase a temperature of the reheat combustor and match a required exhaust temperature; the plurality of variable area nozzle guide vanes are configured to increase a real capacity at a power turbine inlet in proportion with the required exhaust temperature, wherein the real capacity is a capacity of the power turbine based on flow parameters at the power turbine inlet; and a constant apparent capacity at a gas generator exit upstream of the reheat combustor remains constant in response to proportionately increasing the temperature and the real capacity, wherein the apparent capacity is a capacity of the power turbine based on flow parameters at a gas generator exit.
地址 GB