| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | Apparatus for the detection and destruction of incoming objects | EP86301701 | 1986-03-10 | EP0199447A3 | 1988-04-27 | Spector, Yechiel; Cohen, Ilan; Lorber, Azriel |
Detection apparatus which is sensitive both to radiation and to the proximity of the radiation source, as well as destruction apparatus embodying detection apparatus. |
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| 62 | Apparatus for the detection and destruction of incoming objects | EP86301701.8 | 1986-03-10 | EP0199447A2 | 1986-10-29 | Spector, Yechiel; Cohen, Ilan; Lorber, Azriel |
Detection apparatus which is sensitive both to radiation and to the proximity of the radiation source, as well as destruction apparatus embodying detection apparatus. |
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| 63 | Projectile delivery of disruptive media for target protection from directed energy | US15088286 | 2016-04-01 | US09846016B2 | 2017-12-19 | Donald V. Drouin, Jr.; Mark J. Clemen, Jr. |
| Methods, devices, and systems may protect a target from undesirable electromagnetic radiation by detecting electromagnetic radiation (including coherent radiation such as laser beams) aimed at a target from a source; calculating a first release position to disrupt the electromagnetic radiation thereby protecting the target; launching a projectile that may include a disruptive medium or a disruptive-medium precursor; directing the projectile to the first release position; and releasing the disruptive medium from the projectile at the first release position, such that the releasing of the disruptive medium forms a cloud of the disruptive medium. | ||||||
| 64 | Optical sensor arrangement | US14394934 | 2013-03-22 | US09404796B2 | 2016-08-02 | Jochen Barth; Thomas Roth; Christian Czeslik |
| An optical sensor arrangement includes two sensors arranged one behind the other. The operational spectral ranges of the sensors match, and the first sensor forms an attenuation filter for the second sensor, which is arranged behind the first sensor. | ||||||
| 65 | Optical Sensor Arrangement | US14394934 | 2013-03-22 | US20150144794A1 | 2015-05-28 | Jochen Barth; Thomas Roth; Christian Czeslik |
| An optical sensor arrangement includes two sensors arranged one behind the other. The operational spectral ranges of the sensors match, and the first sensor forms an attenuation filter for the second sensor, which is arranged behind the first sensor. | ||||||
| 66 | Optical proximity fuze | US12595003 | 2009-08-06 | US08757064B2 | 2014-06-24 | Martyn Robert Jennings; Lee Douglas Miller |
| Described herein is an optical fuze for a guided missile that comprises an array of a large number of optical apertures distributed about the outer surface of the missile. An optical waveguide network selectively couples the array of apertures to a laser source and to a photodetector such that light from the laser source is emitted by selected ones of said apertures, and light returned from a target is received by selected ones of said apertures and directed by said optical waveguide network to said photodetector. These apertures might be arranged to form a composite target images in a particular direction, and/or may be arranged to perform a sensing operation along selected directions. The optical proximity fuze described herein provides inherent flexibility in the way the fuze can be configured in the missile for optimisation for different applications. | ||||||
| 67 | Method and system for activating the charge of a munition, munition fitted with a high precision activation device and target neutralisation system | US11572565 | 2005-07-22 | US08146499B2 | 2012-04-03 | Jean-Paul Guyvarch; Patrick Doignon |
| This invention relates to a method and a system for activating a munition charge. It also relates to a munition fitted with a high precision activation device. Finally, it relates to a system for neutralization of a target.A laser beam (21) is used for illuminating an object (3) located close to the target (X), firing of the charge (23) of the munition being activated using detection by the munition of the laser spot (24) reflected by the object (3). Firing is activated at a time t1 after the time t0 at which the laser spot (24) is detected.The invention is applicable particularly to hit hidden targets for which a direct impact with these targets is not necessary. | ||||||
| 68 | Spectral filter with dye-impregnated resonant nano-spheres | US11948874 | 2007-11-30 | US07538335B1 | 2009-05-26 | Francis Lawrence Leard |
| Embodiments of spectral filters with dye-impregnated nano-spheres are described herein. Other embodiments may be described and claimed. In some embodiments, a spectral filter comprises a host material that includes a plurality of nano-particles embedded within. The particles include a dye having an absorption band of wavelengths and have a size selected to resonate at a range of wavelengths that is within the absorption band. The particles may be selected to resonate in either a plasmon mode or a whispering-gallery mode. | ||||||
| 69 | Sensor system with modular optical transceivers | US11471926 | 2006-06-21 | US20070295891A1 | 2007-12-27 | Yaujen Wang; Brendan J.D. Irwin; Raj K. Shori |
| An optical sensor system and method includes a plurality of optical transceiver modules arranged across the surface of the optical sensor in a predetermined pattern. A given optical transceiver module includes an optical transmitter that produces at least one light beam and an optical receiver that detects reflected light from the at least one light beam. The optical transceiver module further includes housing for housing the optical transmitter and the optical receiver. | ||||||
| 70 | Method And System For Activating The Charge Of A Munition, Munition Fitted With A High Precision Activation Device And Target Neutralisation System | US11572565 | 2005-07-22 | US20070193466A1 | 2007-08-23 | Jean-Paul Guyvarch; Patrick Doignon |
| This invention relates to a method and a system for activating a munition charge. It also relates to a munition fitted with a high precision activation device. Finally, it relates to a system for neutralisation of a target. A laser beam (21) is used for illuminating an object (3) located close to the target (X), firing of the charge (23) of the munition being activated using detection by the munition of the laser spot (24) reflected by the object (3). Firing is activated at a time t1 after the time t0 at which the laser spot (24) is detected. The invention is applicable particularly to hit hidden targets for which a direct impact with these targets is not necessary. | ||||||
| 71 | Bullet | US10518167 | 2003-06-17 | US07089865B2 | 2006-08-15 | Alon Regev |
| The present invention relates to a hollow bullet for a light weapon which comprises within said hollow: (a) At least one proximity sensor at the front portion of the bullet for sensing an object, and for providing a sensing indication of a proximity object to a control unit;—A control unit for providing a detonation signal to an explosive charge within the bullet upon receipt of said proximity indication;—and An explosive charge for detonating upon receipt of said detonation signal from said control unit. | ||||||
| 72 | Bullet | US10518167 | 2003-06-17 | US20060130696A1 | 2006-06-22 | Alon Regev |
| The present invention relates to a hollow bullet for a light weapon which comprises within said hollow: (a) At least one proximity sensor at the front portion of the bullet for sensing an object, and for providing a sensing indication of a proximity object to a control unit;—A control unit for providing a detonation signal to an explosive charge within the bullet upon receipt of said proximity indication; and—An explosive charge for detonating upon receipt of said detonation signal from said control unit. | ||||||
| 73 | Imaging-infrared skewed cone fuze | US09922360 | 2001-08-04 | US06817296B2 | 2004-11-16 | Hayden N. Ringer; Abraham Shrekenhamer |
| A fuzing system for non-spinning or substantially non-spinning weapons is implemented by means of wide angle optics providing at least forward-hemisphere coverage, an array of infrared detectors and a microprocessor for image and data processing, aim-point selection, directional-warhead aiming and skewed-cone fuzing. The skewed-cone fuzing has a generatrix which is the vector sum of missile velocity, warhead velocity and the negative of target velocity. | ||||||
| 74 | Short pulse automatic ranging anti-ship missile fuze | US05069516 | 1970-08-06 | US06617998B1 | 2003-09-09 | Richard D. Cook; Bennie D. Macomber; William F. Vizard; Eldridge A. Williamson; Anthony Estrada |
| An active short pulse fuze system for arming on a true target acquisition and firing only on the loss of the acquired target signal. The sea surface is tracked by means of a sea tracking loop A target threshold is established and is coupled to the sea tracking loop so as to expand and contract with the sea tracking. A return signal will pass the target threshold only when there is an abrupt reduction in range, indicating the presence of a target. The presence of this signal will arm the firing circuit. An abrupt increase in range will indicate the loss of the target and cause immediate detonation of the warhead. | ||||||
| 75 | Fly over homing guidance for fire and forget missile systems | US806750 | 1997-03-03 | US5932833A | 1999-08-03 | Ricky K. Hammon; Monte K. Helton |
| The fly over homing guidance system for terminal homing missile guidance is fire and forget missile guidance method wherein on board target sensing tracks the target and guides the missile to the target, but instead of being guided to a direct impact as is conventionally done, the missile is guided toward a precise distance over the top of the target, intentionally avoiding impact. A second sensor on the missile detects the leading edge of the target, such as the turret of a tank. The warhead is then fired down onto the top of the target as the missile is guided or directed over it. Further, the shot line of the warhead is substantially perpendicular to the top of the target, maximizing lethality. This allows the use of the same angle of attack and warhead for all modes of target engagement and thus maintains high lethality for every firing scenario. | ||||||
| 76 | Device for optically guiding an autorotating missile | US325330 | 1981-10-28 | US5458298A | 1995-10-17 | Pierre L. M. Lamelot |
| An optical guidance device comprises an entry lens of which the optical axis merges with the axis of rotation of the missile, a filiform infrared detector, sensitive to the infrared radiation of a target, is placed in the focal plane of the lens. The detector is intersected at least twice by circles centered on the axis of rotation of the missile. A circuit elaborates deviation information from the output signals from the detector. Steering means are provided for correcting the path of the missile from the deviation information. | ||||||
| 77 | Infrared proximity detector device for flying missile and detector assembly for autorotating missile including such device | US325356 | 1981-10-28 | US5456179A | 1995-10-10 | Pierre L. M. Lamelot |
| A proximity detector device comprises a lens placed at the front of the missile, two circular infrared detectors of different radii centered on the optical axis of the lens and disposed in its focal plane. An electronic circuit is connected to the detectors for delivering a proximity signal when the time slot separating two pulses emitted by the two detectors is less than a predetermined threshold. The explosion of the missile is controlled by the proximity pulse. | ||||||
| 78 | Munition comprising target detection means | US85052 | 1993-07-02 | US5448500A | 1995-09-05 | Thierry Bredy; Emmanuel Marchand; Philippe Martin; Christophe Redaud |
| A munition including a submunition has a target detector and a core-generating charge with a firing axis .DELTA. for firing a projectile. The munition is designed to move relative to the ground and seek a target. The munition rotates about an axis A with a velocity translation v.sub.0. The target detector includes several detection axes .delta..sub.1 through .delta..sub.n and a device for selecting a detection axis .delta..sub.i from the detection axes .delta..sub.1 -.delta..sub.n for which the distance E between the point M.sub.i at which the axis .delta..sub.i intersects the ground and the point M' at which the projectile strikes the ground is minimal. | ||||||
| 79 | Directed-effect munition | US124012 | 1993-09-21 | US5341743A | 1994-08-30 | Christophe Redaud |
| A directed-effect submunition moves in a substantially vertical direction V with a displacement velocity v parallel to V and a rotation velocity r about an axis parallel to V. The submunition includes a shaped charge with axis D forming an acute angle t with axis V and a detection device with axis d forming an angle u with axis D, a target detecting device, and a triggering device. The submunition also includes a displacement velocity v determining device, and a calculation device for calculating as a function of v a value u.sub.i for angle u that minimizes deviation (e) between the position (M) of a target detected, and impact point (M') of the penetrator of the shaped charge if the latter were triggered upon detection, as well as a device for imparting the value u.sub.i to angle u. | ||||||
| 80 | Target detection and fire control system for parachute-suspended weapon | US321001 | 1981-11-13 | US5339742A | 1994-08-23 | Garry N. Hulderman; Hugh L. Ord |
| A system for controlling the arming and firing of a weapon that is suspended from a parachute at an oblique angle and spun so as to be aimed over a spiral rotational scanning pattern on the earth as the parachute descends toward the earth. The weapon is supported by a platform so that the weapon is aimed in a predetermined direction relative to the platform. A detection system is supported by the platform and aimed in the same direction as the weapon for detecting predetermined radiation characteristics from targets of opportunity. A ranging system is supported by the platform and aimed in the same direction as the weapon for determining the range to the earth in such direction. A first circuit is coupled to the ranging system for enabling the weapon to be armed in response to the ranging system determining that the range to the earth in the direction that the weapon is aimed is less than a first predetermined distance; and a second circuit is coupled to the detection system and the ranging system for enabling an armed weapon to be fired in response to either the detection system detecting the predetermined radiation characteristics or the ranging system determining that the range to the earth in the direction that the weapon is aimed is less than a second predetermined distance that is shorter than the first predetermined distance. | ||||||
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