Fire-suppression system for an aircraft

Fire extinguishers – Special applications

Reexamination Certificate

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Details

C169S062000, C169S068000, C169S070000, C169S007000, C169S008000, C169S016000, C239S054000, C239S046000

Reexamination Certificate

active

07066274

ABSTRACT:
A fire-suppression system for use in an aircraft having at least one cargo compartment is disclosed. Methods of suppressing a fire in the cargo compartment are also disclosed. The fire-suppression system, under one aspect of the present invention, can include at least one fire-suppressant vessel, at least one discharge conduit coupled to the at least one fire-suppressant vessel, and a valve arrangement coupled to the fire-suppressant vessel and the discharge conduit. The valve arrangement can have a first setting to discharge a fire suppressant at a first discharge rate after activation of the fire-suppression system, a second setting to discharge the fire-suppressant at a second discharge rate less than the first discharge rate, and a third setting to discharge the fire-suppressant at a third discharge rate greater than the second discharge rate during descent of the aircraft.

REFERENCES:
patent: 4643260 (1987-02-01), Miller
patent: 4646848 (1987-03-01), Bruensicke
patent: 5038867 (1991-08-01), Hindrichs et al.
patent: 5052493 (1991-10-01), Court
patent: 5211246 (1993-05-01), Miller et al.
patent: 6619404 (2003-09-01), Grabow
patent: 2005/0150663 (2005-07-01), Fabre et al.
International Aviation Safety Association, “Investigation Update Into Fire on Board Air Canada Flight 116”, Investigation No. A02O0123, May 24, 2002, pp. 1-12. as found on the Internet link: http://www.iasa.com.au/folders/sr111/AirCanada116.html.

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