Aircraft excessive fuel dumping ejection parallel to flight...

Aeronautics and astronautics – Aircraft structure – Fuel supply

Reexamination Certificate

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C244S136000

Reexamination Certificate

active

07111809

ABSTRACT:
Excessive fuel is dumped by ejection under a pressurized outflow velocity from an aircraft during flight as jets in a direction parallel to air stream flow relative to the aircraft, from a rearwardly facing exit opening of a fuel jettison device mounted on the lower surface of the aircraft, with the exit fixedly spaced below the lower aircraft surface a short distance to avoid the Coanda effect while reducing or eliminating fuel and fuel mist impingement on aircraft surfaces.

REFERENCES:
patent: 2248308 (1941-07-01), Rice
patent: 2650781 (1953-09-01), Taylor
patent: 3096054 (1963-07-01), Ciminaghi
patent: 5655732 (1997-08-01), Frank
patent: 2002/0088901 (2002-07-01), Moreland
Paper entitled“Simulation and Analysis of V-22 Aircraft Fuel Dumping,”Tsze C. Tai, presented at 42nd AIAA Aerospace Sciences Meeting & Exhibits, Jan. 5-8, 2004, 16 pages.
U.S. Appl. No. 60/580,396, filed Jun. 18, 2004 entitled “Aircraft Fuel Dumping During Flight”.

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