| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Electrical delay arming always impact fuze | US3618524D | 1968-09-04 | US3618524A | 1971-11-09 | BERLIN AARON S; LITTLE VINCENT C |
| A fuze, method, and system for arming munitions for low altitude delivery wherein the energy source for arming the fuze is selfcontained within the mechanism and utilized subsequent to release of the munition from the delivery means.
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| 122 | Percussion fuze for a missile and procedure for the assembly of same | US3500748D | 1968-11-25 | US3500748A | 1970-03-17 | HAGER AUGUST; BIAGGI LOUIS |
| 123 | Self-sealing lanyard device | US2644760 | 1960-05-03 | US3054618A | 1962-09-18 | ABRAMS BERNARD W; HARVEY FREEDER |
| 124 | Means for initiation of detonator | US43092354 | 1954-05-19 | US2873680A | 1959-02-17 | SEVERANCE RALPH H |
| 125 | Supporting spider for use in proximity fuze | US22276351 | 1951-04-25 | US2741181A | 1956-04-10 | MARKS WILLIAM S |
| 126 | Fuse | US25241539 | 1939-01-23 | US2448022A | 1948-08-31 | FIX EUGENE J |
| 127 | Gasket | US50712443 | 1943-10-21 | US2439923A | 1948-04-20 | CLARK EARL K |
| 128 | Firing mechanism | US48576143 | 1943-05-05 | US2419349A | 1947-04-22 | SAMUEL GILBERT |
| 129 | Hand grenade | US38473541 | 1941-03-22 | US2330490A | 1943-09-28 | DOUGLASS HIBBS EARL |
| 130 | Shell or bomb | US5755936 | 1936-01-04 | US2197841A | 1940-04-23 | SLAUGHTER CHARLES E |
| 131 | FUZE SHOCK TRANSFER SYSTEM | EP15800998.5 | 2015-05-29 | EP3218666A1 | 2017-09-20 | CUNDIFF, Brandon J.; SPILOTRO, John J.; LEE, Wayne Y.; CHRISTIANSON, Kim L.; BOOTES, Thomas H.; SHIRE, Jason M.; WADDELL, Jesse T. |
| A munition has a fuze that is mounted nonparallel to the axis of the munition, for example having a largest extent that is perpendicular to the longitudinal axis of the munition. Shocks from the fuze are transferred through a shock transfer device that is in contact with the fuze, to an initiation device that is also in contact with the shock transfer device. Shocks passing through the shock transfer device to the initiation coupler pass through a relatively narrow neck of the shock transfer device. In the shock transfer device the shock is concentrated and located precisely at the neck, before spreading out again and being transferred to the initiation device. In the initiation device the shock may detonate a high explosive material, which in turn is used to detonate a main explosive of the munition, such as a warhead. | ||||||
| 132 | Method for validating fuse heads | EP15382155.8 | 2015-03-30 | EP3076123A1 | 2016-10-05 | Montaño Rueda, Luis Diego; Niekerk, Hendrik Van; Botija González, José Manuel; Zabalo Arena, Íñigo |
Method for the validation of a fuse head (1) in an electronic detonator, wherein said detonator comprises: a reference resistor (R13), a fuse head (1), at least one capacitor and switching means, wherein in a first position of the switching means, the reference resistor is connected to the at least one capacitor forming a first RC circuit, and in a second position of the switching means, the fuse head is connected to the at least one capacitor forming a second RC circuit; the method comprising the following steps: measuring at least once a first charge time; activating the switching means to the second position to replace the reference resistor in the RC circuit with the fuse head; measuring at least once a second charge time; and determining the deviation of the second charge time from the first charge time.
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| 133 | CHANGING THE STATE OF A SWITCH THROUGH THE APPLICATION OF POWER | EP11866905 | 2011-10-11 | EP2697811A4 | 2014-11-26 | BONAVIDES CLOVIS S |
| 134 | CHANGING THE STATE OF A SWITCH THROUGH THE APPLICATION OF POWER | EP11866905.0 | 2011-10-11 | EP2697811A1 | 2014-02-19 | BONAVIDES, Clovis S. |
| A switch includes a spring. The switch includes a collapsing element. The spring has a first spring state in which it is being held in tension by a restraining element and a second spring state in which it is not being held in tension because the restraining element has failed. The collapsing element is situated such that when sufficient power is applied to the collapsing element heat from the collapsing element will cause the restraining element to fail. The switch includes a first contact coupled to the spring. The switch includes a second contact coupled to the spring. The first contact and the second contact have a first 1-2 electrical connection state when the spring is in the first spring state. The first contact and the second contact have a second 1-2 electrical connection state different from the first 1-2 electrical connection state when the spring is in the second spring state. | ||||||
| 135 | Dispositif propulsif à progressivité regulée | EP09290837.5 | 2009-11-04 | EP2192376A1 | 2010-06-02 | Caillaut, Nicolas |
L'invention concerne une cartouche de propulsion d'un projectile (22) de calibre d'au moins 90mm, et un dispositif de propulsion comportant une telle cartouche, la cartouche étant caractérisée en ce qu'elle comprend : |
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| 136 | Shock-resistant electronic circuit assembly | EP00126637.8 | 2000-12-04 | EP1106956B1 | 2005-11-16 | Marshall, Paul N.; Walsh, Brendan M.; Marshall, Thomas C.; Fritz, James E. |
| 137 | Electrowetting battery having a nanostructured electrode surface | EP04256701.6 | 2004-10-29 | EP1533857A1 | 2005-05-25 | Kroupenkine, Timofei N.; Taylor, Joseph A.; Weiss, Donald |
A method and apparatus are disclosed wherein a battery comprises an electrode having at least one nanostructured surface. The nanostructured surface is disposed in a way such that an electrolyte fluid of the battery is prevented from contacting the electrode, thus preventing discharge of the battery when the battery is not in use. When a voltage is passed over the nanostructured surface, the electrolyte fluid is caused to penetrate the nanostructured surface and to contact the electrode, thus activating the battery. In one illustrative embodiment, the battery is an integrated part of an electronics package. In another embodiment, the battery is manufactured as a separate device and is then brought into contact with the electronics package. In yet another embodiment, the electronics package and an attached battery are disposed in a projectile that is used as a military targeting device. |
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| 138 | Munitionsartikel mit Antenne für die Satellitennavigation | EP01118654.1 | 2001-08-03 | EP1178279B1 | 2004-11-10 | Koch, Volker; Hertel, Martin; Wiesbeck, Werner, Dr.; Gschwendtner, Eberhard |
| 139 | SHOCK-RESISTANT ELECTRONIC CIRCUIT ASSEMBLY | EP97911702.5 | 1997-10-09 | EP0935734B1 | 2004-05-26 | MARSHALL, Paul, N.; TSEKA, Thomas, C.; WALSH, Brendan, M.; FRITZ, James, E. |
| A shock-resistant electronic circuit assembly (10) is provided in which an electronic circuit is encased in an encapsulation (14) that engages a surrounding enclosure (18, 22) in shock-dispersing contact therewith. The encapsulation may have a plurality of edges (16, 16a, 16b), fins (24) or bosses (70) that bear against the enclosure. The encapsulation may include a shock-absorbing material (14f) disposed against the enclosure to protect the circuit against vibrations and a structural support material (14e) to protect the circuit against stress. The circuit assembly (10) may contain a capacitor (34) for storing an electrical signal and timing circuitry for releasing the stored energy after a predetermined delay. The circuit assembly (10) may be part of a transducer-circuit assembly (55) that includes a transducer module (58) for converting shock wave energy into electrical energy for the electronic circuit, and the released enregy may be converted into a detonation initiation signal. Assembly (55) may be part of a detonator (100) that receives a non-electric initiation signal and detonates following the delay determined by the electronic circuit. The detonator housing (112) or an optional sleeve (22) provides an enclosure for the assembly (55). | ||||||
| 140 | Munitionsartikel mit Antenne für die Satellitennavigation | EP01118654.1 | 2001-08-03 | EP1178279A3 | 2003-08-20 | Koch, Volker; Hertel, Martin; Wiesbeck, Werner, Dr.; Gschwendtner, Eberhard |
Ein Munitionsartikel (11) soll mit einer Antenne (18) ausgestattet sein, die aufgrund rundum gleichförmiger Charakteristik einen störungsfreien Empfang von Satelliten-Navigationsinformationen auch dann ermöglicht, wenn er nach Art eines Artillerie-Projektiles (12) unter Drall längs einer gestreckten ballistischen Flugbahn verbracht wird, so daß eine Heckantenne mit kugelförmiger Charakteristik keine guten Empfangsgegebenheiten bezüglich möglichst hoch über dem Horizont stehender Navigationssatelliten erwarten läßt. Deshalb ist die Zünder-Spitze (13) des Projektiles (12) mit einem als Rundschlitz-Satellitenantenne (18) ausgelegten Hohlkegelstumpf aus elektrisch leitendem Material wie Leichtmetall ausgestattet, in dem ein koaxialer Ring-Hohlraum (25) über einen radial zur Projektil-Längsachse (16) umlaufenden ringscheibenförmigen Schlitz (23) zur Zünder-Mantelfläche (19) hin geöffnet ist. Als Speisekabel können Koaxialkabel (28) gleichmäßig über den Umfang verteilt mit ihren Innen- bzw. Außenleitern (28.1, 28.2) bei der inneren Mündung (22.2) des Schlitzes (20) zum Hohlraum (25) hin an die Schlitzwände (31) angeschlossen sein. |
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