| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 潜载垂直发射筒固定装置 | CN201610908305.1 | 2016-10-18 | CN106364645A | 2017-02-01 | 邓科; 周成康; 宋策; 于殿君; 朱坤 |
| 本发明涉及一种潜载垂直发射筒固定装置，属于潜载垂直发射筒技术领域。本发明通过设计的压环组件、发射井围栏能够有效解决潜载垂直发射筒与潜艇发射井的连接问题，发射井围栏和发射筒上法兰无需开螺栓孔，压环组件可以作为消耗件，用较小的代价即可保证发射井围栏的防腐层不会遭到破坏，且气水密可靠，操作过程中只需要操作8个不脱落的顶紧螺杆，而不是容易脱落丢失的12个螺栓，确保气水密和防腐措施有效。 | ||||||
| 2 | The method and apparatus of the Marine deployment | JP2011528003 | 2009-09-18 | JP2012503167A | 2012-02-02 | レイ サンプソン、; ジェフリー エヌ ゼルベ、; デイヴィッド イー ボサート、 |
| 【課題】無人機及び他の資源は地上作戦に制限されないが、海上発射システムは、それらを展開するには不十分である。
【解決手段】本発明の様々な態様に応じた海上展開の方法及び装置は、海洋艦船による展開に適用される浮揚性筐体と共同で働くことができる。 前記浮揚性筐体は、海洋艦船から発射され、水面に浮上するように適用され得る。 無人機のような資源は、水面に浮上した前記浮揚性筐体から展開される。 【選択図】 図１ |
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| 3 | LAUNCHED AIR VEHICLE SYSTEM | US15913841 | 2018-03-06 | US20180257792A1 | 2018-09-13 | Thomas William Smoker |
| A launch canister for ejection from a submerged launch platform, the launch canister being adapted for ejection in a direction substantially along a first axis of the launch canister and comprising: an enclosure for carrying a UAV; a nose cap releasably located in a launch opening at a forward end of the launch canister; a launch mechanism for driving a UAV carried in the enclosure out of the launch canister through the launch opening in a direction substantially along said first axis; and a water surface sensor for detecting when the nose cap of the canister broaches the surface of the water; wherein the launch canister is configured to, on the water surface sensor detecting that the nose cap of the canister has broached the surface of the water, immediately release the nose cap and initiate the launch mechanism to drive a UAV carried in the enclosure out of the launch canister through the launch opening. | ||||||
| 4 | Unmanned aerial vehicle launch system | US13367494 | 2012-02-07 | US08662441B2 | 2014-03-04 | David Powell; Earl Mark; John T. Houck; Keith Huber |
| A system for launching an unmanned aerial vehicle (UAV) payload includes a launch tube, liquid rocket, and launch control assembly. The rocket is positioned in the launch tube and contains the UAV payload. A booster assembly may include a canister partially filled with liquid. A gas cylinder is filled with compressed gas. The liquid is pre-pressurized by the gas or mixed with the gas right before launch such that, upon launch, liquid and gaseous thrust stages launch the rocket to a threshold altitude. The UAV payload deploys after reaching the threshold altitude. Optional stability tubes may be connected to the launch tube, which may be buoyant for water-based operations. An optional tether may be connected to the liquid rocket for arresting its flight prior to reaching apogee. The UAV payload is not launched directly by the gas/liquid mix. A method of launching the UAV payload is also disclosed. | ||||||
| 5 | Submarine short-range defense system | US11879528 | 2007-06-25 | US07779772B2 | 2010-08-24 | C. Roger Wallin |
| Disclosed is a launch system of an affixed lower section of launch tubing and an upper section of launch tubing configured to telescope vertically from a stowed position within the hull of a submarine to a position just above the ocean surface for a launch operation of a projectile, with the upper section returning to a stowed position after the launch operation. The launch system is capable of launching a projectile to engage air contacts by the discharge of high pressure fluid air, through the length of the upper and lower sections to impact the projectile for launch. The launch system includes surveillance, command and control elements as well as operational connection to additional projectile stowage and a supply of high pressure fluid. The projectile in use with the launch system can support surveillance and communications operations. | ||||||
| 6 | Submarine short-range defense system | US11879528 | 2007-06-25 | US20100024708A1 | 2010-02-04 | C. Roger Wallin |
| Disclosed is a launch system of an affixed lower section of launch tubing and an upper section of launch tubing configured to telescope vertically from a stowed position within the hull of a submarine to a position just above the ocean surface for a launch operation of a projectile, with the upper section returning to a stowed position after the launch operation. The launch system is capable of launching a projectile to engage air contacts by the discharge of high pressure fluid air, through the length of the upper and lower sections to impact the projectile for launch. The launch system includes surveillance, command and control elements as well as operational connection to additional projectile stowage and a supply of high pressure fluid. The projectile in use with the launch system can support surveillance and communications operations. | ||||||
| 7 | Submarine short-range defense system | US11015804 | 2004-12-20 | US07249567B1 | 2007-07-31 | C. Roger Wallin |
| Disclosed is a launch system of an affixed lower section of launch tubing and an upper section of launch tubing configured to telescope vertically from a stowed position within the hull of a submarine to a position just above the ocean surface for a launch operation of a projectile, with the upper section returning to a stowed position after the launch operation. The launch system is capable of launching a projectile to engage air contacts by the discharge of high pressure fluid air, through the length of the upper and lower sections to impact the projectile for launch. The launch system includes surveillance, command and control elements as well as operational connection to additional projectile stowage and a supply of high pressure fluid. The projectile in use with the launch system can support surveillance and communications operations. | ||||||
| 8 | Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea | US10823434 | 2004-04-13 | US07097136B2 | 2006-08-29 | Robert A. Ruszkowski, Jr. |
| A sea-launched and recovered unmanned aircraft is disclosed. The aircraft is jet-powered and has features and systems to maintain watertight integrity such that it may be released from a submerged submarine or dropped into a body of water by a ship or an aircraft. The aircraft is buoyant and remains at or near the water surface before its rockets are ignited. The rockets propel the air vehicle out of the sea and accelerate it to flying speed at which time a jet engine is started and the rockets are jettisoned. The air vehicle performs its mission independently or in conjunction with other ones of the air vehicles. The air vehicle then returns to an assigned splashdown point at sea via, for example, an engine-off “whip-stall” maneuver. A submarine or ship may retrieve the air vehicle and readies it for another mission. | ||||||
| 9 | Elastomeric launch assembly and method of launch | US10267091 | 2002-10-08 | US06672239B1 | 2004-01-06 | Thomas J. Gieseke |
| A launch assembly having an elastomeric tube for launching a device is disclosed. To launch the device an outboard end of the tube is movable outwardly along the length of a housing by an extending device, while the inboard end of the tube is restrained by a release mechanism and remains stationary. Thus, as the outboard end moves and the inboard end remains stationary, the elastomeric tube elongates. The tube may be elongated a predetermined amount, at which time the inboard end of the tube is released by the release mechanism. Releasing the inboard end allows it to travel toward the now stationary outboard end with a sufficient velocity to launch the device. The amount of elongation of the tube is related to the amount of possible launch energy. Thus, greater elongation of the tube provides a greater launch velocity, while shorter elongation provides a reduced launch velocity, as desired. | ||||||
| 10 | SMALL DEVICE LAUNCH SYSTEM | US09968017 | 2001-10-01 | US20030061981A1 | 2003-04-03 | Nicholas O. Venier; Nicholas Bitsakis |
| A system for providing pressurized fluid for a small device launch system is shown. The system includes a piston housing an air source aperture, a launcher bore, and a shaft aperture. A piston and piston shaft slide in the chamber with the piston shaft extending out the shaft aperture. A hydraulic control cylinder is connected to the piston shaft and a controller is joined to control the cylinder. In a preferred embodiment, the controller controls flow through a variable restriction valve positioned in hydraulic communication between sides of the hydraulic cylinder. A position indicator can also be provided for communicating the position of the piston shaft to the controller. | ||||||
| 11 | Submarine countermeasure launcher with gas capture | US08297661 | 1994-08-26 | US06367401B1 | 2002-04-09 | Ronald Correia; John J. Silvera; Nicholas O. Venier |
| A countermeasure launcher system, for use by a submarine, reducing any detectable signature by preventing the escape of pressurized gas into seawater at the forward end of the system's launch tube upon launching a countermeasure. The pressurized gas that is used in launching the countermeasure is trapped within the launch tube by a unique arrangement of specific components. The pressurized gas is then permitted to slowly exit at a later time via a pressure relief valve in the launch tube's wall. | ||||||
| 12 | Break-away muzzle cap retention mechanism | US09562995 | 2000-05-01 | US06336641B1 | 2002-01-08 | Michael W. Williams |
| A break-away end cap assembly includes a tube member of predetermined characteristics and an end cap member for releasably securing the open end of the tube member. An annular recessed groove is formed in the inner surface of the tube member. The end cap member includes an outer flange portion having an outer peripheral surface consistent in diameter with an outer diameter of the tube member and a body portion depending from the outer flange portion. At least one recessed opening is laterally formed within the body portion with a pilot hole formed at the base end of each recessed opening. A normally biased spring member is seated in a base of the recessed opening and a retractable pin is positioned over the normally biased spring member. The retractable pin has an outer beveled surface end which seats within the annular recessed groove and is held therein with the normally biased pressure of the spring member until a force greater than the normal bias of the spring member is applied against the inner surface of the end cap. | ||||||
| 13 | Scavenger energy converter system its new applications and its control systems | US08999729 | 1997-12-23 | US06327994B1 | 2001-12-11 | Gaudencio A. Labrador |
| What has been invented is a series of scientific applications of the wideface energy converter device, be it in the form of a wideface solar heat receiver or a wideface fluid impeder device. The wider is the solar heat receiver, the more solar power is available for conversion. The wider is the sail of the boat, the more wind is available to push the boat. Wherefore, the wideface solar trap made up of multi-layer transparent roofs covering a heat insulated box is used to heat up a radiator tubings that contain water. The multilayer transparent roof, having spaces in between sheets, prevents solar heat from backing out hence the trap becomes hoter and hoter because the inner sheet is not in contact with the cold wind. This solar trap is now used to heat up radiator pipes of compressed air coming from a gas turbine engine and then returned back to the exhaust turbine of same engine. Applying the principle of the wind sail, the turbine blades of the compressor and the turbine blades of the exhaust turbine are made wideface as much as possible to produce maximum impedance against the expanding exhaust hot air and to produce maximum push upon the fresh air being compressed. This wideface fluid impeder is now expanded into an underwater platform from One Acre or much more and attached to floating hotels, large/small boats, and floating sea walls, to prevent oscillation by the surfs. | ||||||
| 14 | Appended pod underwater gun mount | US09515216 | 2000-02-28 | US06305263B1 | 2001-10-23 | C. Roger Wallin |
| An appended pod underwater gun mount for a submersible host vessel includes a strut member having a base end fixed to an outer hull of the submersible host vessel and a distal end protruding outwardly from the host vessel, the distal end being angled with respect to the base end, and an ammunition housing moveably fixed to the distal end of the strut member. A train control mechanism is positioned between the strut member and the ammunition housing for controlling the horizontal rotation of the ammunition housing with respect to the host vessel, and a tilt control mechanism is positioned between the strut member and the ammunition housing for controlling the vertical rotation of the ammunition housing with respect to the host vessel. A flexible boot is connected to the ammunition housing and surrounds each of the train control mechanism and the tilt control mechanism to protect the mechanisms from an underwater environment. The ammunition housing is movable both vertically and horizontally with respect to the distal end of the strut member and is spaced apart from the host vessel so as to avoid contacting the host vessel during directional movement of the ammunition housing. | ||||||
| 15 | Submarine deck and missile-launching construction | US72833558 | 1958-04-14 | US2948246A | 1960-08-09 | SULLIVAN JOHN J |
| 16 | Gun-mounting | US23691818 | 1918-05-27 | US1327084A | 1920-01-06 | TREVOR DAWSON ARTHUR; THOMAS BUCKHAM GEORGE |
| 17 | Submarine gun-turret. | US13679116 | 1916-12-13 | US1296688A | 1919-03-11 | NOAH ROBERT S |
| 18 | Housing for guns. | US1914860299 | 1914-09-04 | US1170577A | 1916-02-08 | STRAUSS JOSEPH; HALSEY ARTHUR S |
| 19 | Gun adapted preferably for use in submarine boats. | US1913793121 | 1913-10-03 | US1095049A | 1914-04-28 | VOELLER KARL |
| 20 | Launched air vehicle system | US14294073 | 2014-06-02 | US09938021B2 | 2018-04-10 | Thomas William Smoker |
| A launch canister for ejection from a submerged launch platform, the launch canister being adapted for ejection in a direction substantially along a first axis of the launch canister and comprising: an enclosure for carrying a UAV; a nose cap releasably located in a launch opening at a forward end of the launch canister; a launch mechanism for driving a UAV carried in the enclosure out of the launch canister through the launch opening in a direction substantially along said first axis; and a water surface sensor for detecting when the nose cap of the canister broaches the surface of the water; wherein the launch canister is configured to, on the water surface sensor detecting that the nose cap of the canister has broached the surface of the water, immediately release the nose cap and initiate the launch mechanism to drive a UAV carried in the enclosure out of the launch canister through the launch opening. | ||||||
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