|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 11|
Improvements in aircraft on-board inert gas generating systems wherein generally excess or surplus compressed airflow from a radial flow centrifugal compressor, produced in order to keep the compressor from surging in predetermined "reduced speed/reduced pressure ratio" operating modes, is utilized for at least one of driving a turbofan for conditioning the air separator module inlet air, or warming up/heating an air separator module in the inert gas generating system, thereby utilizing at least some of the energy of this excess/surplus compressed air th...
What is claimed is: 1. In an aircraft, a method for utilizing surplus compressed elevated temperature air produced in an inert gas generating system, said method comprising: a. initially directing hot air, from a compressor source, thereof, through a heat exchanger within said system; b. cooling said hot air to warm air within said heat exchanger and further directing a first non-surplus portion of said warm air, from said heat exchanger, and through the interiors of multiple permeable membrane bundles encased within an outer shell portion of an air sep...