This application is related to co-pending patent application entitled “BUOYANCY DISSIPATER AND METHOD TO DETER AN ERRANT VESSEL” filed Jan. 30, 2009 having Ser. No. 12/362,547 which is incorporated herein by reference.
This application is related to co-pending patent application entitled “BUOYANCY DISSIPATER AND METHOD TO DETER AN ERRANT VESSEL” filed Feb. 2, 2010 having Ser. No. 12/698,611 which is incorporated herein by reference.
This application is related to patent application entitled “VORTICE AMPLIFIED DIFFUSER FOR BUOYANCY DISSIPATER AND METHOD FOR SELECTABLE DIFFUSION” filed concurrently herewith and which is incorporated herein by reference.
Embodiments pertain to inhibiting movement of vessels by buoyancy reduction of water. Some embodiments pertain to bubble weapons and systems of bubble weapons. Some embodiments pertain to the use of bubble plumes to inhibit the effectiveness of sonar systems to protect ships from torpedoes and to locate enemy submarines.
There are currently general needs to protect ships as well as fixed assets and critical locations, such as dams and harbors, from errant vessels. These needs include the ability to disrupt operations of the errant vessel or inhibit movement of the vessel while ensuring non-lethality.
Thus, there are general needs for inhibiting movement of vessels and weapons configured to inhibit movement of vessels or disrupt operations of vessels. There are also general needs for inhibiting the effectiveness of sonar systems for protecting ships from torpedoes and for locating enemy submarines.
The following description and the drawings sufficiently illustrate specific embodiments to enable those skilled in the art to practice them. Other embodiments may incorporate structural, logical, electrical, process, and other changes. Portions and features of some embodiments may be included in, or substituted for, those of other embodiments. Embodiments set forth in the claims encompass all available equivalents of those claims.
In some embodiments, the bubble weapon may include a diffuser section to generate the plume 103 of bubbles. The diffuser may be a configurable diffuser section. When a configurable diffuser section is used, the configurable diffuser section may be configured in a thrust-neutral configuration to provide neutral thrust. The neutral thrust may offset any thrust generated during the generation of the plume 103, thereby allowing the bubble weapon to remain stationary. In other embodiments, discussed in more detail below, the configurable diffuser section may be configured in a thrust-engaged configuration. When configured in the thrust-engaged configuration, the configurable diffuser section may provide thrust to the bubble weapon to allow the bubble weapon to move through the water.
As illustrated in
Embodiments described herein are not limited to the use of a bubble weapon to generate a bubble plume, but are applicable to the generation of a bubble plume using any pressurized gas source. For example, compressed air may be used. For defense of many stationary targets, a gas can be deployed to a release location via a pipe. For fixed assets, such as dams and harbors, a ground-based compressor and a pipe may also be used. In some embodiments, a ship's onboard compressor can also act as a source of gas to generate a bubble plume.
In the embodiments illustrated in
To achieve a tangential collision, the large plume 203A may be released asymmetric to the traveling vector 201 of the vessel 204 and the large plume 203A may be large enough that greater than half of the vessel's length and beam enters the plume. Alternatively, the ribbon plume 203B of bubbles may be configured to transverse the traveling vector 201 of the vessel at an angle. The depth of the bubble plume may also be configured for capsizing the vessel. The submerged portion of the vessel 204 may have buoyancy restored when it leaves or dives beneath the bubble plume. This action will lift the vessel toward the surface.
In some of these embodiments, one or more bubble weapons are configured to selectively submerge either the bow or stern of the vessel. In these embodiments, if the vessel 204 is of significant length, the submerged section of the vessel 204 may be deep enough to be crushed or ruptured when the bubble plume dissipates.
In these embodiments, the configurable diffuser section may be configured in the thrust-neutral configuration. In these embodiments, the array of bubble weapons 302 may be configured for protection of fixed assets such as harbors or dams. The location of each of the bubble weapons 302 may be fixed by a tether 304, although this is not a requirement. These embodiments may allow assets such as high traffic areas, harbors and dams to have permanent bubble weapon systems installed on the critical perimeters.
In some embodiments, one or more of the bubble weapons 302 may be discharged under an errant vessel, swamping it in before it crosses a border or into a critical perimeter. To help ensure non-lethality, the bubble weapon system 300 may be operated for two configurations, one configuration for open cabin craft and another configuration for closed cabin craft. For the open cabin craft, the bubble weapons 302 may be used without rigor because swamping a vessel and ejecting the crew by a sudden loss of forward momentum may put the crew in the water and normal buoyancy may return as soon as the bubble plume has passed. For closed cabin craft, asymmetric loading may be used. Embodiments that apply asymmetric loading to vessels are discussed in more detail below.
In some of these embodiments, each of bubble weapons 302 may include a proximity sensor to sense a vessel and discharge under or below the vessel based on the vessel's proximity before the vessel crosses a critical perimeter. In some alternate embodiments, each of bubble weapons 302 may be signaled to discharge by a control signal provided a system controller external to the bubble weapons 302.
In these embodiments, the configurable diffuser section may be configured in either the thrust-engaged configuration or the thrust-neutral configuration depending on the target. As illustrated in
As illustrated in
As illustrated in
In the embodiments illustrated in
In these embodiments, the configurable diffuser section may be configured in either the thrust-engaged configuration or the thrust-neutral configuration, depending on the target. For example, in these embodiments, the location of the enemy sub 508 may be determined from triangulation techniques. The length, breadth, orientation, radius and other information about the enemy sub 508 may be calculated from the refractive dispersion. In these embodiments, the one or more vessels 504 may transmit the received spectral characteristics of sound signals 509 to a central location for processing. In these embodiments, a data analysis for processing the spectral and phase characteristics of sound signals 509 may include performing Doppler shift corrections.
In these embodiments, the bubble weapons 602 create thrust by streaming bubbles from a nozzle that is part of the configurable diffuser section. Through the use of thrust, the one or more bubble weapons 602 may be located very accurately and the size of the bubble plume 603 may be controlled. Bubble weapon 602 may place the bubble plume 603 in a location to controllably disperse the buoyancy of the water under the moving vessel 604. In this way, the bow or stern may be selectively sunk. This may cause the moving vessel 604 to pitch down at the bow with a bow plume or pitch up with a stern plume. In these embodiments, the configurable diffuser section may be configured in either the thrust-engaged configuration or the thrust-neutral configuration depending on the target.
In some embodiments, to stop an errant closed cabin vessel, one or more bubble weapons may be configured to cause the moving vessel 604 to pitch down, driving the bow into the water. As illustrated in
In the embodiments illustrated in
In these embodiments, a sudden and dramatic loss of counter force on the vessel's propulsion system would result in several effects. It may reduce overall thrust and power output, slowing the vessel. Loss of coupling may also over rev the engines forcing the power train to reduce output or risk over speeding the engine and possibly destroying it. For many large vessels, powering down and then returning to full power requires a significant period of hysteresis. For many vessels, a rapid loss of power may damage the power train.
In some embodiments, the one or more bubble weapons 802 may be configured to generate a pulsed-bubble plume that is streamed into the propeller 805. In these embodiments, the pulsed-bubble plume may cause a hammering effect to the propellers and drive train that would compel any reasonable engineer to shut down power to avoid catastrophic failure.
When a bubble plume asymmetrically flows into a propeller, a torque, pivoting about the asymmetric axis, is applied to the propeller 805. The difference in forces on one side of the propeller 805 versus the other will be between 500-1000 times. This torque may be tremendous and it may be applied in a vector that the propeller shaft and bearings are not designed for, which may tend to shear off the propeller from its shaft. If the propeller 805 survives this attack, the asymmetric load on the propeller may cause a further hammering effect on the propeller. Each time a propeller blade leaves and enters the bubble stream, the differential loading may hammer the propeller and the synergy of these forces may damage the propeller shaft and bearings or force a quick shutdown of the engine.
In some embodiments, the system may be configured to neutralize a vessel's thrust without damaging the power train by throttling the bubble weapons output. This may allow the power system of the vessel 804 to slowly accelerate into an over-speed condition and reduce the thrust of the vessel 804.
In some embodiments, these effects may be applied to make the thrust of the vessel 804 asymmetric. On multi-propeller ships, one propeller can be bubbleized which may cause the other propeller to generate greater thrust, causing the vessel 804 to turn away from the higher thrust propeller. On single propeller vessels, bubbles may be throttled into one side of the propeller, causing an unperturbed side of the propeller to have greater thrust. In these embodiments illustrated in
In some embodiments, one or more bubble weapons may be configured to generate the plume of bubbles under a sonar transducer of the vessel 804 to disrupt a sonar power output of the sonar transducer. In these embodiments, the configurable diffuser section may be configured in either the thrust-engaged configuration or the thrust-neutral configuration depending on the target. In these embodiments, a bubble weapon 802 may be deployed so that the bubble plume may come into physical contact with a vessel's sonar transducer. When the acoustic power from the transducer into the water is disrupted, the output power from the transducer may not flow as efficiently from the transducer into the surrounding water. If this energy remains within the transducer, the transducer may be shut off or destroyed. In some embodiments, when bubbles are released slowly over time, a low density of bubbles may cause refractive disruptions of the transducer water interface. This refractive discontinuity may cause phase deviations and spectral dispersions of the sonar waves, thus increasing the noise of the system.
As illustrated in
A torpedo is generally neutrally buoyant in water, but it is not neutrally buoyant when in the bubble plume 903. Several effects will occur when the bubble plume 903 is released ahead of a torpedo. As illustrated in
As further illustrated in
In some embodiments, the system of one or more bubble weapons 902 may be configured to provide a defense against high speed cavitating torpedoes. Since bubbleized water has a greatly different density than the surrounding water, when the cavitating torpedo hits this water, the displacement drag of the weapon may drop proportionally (e.g., 500-1000 times). This may cause a dramatic acceleration in the torpedo. When the torpedo 905 passes through the bubble plume 903, it will have a directly proportional deceleration. Given the short time of transit through the bubble plume, a hammering effect upon the torpedo 905 may result. This impulse may be great enough to damage the structure of the torpedo 905, which may also damage gyros and navigation systems of the torpedo 905.
In these embodiments illustrated in
In these embodiments, the bubbles emitted from the bubble weapon 1002 may comprise a non-conductive gas such as carbon dioxide. Since the water is conductive, when the nonconductive gas slides through the water, a static charge may build up that rises with the bubbles of the plume 1003. The motion of the charge may be viewed as current resulting in the magnetic field 1005 that is circulating around the bubble plume 1003 (i.e., per the right-hand rule). The magnetic field 1005 may be utilized for naval purposes. For example, the magnetic field 1005 may be used to jam or confuse various electronic warfare operations as it may affect circuits that are not shielded in a Faraday cage. The magnetic field 1005 may also be used to magnetize the hull of an enemy ship, such as vessel 1004. Once a ship's hull has been magnetized, it may be more easily identified by common galvanometer techniques. To eliminate the magnetic signature on the vessel 1004, the vessel 1004 may need to return to port and undergo an extensive and expensive degaussing procedure. In these embodiments illustrated in
In some embodiments, the configurable diffuser section 1102 may be further configurable by the diffuser control circuitry 1104 to generate spin to spin-stabilize the bubble weapon, configured for generating a predetermined size of the bubbles of the bubble plume, and configured for generating a streaming plume by varying a rate of bubble generation. In these embodiments, diffuser control circuitry 1104 may be configured to control the reaction pressure within the reaction chamber to control the burn rate of the propellant 1108. In these embodiments, the amount of thrust, the amount of spin, the size of the bubbles, the size of the bubble plume and the rate of bubbles of the streaming plume may be varied by the configurable diffuser section 1102.
In some embodiments, the bubble weapon 1100 may also include propellant charge-size control circuitry 1106 to vary a charge size to control an amount of the propellant 1108 that is ignited in order to vary an amount of gas generated when generating the bubble plume. In some embodiments, the bubble weapon 1100 may also include control circuitry 1110 to control the operations of the bubble weapon 1100. In some embodiments, the bubble weapon 1100 may also include one or more optional proximity sensors 1112 to detect the proximity of a vessel for detonation or intelligence. In some embodiments, the bubble weapon 1100 may also include an on-board navigation system 1114 and its accompanying sensors for use in navigating the bubble weapon 1100 through water. In some embodiments, the bubble weapon 1100 may also include a wireless or wired receiver 1116 for receiving command and control signals. In some embodiments, the bubble weapon 1100 may also include a transceiver, to transmit images, location or other data.
In response to a discharge signal 1107, the propellant 1108 may be ignited within a pressure vessel section and discharged into the configurable diffuser section 1102 to generate an expanding gas bubble or a bubble plume. In some embodiments, the discharge signal 1107 may ignite a selected portion of the propellant 1108 to control the amount of gas that is generated. The size and the type of the expanding gas bubble or bubble plume may be based on the configuration selected for the configurable diffuser section 1102 as well as the amount of propellant 1108 that is selected. The configurable diffuser section 1102 may also be configured to utilize the energy of the ejected gas to thrust the weapon for navigation.
In some other embodiments, one or more bubble weapons 1100 may be configured for anoxic pressure discharge into a large volume. In these embodiments, a bubble weapon 1100 may be positioned near an air-intake of an engine of an errant vessel and may discharge an anoxic gas. The anoxic gas may cause the engine to stall. The discharge rate of the gas may be selected based on the engine. In these embodiments, the configurable diffuser section 1102 may be configured in the thrust-neutral configuration. In these embodiments, a bubble weapon 1100 may be used as a source of high-pressure high-volume gas. This gas may be carbon-dioxide and other trace reaction products. In these embodiments, the bubble weapon 1100 may be placed in the intake of an errant ship. Placement may be by means of a delivery vehicle or by special troops. Discharged, the anoxic gas may quench the engine. The discharge rate of the bubble weapon may be adjusted for the capacity and type of target engine.
In some other embodiments, a bubble weapon 1100 may be deployed inside a vessel. A burst deployment of the bubble weapon 1100 very rapidly raises the barometric pressure inside the vessel, which may disable the crew and the ship's systems. Pressure operated systems on the vessel may go into a failure mode because reference pressures went well out of limits. The build-up in pressure within the vessel may cause other effects to the hull, such as blowing out windows and doors and/or blowouts of hull walls. In these embodiments, because the bubble weapon's gasses are anoxic, the bubble weapon 1100 can be used as an emergency fire extinguisher. The bubble weapon 1100 may also be detonated to drive out atmosphere from a ship's volume to quench a fire. It may also be connected to plumbed fire extinguishing systems as spare sources. In the event of a sinking, the weapon can be discharged into a water-tight section of the vessel to displace encroaching water.
In some embodiments, the buoyancy dissipater described in the US patent application, entitled “BUOYANCY DISSIPATER AND METHOD TO DETER AN ERRANT VESSEL” filed Jan. 30, 2009 having Ser. No. 12/362,547 and which is incorporated herein by reference, may be suitable for use as any one of the bubble weapons described herein. In some embodiments, the configurable diffuser described in patent application entitled “VORTICE AMPLIFIED DIFFUSER FOR BUOYANCY DISSIPATER AND METHOD FOR SELECTABLE DIFFUSION” filed concurrently herewith and which is incorporated herein by reference may be suitable for use as the configurable diffuser section 1102.
The Abstract is provided to comply with 37 C.F.R. Section 1.72(b requiring an abstract that will allow the reader to ascertain the nature and gist of the technical disclosure. It is submitted with the understanding that it will not be used to limit or interpret the scope or meaning of the claims. The following claims are hereby incorporated into the detailed description, with each claim standing on its own as a separate embodiment.
This invention was not made with United States Government support. The United States Government does not have certain rights in this invention.
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Number | Date | Country | |
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20120042954 A1 | Feb 2012 | US |