发明名称 TURBINE ENGINE WITH A TURBO-COMPRESSOR
摘要 A turbine engine is provided that includes a turbo-compressor and a combustor section. The turbo-compressor includes a compressor section and a turbine section. The combustor section is fluidly coupled between the compressor section and the turbine section. The compressor section includes a first number of stages. The turbine section includes a second number of stages that is different than the first number.
申请公布号 US2016237895(A1) 申请公布日期 2016.08.18
申请号 US201514622438 申请日期 2015.02.13
申请人 United Technologies Corporation 发明人 Kupratis Daniel B.;Sheridan William G.
分类号 F02C6/12;F02K3/00;F01D5/02;F04D29/32;F02C3/06;F02C3/107 主分类号 F02C6/12
代理机构 代理人
主权项 1. A turbine engine, comprising: a turbo-compressor including a compressor section and a turbine section; and a combustor section fluidly coupled between the compressor section and the turbine section; wherein the compressor section includes a first number of stages and the turbine section includes a second number of stages that is different than the first number.
地址 Hartford CT US