IP Library Granted Patent US 9,242,132
Granted Patent B2
US 9,242,132 · App. 11/929,743 · Granted Jan 26, 2016

Fire suppression systems

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,242,132
App. No.
11/929,743
Granted
Jan 26, 2016
Kind
B2
Abstract

A method of fire suppression may include injecting a reactive agent into a reaction zone to produce a catalytically active species for fire suppression and conveying the catalytically active species to a fire to catalytically interfere with flame chemistry of the fire. Fire in a fuel tank may be suppressed by injecting the reactive agent into a convective flow of a mixture of fuel and oxidizer in a fuel tank, the reactive agent reacting in the fuel tank to release a species which catalytically interferes with flame chemistry to suppress fire in the fuel tank. Fire at an airplane crash may be suppressed by releasing the reactive agent from the container at the crash site to produce an active species to catalytically interfere with a fire at the crash site.

Claims (40)

1. A method of fire suppression, comprising:

providing a structure having a volume, a source of fuel, an air intake, and an outlet, wherein an air flow path is defined through the structure between the air intake and the outlet and wherein the structure defines a flame holding region capable of sustaining a spatially stable flame in the presence of an oxidizer and a fuel and a flow of at least one of an oxidizer and a fuel to the flame holding region;

providing a supply of a reactive agent;

injecting the reactive agent into a reaction zone in the volume at which the reactive agent reacts to produce a chemical species that catalytically interferes with flame chemistry; and

conveying the catalytic chemical species from the reaction zone to said flame holding region by the flow.

2. The method of claim 1 , wherein the injecting step comprises injecting the reactive agent at an injection point disposed at the structure with respect to the reaction zone and to the flow so that a minimum amount of the reactive agent capable of suppressing a fire at the flame holding region by production of the chemical species at the reaction zone upon injecting the reactive agent at the injection point is less than a minimum amount of the reactive agent capable of suppressing the fire by flooding the volume.

3. The method of claim 2 , wherein, at the providing step, the structure has

a predetermined one or more said flame holding regions,

a predetermined one or more said flows that respectively flow to at least one of the

predetermined one or more said flame holding regions, and

one or more said injection points respectively corresponding to at least one of the predetermined one or more said flows.

4. The method of claim 3 , wherein, at the providing step, the one or more injection points are disposed with respect to their corresponding at least one predetermined one or more flows so that a ratio of

a first minimum amount of the reactive agent capable of suppressing a fire at any said flame holding region within the volume by flooding the volume to

a second minimum amount of the reactive agent capable of suppressing fire at the at least one of the predetermined one or more flame holding regions upon injecting the second minimum amount at the one or more injection points is greater than 1.

5. The method of claim 4 wherein the ratio is at least 1.1.

6. The method of claim 4 wherein the ratio is at least 1.5.

7. The method of claim 4 wherein the ratio is at least 1.75.

8. The method of claim 1 , wherein the injecting step comprises:

propelling the catalytic chemical species toward a said flame holding region in a direction against a direction of the flow to increase a dwell time of the catalytic chemical species at the flame holding region.

9. The method of claim 1 , wherein the flow is an air flow of the air flow path.

10. The method of claim 1 , wherein, at the providing step, the structure defines multiple said flame hold regions and respective said flows for the multiple flame holding regions.

11. The method of claim 10 , wherein the injecting step comprises injecting the reactive agent at one or more of multiple injection points at the structure and respectively corresponding to the multiple respective flows.

12. The method of claim 11 , wherein the reactive agent is at least one of the group consisting of labile bromine, labile chlorine, and labile iodine.

13. The method of claim 1 , further comprising:

dissolving a sufficient quantity of a gaseous propellant in the reactive agent prior to the injecting step to maintain the reactive agent in a liquid form from ambient conditions to −65° C.

14. The method of claim 1 , wherein the reactive agent is at least one of the group consisting of labile bromine, labile chlorine, and labile iodine.

15. A method of suppressing fire in a fuel tank, comprising:

providing a fuel tank having a mixture of fuel and oxidizer;

providing a supply of a reactive agent; and

injecting the reactive agent into a reaction zone in the tank at which the reactive agent reacts to release, into a convective flow of the mixture of fuel and oxidizer, a chemical species which catalytically interferes with flame chemistry so that the convective flow conveys the chemical species to a fire in the fuel tank.

16. The method of claim 15 wherein the injecting step further comprises:

detecting the fire in the fuel tank before detonation of supersonic combustion waves to decrease velocity of combustion waves arising from the fire and reduce prospects of detonation.

17. The method of claim 15 wherein the injecting step further comprises:

detecting initial subsonic combustion of the mixture of fuel and oxidizer; and

injecting the reactive agent fast enough to prevent supersonic combustion in the fuel tank.

18. The method of claim 15 wherein the injecting step further comprises:

detecting initial subsonic combustion waves in the fuel tank with a high speed optical or acoustic ignition detector; and

triggering a rapid injection of the reactive agent sufficient to suppress the fire before detonation of the fuel tank.

19. The method of claim 15 wherein, in the providing step, a container containing the reactive agent is mounted in the fuel tank.

20. The method of claim 15 , wherein the reactive agent is at least one of the group consisting of labile bromine, labile chlorine, and labile iodine.

Assignments (13)
PURCHASE AGREEMENT Recorded Oct 12, 2022
From: ECLIPSE AEROSPACE, INC.
To: AML GLOBAL ECLIPSE LLC
Reel/Frame 062215/0089 →
ASSIGNMENT OF PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Nov 28, 2017
From: ECLIPSE AEROSPACE, INC.; CRYSTAL FINANCIAL SBIC LP
To: CANTOR FITZGERALD SECURITIES
Reel/Frame 044512/0618 →
SECURITY INTEREST Recorded Nov 20, 2017
From: ECLIPSE AEROSPACE, INC.
To: CANTOR FITZGERALD SECURITIES
Reel/Frame 044177/0821 →
ASSIGNMENT OF PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Jul 15, 2015
From: WILMINGTON TRUST, NATIONAL ASSOCIATION
To: CRYSTAL FINANCIAL SBIC LP
Reel/Frame 036106/0876 →
SECURITY INTEREST Recorded Apr 20, 2015
From: ECLIPSE AEROSPACE, INC.
To: WILMINGTON TRUST, NATIONAL ASSOCIATION
Reel/Frame 035450/0910 →
ASSIGNMENT OF PATENT AND TRADEMARK SECURITY AGREEMENT Recorded Apr 20, 2015
From: WELLS FARGO BANK, NATIONAL ASSOCIATION
To: WILMINGTON TRUST, NATIONAL ASSOCIATION
Reel/Frame 035470/0074 →
SECURITY INTEREST Recorded Jul 26, 2012
From: ECLIPSE AEROSPACE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 028641/0549 →
SECURITY AGREEMENT Recorded Oct 14, 2009
From: ECLIPSE AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 023364/0639 →
SECURITY AGREEMENT Recorded Oct 14, 2009
From: ECLIPSE AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A. AS COLLATERAL AGENT
Reel/Frame 023364/0720 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 14, 2009
From: ECLIPSE AVIATION CORPORATION
To: ECLIPSE AEROSPACE, INC.
Reel/Frame 023220/0472 →
RELEASE OF SECURITY INTEREST Recorded Feb 15, 2008
From: THE BANK OF NEW YORK
To: ECLIPSE AVIATION CORPORATION
Reel/Frame 020518/0395 →
GRANT OF SECURITY INTEREST IN UNITED STATES PATENTS Recorded Dec 28, 2007
From: ECLIPSE AVIATION CORPORATION
To: THE BANK OF NEW YORK
Reel/Frame 020299/0220 →
GRANT OF SECURITY INTEREST IN UNITED STATES TRADEMARKS AND PATENTS Recorded Dec 28, 2007
From: ECLIPSE AVIATION CORPORATION
To: THE BANK OF NEW YORK
Reel/Frame 020299/0331 →