The subject matter disclosed herein relates to a fire extinguisher actuator. More specifically, the subject matter disclosed relates to a fire extinguisher actuator that activates the release of a fire extinguishing agent.
In an aircraft environment, hermetically sealed fire extinguishers are typically activated by direct explosive impingement energy using a pyrotechnic trigger device, such as a pyrotechnic cartridge or squib. The impingement energy is focused on a dome-shaped fire extinguisher outlet burst disc such that the fire extinguisher outlet burst disc will rupture as a result of the impingement. The fire extinguisher outlet burst disc is typically fabricated from corrosion resistant steel. Normally, the pyrotechnic trigger device is retained in a discharge head in such a manner that it directly faces the fire extinguisher outlet burst disc. The discharge head is attached to an outlet of the fire extinguisher and is typically used to direct the flow of extinguishing agent to an aircraft interface, such as plumbing or tubing, which directs the extinguishing agent to a desired location. A filter screen is located within the discharge head to catch any large fire extinguisher outlet burst disc fragments created as a result of the explosive impingement energy.
The use of pyrotechnic trigger devices can be effective; however, pyrotechnic trigger devices require special handling procedures and training that add to overall aircraft management and maintenance costs. Additionally, pyrotechnic trigger devices may have a limited expected life span and thus require periodic replacement.
According to one aspect, a fire extinguisher actuator assembly for a fire extinguisher is provided. The fire extinguisher includes a fire extinguisher reservoir and a fire extinguisher outlet burst disc that forms a discharge barrier between the fire extinguisher reservoir and a discharge head to retain a pressurized fire extinguishing agent at an internal fire extinguisher pressure within the fire extinguisher reservoir. The fire extinguisher actuator assembly includes a cutter detained within the fire extinguisher proximate the fire extinguisher outlet burst disc. The fire extinguisher actuator assembly also includes an interior container within the fire extinguisher reservoir, the interior container having a container pressure and sealed with a container burst disc. The fire extinguisher actuator assembly further includes an activation device having a piercing member. The activation device is operable to pierce the container burst disc and diffuse the container pressure to create a pressure differential relative to the internal fire extinguisher pressure at the cutter, thereby driving the cutter through the fire extinguisher outlet burst disc to release the pressurized fire extinguishing agent through the discharge head.
According to another aspect, a method of installing a fire extinguisher actuator assembly in a fire extinguisher is provided. The fire extinguisher includes a fire extinguisher reservoir and a fire extinguisher outlet burst disc that forms a discharge barrier between the fire extinguisher reservoir and a discharge head to retain a pressurized fire extinguishing agent at an internal fire extinguisher pressure within the fire extinguisher reservoir. The method includes detaining a cutter within the fire extinguisher proximate the fire extinguisher outlet burst disc. An interior container is placed within the fire extinguisher reservoir, where the interior container has a container pressure and is sealed with a container burst disc. An activation device including a piercing member is positioned within the fire extinguisher. The activation device is operable to pierce the container burst disc and diffuse the container pressure to create a pressure differential relative to the internal fire extinguisher pressure at the cutter, thereby driving the cutter through the fire extinguisher outlet burst disc to release the pressurized fire extinguishing agent through the discharge head.
The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
In an exemplary embodiment, a fire extinguisher actuator assembly for a fire extinguisher is provided that is activated without a pyrotechnic trigger device. The fire extinguisher actuator assembly includes a two-part activation and release of a pressurized fire extinguishing agent using an activation device in combination with a cutter driven by rapid pressure diffusion. The activation device pierces a container burst disc of an interior container within a fire extinguisher reservoir, where the interior container and the fire extinguisher reservoir have different pressures. A change in pressure upon opening the interior container causes pressure diffusion which results in a pressure differential at the cutter to drive it through a fire extinguisher outlet burst disc. Using a cutter to rapidly open a fire extinguisher outlet burst disc of a fire extinguisher may remove the need to include a debris screen in a discharge head of the fire extinguisher system, as loose fire extinguisher outlet burst disc fragments typically resulting from pyrotechnic trigger device ignition are no longer present.
Turning now to
The interior container 215 within the fire extinguisher reservoir 106 is hermetically sealed by a container burst disc 219 to keep a container pressure 221 isolated from the internal fire extinguisher pressure 214 until the container burst disc 219 is ruptured. The interior container 215 may also include a pressure transducer 223 operable to monitor the container pressure 221 of the interior container 215. The container pressure 221 is nominally sealed at about one atmosphere of pressure (101.3 kPa) at 70 degrees F. (21.1 degrees C.).
The fire extinguisher actuator assembly 200 also includes an activation device 220 having a piercing member 222 (
A support collar 227 can retain the container support tube 225 within the fire extinguisher reservoir 106. The support collar 227 can also serve as a detaining surface for one of the flexible seals 210 used to detain the cutter shuttle assembly 202. The cutter shuttle assembly 202 may also be detained by another of the flexible seals 210 installed between the shuttle body 206 and the container support tube 225. The shuttle body 206 may also include a ledge 229 upon which the internal fire extinguisher pressure 214 is applied from the main interior region 218 of the fire extinguisher reservoir 106. Until the activation device 220 is triggered, the pressure equalization region 208 contains pressurized fire extinguishing agent 212 at the internal fire extinguisher pressure 214. As the pressurized fire extinguishing agent 212 exits the pressure equalization region 208, the internal fire extinguisher pressure 214 in the main interior region 218 overcomes the detaining force of the flexible seals 210 and drives the cutter shuttle assembly 202 toward the fire extinguisher outlet burst disc 108 where the cutter 204 cuts the fire extinguisher outlet burst disc 108 open to discharge the pressurized fire extinguishing agent 212 from the main interior region 218 of the fire extinguisher reservoir 106 out of the discharge head 104.
As will be understood, the fire extinguisher actuator assembly 200 can include other structure elements to support and stabilize the interior container 215 and the activation device 220, as well as electrical connections, which are not depicted to simplify the drawings. Also, not shown for drawing simplicity, is that the shuttle body 206 is restrained internally so it cannot become a projectile if the fire extinguisher 102 is inadvertently discharged while the discharge head 104, or other protective device, is not in place at the time of the inadvertent discharge. The fire extinguisher reservoir 106 can be sized to accommodate a wide variety of installations. For example, the fire extinguisher reservoir 106 can range in size from 40 cubic inches (655.5 cm3) to 2,500+ cubic inches (40,968+ cm3). Pressure changes within the fire extinguisher reservoir 106 can occur due to ambient temperature variations. For example, in an aircraft environment, the fire extinguisher 102 may be at 240 degrees F. (115.6 degrees C.) on the ground on a hot day and after takeoff be at −65 degrees F. (−53.9 degrees C.) at altitude. These temperature changes cause substantial changes to the internal fire extinguisher pressure 214. As changes occur to the internal fire extinguisher pressure 214, pressure equalization holes 216 (
A volume-pressure equation (equation 1) can be used to calculate pressure values when the volume of the interior container 215 and the combined volume of the container support tube 225 and pressure equalization region 208 are known. In equation 1, P1, V1, and T1 are starting values of pressure, volume, and temperature; and P2, V2, and T2 are ending values of pressure, volume, and temperature.
P1×V1=(T1×P2×V2)/T2 (equation 1)
Since the transition of pressure occurs rapidly (e.g., less than 20 milliseconds), the effects of temperature can be eliminated. This yields equation 2, which can be used to predict the final value of the container pressure 221 after diffusion upon piercing the container burst disc 219.
P2=(P1×V1)/V2 (equation 2)
With reference to
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments. Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
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