| 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 | Proximity fuze | US189250 | 1962-04-18 | US4163423A | 1979-08-07 | Hans W. Kohler |
| 4. In a projectile comprising a casing having a first electrically conducg part, a second electrically conducting part and an electrically insulating part interposed between said first and second conducting part, a proximity detector comprising:(a) a bridge circuit;(b) said bridge circuit having a first terminal connected to said first electrically conducting part of said projectile casing; and(c) said bridge circuit having a second terminal adjacent to said first terminal and connected to said second electrically conducting part of said projectile casing. | ||||||
| 2 | Proximity fuse | US56458856 | 1956-02-09 | US2998775A | 1961-09-05 | CRAFT JOHN B |
| 3 | Electric field enabled proximity fusing system | JP32052290 | 1990-11-22 | JPH03217799A | 1991-09-25 | RICHIYAADO TOOMASU TSUIINBA |
| PURPOSE: To restrict explosion of a warhead until encountering a flying target, by a method wherein an arming signal generated in response to a voltage of a probe as a missile approaches into an electric field inherently associated with the flying target is applied to a first detecting part to detonate the warhead. CONSTITUTION: Current proportional to the voltage of a probe 24 to be generated as a missile approaches an electric field of a target is converted to a voltage of a signal and amplified to be supplied to a microprocessor 30. When an attack target is captured, the microprocessor 30 outputs an arming signal to make a fuse 36 of a warhead of the missile ready for operation. An RF receiver 38 of an active type proximity searching part transmits a signal via a radar antenna 26 and receives a signal returned from the target 10 to generate a signal for triggering the fuse by a microprocessor 40, which is applied to the other output side of a coincidence gate 34. But a gate 34 will not operate until the missile enters a range of a target detecting distance of a passive type detecting part 29, thereby preventing earlier detonation of the fuser 36. COPYRIGHT: (C)1991,JPO | ||||||
| 4 | Electrostatic passive proximity fusing system | JP32222590 | 1990-11-26 | JPH03217800A | 1991-09-25 | RICHIYAADO TOOMASU TSUIINBA; DEIBITSUDO JIYOOJI HOITO |
| PURPOSE: To shoot down an attacking target with the maximum damage, by a method wherein it is judged whether the initial slope of a waveform of a probe current increases or not within a set range of a value of a characteristic slope of the attacking target, and, when the reference is met, a warhead is detonated by the first zero current crossing made in the waveform of the signal. CONSTITUTION: Current of a probe short circuiting circuit flows in the form of a slope Part 38a increasing on the initial negative side. As a distance to a target is shorter, the waveform of the current of the short circuiting circuit is rapidly inverted in slope to cause a crossing of the zero level at a point 38b and further rises up to a peak 38c. As the polarity of the peak 38c is opposite to the polarity of the initial current, the peak 38c is a point which coincides with a position where a missile approaches the target the most on a target proximity effective destruction flying path 16a. A microprocessor 34 converts an amplified analog probe signal to a digital signal to enable the determination of the timing for the detonation of a fuser and the explosion of a warhead when the missile is precisely flying over the target proximity effective destruction flying path 16a. COPYRIGHT: (C)1991,JPO | ||||||
| 5 | Radome nose cone probe apparatus for use with electrostatic sensor | EP97110242.1 | 1997-06-23 | EP0816762A3 | 1999-04-07 | Crist, Scott D. |
A radome probe apparatus for use with an electrostatic proximity sensor is disclosed. The apparatus comprises a radome nose cone probe connected to a projectile and having an inner surface. The nose cone is made of a dielectric material. Single or multiple electrically conducting areas are connected to the inner surface of the nose cone. The conducting areas are dielectrically isolated. Electronics are utilized to sense the time rate of change voltage or current between the areas due to the intrinsic electrostatic charge on a target aircraft. |
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| 6 | Electrical fuze with a plurality of modes of operation | US97763 | 1979-11-27 | US4291627A | 1981-09-29 | Richard T. Ziemba; Joseph A. Kinzel; Myron D. Egtvedt |
| A feature of this invention is the provision of a fuze having a plate which serves both as a full frontal area impact switch and an electrostatic sensor to provide detonation signals. | ||||||
| 7 | Fluidic capacitance device | US527177 | 1974-11-25 | US3948183A | 1976-04-06 | Evan D. Fisher; Carl J. Campagnuolo; Stacy E. Gehman |
| The transmitter for an A.C. capacitance proximity fuze consists of an A.C.enerator whose output is directly connected to the transmitter probes of an A.C. capacitance fuze. The A.C. generator may be either a wind driven alternator or a fluid oscillator power supply driven by the ram pressure of the air. This arrangement eliminates the need for a separate oscillator as the power supply is now also the transmitter. | ||||||
| 8 | Field fuze | US66799757 | 1957-06-25 | US3877382A | 1975-04-15 | KALMUS HENRY P |
| 1. A missile fusing system of the quasi-stationary field type, said system comprising in combination: an explosive missile having a case; two electrodes each extending through and insulated from the case of said missile and located at diametrically opposed positions around the periphery of said case; neutralizing means for reducing the free space transfer capacitance between said electrodes in order to make the increase in transfer capacitance between said electrodes, as said missile approaches a target, a readily detectable portion of the total transfer capacitance; said neutralizing means including external electrostatic shielding means consisting of the case of said missile and internal electrostatic shielding means consisting of an internal projection of said case; balancing means for balancing out the remainder of said free space transfer capacitance not eliminated by said neutralizing means; and means responsive to a predetermined increase in the transfer capacitance between said electrodes caused by target proximity to detonate said missile.
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| 9 | Electrostatic proximity fuse | US21765251 | 1951-03-26 | US3871296A | 1975-03-18 | HEILPRIN LAURENCE B; NORDQUIST GEORGE; KRUPEN PHILIP |
| 1. In combination with an explosive missile, an electrostatic fuse comprising: a conical casing mounted at the nose end of said missile, said casing having a metal cap at its narrow end and an insulating skirt between said cap and the body of said missile whereby a capacitance C exists between said cap and said body, said cap and said body having a charge placed thereon during missile launching; a resistance R connected between said cap and said body, said resistance R thereby being in parallel with the capacitance C, the value of said resistance R being such that the time constant RC is long compared to the time the missile is within proximity of a target, but short compared to the time of flight of the missile; a pentode mounted within said missile at its nose end, said pentode having an anode, a cathode, and three grids, the number 2 grid of said pentode being connected to said cap, and the number 1 and number 3 grids of said pentode being connected to said cathode, said cathode being connected to the body of said missile, said number 2 grid thereby being shielded from both said anode and said cathode; a positive voltage source within said missile; a resistor connected between the anode of said pentode and said source; a firing circuit having a thyratron, a charged capacitor, and a detonator, said thyratron having an anode, a cathode, and a grid, said charged capacitor and detonator being connected in the anode circuit of said thyratron; and a coupling network connected between the anode of said pentode and the grid of said thyratron; the greater increase in the capacitance of said cap than that of said body upon approach of said missile to a target causing a change in the voltage across said parallel capacitance C and resistance R, this voltage change being amplified by said pentode and transferred by said coupling network to the grid of said thyratron, whereupon said thyratron conducts causing said charged capacitor to pass a current through said detonator causing functioning thereof.
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| 10 | Proximity fuze improvement | US30245672 | 1972-10-31 | US3838645A | 1974-10-01 | FINGER D; WOOD G; HIGH R; HARRISON E |
| Projectiles utilizing proximity fuzes wherein the windshield structure thereof is capable of withstanding the buildup of static electrical charges on the surface thereof resulting in the prevention of premature functioning of said fuzes comprising in combination a conical windshield portion and a cylindrical base portion. The conical windshield comprises an electrically conductive surface capable of withstanding and rapidly dispersing electrical charges on the surface and having a surface resistivity of between about 1.0 and 200 megohms per square.
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| 11 | 3 plate proximity scorer | US10407561 | 1961-04-19 | US3218623A | 1965-11-16 | BUNTENBACH RUDOLPH W |
| 12 | Radome nose cone probe apparatus for use with electrostatic sensor | EP97110242.1 | 1997-06-23 | EP0816762A2 | 1998-01-07 | Crist, Scott D. |
A radome probe apparatus for use with an electrostatic proximity sensor is disclosed. The apparatus comprises a radome nose cone probe connected to a projectile and having an inner surface. The nose cone is made of a dielectric material. Single or multiple electrically conducting areas are connected to the inner surface of the nose cone. The conducting areas are dielectrically isolated. Electronics are utilized to sense the time rate of change voltage or current between the areas due to the intrinsic electrostatic charge on a target aircraft. |
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| 13 | Proximity fuzing system | EP90312909.6 | 1990-11-28 | EP0434242A2 | 1991-06-26 | Ziemba, Richard Thomas; Hoyt, David George |
A proximity fuzing system for missile warhead utilizes an electrostatic probe (24) to detect the electric field inherently associated with an airborne target. The probe plates (26,28) are oriented perpendicular to the missile longitudinal axis (17) and are short circuit loaded to develop a probe current signal whose initial slope is analyzed to qualify the target being engaged on a near-miss trajectory as a valid target and whose first zero current crossing is utilized as a trigger point for detonating the missile warhead before the missile reaches a position of minimum miss-distance relative to the target. |
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| 14 | Annäherungsschalter zum Zünden einer Hohlladung, insbesondere für eine Mine | EP87890004.2 | 1987-01-14 | EP0235115B1 | 1989-10-04 | Zierler, Reinhard |
| 15 | Dual purpose munition | US11306024 | 2005-12-14 | US07654458B1 | 2010-02-02 | Victor N. Kokodis; Arnold S. Klein |
| A dual purpose munition includes a housing; a shaped warhead disposed in a front interior of the housing; a vertically orienting explosive disposed on a front end of the housing; a safe and arm device explosively connected to the shaped warhead for arming and detonating the shaped warhead; a dual sensor circuit comprising an E-field sensor board, a B-field sensor board and a processor board; and a power source connected to the dual sensor circuit and the safe and arm device. | ||||||
| 16 | Systems and methods for reducing common-mode platform noise in electric-field sensors | US11514980 | 2006-09-05 | US07411401B1 | 2008-08-12 | David M. Hull; Mark R. Probst |
| Systems and methods for reducing electrostatic platform noise in electric-field sensors due to various self-charging and discharging processes are provided. A representative method includes: identifying avoidance regions of an electrostatically-floating sensor platform that have a propensity for self-induced charging and discharging; locating a first electrode and a second electrode on the electrostatically-floating sensor platform, wherein the first electrode and the second electrode are positioned and dimensioned to receive substantially equal amounts of distributed charge via self-charging; and obtaining a differential signal from these two electrodes that is proportional to an external ambient E-field of interest, while at the same time nulling out the common-mode signal that results from sensor platform self-charging and/or discharging. | ||||||
| 17 | Radome nose cone probe apparatus for use with electrostatic sensor | US668690 | 1996-06-24 | US6094054A | 2000-07-25 | Scott D. Crist |
| A radome probe apparatus for use with an electrostatic proximity sensor is disclosed. The apparatus comprises a radome nose cone probe connected to a projectile and having an inner surface. The nose cone is made of a dielectric material. Single or multiple electrically conducting areas are connected to the inner surface of the nose cone. The conducting areas are dielectrically isolated. Electronics are utilized to sense the time rate of change voltage or current between the areas due to the intrinsic electrostatic charge on a target aircraft. | ||||||
| 18 | Electric field enabled proximity fuzing system | US451901 | 1989-12-18 | US4991508A | 1991-02-12 | Richard T. Ziemba |
| A proximity fuzing system includes a passive proximity detection section including an electrostatic probe for detecting initial missile entry into the electric field inherently associated with an airborne target. Probe signals are processed to determine that the intercepted electric field is characteristic of a valid target, and, if so, an active proximity detection section, such as a radar proximity detector, is rendered operational to trigger a warhead detonator at the optimum point in the missile's engaging trajectory to inflict maximum possible damage on the target. | ||||||
| 19 | Electrostatic passive proximity fuzing system | US452151 | 1989-12-18 | US4972775A | 1990-11-27 | David G. Hoyt; Richard T. Ziemba |
| A proximity fuzing system for missile warhead utilizes an electrostatic probe to detect the electric field inherently associated with an airborne target. The probe plates are oriented perpendicular to the missile longitudinal axis and are short circuit loaded to develop a probe current signal whose initial slope is analyzed to qualify the target being engaged on a near-miss trajectory as a valid target and whose first zero current crossing is utilized as a trigger point for detonating the missile warhead before the missiles reaches a position of minimum miss-distance relative to the target. | ||||||
| 20 | Underwater electric current and alternating magnetic field detector | US295142 | 1952-06-23 | US4218975A | 1980-08-26 | Donald F. Ream |
| 1. An underwater eddy current detector comprising a hollow elongated conding member, said conducting member having a plurality of longitudinal conducting paths forming portions of the exterior surface of said conducting member, a portion of said conducting member formed of material having conductivity of lesser degree than said conducting member and arranged to direct eddy currents induced in said conducting member to said conducting paths, a plurality of toroidal detector coils wound upon annular laminated structures, each of said detector coils encircling one of said conducting paths, whereby a potential which is proportional to a detected signal is induced in said coils when said conducting member is submerged in a conducting medium and located in the path of flow of a plurality of currents flowing in said conducting medium. | ||||||
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