Aeronautics and astronautics – Aircraft structure – Fuel supply
Patent
1978-12-07
1985-12-03
Blix, Trygve M.
Aeronautics and astronautics
Aircraft structure
Fuel supply
55158, B64D 3732
Patent
active
045561800
ABSTRACT:
A pump is used to exhaust oxygen rich waste gas to ambient pressure in an inert gas generating system in order to improve the performance of the permeable membrane air separator component and to insure sufficient generation of inert gas when available source air pressure is low.
REFERENCES:
patent: 2889955 (1959-06-01), Naulty et al.
patent: 2923288 (1960-02-01), Burtt
patent: 3165390 (1965-01-01), Parken et al.
patent: 3350844 (1967-11-01), Robb
patent: 3442002 (1969-05-01), Geary et al.
patent: 3691730 (1972-09-01), Hickey et al.
patent: 3735558 (1973-05-01), Skarstrom et al.
patent: 4140499 (1979-02-01), Ozaki et al.
Blix Trygve M.
Corl Rodney
McFarland James W.
Miller Albert J.
Talcott Joel D.
LandOfFree
Fuel tank inerting system does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Fuel tank inerting system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel tank inerting system will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1390891