Ge Aviation Systems Limited

Bradley J Burie

Peter C Hightower

Athanasios Kyriazopoulos

Kent I Weber

William M Martz

Kent Weber

A method and system for an integrated ejector valve assembly is provided. The integrated ejector valve assembly includes a first valve assembly configured to control a flow of relatively lower pressure fluid from a first inlet port, a second valve assembly configured to control a flow of relatively higher pressure fluid from a second inlet port, a first actuation chamber configured to close the first valve assembly, a second actuation chamber configured to close the second valve assembly, and a third actuation chamber configured to open the second valve assembly.

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Rockton, IL, United States of America

Bradley J Burie