Multi-port bleed system with variable geometry ejector pump
作者： Paul W. Banta , John A. Vasquez
DOI:
关键词:
摘要: A bleed air system selectively supplies engine from one or more of at least three sources to a variable geometry ejector pump. The provides improved performance over current systems, and decreases overall weight cost. includes controllable valve stage that controllably directs the
lens.org 参考文章(24)
Alan W. Smith, Engine bleed air supply system ,(1990)
Larry L. Linscheid, Philip M. Mueller, Apparatus for mixing high and low pressure air from a jet engine ,(1980)
Joseph M. Kos, Eugene R. Bruun, Control of aircraft bleed air stage mixing ,(1991)
Masakichi Kawada, Yoji Ise, Ejector pump having an electromagnetic motive fluid valve ,(1985)
Anthony I. Skur, Bleed air heat exchanger integral to a jet engine ,(2000)
Bradley D. Hitch, Donald Y. Davis, Fluid channeling system ,(1992)
Hercules Georgeou, Michael D. Loschiavo, Per Lars R. Stubbendorff, System and meth0d for automatically controlling cabin air temperature in an aircraft ,(1997)
Matthew R. Feulner, Rotor tip bleed in gas turbine engines ,(1999)
John T. Exley, Charles Kuintzle, Diffuser vane cusp bleed aperture with automatic ejector control device ,(1978)
David John Huber, Michael Scot Briesch, Closed loop air cooling system for combustion turbines ,(1997)