发明名称 Energy extraction and transfer system for a gas turbine engine
摘要 A gas turbine engine is provided having a variety of forms and features. The gas turbine engine can include a compressor having movable vanes. In one form of operation the compressor can close down the vanes to a relatively low flow capacity position and the compressor can be operated at a higher speed, whereupon the vanes can be repositioned and the gas turbine engine operated at a different condition. The gas turbine engine can include a turbine having movable vanes. In one form of operation the turbine can change the vane positions to a relatively low torque position and the engine operated at a higher fuel flow condition, whereupon the vanes can be repositioned and the gas turbine engine operated at a different condition. The gas turbine engine can have a heater that adds heat to a flow stream, a motor that provides energy to a shaft, and an external load.
申请公布号 US9021780(B2) 申请公布日期 2015.05.05
申请号 US200912646385 申请日期 2009.12.23
申请人 Rolls-Royce Corporation 发明人 Bowman Ray F.;Owen Philip Ray
分类号 F02C9/00;F02G3/00;F02C9/22;F02C7/32;F02C7/36 主分类号 F02C9/00
代理机构 Krieg DeVault LLP 代理人 Krieg DeVault LLP
主权项 1. An apparatus comprising: a gas turbine engine comprising a combustor, a high pressure spool and a low pressure spool, wherein the high pressure spool comprises a high pressure turbine, wherein the low pressure spool comprises a low pressure turbine, wherein the low pressure turbine is downstream of the high pressure turbine, and wherein the low pressure turbine is operable to convert energy from a working fluid of the gas turbine engine into a mechanical energy; an electrical generator coupled to the low pressure turbine for converting the mechanical energy into an electrical energy; and an energy transferring device comprising an electrical heater and a power allocation circuit; wherein the energy transferring device receives electrical energy from said generator, wherein the heater is in thermal communication with the working fluid, wherein the power allocation circuit is programmed to allocate the electrical energy in selectable ratios between the heater and an electrically powered system external to the gas turbine engine.
地址 Indianapolis IN US
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