发明名称 GAS TURBINE ENGINE AND SYSTEM FOR MODULATING SECONDARY AIR FLOW
摘要 One embodiment of the present invention is a unique gas turbine system having a system for modulating secondary air flow. Another embodiment is a compressor vane stage with a plenum employed in providing secondary air flow. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for secondary air flow systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
申请公布号 US2012167589(A1) 申请公布日期 2012.07.05
申请号 US201113336352 申请日期 2011.12.23
申请人 FRITSCH THEODORE JOSEPH 发明人 FRITSCH THEODORE JOSEPH
分类号 F02C6/08;F01D1/04 主分类号 F02C6/08
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