MINIATURE TORPEDO |
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申请号 | EP13770517.4 | 申请日 | 2013-03-07 | 公开(公告)号 | EP2859300B1 | 公开(公告)日 | 2017-07-05 |
申请人 | The Boeing Company; | 发明人 | RIVOLI, Louis; | ||||
摘要 | |||||||
权利要求 | |||||||
说明书全文 | The present disclosure relates to a miniature torpedo and more particularly, to a lightweight, miniature torpedo that can be carried by and launched from an unmanned aerial vehicle. Typical anti-ship torpedos are too heavy and too large to be carried by and launched from an unmanned aerial vehicle (UAV). Such a torpedo is known from Embodiments of a miniature torpedo in accordance with the appended independent claim 1 overcome the size and weight disadvantages of conventional torpedoes that prevent them from being carried by and launched from smaller UAVs in addition to significantly increasing the torpedo payload capability of both larger UAVs and conventional manned anti-ship aircraft, and anti sub-surface ship aircraft. According to one embodiment, a miniature torpedo has an overall length of approximately 18.5 inches and approximate weight of less than 10 pounds. This miniature torpedo is therefore well suited for being carried by and launched from small UAVs while also increasing the torpedo carrying capacity of larger UAVs and conventional manned aircraft. According to the invention, a miniature torpedo includes a contact and attachment assembly, a chamber containing at least one or more flammable element(s), and an ignition assembly, for example magnesium or a magnesium alloy. The contact and attachment assembly may attach the torpedo to a ship's hull. One or more flammable element(s) is respectively are moveable by a drive mechanism through the chamber and toward the ship's hull. The ignition assembly ignites one or more flammable element(s) and release the ignited element(s) from the chamber. The drive mechanism positions the ignited element against the ship's hull where the high temperature heat of the burning element(s) may melt a hole through the ship's hull. The miniature torpedo may also include a propulsion and steering assembly that is operable to propel and steer the torpedo through water below the water line. The miniature torpedo may also include a navigation and guidance assembly that controls the propulsion and steering assembly to direct the torpedo through the water toward the ship's hull. The apparatus may also include a targeting sensor and guidance transducer assembly that intercepts information on a location of the ship's hull and communicates the information to the navigation and guidance assembly. The navigation and guidance assembly may use the communicated information to control the propulsion and steering assembly to direct the miniature torpedo through the water to the ship's hull. In the figures and the text, a lightweight miniature torpedo 12 apparatus is disclosed including a contact and attachment assembly 22 that is operable to attach the apparatus to a ship's hull in response to the contact and attachment assembly 22 coming into contact with the ship's hull, a chamber 24 operatively connected to the contact and attachment assembly 22, the chamber 24 containing at least one flammable element 132 that is moveable in the chamber 24, the chamber 24 containing a drive mechanism 128 that is operable to drive the at least one flammable element 132 from the chamber 24 and toward the ship's hull in response to the contact and attachment assembly 22 attaching the apparatus to the ship's hull, and an ignition assembly 74 connected to the contact and attachment assembly 22, the ignition assembly 74 being operable to ignite the at least one flammable element 132 as the at least one flammable element 132 is driven toward the ship's hull. In one variant, the apparatus further includes the at least one flammable element 132 being constructed to oxidize when ignited by the ignition assembly 74. In another variant, the apparatus further includes the at least one flammable element 132 being constructed of at least magnesium. In yet another variant, the apparatus further includes the at least one flammable element 132 having a combustion temperature that is higher than a melting temperature of a target vessel hull metal. In still yet another variant, the apparatus further includes the contact and attachment assembly 22 includes a permanent magnet assembly 32 comprising at least one permanent magnet. In one instance, the apparatus further includes at least a portion of the chamber 24 being constructed of a ceramic material having a melting temperature that is higher than a combustion temperature of the at least one flammable element 132. In another instance, the apparatus further includes the chamber 24 containing a plurality of flammable elements 132 and a spring drive mechanism 128, the spring drive mechanism 128 driving the plurality of flammable elements 132 from the chamber 24 toward the ignition assembly, the ignition assembly 74 being operable to sequentially ignite the plurality of flammable elements 132. In yet another instance, the apparatus further includes the chamber 24 being operatively connected to the contact and attachment assembly 22 by a hollow universal joint that enables the chamber 24 to move in rotation and through an arc relative to the contact and attachment assembly 22. In still another instance, the apparatus further includes the apparatus being constructed to be carried and launched by an unmanned aerial vehicle, a conventionally manned, anti ship aircraft, and a conventionally manned anti sub-surface ship aircraft. In one example, the apparatus further includes a propulsion and steering assembly 26 operatively connected to the contact and attachment assembly 22 and the chamber 24, the propulsion and steering assembly 26 being operable to propel and direct the apparatus through water. In another example, the apparatus further includes a navigation guidance assembly 48 operatively communicating with the propulsion and steering assembly 26, the navigation guidance assembly 48 being operable to control the propulsion and steering assembly 26 to direct the apparatus through water. In still another example, the apparatus further includes a targeting sensor assembly operatively communicating with the navigation guidance assembly 48, the targeting sensor assembly being operable to intercept information on a location of a ship hull and provide the information to the navigation guidance assembly 48, the navigation guidance assembly 48 being operable to use the information provided by the targeting sensor assembly to control the propulsion and steering assembly 26 to direct the apparatus through the water to the location of the ship hull. The invention also provides a method according to appended claim 13, in particular a method of using a lightweight miniature torpedo 12 apparatus to damage a ship hull, the method includes providing the apparatus with a contact and attachment assembly 22 and attaching the apparatus to the ship hull below a water line by contacting the ship hull below the water line with the contact and attachment assembly 22, providing the apparatus with at least one flammable element 132 having a combustion and oxidation temperature that is higher than a melting temperature of a material of the ship hull and igniting the at least one flammable element 132, engaging the ignited flammable element 132 against the material of the ship hull, and melting a portion of the material of the ship hull with the ignited flammable element 132 and thereby producing a hole through the material of the ship hull. In one variant, the method further includes providing the apparatus with a propulsion and steering assembly 26 and propelling and directing the apparatus through the water to the ship hull. In another variant, the method further includes carrying the apparatus by an aerial vehicle and launching the apparatus from the aerial vehicle to below the water line. In another variant, the apparatus further includes providing the apparatus with a plurality of flammable elements 132 and sequentially igniting each flammable element 132 of the plurality of flammable elements 132 and engaging the ignited flammable element with the material of the ship hull. In one aspect, a lightweight miniature torpedo 12 apparatus is disclosed including a chamber 24 having a length with opposite forward and rearward ends 16, 18 and an interior bore extending through the length of the chamber 24, at least one flammable element 132 in the chamber interior bore, a spring mechanism in the chamber interior bore, the spring mechanism urging the at least one flammable element 132 toward the chamber forward end 16, a contact and attachment assembly 22 at the chamber forward end 16, the contact and attachment assembly 22 including a permanent magnet assembly 32 that is operable to attach the apparatus to a ship's hull in response to the contact and attachment assembly 22 coming into contact with the ship's hull, and a retention and ignition assembly 74 at the chamber forward end 16, the retention and ignition assembly 74 being operable to retain the at least one flammable element 132 in the chamber interior bore against the urging of the spring mechanism and being operable to ignite the at least one flammable element 132 and release the at least one flammable element 132 from the chamber interior bore enabling the spring mechanism to urge the at least one flammable element 132 through the chamber interior bore and then into the ship's hull. In one variant, the apparatus further includes the chamber 24 being operatively connected to the contact and attachment assembly 22 by a hollow universal joint that enables the chamber 24 to move in rotation and through an arc relative to the contact and attachment assembly 22. In another variant, the apparatus further includes the at least one flammable element 132 being one of a plurality of separate elements comprised of at least magnesium contained in the chamber interior bore, the spring mechanism urging the plurality of elements through the chamber interior bore toward the retention and ignition assembly, and the retention and ignition assembly 74 being operable to retain the plurality of elements in the chamber interior bore against the urging of the spring mechanism and being operable to ignite at least one element of the plurality of elements and then release the elements from retention in the chamber interior bore enabling the spring mechanism to urge the plurality of elements through the chamber interior bore and toward the chamber forward end 16. In another variant, the apparatus further includes a propulsion and steering assembly 26 at the chamber rearward end 18, the propulsion and steering assembly 26 being operable to propel and direct the apparatus through water. Further features are set forth in the following description and in the drawing figures.
The miniature torpedo 12 is basically comprised of a contact and attachment assembly 22 at the forward end 16 of the apparatus, a chamber 24 operatively connected to the contact and attachment assembly 22 and extending rearwardly thereof, and a propulsion and steering assembly 26 operatively connected to the chamber 24 at the rearward end 18 of the apparatus. Referring to Four or more guidance transducer assemblies 44 are secured to the magnet exterior surface 42 at equal circumferentially spaced positions. The transducer assemblies 44 are positioned or oriented parallel with the apparatus center axis 14. Sonic signal receiving surfaces 46 of the assemblies 44 face forwardly of the apparatus. The guidance transducer assemblies 44 function as target sensors. A sonic navigation guidance assembly 48 is secured to the magnet assembly's rearward surface 36. The sonic navigation guidance assembly 48 communicates with and receives signals from the guidance transducer assemblies 44. A control system 52, for example, a central processing unit (CPU) 52 is secured to the magnet assembly rearward surface 36. The CPU communicates with the guidance transducer assemblies 44 and the sonic navigation guidance assembly 48 and controls the operations of these assemblies. The CPU also communicates with the propulsion and steering assembly 26 and controls the operation of this assembly. A power source 54 is also secured to the magnet rearward surface 36, and, or alongside chamber 24. The power source 54 is comprised of one or more batteries and communicates with the guidance transducer assemblies 44, the sonic navigation guidance assembly 48, the CPU 52 and the propulsion and steering assembly 26 and provides power to all these components. A pair of tethers 114 connects to contact release mechanisms 56, and are secured to the magnet assembly 32 at diametrically opposite sides of the magnet assembly exterior surface 42. Each mechanism 56 has a cylindrical housing 58 that is connected to a base 62. Each base 62 is secured to the magnet assembly's rearward surface 36. The cylindrical housings 58 are positioned at diametrically opposite sides of the magnet assembly's exterior surface 42 with center axes of the cylindrical housings being aligned parallel with the apparatus center axis 14. A plunger 64 is mounted in each cylindrical housing 58 for axial reciprocating movements forwardly and rearwardly through the housing. Each plunger 64 has a forward contact end 66 and an axially opposite hook end 68. Springs 72 in the cylindrical housings 54 bias the plungers 64 forwardly to their positions shown in A retention and ignition assembly 74 is secured to the magnet assembly 32 at the center of the magnet forward surface 34. The retention and ignition assembly 74 is formed as a flat strip that extends radially across the magnet assembly center bore and then axially across opposite sides of the magnet assembly's cylindrical interior surface 38. The strip 74 is constructed of a material that will ignite and burn when supplied with an electric current, for example magnesium or a magnesium alloy. The strip 74 is connected in communication with the power source 52 through the CPU 54 and its ignition is controlled by the CPU. A cylindrical housing 82 extends into the magnet assembly's center bore and is secured to the magnet assembly interior surface 38 and to a portion of the magnet rearward surface 36. The cylindrical housing 82 is shown in A hollow universal joint or hollow u-joint assembly 92 is secured inside the large portion 86 of the cylindrical housing 82. The hollow u-joint assembly 92 is comprised of a cylindrical forward portion 94 and a cylindrical rearward portion 96. The joint forward portion 94 has a bearing ring 98 secured to its exterior surface. The bearing ring 98 interfaces the interior surface of the large portion 86 of the cylindrical housing 82, thereby operatively connecting the hollow u-joint assembly 92 to the contact and attachment assembly 22. A retaining ring 102 is press-fit into the large portion 86 of the cylindrical housing 82 to secure the hollow u-joint forward portion 94 to the housing 82. The bearing ring 98 allows the hollow u-joint assembly 92 to rotate freely about the apparatus center axis 14 relative to the contact and attachment assembly 22. The retaining ring 102 prevents the u-joint assembly 92 from moving axially relative to the contact and attachment assembly 22. Referring to Together, the bearing ring 98 and the joint assembly between the joint forward portion 94 and the joint rearward portion 96 form a hollow universal joint between the contact and attachment assembly 22 and the joint rearward portion 96 that enables the joint rearward portion 96 to rotate freely around the center axis 14 of the apparatus 12 and allows the joint rearward portion 96 to move through a 180 degree arc relative to the contact and attachment assembly 22. A pair of tethers 114 are secured to diametrically opposite sides of the joint assembly rearward portion 96. The tethers 114 are shown in the drawing figures as small link chains. However, other equivalent flexible cords could be substituted for the link chains. The tethers extend from the joint assembly rearward portion 96 to the plunger hook ends 68 of the harness contact release mechanisms 56. The springs 72 of the harness contact release mechanisms 56 pull the tethers 114 tight as they extend between the harness contact release mechanisms 56 and the joint assembly rearward portion 96. In this manner, the tethers 114 hold the joint rearward hollow u-joint assembly 96 in a position relative to the contact and attachment assembly 22 shown in The tubular chamber 24 is operatively connected between the contact and attachment assembly 22 and the propulsion and steering assembly 26. The chamber 24 has a cylindrical exterior surface 116 and a cylindrical interior surface 118. The chamber 24 has a straight length that extends forward 122 between rearward u-joint assembly 96 and axially opposite rearward end 124 of the chamber. The chamber forward end 122 is open and extends into the joint assembly rearward portion 96 and is secured thereto, thereby operatively connecting the chamber 24 to the contact and attachment assembly 22. The chamber rearward end 124 is closed and is secured to the propulsion and steering assembly 26. The chamber 24 has an interior diameter dimension that is substantially the same as that of the joint assembly rearward portion 96, the hollow u-joint assembly forward portion 94 and the small portion 86 of the cylindrical housing 82. Thus, there is a continuous interior bore that extends through the chamber 24 from the chamber rearward end 124, through the joint assembly 92 and through the permanent magnet assembly 32. A spring drive mechanism 128 is positioned in the chamber 24 at the chamber rearward end 124. The spring drive mechanism 128 is illustrated in the drawing figures as a coil spring. Other equivalent spring drive mechanisms could be employed instead of the coil spring. The spring drive mechanism 128 is shown in a compressed condition in A plurality of flammable elements 132 are contained in the chamber 24, the hollow u-joint assembly 92 and the cylindrical housing 82. Adjacent flammable elements 132 are linked together, for example by a short cord (not shown). The spring drive mechanism 128 urges the flammable elements 132 toward the forward end 16 of the miniature torpedo apparatus 12 where a forward end of the elements 132 engages against and is retained by the retention and ignition assembly 74. Each of the flammable elements 132 has a spherical configuration that can be driven and moved easily through the chamber 24, the hollow u-joint assembly 92 and the cylindrical housing 82 by the spring drive mechanism 128. Each of the elements 132 is constructed of a flammable material such as magnesium or a magnesium alloy that can be easily ignited and will oxidize when ignited and burn at a combustion temperature that is sufficiently high to melt through a metal ship's hull. An additional alternate embodiment of the apparatus is shown in The apparatus 12 is designed to be carried by a UAV to the general geographic area of a ship detected by a remote acoustic sensor. The apparatus 12 is designed to be effective against both surface ships and sub-surface ships. Following detection of the ship by the remote acoustic sensor, a UAV carrying the apparatus 12 will launch or deploy the apparatus 12 in the general geographic area of the detected ship. A small parachute attached to the apparatus 12 will allow it to slowly fall from the UAV to the water surface. Once in the water, the CPU 52 will control the apparatus 12 to release the parachute, target the ship hull with the guidance transducer assemblies 44 and travel to the targeted hull using the sonic navigation guidance assembly 48 and the propulsion and steering assembly 26. When the targeted ship hull is reached, the apparatus 12 will attach to the metal of the ship hull by the permanent magnet assembly 32. Attachment of the magnet assembly 32 to the ship hull depresses the plungers 64 of the harness contact release mechanism 56 causing the tethers 114 to disengage from the plunger hook ends 68 and freeing the hollow u-joint assembly rearward portion 96 to rotate and pivot relative to the contact and attachment assembly 22. This allows the chamber 24 of the apparatus to rotate around the apparatus center axis 14 and pivot up to 90 degrees to conform the chamber 24 to the hydrodynamic forces of a moving ship hull. The releasing of the harness contact release mechanism 56 also causes the CPU 52 to concurrently trigger the electrical ignition of the retention and ignition assembly 74. This in turn ignites and releases the forward most of the flammable elements 132 to be moved forwardly by the drive mechanism 128 and engage against the ship hull. Once ignited, the combustion temperature of the flammable element 132 will cause the area of the ship's hull engaged by the element to melt and will bore through the hull of the targeted ship. As the combustion of one flammable element 132 is completed it ignites the next in line flammable element which is then pressed against the melting area of the ship hull by the drive mechanism 128. This continues until the burning flammable elements 132 bore a hole through the ship hull. |