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.
申请公布号
WO2011008331(A2)
申请公布日期
2011.01.20
申请号
WO2010US34759
申请日期
2010.05.13
申请人
GE AVIATION SYSTEMS LLC;WEBER, KENT;KYRIAZOPOULOS, ATHANASIOS;HIGHTOWER, PETER C.;BURIE, BRADLEY J.
发明人
WEBER, KENT;KYRIAZOPOULOS, ATHANASIOS;HIGHTOWER, PETER C.;BURIE, BRADLEY J.