US4646848A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fire suppression system for an aircraft
Assignee: Lockheed Martin Corp
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Filing: 1984-10-26
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Granted: 1987-03-03
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Expires: 2004-10-26
Abstract
Abstract The invention is a fire suppression system for an aircraft 10 of the type having a main cabin compartment 12, such as a passenger compartment and a plurality of closable or closed-off subcompartments. These subcompartments can be any area which is separated by fixed structure from the main cabin and therefore are normally not accessible. The fire suppression system comprises a plurality of ducts 57 coupling a plurality of subcompartments 14, 15, 22 to the main compartment. The plurality of ducts 57 have first ends of the ducts 57 terminate in nozzles 58 within the subcompartments adapted to distribute the fire suppression chemical in a specific pattern and second ends terminating in disconnect valve halves 59 accessible from the main cabin compartment. A portable unit 30 having a tank 42 filled with a fire suppression chemical under pressure is moveable within the main compartment 12. Preferably, the fire suppression chemical is Halon stored under nitrogen gas pressure. The unit 30 has a length of flexible line 54 coupled to the tank 42 and terminating in a nozzle assembly 55 having a disconnect valve half 159 mounted thereon. This disconnect valve half 159 is connectable to the disconnect valve half 59 attached to any one of the ducts 57.
Inventors
- 👤 Wilhelm A. Bruensicke
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 10:44
CPC Classifications
A; A62; A62C; A62C3/00; A62C3/07; A62C3/08
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
247 words
An improvement to a fire suppression system for an aircraft, the aircraft having a main compartment and a plurality of subcompartments, the fire suppression system comprising a plurality of ducts having first and second ends, each duct separately coupling a subcompartment to the min compartment, the ducts having a first end coupled to the subcompartment and a second end coupled to the main compartment, and a portable fire extinguisher movable within the main compartment, the improvement comprising: a first disconnect valve half coupled to each second end of the plurality of ducts; and a nozzle assembly coupled to the fire extinguisher comprising; a housing having an inlet port and a discharge port coupled by a passageway therebetween; a second disconnect valve half coupled to said housing mountable with said first disconnect valve half; a valve seat support located in said passageway having an opening therethrough; a diaphragm assembly sealing said inlet port from said discharge port, said diagragm assembly having a breakable center portion positioned over said opening and a valve seat conforming to and in contact with said valve seat support; a shaft mounted within said passageway and translatable therein, said shaft including: a plurality of cutters mounted thereon and a chamfered sealing surface mounted about said cutters adapted to mate with said valve seat; and means to drive said shaft toward said diaphgram assembly such that said cutters pierce said center portion of said diaphragm assembly, thus, connecting said inlet port to said discharge port.
Claim 2
Dependent Claim
247 words
An improvement to a fire suppression system for an aircraft, the aircraft having a main compartment and a plurality of subcompartments, the fire suppression system comprising a plurality of ducts having first and second ends, each duct separately coupling a subcompartment to the min compartment, the ducts having a first end coupled to the subcompartment and a second end coupled to the main compartment, and a portable fire extinguisher movable within the main compartment, the improvement comprising: a first disconnect valve half coupled to each second end of the plurality of ducts; and a nozzle assembly coupled to the fire extinguisher comprising; a housing having an inlet port and a discharge port coupled by a passageway therebetween; a second disconnect valve half coupled to said housing mountable with said first disconnect valve half; a valve seat support located in said passageway having an opening therethrough; a diaphragm assembly sealing said inlet port from said discharge port, said diagragm assembly having a breakable center portion positioned over said opening and a valve seat conforming to and in contact with said valve seat support; a shaft mounted within said passageway and translatable therein, said shaft including: a plurality of cutters mounted thereon and a chamfered sealing surface mounted about said cutters adapted to mate with said valve seat; and means to drive said shaft toward said diaphgram assembly such that said cutters pierce said center portion of said diaphragm assembly, thus, connecting said inlet port to said discharge port.
Claim 3
Dependent Claim
45 words
The fire suppression system as set forth in claim 1 further including a diaphragm seal mounted within said housing having first and second ends, said first end attached to said housing and said second end attached to said shaft sealing said housing to said shaft.
Claim 4
Dependent Claim
102 words
The fire suppression system as set forth in claim 2 wherein said second disconnect valve half comprises: said housing having an external circumferential groove on the surface of said housing located mounted in proximity to said discharge port; a constant diameter guide portion at said discharge port end; and a conical surface extending inward from said groove to said constant diameter portion; a sleeve mounted about said housing, slidable from a first position clear of said groove to a second position extending over said groove; and two-position detent means adapted to releasably lock said sleeve in either said first or second positions.
Claim 5
Dependent Claim
168 words
The fire suppression system of claim 3 wherein said first disconnect valve half comprises: a hollow housing mounted to a wall of the main compartment, said housing having an aperture adapted to engage and position said nozzle assembly within said housing; a plurality of circumferentially disposed fingers terminating in inwardly directed protrusions mounted within said housing, said protrusions adapted to mate with said groove on said nozzle assembly; seal means mounted within said housing adapted to seal said constant diameter guide portion of said nozzle assembly when said nozzle assembly is coupled to said first half of said disconnect valve; such that when said nozzle assembly is coupled to said first disconnect valve half by inserting said constant diameter guide portion into said aperture of said housing, said protrusions contact said conical surface spreading said fingers radially apart until such time as said protrusions enter said groove after which said fingers assume their first position and said sleeve is moved from said second position to said first position.
Claim 6
Dependent Claim
61 words
The fire suppression system of claim 3 further including a nozzle extension having a disconnect valve half couplable to said second disconnect valve half on said nozzle assembly such that when a fire occurs in said main compartment said nozzle extension can be attached to said nozzle assembly to aid in the dispersion of said fire suppression chemical on the fire.
References Cited (Backward Citations)
US1297024A
Cited
US1660992A
Cited
US1925669A
Cited
FR879145A
Cited
US3719232A
Cited
US3972373A
Cited
US4351394A
Cited
US4420047A
Cited
US4482012A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-02 | 1990-09-01 | 1991-03-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-02 | 1994-09-01 | 1995-03-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-02 | 1998-09-01 | 1999-03-03 | $7700.00 | Window Closed / Lapsed |