The instant invention relates to air deployment of an inflatable device and in particular to a water activated inflator for use in an air deployable device and a method of air deployment using the same.
There is a continuing need for development of methods of accurately dropping inflatable devices from an aircraft, for example, life rafts to survivors in a body of water. The most advanced method, presently in use, is dropping an inflatable device in a deployment container using a parachute and a timer as disclosed, for example, in U.S. Pat. No. 4,639,229. Use of the parachute substantially ensures correct orientation of the container on impact with the body of water and a predetermined range of speed at impact through aerodynamically braking the descent of the container. After impact the container is partially or completely submerged in the water, bobbing in the water and then floating on the surface until the device is inflated. Using a timer, the inflation is initiated after a preset time interval elapses, predetermined at time of manufacturing the inflatable device based on an expected altitude of an aircraft flying above the water surface such that the inflation starts shortly after impact of the container on the body of water. However, the exact timing for initiating the inflation is a major problem of the method of air deployment using a timer. If the inflation is initiated too early, the device is inflated while still in the air resulting in the inflated device being blown away from a target zone in the presence of wind—even at a relatively small wind speed. On the other hand, if the inflation is initiated too late the container is floating on the surface for a considerable amount of time reducing the likelihood of the device being inflated in its proper orientation. In most rescue operations survivors have to be rescued from rough seas. Under such conditions it is likely for a container to be toppled by the rough sea while floating on the surface resulting in the device being inflated upside down rendering it problematic for rescuing survivors. One solution to this problem is the use of a reversible life raft as taught in U.S. Pat. No. 6,375,529. However, use of a reversible life raft requires physical action from survivors—people in distress—in order to set up a canopy for protecting them from the elements. In particular, for rescue operations in cold climates it is essential to provide life rafts with a canopy in order to protect survivors from hypothermia.
Auto-inflation of life vests and other personal floatation devices using water activated inflators is known in the art. Water activated inflators using a water soluble element for holding a membrane piercing mechanism in a cocked position are disclosed, for example, in U.S. Pat. Nos. 6,589,087; 5,852,986; 5,694,986; 5,370,567; and 5,333,656.
In order to quickly inflate a large floatation device such as a life raft, a large gas flow is needed. Therefore, the inflator has to quickly open a sealing mechanism of a gas cylinder containing a large volume of gas under high pressure. In order to quickly and reliably create a large opening, it is preferred to provide a sufficient stroke to a valve—defining the opening—of the sealing mechanism, rather than piercing a sealing membrane. However, for providing a sufficient stroke a relatively strong force acting along a relatively long distance is applied. Timed actuators, explosive actuators, and electronic actuators are typically used to provide the force and distance required in inflating a large inflatable device. As is evident to those of skill in the art, such devices cause serious storage and maintenance problems as well as safety problems during transport in an aircraft and, therefore, are not considered useful for air rescue missions. Conversely, none of the passive water activated devices provide for the force and distance of operation required for quickly and reliably inflating a life raft.
It would be advantageous to provide a passive water activated device for supporting inflation of a life raft.
In accordance with an embodiment of the present invention there is provided a water activated inflator comprising:
a gas cylinder opening device for opening a sealing mechanism of a gas cylinder, the gas cylinder opening device being disposed at least partially within a housing and being movable between a cocked position and a fired position along a first axis having a first orientation relative to the housing;
a tension mechanism in mechanical communication with the housing and the gas cylinder opening device for providing tension acting along the first axis for moving the gas cylinder opening device from the cocked position to the fired position;
a plunger for holding the gas cylinder opening device in the cocked position, the plunger being disposed in the housing and movable between a first position and a second position along a second axis having a second different orientation relative to the housing;
a water soluble element for holding the plunger in the first position through mechanical communication along the second axis with the plunger and the housing;
a conduit for providing water to the water soluble element;
a first interacting element in mechanical communication with the gas cylinder opening device having a first interacting surface, wherein a portion of the first interacting surface is disposed at a predetermined angle other than 90 or 180 degrees to the first axis; and,
a second interacting element in mechanical communication with the plunger having a second interacting surface for interacting with the first interacting surface at the predetermined angle when the plunger is in the first position for holding the gas cylinder opening device in the cocked position, wherein the predetermined angle is determined such that a component along the second axis of a component of the tension acting onto the second interacting surface is within a predetermined range for ensuring structural integrity of the water soluble element in the cocked position and for ensuring movement of the plunger when a portion of the water soluble element is dissolved.
In accordance with an embodiment of the present invention there is further provided a water activated inflatable device comprising:
an inflatable device body;
a gas cylinder connected to the inflatable device body; and,
a water activated inflator for opening a sealing mechanism of the gas cylinder, the water activated inflator comprising:
a gas cylinder opening device for opening a sealing mechanism of a gas cylinder, the gas cylinder opening device being disposed at least partially within a housing and being movable between a cocked position and a fired position along a first axis having a first orientation relative to the housing;
a tension mechanism in mechanical communication with the housing and the gas cylinder opening device for providing tension acting along the first axis for moving the gas cylinder opening device from the cocked position to the fired position;
a plunger for holding the gas cylinder opening device in the cocked position, the plunger being disposed in the housing and movable between a first position and a second position along a second axis having a second different orientation relative to the housing;
a water soluble element for holding the plunger in the first position through mechanical communication along the second axis with the plunger and the housing;
a conduit for providing water to the water soluble element;
a first interacting element in mechanical communication with the gas cylinder opening device having a first interacting surface, wherein a portion of the first interacting surface is disposed at a predetermined angle other than 0 or 90 degrees to the first axis; and,
a second interacting element in mechanical communication with the plunger having a second interacting surface for interacting with the first interacting surface at the predetermined angle when the plunger is in the first position for holding the gas cylinder opening device in the cocked position, wherein the predetermined angle is determined such that a component along the second axis of a component of the tension acting onto the second interacting surface is within a predetermined range for ensuring structural integrity of the water soluble element in the cocked position and for ensuring movement of the plunger when a portion of the water soluble element is dissolved.
In accordance with another embodiment of the present invention there is provided a method of air deployment of a water activated inflatable device comprising:
providing from an aircraft over a body of water a deployment container comprising an inflatable device body, a gas cylinder connected to the inflatable device body and a water activated inflator for opening a sealing mechanism of the gas cylinder;
deploying a parachute attached to the deployment container for aerodynamically braking the descent of the deployment container and for providing a predetermined orientation of the deployment container at impact on the body of water;
activating the water activated inflator through contact with water after impact of the deployment container on the body of water;
using the water activated inflator, pulling a sealing mechanism of the gas cylinder for opening the same; and,
inflating the inflatable device body.
In accordance with the other embodiment of the present invention there is further provided a water activated inflatable device for air deployment over a body of water comprising:
an inflatable device body;
a gas cylinder connected to the inflatable device body;
a water activated inflator for opening a sealing mechanism of the gas cylinder, the water activated inflator comprising a gas cylinder opening device attached to the sealing mechanism of the gas cylinder for opening the gas cylinder by pulling the sealing mechanism;
a deployment container containing the inflatable device body, the gas cylinder and the water activated inflator, the deployment container comprising a conduit for enabling provision of water to the water activated inflator after impact of the deployment container on the body of water; and,
a parachute attached to the deployment container for aerodynamically braking the descent of the deployment container and for providing a predetermined orientation of the deployment container at impact on the body of water.
Exemplary embodiments of the invention will now be described in conjunction with the following drawings, in which:
a and 1b are simplified block diagrams schematically illustrating a water activated inflator according to an embodiment of the invention;
c and 1d are simplified block diagrams schematically illustrating a connection of the water activated inflator shown in
e and 1f are simplified block diagrams schematically illustrating a connection of an embodiment of the water activated inflator shown in
g is a simplified block diagram schematically illustrating a detail of the water activated inflator shown in
a to 2c are simplified block diagrams schematically illustrating various embodiments of interacting elements of the water activated inflator according to the invention;
The following description is presented to enable a person skilled in the art to make and use the invention, and is provided in the context of a particular application and its requirements. Various modifications to the disclosed embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be applied to other embodiments and applications without departing from the scope of the invention. Thus, the present invention is not intended to be limited to the embodiments disclosed, but is to be accorded the widest scope consistent with the principles and features disclosed herein.
Referring to
Alternatively, the inflator 100 is used in combination with a gas cylinder having an opening mechanism attached thereto, as shown in
The gas cylinder opening device 106 is movable along the first axis 108 between the cocked position, shown in
a to 2c illustrate alternative embodiments comprising various combinations of spherical and conical surfaces. However, the embodiment shown in
In operation the inflator 100 is connected, for example, via connecting mechanism 104 to the T-section 154 mounted to the neck of a gas cylinder with the gas cylinder opening device being connected to the sealing mechanism of the gas cylinder. During storage and transport of an inflatable life raft the inflator 100 is in the cocked position with the tension mechanism 110 under compression and held in this position by the plunger 120, as shown in
The water activated inflator 100 according to an embodiment of the invention is beneficial for air deployment of a life raft by providing a safe, reliable, compact, light weight and simple apparatus which is cost effective to manufacture. It allows use of a simple water soluble element as trigger in a device providing strong force acting along a large distance. Furthermore, the device is easily adaptable to a different stroke by only adjusting the angle α of the interacting surface allowing use of substantially same parts of the inflator for different applications.
Referring to
Referring to
Hereinbelow, a method of air deployment of a water activated inflatable device over a body of water according to an embodiment of the invention will be described. For example, a water activated inflatable device 300 as described above is employed for executing the method. The water activated inflatable device 300 is dropped from an aircraft over a body of water in a target zone where survivors are suspected. After dropping the water activated inflatable device 300 from the aircraft pulling action on pull cord 316 pulls the folded parachute 314 from the deployment container 302 for deployment through interaction with the airflow around the falling deployment container 302. Pulling action on pull cord 310 removes the safety pin from the inflator 312. Alternatively, a same pull cord is used for deploying the parachute as well as for removing the safety pin. The water activated inflatable device 300 is deployed in various different ways, for example, by release from a loading bay of a transport aircraft such as for instance an airplane or helicopter, or from a release mechanism mounted to the outside of an aircraft at the fuselage or under a wing. Deployment of the parachute provides aerodynamically braking of the descent of the water activated inflatable device 300 and ensures a predetermined orientation of the deployment container 302 at impact on the body of water. After impact, the deployment container 302 is first immersed in the body of water, then bobbing in the water and finally floating on the water surface. After impact water is provided through the conduit 308 to the inflator, dissolving a water soluble element of the inflator. After a portion of the water soluble element is dissolved the tension mechanism of the inflator is capable of pushing the plunger and, thus, moving the gas cylinder opening device for providing a sufficient stroke to the sealing mechanism of the gas cylinder. Using the water activated inflator 100 a large opening of the gas cylinder is provided quickly after dissolving a portion of the water soluble element enabling quick inflation of the inflatable device body 304. The inflator 312 and conduit 308 are, for example, placed such that the water soluble element is exposed to water within a short time interval after impact. The deployment container 302 is opened prior inflation of the inflatable device 304 through the force acting at impact or using an opening mechanism activated by the inflator. Alternatively, the deployment container 302 is opened through expansion of the inflating device 304.
Using a water activated inflatable device according to an embodiment of the invention is beneficial for air rescue operations over a body of water. The water activated inflator provides proper timing of the inflation shortly after impact independent of the height of the air plane at the time instant the water activated inflatable device is dropped substantially increasing the likelihood of proper placement of the inflatable device in a target zone as well as substantially increasing safety of the rescue personnel in the aircraft. Since most rescue operations are executed under severe weather conditions, employment of prior art rescue kits using, for example, timing devices, either puts the lives of the rescue personnel in the aircraft at risk by requiring the pilot to fly the aircraft at dangerous heights—below or within a cloud cover for example—for dropping the rescue kit at a given height or substantially reducing the likelihood of proper deployment of the rescue kit by dropping it from a height considered safe by the pilot. Employment of the method of air deployment according to the invention overcomes this dilemma by enabling dropping of the rescue kit from an arbitrary safe height for the aircraft and still providing proper deployment and inflation of the life raft.
Executing numerous drop tests, it has been found that the method for air deployment according to an embodiment of the invention ensures a high success rate for deployment and inflation of the inflatable device. The likelihood of inflation of the life raft upside down has been substantially reduced despite the fact that after impact the rescue kit is immersed in water and then bopping prior inflation.
Numerous other embodiments of the invention will be apparent to persons skilled in the art without departing from the spirit and scope of the invention as defined in the appended claims.
Number | Date | Country | |
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60566170 | Apr 2004 | US |
Number | Date | Country | |
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Parent | 11115174 | Apr 2005 | US |
Child | 12213420 | US |