Gas turbine engine systems and related methods involving multiple gas turbine cores
作者： Gary D. Roberge
DOI:
关键词: Blade (geometry) 、 Automotive engineering 、 Rotational energy 、 Engineering 、 Gas turbines 、 Mechanical engineering 、 Inlet
摘要: Gas turbine engine systems and related methods involving multiple gas cores are provided. In this regard, a representative includes: an inlet; blade assembly mounted to receive intake air via the located downstream of assembly, each being independently operative in first state, which rotational energy is provided rotate second not assembly.
lens.org 参考文章(23)
Mark R. Barchenko, Jet propulsion engine assembly for aircraft ,(1977)
John A. Violette, Pitch-change apparatus for a ducted thrust fan ,(1974)
Whittle Frank, Multiunit gas turbine power plant for aircraft propulsion ,(1945)
Jeffrey S. Zimmerman, Michael W. Scott, Variable fuel heating value adaptive control for gas turbine engines ,(2000)
Elmore V. Sprunger, Arthur P. Adamson, Variable cycle engine ,(1977)
Elmore Verne Sprunger, James Edward Johnson, John Robert Simmons, Variable cycle turbofan-ramjet engine ,(1990)
David W. Crall, Rollin G. Giffin, John W. Salvage, James E. Johnson, Peter N. Szucs, Turbofan engine with a core driven supercharged bypass duct ,(1996)
Paul E. Hagseth, Billy D. Couch, Louis G. Hunter, Combined cycle pulse combustion/gas turbine engine ,(2000)
Daniel P. Guinan, David E. Wendt, Flow diverter system for multiple streams for gas turbine engine ,(1998)
Kevin Allan Dooley, Relighting a turbofan engine ,(2014)