| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | Device for launching torpedoes | US58517045 | 1945-03-27 | US2435444A | 1948-02-03 | FRIEDER LEONARD P; BJORNULF JOHNSEN |
| 22 | Method of producing missile nose cones | US12491953 | 2009-06-25 | US08256086B2 | 2012-09-04 | Robert A. Shutler; 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. | ||||||
| 23 | Air-to-subsurface missile system | US402060 | 1964-09-29 | US5012717A | 1991-05-07 | Morton L. Metersky; James R. Howard |
| The invention is an air-to-subsurface missile system which has an acousticoming torpedo and a directional sonobuoy held in the missile behind the torpedo by a cowling means which includes fins for aerodynamic stability. When the missile reaches the desired location in a body of water, the torpedo and sonobuoy are released. The sonobuoy has the ability to search for targets and to communicate both with the homing torpedo and with a tactical command station. Thus the torpedo can be guided to a target by the sonobuoy and command station, even at ranges at which the torpedo could not locate a target with its own homing system. | ||||||
| 24 | Missile nosepiece | US153110 | 1988-02-08 | US4788914A | 1988-12-06 | James T. Frater |
| A nosepiece for the forward end of a missile that is launched into the atmosphere for a ballistic trajectory and a water entry impact comprises a frangible base and a separable nosecap, the base having multiple segments of rigid foam defining an axial bore into the base and a volume of soft cellular foam within the bore to protect the forward end of the missile. The nosecap is in seated relationship within the bore opening on the tip end of the base during airborne flight and separates therefrom to expose the axial bore opening prior to water entry impact such that upon impact the base is fractured by the force of water entering the exposed bore and thus separated from the missile. | ||||||
| 25 | Mercury button switch | US39814564 | 1964-09-02 | US3327084A | 1967-06-20 | COOK LEONARD W; COUTANT EDWARD R; GILMORE ARVILLE W |
| 26 | Parachute release mechanism | US85120359 | 1959-11-05 | US3066632A | 1962-12-04 | BEMIS WALDO E |
| 27 | Autopilot | US26697852 | 1952-01-17 | US3011738A | 1961-12-05 | SKRAMSTAD HAROLD K; HART JOHN A |
| 28 | Breakaway suspension band | US32416152 | 1952-12-04 | US2786392A | 1957-03-26 | JOSEPH NIEDLING HERMAN |
| 29 | Propulsion assembly for torpedoes | US71142046 | 1946-11-21 | US2568433A | 1951-09-18 | DALY THOMAS A; HOGUE PAUL M |
| 30 | Apparatus for decelerating torpedoes | US66802746 | 1946-05-08 | US2539643A | 1951-01-30 | SMYTHE WILLIAM R |
| 31 | Torpedo | US17013817 | 1917-05-22 | US1382166A | 1921-06-21 | CHARLES BLUM |
| 32 | Torpedo. | US19763217 | 1917-10-20 | US1290829A | 1919-01-07 | CARPENTER GEORGES J N |
| 33 | 유도탄의 보호덮개, 이를 구비하는 유도탄 및 유도탄의 충격완화방법 | KR1020100117683 | 2010-11-24 | KR1020120056123A | 2012-06-01 | 김인학; 김형렬; 독고욱 |
| PURPOSE: A protection cover of a guided missile and a shock relieving method of the guided missile are provided to protect machines or electric devices of a guided missile with added reliability because a protection cover fractures to buffer an impact when the guided missile flies into water. CONSTITUTION: A protection cover of a guided missile(100) comprises a shell assembly(130), a shock absorbing ball(150), and a closing plate(120). The shell assembly comprises a plurality of supporters. One end of the shell assembly forms a closed plane and the other end of the shell assembly is formed into a shape of an opened hollow cylinder. The shock absorbing ball is housed inside the shell assembly. The closing plate is joined to the closed plane of the shell assembly and blocks the inflow of fluid. | ||||||
| 34 | Imaging lidar transmitter downlink for command guidance of underwater vehicle | US62467 | 1993-05-13 | US5442358A | 1995-08-15 | R. Norris Keeler; Robert S. Manthy; Troy J. LaMontague; Randall McGee |
| An underwater maneuverable vehicle is presented which carries an explosive charge and can be used for immediate removal or destruction of various menaces to navigation and other underwater hazards. The battery powered vehicle is air dropped from a platform which carries an imaging lidar system for detection and is operated and navigationally controlled in conjunction with an imaging lidar system. In accordance with an important feature of this invention, an optical lidar downlink is used to control the submerged underwater maneuverable vehicle from an airborne platform. The downlink is pulse spaced modulated. Command signals are secure, and are decoded aboard the vehicle. Control in speed, heading and depth, as well as command detonation are available using this technique. | ||||||
| 35 | Underwater guide vehicle for removal of submerged and floating navigational hazards | US760872 | 1991-09-16 | US5248978A | 1993-09-28 | Robert S. Manthy; R. Norris Keeler; Kirk Daniels; Patrick L. Renehan; Anthony R. Wells |
| An underwater maneuverable vehicle is presented which carries an explosive charge and can be used for immediate removal or destruction of various menaces to navigation and other underwater hazards. The battery powered vehicle is air dropped from a platform which carries an imaging lidar system for detection and is operated and navigationally controlled in conjunction with an imaging lidar system. | ||||||
| 36 | Release mechanism | US60972467 | 1967-01-13 | US3403650A | 1968-10-01 | BLACK WALTER L |
| 37 | Stabilizing device | US56873944 | 1944-12-18 | US2943568A | 1960-07-05 | PAVIAN HENRY C |
| 38 | Air stabilizer release mechanism | US51710755 | 1955-06-21 | US2880687A | 1959-04-07 | KILVERT CHARLES A |
| 39 | Electric control system | US66320246 | 1946-04-18 | US2700356A | 1955-01-25 | HUGHES ARTHUR V; RADEMACHER LAWRENCE B |
| 40 | Aerial torpedo | US39929041 | 1941-06-23 | US2401853A | 1946-06-11 | BAILEY ROBERT A |
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