| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | John ericsson | US298455D | US298455A | 1884-05-13 | ||
| 42 | Lius h | US245804D | US245804A | 1881-08-16 | ||
| 43 | Surface skimming munition | US14562876 | 2014-12-08 | US09448049B2 | 2016-09-20 | Anthony Joseph Cesaroni |
| A surface skimming munition comprises a hull, a traction propulsion motor positioned in the hull and having a combustion chamber for combustion of a propellant, at least one aft directed nozzle coupled to the hull at a position forward of a center of gravity of the hull and comprising an inlet section and an outlet section, the inlet section in fluid communication with the combustion chamber and the outlet section directing combustion gas received from the combustion chamber through the inlet section in the aft direction, and at least one stabilizing plane coupled to the hull and moveable between a stowed position and a deployed position. | ||||||
| 44 | STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES | US14228686 | 2014-03-28 | US20150375840A1 | 2015-12-31 | Kyle Stowers |
| Embodiments described herein provide apparatus and method for stand-off deployment of UUVs utilizing self-directed projectiles that include guidance kits. One embodiment is a projectile that includes a guidance kit that directs the projectile in flight. The projectile further includes a shell and a hollow nose cone. The shell mates with the guidance kit and the nose cone couples with the shell. The nose cone includes an interior surface configured to house a UUV. The projectile further includes a controller that identifies a condition for deploying the UUV in flight, and detaches the nose cone from the shell in response to determining that the condition is satisfied. | ||||||
| 45 | Surface skimming munition | US13416296 | 2012-03-09 | US08939084B2 | 2015-01-27 | Anthony Joseph Cesaroni |
| A surface skimming munition comprises a hull, a traction propulsion motor positioned in the hull and having a combustion chamber for combustion of a propellant, at least one aft directed nozzle coupled to the hull at a position forward of a center of gravity of the hull and comprising an inlet section and an outlet section, the inlet section in fluid communication with the combustion chamber and the outlet section directing combustion gas received from the combustion chamber through the inlet section in the aft direction, and at least one stabilizing plane coupled to the hull and moveable between a stowed position and a deployed position. | ||||||
| 46 | Device and method for launching an underwater moving body | US13265170 | 2010-04-22 | US08561564B2 | 2013-10-22 | Axel Brenner; Ralf Bartholomäus; Wolfgang Bünsch; Sönke Huckfeldt; Dirk Fuhrmann |
| A method and a device for launching an underwater moving body. In order to reduce the expenses arising from furnishing watercraft, a land supported deployment of underwater moving bodies in coastal waters using a launching device is provided with a land-based carrier system for transporting the underwater moving body and a corresponding land-based deploying system. | ||||||
| 47 | Device and Method for Launching an Underwater Moving Body | US13265170 | 2010-04-22 | US20130011196A1 | 2013-01-10 | Axel Brenner; Ralf Bartholomäus; Wolfgang Bünsch; Sönke Huckfeldt; Dirk Fuhrmann |
| A method and a device for launching an underwater moving body. In order to reduce the expenses arising from furnishing watercraft, a land supported deployment of underwater moving bodies in coastal waters using a launching device is provided with a land-based carrier system for transporting the underwater moving body and a corresponding land-based deploying system. | ||||||
| 48 | SURFACE SKIMMING MUNITION | US13416296 | 2012-03-09 | US20120234195A1 | 2012-09-20 | Anthony Joseph Cesaroni |
| A surface skimming munition comprises a hull, a traction propulsion motor positioned in the hull and having a combustion chamber for combustion of a propellant, at least one aft directed nozzle coupled to the hull at a position forward of a center of gravity of the hull and comprising an inlet section and an outlet section, the inlet section in fluid communication with the combustion chamber and the outlet section directing combustion gas received from the combustion chamber through the inlet section in the aft direction, and at least one stabilizing plane coupled to the hull and moveable between a stowed position and a deployed position. | ||||||
| 49 | Drag-stabilized water-entry projectile and cartridge assembly | US12409265 | 2009-03-23 | US08222583B2 | 2012-07-17 | Jyun-Horng Fu; Antonio Paulic |
| A drag-stabilized water-entry projectile having a projectile body, one or more drag-stabilizing elements, such as fins, flares or canards, and one or more attachment members adapted to hold the one or more drag-stabilizing elements to the projectile body. The one or more attachment members are coated with a thermally reactive material. A projectile and cartridge assembly has a shear pin, a projectile having a first cutout portion, the cutout portion sized to receive the shear pin. The assembly also includes a sabot configured to house the projectile and having a second cutout portion, the second cutout portion sized to receive the shear pin. The cutout portion is positioned to provide an offset region between an aft end of the projectile and a base of the sabot. | ||||||
| 50 | SUPERCAVITATING PROJECTILE HAVING A MORPHABLE NOSE | US12397182 | 2009-03-03 | US20120097061A1 | 2012-04-26 | Jyun-Horng Fu |
| A supercavitating projectile having a nose that is capable of morphing its shape or length for extended operating range is disclosed. | ||||||
| 51 | Counter-mine dart | US12265602 | 2008-11-05 | US08047135B1 | 2011-11-01 | Antonio Paulic; Lance Hamilton Benedict |
| Some embodiments of the invention provide a dart that contains an HE payload, two time-delay fuses, one providing a relatively longer delay and the other providing a relatively shorter delay and two triggering mechanisms for triggering the fuses. The first triggering mechanism, which triggers on contact with a mine lid, triggers the relatively shorter time-delay fuse. The second mechanism, which triggers on overburdening exposure to water, sand, or soil, triggers the relatively longer time-delay fuse. | ||||||
| 52 | COUNTER-MINE DART | US12265602 | 2008-11-05 | US20110252996A1 | 2011-10-20 | Antonio Paulic; Lance Hamilton Benedict |
| Some embodiments of the invention provide a dart that contains an HE payload, two time-delay fuses, one providing a relatively longer delay and the other providing a relatively shorter delay and two triggering mechanisms for triggering the fuses. The first triggering mechanism, which triggers on contact with a mine lid, triggers the relatively shorter time-delay fuse. The second mechanism, which triggers on overburdening exposure to water, sand, or soil, triggers the relatively longer time-delay fuse. | ||||||
| 53 | METHOD OF PRODUCING MISSILE NOSE CONES | US12491953 | 2009-06-25 | US20100326182A1 | 2010-12-30 | Robert A. Shulter; Margaret Rose Manning; Paul A. Leitch; Paul E. Liggett |
| A method for producing a missile nose cone is disclosed. The method consists of manufacturing a first missile nose cone from a first lot of polymeric material and determining a first rupture value. The method further consists of manufacturing a second missile nose cone from a second lot of polymeric material and determining a second rupture value of the second missile nose cone. Both first and second lots of material are mixed into a test batch with one another based on their associated rupture values. An evaluation missile nose cone is then manufactured from the test batch and a determination is made as to whether the evaluation missile nose cone has a desired rupture value. If a desired rupture value is not obtained, then the mixing and evaluation steps are repeated. | ||||||
| 54 | Method of operating a supercavitating projectile based on velocity constraints | US12327550 | 2008-12-03 | US07832336B2 | 2010-11-16 | Jyun-Horng Fu |
| A method for operating a thrust-generating supercavitating projectile involves launching the projectile at a velocity above the minimum required to maintain supercavitating movement, delaying initiation of thrust until the projectile slows to a velocity that is near that minimum velocity, and then applying thrust to maintain the near-minimum velocity until a target is reached. | ||||||
| 55 | High resolution projectile based targeting system | US10947789 | 2004-09-20 | US07392733B1 | 2008-07-01 | Robert Kuklinski; Thomas J. Gieseke |
| A projectile based targeting system for underwater objects includes a trainable gun terminal mounted in a waterproof housing. The gun terminal includes plural gun barrels terminating in waterproof breeches. Noise generating projectiles are launched from the gun barrels, and a fire control system selectively fires the projectiles from each of the plural gun barrels in a noise pattern. A host controller detects and processes noise generated by a launched pattern of the noise generating projectiles to give information about the objects. The projectiles each include a void region connected to an outer surface of the projectile by a hole formed in a neck of the projectile. Launching of the projectile creates a vaporous cavity around the projectile and thus the hole, thereby causing the void region to resonate at a noise generating frequency. | ||||||
| 56 | EXPENDABLE SONOBUOY FLIGHT KIT WITH AERODYNAMICALLY ASSISTED SONOBUOY SEPARATION | US11782487 | 2007-07-24 | US20080035786A1 | 2008-02-14 | Derek BILYK; Patrick Zdunich; Marc MacMaster |
| Disclosed herein is an expendable flight kit attachable to a sonobuoy for making use of said sonobuoy as a central structural load-bearing component of a flying assembly, the kit comprising rigid aerodynamic surfaces to provide lift and stability; a propulsion system; a plurality of control surfaces; a plurality of control surface actuators operable for moving the control surfaces in response to control signals; a flight control system, the fight control system including a GPS receiver and attitude and airspeed sensors, the flight control system being operable for receiving mission parameters including sonobuoy deployment co-ordinates, the flight control system being operable for autonomously navigating and steering the vehicle in flight using information from the GPS receiver and the attitude and airspeed sensors, the fight control system being operable for sending control signals to control the control surface actuators, the flying assembly operable to be launched from a ship; the flight control system operable for separating the sonobuoy from the flight kit while in flight at an acceptable proximity to a pre-designated set of co-ordinates, wherein after separation of the sonobuoy from the flight kit, both the sonobuoy and the flight kit fall into the water. | ||||||
| 57 | Surface launched sonobuoy | US62887 | 1998-04-20 | US5973994A | 1999-10-26 | Robert Woodall |
| A sonobuoy device for tracking and targeting submarines. The sonobuoy dev comprises a sonobuoy having aft and forward sections interconnected with each other, fin means mounted on the aft section for flight stabilization of the device during travel above water from the platform, separation means responsive to impact of the device with the water upon completion of the travel thereof for separating the sections of the device from each other, payload means within the forward section of the device for listening for an acoustical signal in response to submergence thereof within the water following the separation of the sections of the device, flotation means mounted within the device and inflated in response to the impact with the water for anchoring the payload means and tethering means connecting the flotation means to the payload means for limiting the submergence thereof while anchored by the flotation means to a predetermined depth at which the payload means receives an acoustical signal. An apparatus comprising the device with a launching system and a method for deploying the device also is disclosed. | ||||||
| 58 | Air-launched supercavitating water-entry projectile | US14688 | 1998-01-28 | US5955698A | 1999-09-21 | Thomas K. Harkins; Howard K. Steves; Jacques E. Goeller |
| A supercavitating water-entry projectile having empennage on the aft end ch provides both aerodynamic and hydrodynamic stability and a supercavitating nose section is provided. A representative projectile is a subcaliber munition adapted for use in a 25 mm weapon using a sabot currently in use with the M919 round. The projectile has circumferential grooves around its center section to match these sabots. A key feature in the invention is the size and shape of the nose section. The projectile has a novel high strength extended blunt nose section followed by a truncated conical section which angles towards the body of the projectile in the range of five degrees. During underwater trajectory, the entire projectile is contained within the cavitation bubble formed by the blunt nose tip. The projectile's aft empennage, which provides both aerodynamic and hydrodynamic stability, fits within the bore of the weapon. | ||||||
| 59 | Rocket assisted torpedo | US81600859 | 1959-05-26 | US3088403A | 1963-05-07 | BARTLING JAMES T; SAHOLT ORVILLE J; BERNARD SMITH |
| 60 | Single ended amplifier with double ended output | US33892553 | 1953-02-25 | US3050690A | 1962-08-21 | SKRAMSTAD HAROLD K; HART JOHN A |
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