US3524506A - Fire extinguishing apparatus - Google Patents

Fire extinguishing apparatus Download PDF

Info

Publication number
US3524506A
US3524506A US755031A US3524506DA US3524506A US 3524506 A US3524506 A US 3524506A US 755031 A US755031 A US 755031A US 3524506D A US3524506D A US 3524506DA US 3524506 A US3524506 A US 3524506A
Authority
US
United States
Prior art keywords
fire extinguishing
agent
extinguishing agent
nozzle
fire
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US755031A
Inventor
Carl A Weise
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
McDonnell Douglas Corp
Original Assignee
McDonnell Douglas Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by McDonnell Douglas Corp filed Critical McDonnell Douglas Corp
Application granted granted Critical
Publication of US3524506A publication Critical patent/US3524506A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C3/00Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/07Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
    • A62C3/08Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft

Definitions

  • a fire extinguishing system including a supply system for an extinguishing agent such as bromotrifiuoromethane, a control system, and a diffuser assembly.
  • the diffuser assembly is adapted for placement in a space to be protected from fire and includes a nozzle connected to the supply assembly by suitable conduit means, and an aspirator positioned to receive the output of the nozzle.
  • the construction of the diffuser assembly is such as, upon energization, to provide a rapid, diffused and blanketing discharge of the extinguishing agent in an appropriate concentration with air or other gases.
  • the control system may be controlled by a detector unit placed in the protected space.
  • Bromotrifiuoromethane has long been employed as a fire extinguishing agent. Its high efficiency, low toxicity and light weight are significant factors when used in aircraft. On a weight-of-agent basis, this agent is more effective than carbon tetrachloride, carbon dioxide and chemicals of the bicarbonate of soda type. It is particularly advantageous for use against fires in delicate electrical, mechanical or electronic equipment as unlike dry powder types, it leaves no residue which in itself might be troublesome to remove in the post extinguishment stage, or which might damage equipment beyond salvage or operation.
  • Bromotriiiuoromethane like carbon dioxide, is normally supplied as a liquified, compressed gas. It is especially useful as a fire extinguishing agent in total flooding types of fire extinguishing systems. A three to five percent concentration in air or other gases is sufficient to extinguish fires on contact or to eliminate any possibility of explosions of flammable atmospheres.
  • bromotrifiuoromethane must 'be distributed thoroughly throughout the space to be protected in no less than a three to five percent concentration, and preferably within twenty seconds after detection of fire. Since bromotrifiuoromethane is about five times as heavy as air, vigorous mixing is required to achieve this disbursion in such a short time duration.
  • Prior fire extinguishers have failed to solve this significant problem; it is a direct improvement upon the state-of-the-art to provide a fire extinguishing system which incorporates a diffuser arranged to mix a fire extinguishing agent such as bromo trifluoromethane and air or other gaseous elements in the protected space, so that the agent is thoroughly distributed,
  • a fire extinguishing agent such as bromo trifluoromethane and air or other gaseous elements
  • a diffuser which includes a nozzle having an attachment at one end for connection to a container of a pressurized fire extinguishing agent such as liquid bromotrifiuoromethane.
  • the nozzle includes an orifice having a diameter adequate to regulate flow of the pressurized agent therethrough, and an expansion chamber, having a sufficient length and a diameter substantially greater than the diameter of the orifice, for expanding substantially all the fire extinguishing agent output of the orifice into a gaseous form and for accelerating the gaseous agent to near sonic velocity.
  • the diffuser further includes an elongated tubular member having two open ends and a diameter substantially greater than the diameter of the expansion chamber.
  • the tubular member is in axial alignment and positioned to receive the output of the expansion chamber whereby the extinguishing agent emitted from the expansion chamber may pass into and mix with air or other gaseous elements in the tubular member.
  • the diffuser in combination with a pressurized fire extinguishing agent source, a discharge valve for regulating the flow of the agent to the diffuser, and a fire detector for sensing the existence of a fire and for closing an electrical circuit to energize and open the discharge valve, form an eificient automatic flooding type fire extinguishing apparatus which is useful for protection of a substantially enclosed space such as an interior compartment of an aircraft.
  • FIG. 1 is a diagrammatic illustration of an automatic fire extinguishing system shown in use with aircraft;
  • FIG. 2 is a partially schematic diagram illustrating details of the present invention
  • FIG. 3 is an enlarged fragmentary, partially pictorial illustration of the diffuser assembly used in the system shown in FIG. 1, and including a pair of diffusers;
  • FIG. 4 is a schematic diagram of a control system which may be used with the systemshown in FIG. 1;
  • FIG. 5 illustrates a fire detector which may be used with the system shown in FIG. 4.
  • FIG. 1 An automatic, total flooding fire extinguishing system employed to protect aircraft interior compartments 10.
  • a pressurized fire extinguishing agent supply assembly 12 a diffuser assembly 22, and a control system 18.
  • the diffuser assembly 22 is placed in the aircraft interior compartment 10 and connected to the supply assembly 12 by a conduit 16.
  • the control system 18 includes an electrically operated solenoid valve 20, which is positioned in the conduit 16, for controlling the delivery of the fire extinguishing agent from a casing 14 of the supply assembly 12 to the diffuser assembly 22.
  • the diffuser assembly 22 distributes the fire extinguishing agent throughout the protected enclosures 10 by mixing the agent with air or other gaseous elements in the compartment 10.
  • FIG. 2 there is shown a fire extinguishing agent casing 14 adapted to contain, under pressure, a
  • a tube 28 extends down to the bottom of the container so that the gaseous nitrogen can force the liquid bromotrifluoromethane through a conduit or hose 16 which includes inlet and outlet portions, the inlet portion being connected to the tube 28.
  • a conventional discharge valve 20, which may be manually or electrically operated, positioned in the conduit controls the delivery of bromotrifluoromethane therethrough.
  • a diifuser 30 adapted to be connected to the discharge outlet of the hose 16.
  • the diffuser 30 comprises a vaporizing nozzle 32 and an aspirator 34.
  • the nozzle or expanding means 32 includes an end fitting 36 adapted to be con nected to the outlet of the hose 16, and an orifice 38 having a diameter adequate to regulate the flow of bromotrifluoromethane therethrough.
  • the nozzle 32 further includes an expansion chamber 40, having a sufficient length and a diameter substantially greater than that of the orifice 38, for expanding the bromotrifluoromethane output of the orifice into gaseous form and for accelerating the bromotrifluoromethane to near sonic velocity.
  • the expansion chamber 40 is arranged to discharge into the aspirator or mixing means 34 which is a hollow tube-like member having a diameter greater than the diameter of the expansion chamber 40.
  • the aspirator includes open ends 42 and 44 with the open end 42 positioned to receive the output of the nozzle 32. Since the diameter of the aspirator 34 is greater than that of the expansion chamber 40, the open end 42 functions as an inlet for atmospheric air to enter the aspirator tube 34 for mixing with the extinguishing agent bromotrifluoromethane.
  • the aspirator 34 is of sufiicient length to cause thorough mixing of the extinguishing agent with incoming air.
  • the pressurized liquid bromotrifluoromethane is directed to the nozzle 32, at which location, at least a major portion of the liquid bromotrifluoromethane vaporizes and accelerates to near sonic velocity as it expands, carrying the unvaporized portion of the bromotrifluoromethane with it.
  • This output mixture of the nozzle 32 is directed to mix with air in the aspirator 34 and the mixture emitted therefrom is directed to a fire.
  • a heater 46 provided to heat the liquid bromotrifluoromethane in the conduit 16 to a suitable temperature to achieve the desired bromotrifluoromethane velocity at the exit of the nozzle 32.
  • the heater 46 is of conventional construction well known in the art, such as, for example, the type disclosed in US. Pat. No. 2,450,537, or preferably, the commercially available electric heating units which can be inserted into the conduit 16.
  • FIG. 3 which shows details of the ditfuser assembly 22 employed in the system shown in FIG. 1, there is shown identical diffusers 50 and 52 arranged to discharge in a direction opposite to each other so the discharge reaction forces would substantially cancel.
  • the diffusers 50 and 52 constructed and operated substantially similar to the corresponding parts shown in FIG. 2 and described above, each comprises a vaporizing nozzle 54- 56.
  • Each diffuser further includes an inverted L-shaped tubular member or aspirator 58-60.
  • the aspirator 58 includes open ends 62A and 64A and the aspirator 60 includes open ends 62B and 64B.
  • the fire extinguishing agent is delivered to the diffusers through the common conduit 16 which includes a divider or T 68.
  • the identical aspirators are held to discharge in opposite directions by relatively rigid connecting members 70 and 72, while the nozzles 54 and 56 are mounted in proper relation to the aspirators by rigid conduit portions 16A and 16B.
  • the entire diffuser assembly 22 is supported by a structural member 74 which is fixed to and vertically extended from a base 76.
  • the base is a fiat, rigid T shape member fixedly secured to seat tracks 78 of the aircraft interior compartment 10. It has been found that if the aspirator 58-60 is mounted in proper relation to one of the surfaces of the space to be protected, for example, near a surface 80 of the aircraft interior compartment 10 as shown in FIG.
  • the effectiveness of the mixing of the agent bromotrifiuoromethane and air or other gaseous element is enhanced by an aspirator-like action in the protected enclosure.
  • the air or other gaseous element in the enclosure and the 'bromotrifluoromethane tend to violently circulate within the protected space, thus the agent, bromotrifluoromethane, can reach a fire anywhere in the protected enclosure.
  • FIG. 4 is a schematic diagram of the control system 18 employed in the system shown in FIG. 1, there is shown an electrically operated, conventional solenoid discharge valve 82 used to control the flow of extinguishing agent through the conduit 16, a battery 84 for supplying the power to energize the valve 82, and a fire detector 86 which functions as a switch and is located in the aircraft interior compartment 10.
  • the solenoid valve 82 is connected at one terminal to a ground 88 and its other end to the detector or switch 86.
  • the detector 8 6 is connected to the power source 84 which, in turn, is connected to the ground 88 to complete the circuit when the switch 86 is closed.
  • the detector 86 In operation, when a fire is detected by the detector 86, it functions as a switch to close the electrical circuit to energize and open the discharge valve 82, thereby allowing the pressurized fire extinguishing agent bromotrifluoromethane to pass through the condiut 16 to the diffuser assembly 22 for mixing with air in the compartment 10.
  • FIG. 5 shows additional details of the fire detector 86 which may be used in the system shown in FIG. 1, there is shown a detector hav ing a detector tube 90', which is located in the aircraft interior compartment 10.
  • the air in the tube 90 expands and the resultant pressure, via a copper tube 94, causes two bellows type diaphragms to make contact, thus closing the circuit shown in FIG. 4.
  • the pressure created by heat in the protected area travels in opposite directions from the source of heat to the diaphrgams 95 through the detector tube 90.
  • Each end of the tube 90 terminates at a compensator 92 through terminals 100.
  • the compensator is a hollow closed cylinder of predetermined capacity used to compensate or cushion any sudden but momentary expansion of the air in the detector tube 90. From the compensators 92 the expanded air travels through the breathers 93, which are the devices that permit the expanded air in the detector tube and the compensators to be released to the outside atmosphere at a predetermined rate.
  • a slow gradual rise, or a sudden but momentary rise in temperature in the protected area, and the resulting expansion of air in the detector tube 90, will not cause the diaphragms 95 to make contact, since any moderate excess volume of air can be absorbed by the compensators 92 and gradually breathed out into the atmosphere. If an abnormal, continued rise in temperature, such as a fire would produce, causes the air to expand in the detector tube 90 faster than the compensators 92 can absorb it,
  • the builtup pressure travels through the insulator tubes 94, which lead from the compensator 92 and the breather 93 to each bellows type diaphragm 95.
  • the pressure behind the two opposing diaphragms 95 forces them toward each other.
  • Two platinum-faced contact points 96 are provided to facilitate contact and when the points 96 meet, the electrical circuit shown in FIG. 4 is closed, through connections 97, to energize and open valve 82 to allow the pressurized extinguishing agent to reach the diffuser assembly 22 for distribution.
  • extinguishing agent bromotrifiuoromethane and discharge agent nitrogen as the two components of the present extinguisher, nevertheless, if desired, other agents having equivalent characteristics may be used.
  • An apparatus comprising:
  • each of said diffusers including:
  • a nozzle having an attachment at one end for connection to a container of a liquefied, pressurized fire extinguishing agent, said nozzle having an orifice of a diameter adequate to regulate flow of said pressurized agent therethrough;
  • an expansion chamber forming a portion of said nozzle and having a length sufiicient to permit desired expansion of said agent and having a diameter substantially greater than the diameter of said orifice, said agent being substantially wholly converted to a gaseous form as emitted from said nozle and accelerated to near sonic velocity;
  • an elongated tubular member having two open ends and a diameter substantially greater than the diameter of said expansion chamber, in axial alignment and positioned to receive the output of said expansion chamber whereby the high velocity output of said expansion chamber may pass into and mix with gaseous elements in said tubular member;
  • said first diffuser is positioned and arranged to discharge in a direction opposite to said second diffuser so that substantially all reaction forces will cancel upon a simultaneous discharge;
  • common delivery means for delivering a liquified, pressurized fire extinguishing agent to said diffusers.
  • a fire extinguishing apparatus for protection of a substantially enclosed space comprising:
  • liquified bromotrifluoromethane such as liquified bromotrifluoromethane, and a discharging agent, such as gaseous nitrogen, under pressure;
  • conduit having inlet and outlet portions and said inlet being connected to said container, for delivering the fire extinguishing agent from said container to a place of use;
  • control unit having a discharge valve positioned in said conduit for controlling the passage of the fire extinguishing agent therethrough, and a fire detector, positioned in the substantially enclosed space, for providing an electrical output signal to open said discharge valve when fire is detected, thereby allowing the fire extinguishing agent to pass through said conduit;
  • heating means connected to said conduit, for heating the fire extinguishing agent in said conduit to increase the energy available in the fire extinguishing agent resulting in higher agent velocity as it emits from said expansion chamber;
  • said diffuser includes:
  • a nozzle having an attachment at one end for connection to a container of a liquified, pressurized fire extinguishing agent, said nozzle having an orifice of a diameter adequate to regulate flow of said pressurized agent therethrough;
  • an expansion chamber forming a portion of said nozzle and having a length sufficient to permit desired expansion of said agent and having a diameter substantially greater than the diameter of said orifice, said agent being substantially wholly converted to a gaseous form as emitted from said nozzle and accelerated to near sonic velocity;
  • an elongated tubular member having two open ends and a diameter substantially greater than the diameter of said expansion chamber, in axial alignment and positioned to receive the output of said expansion chamber 'whereby the high velocity output of said expansion chamber may pass into and mix with gaseous elements in said tubular member.
  • common delivery means for delivering the liquified, pressurized fire extinguishing agent to said diffusers.

Description

g- 18, 1970 c. A. WEISE 3,524,503
FIRE EXTINGUISHING APPARATUS Filed Aug. 26, 1968 INVENTOR. [14,21 A, %-'/5.-s
BY I
United States Patent Office 3,524,505 Patented Aug. 18, 1970 3,524,506 FIRE EXTINGUISHING APPARATUS Carl A. Weise, San Pedro, Calif., assignor to McDonnell Douglas Corporation, a corporation of Maryland Filed Aug. 26, 1968, Ser. No. 755,031 Int. Cl. A62c 3/00 US. Cl. 169-2 3 Claims ABSTRACT OF THE DISCLOSURE A fire extinguishing system including a supply system for an extinguishing agent such as bromotrifiuoromethane, a control system, and a diffuser assembly. The diffuser assembly is adapted for placement in a space to be protected from fire and includes a nozzle connected to the supply assembly by suitable conduit means, and an aspirator positioned to receive the output of the nozzle. The construction of the diffuser assembly is such as, upon energization, to provide a rapid, diffused and blanketing discharge of the extinguishing agent in an appropriate concentration with air or other gases. The control system may be controlled by a detector unit placed in the protected space.
BACKGROUND OF THE INVENTION Bromotrifiuoromethane has long been employed as a fire extinguishing agent. Its high efficiency, low toxicity and light weight are significant factors when used in aircraft. On a weight-of-agent basis, this agent is more effective than carbon tetrachloride, carbon dioxide and chemicals of the bicarbonate of soda type. It is particularly advantageous for use against fires in delicate electrical, mechanical or electronic equipment as unlike dry powder types, it leaves no residue which in itself might be troublesome to remove in the post extinguishment stage, or which might damage equipment beyond salvage or operation.
Bromotriiiuoromethane, like carbon dioxide, is normally supplied as a liquified, compressed gas. It is especially useful as a fire extinguishing agent in total flooding types of fire extinguishing systems. A three to five percent concentration in air or other gases is sufficient to extinguish fires on contact or to eliminate any possibility of explosions of flammable atmospheres.
Effectiveness of the chemical agent alone, however, is only one key to an effective fire extinguisher. The agent must be properly applied, and the problem is not as simple as taking an extinguisher designed for carbon tetrachloride or carbon dioxide, for example, and simply replacing the agent with bromotrifiuoromethane. Experi ments have shown that to be effective in fixed fire extinguishing systems, bromotrifiuoromethane must 'be distributed thoroughly throughout the space to be protected in no less than a three to five percent concentration, and preferably within twenty seconds after detection of fire. Since bromotrifiuoromethane is about five times as heavy as air, vigorous mixing is required to achieve this disbursion in such a short time duration. Prior fire extinguishers have failed to solve this significant problem; it is a direct improvement upon the state-of-the-art to provide a fire extinguishing system which incorporates a diffuser arranged to mix a fire extinguishing agent such as bromo trifluoromethane and air or other gaseous elements in the protected space, so that the agent is thoroughly distributed,
utilizing, to the full, the energy readily available from the expansion of bromotrifiuoromethane as well as pressure in the supply system to achieve the mixing and distribution.
SUMMARY OF THE INVENTION In carrying out the principles of this invention according to one embodiment thereof, there is provided a diffuser which includes a nozzle having an attachment at one end for connection to a container of a pressurized fire extinguishing agent such as liquid bromotrifiuoromethane. The nozzle includes an orifice having a diameter adequate to regulate flow of the pressurized agent therethrough, and an expansion chamber, having a sufficient length and a diameter substantially greater than the diameter of the orifice, for expanding substantially all the fire extinguishing agent output of the orifice into a gaseous form and for accelerating the gaseous agent to near sonic velocity. The diffuser further includes an elongated tubular member having two open ends and a diameter substantially greater than the diameter of the expansion chamber. The tubular member is in axial alignment and positioned to receive the output of the expansion chamber whereby the extinguishing agent emitted from the expansion chamber may pass into and mix with air or other gaseous elements in the tubular member.
The diffuser in combination with a pressurized fire extinguishing agent source, a discharge valve for regulating the flow of the agent to the diffuser, and a fire detector for sensing the existence of a fire and for closing an electrical circuit to energize and open the discharge valve, form an eificient automatic flooding type fire extinguishing apparatus which is useful for protection of a substantially enclosed space such as an interior compartment of an aircraft.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a diagrammatic illustration of an automatic fire extinguishing system shown in use with aircraft;
FIG. 2 is a partially schematic diagram illustrating details of the present invention;
FIG. 3 is an enlarged fragmentary, partially pictorial illustration of the diffuser assembly used in the system shown in FIG. 1, and including a pair of diffusers;
FIG. 4 is a schematic diagram of a control system which may be used with the systemshown in FIG. 1; and
FIG. 5 illustrates a fire detector which may be used with the system shown in FIG. 4.
DESCRIPTION OF THE PRESENT EMBODIMENT There is shown in FIG. 1 an automatic, total flooding fire extinguishing system employed to protect aircraft interior compartments 10. There is shown a pressurized fire extinguishing agent supply assembly 12, a diffuser assembly 22, and a control system 18. The diffuser assembly 22 is placed in the aircraft interior compartment 10 and connected to the supply assembly 12 by a conduit 16. The control system 18 includes an electrically operated solenoid valve 20, which is positioned in the conduit 16, for controlling the delivery of the fire extinguishing agent from a casing 14 of the supply assembly 12 to the diffuser assembly 22. The diffuser assembly 22 distributes the fire extinguishing agent throughout the protected enclosures 10 by mixing the agent with air or other gaseous elements in the compartment 10.
Referring to FIG. 2, there is shown a fire extinguishing agent casing 14 adapted to contain, under pressure, a
fire extinguishing agent liquid bromotrifiuoromethane 24, and a discharge agent such as gaseous nitrogen 26. By virtue of being lighter than the liquid bromotrifluoromethane, the discharge agent, gaseous nitrogen, occupies the uppermost position within the container 14. A tube 28 extends down to the bottom of the container so that the gaseous nitrogen can force the liquid bromotrifluoromethane through a conduit or hose 16 which includes inlet and outlet portions, the inlet portion being connected to the tube 28. A conventional discharge valve 20, which may be manually or electrically operated, positioned in the conduit controls the delivery of bromotrifluoromethane therethrough.
In accordance with this invention, there is provided a diifuser 30 adapted to be connected to the discharge outlet of the hose 16. The diffuser 30 comprises a vaporizing nozzle 32 and an aspirator 34. The nozzle or expanding means 32 includes an end fitting 36 adapted to be con nected to the outlet of the hose 16, and an orifice 38 having a diameter adequate to regulate the flow of bromotrifluoromethane therethrough. The nozzle 32 further includes an expansion chamber 40, having a sufficient length and a diameter substantially greater than that of the orifice 38, for expanding the bromotrifluoromethane output of the orifice into gaseous form and for accelerating the bromotrifluoromethane to near sonic velocity. The expansion chamber 40 is arranged to discharge into the aspirator or mixing means 34 which is a hollow tube-like member having a diameter greater than the diameter of the expansion chamber 40. The aspirator includes open ends 42 and 44 with the open end 42 positioned to receive the output of the nozzle 32. Since the diameter of the aspirator 34 is greater than that of the expansion chamber 40, the open end 42 functions as an inlet for atmospheric air to enter the aspirator tube 34 for mixing with the extinguishing agent bromotrifluoromethane. The aspirator 34 is of sufiicient length to cause thorough mixing of the extinguishing agent with incoming air.
Thus, in operation, the pressurized liquid bromotrifluoromethane is directed to the nozzle 32, at which location, at least a major portion of the liquid bromotrifluoromethane vaporizes and accelerates to near sonic velocity as it expands, carrying the unvaporized portion of the bromotrifluoromethane with it. This output mixture of the nozzle 32 is directed to mix with air in the aspirator 34 and the mixture emitted therefrom is directed to a fire.
Laboratory experiments have shown that the time duration required for mixing and distributing the fire extinguishing agent bromotrifiuoromethane throughout an enclosure is directly related to the velocity of the bromotrifluoromethane as it leaves the nozzle 32, the relationship being that the higher the bromotrifluoromethane velocity, the shorter the required distribution time duration. Experiments have further indicated that the velocity of the bromotrifluoromethane as it leaves the nozzle 32 can be substantially increased by heating the liquid bromotrifluoromethane prior to its entrance to the nozzle 32. Generally indicated in FIG. 2 is a heater 46, provided to heat the liquid bromotrifluoromethane in the conduit 16 to a suitable temperature to achieve the desired bromotrifluoromethane velocity at the exit of the nozzle 32. The heater 46, the details of which are not part of this invention, is of conventional construction well known in the art, such as, for example, the type disclosed in US. Pat. No. 2,450,537, or preferably, the commercially available electric heating units which can be inserted into the conduit 16.
Referring to FIG. 3, which shows details of the ditfuser assembly 22 employed in the system shown in FIG. 1, there is shown identical diffusers 50 and 52 arranged to discharge in a direction opposite to each other so the discharge reaction forces would substantially cancel. The diffusers 50 and 52, constructed and operated substantially similar to the corresponding parts shown in FIG. 2 and described above, each comprises a vaporizing nozzle 54- 56. Each diffuser further includes an inverted L-shaped tubular member or aspirator 58-60. The aspirator 58 includes open ends 62A and 64A and the aspirator 60 includes open ends 62B and 64B. The fire extinguishing agent is delivered to the diffusers through the common conduit 16 which includes a divider or T 68. The identical aspirators are held to discharge in opposite directions by relatively rigid connecting members 70 and 72, while the nozzles 54 and 56 are mounted in proper relation to the aspirators by rigid conduit portions 16A and 16B. The entire diffuser assembly 22 is supported by a structural member 74 which is fixed to and vertically extended from a base 76. The base is a fiat, rigid T shape member fixedly secured to seat tracks 78 of the aircraft interior compartment 10. It has been found that if the aspirator 58-60 is mounted in proper relation to one of the surfaces of the space to be protected, for example, near a surface 80 of the aircraft interior compartment 10 as shown in FIG. 3, the effectiveness of the mixing of the agent bromotrifiuoromethane and air or other gaseous element is enhanced by an aspirator-like action in the protected enclosure. The air or other gaseous element in the enclosure and the 'bromotrifluoromethane tend to violently circulate within the protected space, thus the agent, bromotrifluoromethane, can reach a fire anywhere in the protected enclosure.
Referring to FIG. 4, which is a schematic diagram of the control system 18 employed in the system shown in FIG. 1, there is shown an electrically operated, conventional solenoid discharge valve 82 used to control the flow of extinguishing agent through the conduit 16, a battery 84 for supplying the power to energize the valve 82, and a fire detector 86 which functions as a switch and is located in the aircraft interior compartment 10. The solenoid valve 82 is connected at one terminal to a ground 88 and its other end to the detector or switch 86. The detector 8 6 is connected to the power source 84 which, in turn, is connected to the ground 88 to complete the circuit when the switch 86 is closed. In operation, when a fire is detected by the detector 86, it functions as a switch to close the electrical circuit to energize and open the discharge valve 82, thereby allowing the pressurized fire extinguishing agent bromotrifluoromethane to pass through the condiut 16 to the diffuser assembly 22 for mixing with air in the compartment 10.
Referring now to FIG. 5, which shows additional details of the fire detector 86 which may be used in the system shown in FIG. 1, there is shown a detector hav ing a detector tube 90', which is located in the aircraft interior compartment 10. When heated, the air in the tube 90 expands and the resultant pressure, via a copper tube 94, causes two bellows type diaphragms to make contact, thus closing the circuit shown in FIG. 4.
More specifically, the pressure created by heat in the protected area travels in opposite directions from the source of heat to the diaphrgams 95 through the detector tube 90. Each end of the tube 90 terminates at a compensator 92 through terminals 100. The compensator is a hollow closed cylinder of predetermined capacity used to compensate or cushion any sudden but momentary expansion of the air in the detector tube 90. From the compensators 92 the expanded air travels through the breathers 93, which are the devices that permit the expanded air in the detector tube and the compensators to be released to the outside atmosphere at a predetermined rate.
A slow gradual rise, or a sudden but momentary rise in temperature in the protected area, and the resulting expansion of air in the detector tube 90, will not cause the diaphragms 95 to make contact, since any moderate excess volume of air can be absorbed by the compensators 92 and gradually breathed out into the atmosphere. If an abnormal, continued rise in temperature, such as a fire would produce, causes the air to expand in the detector tube 90 faster than the compensators 92 can absorb it,
and faster than the breathers 93 can exhaust it, the builtup pressure travels through the insulator tubes 94, which lead from the compensator 92 and the breather 93 to each bellows type diaphragm 95. The pressure behind the two opposing diaphragms 95 forces them toward each other. Two platinum-faced contact points 96 are provided to facilitate contact and when the points 96 meet, the electrical circuit shown in FIG. 4 is closed, through connections 97, to energize and open valve 82 to allow the pressurized extinguishing agent to reach the diffuser assembly 22 for distribution.
While it is preferred to use the extinguishing agent bromotrifiuoromethane and discharge agent nitrogen as the two components of the present extinguisher, nevertheless, if desired, other agents having equivalent characteristics may be used.
I claim:
1. An apparatus comprising:
a first diffuser and a second diffuser, each of said diffusers including:
a nozzle having an attachment at one end for connection to a container of a liquefied, pressurized fire extinguishing agent, said nozzle having an orifice of a diameter adequate to regulate flow of said pressurized agent therethrough;
an expansion chamber forming a portion of said nozzle and having a length sufiicient to permit desired expansion of said agent and having a diameter substantially greater than the diameter of said orifice, said agent being substantially wholly converted to a gaseous form as emitted from said nozle and accelerated to near sonic velocity; and
an elongated tubular member having two open ends and a diameter substantially greater than the diameter of said expansion chamber, in axial alignment and positioned to receive the output of said expansion chamber whereby the high velocity output of said expansion chamber may pass into and mix with gaseous elements in said tubular member;
said first diffuser is positioned and arranged to discharge in a direction opposite to said second diffuser so that substantially all reaction forces will cancel upon a simultaneous discharge;
mounting means for maintaining the relative positions of said diffusers; and
common delivery means for delivering a liquified, pressurized fire extinguishing agent to said diffusers.
2. A fire extinguishing apparatus for protection of a substantially enclosed space, comprising:
a container for storing a fire extinguishing agent,
such as liquified bromotrifluoromethane, and a discharging agent, such as gaseous nitrogen, under pressure;
a conduit, having inlet and outlet portions and said inlet being connected to said container, for delivering the fire extinguishing agent from said container to a place of use;
a control unit having a discharge valve positioned in said conduit for controlling the passage of the fire extinguishing agent therethrough, and a fire detector, positioned in the substantially enclosed space, for providing an electrical output signal to open said discharge valve when fire is detected, thereby allowing the fire extinguishing agent to pass through said conduit;
heating means, connected to said conduit, for heating the fire extinguishing agent in said conduit to increase the energy available in the fire extinguishing agent resulting in higher agent velocity as it emits from said expansion chamber; and
a diffuser, connected to the outlet of said conduit,
for mixing the fire extinguishing agent with gaseous elements in the protected space, said diffuser includes:
a nozzle having an attachment at one end for connection to a container of a liquified, pressurized fire extinguishing agent, said nozzle having an orifice of a diameter adequate to regulate flow of said pressurized agent therethrough;
an expansion chamber forming a portion of said nozzle and having a length sufficient to permit desired expansion of said agent and having a diameter substantially greater than the diameter of said orifice, said agent being substantially wholly converted to a gaseous form as emitted from said nozzle and accelerated to near sonic velocity; and
an elongated tubular member having two open ends and a diameter substantially greater than the diameter of said expansion chamber, in axial alignment and positioned to receive the output of said expansion chamber 'whereby the high velocity output of said expansion chamber may pass into and mix with gaseous elements in said tubular member.
3. The apparatus of claim 2 wherein said diffuser is positioned and arranged to discharge in a direction opposite to a second diifuser of claim 2, so that substantially all reaction forces will cancel upon a simultaneous discharge;
mounting means for maintaining the relative positions of said diffusers; and
common delivery means for delivering the liquified, pressurized fire extinguishing agent to said diffusers.
U.S. Cl. XaR.
US755031A 1968-08-26 1968-08-26 Fire extinguishing apparatus Expired - Lifetime US3524506A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75503168A 1968-08-26 1968-08-26

Publications (1)

Publication Number Publication Date
US3524506A true US3524506A (en) 1970-08-18

Family

ID=25037427

Family Applications (1)

Application Number Title Priority Date Filing Date
US755031A Expired - Lifetime US3524506A (en) 1968-08-26 1968-08-26 Fire extinguishing apparatus

Country Status (1)

Country Link
US (1) US3524506A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830307A (en) * 1970-05-11 1974-08-20 Parker Hannifin Corp Fire prevention and/or suppression system
EP0054200A1 (en) * 1980-12-13 1982-06-23 Rheinmetall GmbH Process for at least temporarily shutting down an internal- combustion engine having an ambient-air intake
US4643260A (en) * 1985-09-26 1987-02-17 The Boeing Company Fire suppression system with controlled secondary extinguishant discharge
EP0234056A1 (en) * 1986-01-24 1987-09-02 The Boeing Company Fire extinguishment system for an aircraft passenger cabin
US5211246A (en) * 1989-05-30 1993-05-18 The Boeing Company Scouring method and system for suppressing fire in an enclosed area
US20050115722A1 (en) * 2003-12-02 2005-06-02 Lund Gary K. Method and apparatus for suppression of fires
US20050115721A1 (en) * 2003-12-02 2005-06-02 Blau Reed J. Man-rated fire suppression system
US20060283977A1 (en) * 2005-06-20 2006-12-21 Macdonald Leo S Novel cryogenic firefighting and hazardous materials suppression apparatus
US20090200046A1 (en) * 2005-06-20 2009-08-13 Macdonald Leo Spitz Novel cryogenic firefighting and hazardous materials suppression system
US20100307775A1 (en) * 2009-06-04 2010-12-09 Alliant Techsystems Inc. Gas-generating devices with grain-retention structures and related methods and systems
US8616128B2 (en) 2011-10-06 2013-12-31 Alliant Techsystems Inc. Gas generator
US8939225B2 (en) 2010-10-07 2015-01-27 Alliant Techsystems Inc. Inflator-based fire suppression
US8967284B2 (en) 2011-10-06 2015-03-03 Alliant Techsystems Inc. Liquid-augmented, generated-gas fire suppression systems and related methods

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2820418A (en) * 1954-04-02 1958-01-21 Gen Motors Corp Jet assembly for pumps
US2821257A (en) * 1955-12-09 1958-01-28 Fyr Fyter Co Non-corrosive bromochloromethane fire extinguisher composition and fire extinguishercontaining the composition

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2820418A (en) * 1954-04-02 1958-01-21 Gen Motors Corp Jet assembly for pumps
US2821257A (en) * 1955-12-09 1958-01-28 Fyr Fyter Co Non-corrosive bromochloromethane fire extinguisher composition and fire extinguishercontaining the composition

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830307A (en) * 1970-05-11 1974-08-20 Parker Hannifin Corp Fire prevention and/or suppression system
EP0054200A1 (en) * 1980-12-13 1982-06-23 Rheinmetall GmbH Process for at least temporarily shutting down an internal- combustion engine having an ambient-air intake
US4643260A (en) * 1985-09-26 1987-02-17 The Boeing Company Fire suppression system with controlled secondary extinguishant discharge
EP0234056A1 (en) * 1986-01-24 1987-09-02 The Boeing Company Fire extinguishment system for an aircraft passenger cabin
US4726426A (en) * 1986-01-24 1988-02-23 The Boeing Company Fire extinguishment system for an aircraft passenger cabin
US5211246A (en) * 1989-05-30 1993-05-18 The Boeing Company Scouring method and system for suppressing fire in an enclosed area
US7337856B2 (en) 2003-12-02 2008-03-04 Alliant Techsystems Inc. Method and apparatus for suppression of fires
US20110226493A1 (en) * 2003-12-02 2011-09-22 Alliant Techsystems Inc. Man rated fire suppression system and related methods
US20060278409A1 (en) * 2003-12-02 2006-12-14 Blau Reed J Man-rated fire suppression system and related methods
US9919173B2 (en) 2003-12-02 2018-03-20 Orbital Atk, Inc. Man-rated fire suppression system and related methods
US20050115722A1 (en) * 2003-12-02 2005-06-02 Lund Gary K. Method and apparatus for suppression of fires
US20080149352A1 (en) * 2003-12-02 2008-06-26 Alliant Techsystems Inc. Method and apparatus for suppression of fires
US8408322B2 (en) 2003-12-02 2013-04-02 Alliant Techsystems Inc. Man-rated fire suppression system and related methods
US7845423B2 (en) 2003-12-02 2010-12-07 Alliant Techsystems Inc. Method and apparatus for suppression of fires
US20050115721A1 (en) * 2003-12-02 2005-06-02 Blau Reed J. Man-rated fire suppression system
US20090200046A1 (en) * 2005-06-20 2009-08-13 Macdonald Leo Spitz Novel cryogenic firefighting and hazardous materials suppression system
US20060283977A1 (en) * 2005-06-20 2006-12-21 Macdonald Leo S Novel cryogenic firefighting and hazardous materials suppression apparatus
US20100307775A1 (en) * 2009-06-04 2010-12-09 Alliant Techsystems Inc. Gas-generating devices with grain-retention structures and related methods and systems
US8672348B2 (en) 2009-06-04 2014-03-18 Alliant Techsystems Inc. Gas-generating devices with grain-retention structures and related methods and systems
US8939225B2 (en) 2010-10-07 2015-01-27 Alliant Techsystems Inc. Inflator-based fire suppression
US8616128B2 (en) 2011-10-06 2013-12-31 Alliant Techsystems Inc. Gas generator
US8967284B2 (en) 2011-10-06 2015-03-03 Alliant Techsystems Inc. Liquid-augmented, generated-gas fire suppression systems and related methods
US9682259B2 (en) 2011-10-06 2017-06-20 Orbital Atk, Inc. Fire suppression systems and methods of suppressing a fire

Similar Documents

Publication Publication Date Title
US3524506A (en) Fire extinguishing apparatus
JP4190249B2 (en) Fire extinguishing system to extinguish a fire that occurred in the cabin or cargo compartment of a passenger aircraft
US3342271A (en) Foam plug generator
US3713491A (en) Fire protection apparatus
US3893514A (en) Suppression of fires in confined spaces by pressurization
JP5628980B2 (en) Fire suppression system
JP4031832B2 (en) Method and apparatus for ejecting liquid fire extinguishing agent in fire extinguishing equipment
US20100294518A1 (en) Hybrid inert gas fire suppression system
US6257341B1 (en) Compact affordable inert gas fire extinguishing system
ES2275494T3 (en) COMPACT, AFFORDABLE, FIRE EXTINGUISHING SYSTEM FOR INERT GAS.
US20130037282A1 (en) Expansion nozzle assembly to produce inert gas bubbles
WO1996032988A1 (en) Apparatus for providing a conditioned airflow inside a microenvironment and method
JP2017074379A (en) Fire suppression systems and method of adapting fire suppression systems
US6672397B2 (en) Breathable fire control system
US3605901A (en) Fire protection apparatus
US7028782B2 (en) System and method for suppressing fires
HRP20000779A2 (en) Method and high-capacity apparatus for producing fire fighting foam and foam expanding spreading device
US3402771A (en) Device for the production of physical fire-fighting foam having a high degree of foaminess
WO2017216851A1 (en) Fire extinguisher
US2287873A (en) Fire extinguishing apparatus
CZ291595A3 (en) Fire extinguishing device
JP6612173B2 (en) Fire extinguisher
RU2530410C1 (en) Mobile fire extinguisher
US2259501A (en) Fire-extinguishing method and apparatus
SU1430038A1 (en) Fire-fighting apparatus