| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | Infrared detection device | US999671 | 1992-12-30 | US5299499A | 1994-04-05 | Bernard M. E. Christophe; Roger Muller |
| Infrared detection device carried by a missile falling to earth and rotating about its axis with a given inclination, said device being intended to trigger off firing of the missile when it detects a source of infrared emission of predetermined type, the device comprising at least one infrared detector sensitive to the infrared emission of said sources and an amplifier device connected to the output of the detector. | ||||||
| 82 | Device and method for monitoring the presence of an object in space | US518620 | 1990-05-03 | US5018447A | 1991-05-28 | Walter E. Miller, Jr.; Robert R. Mitchell; Donald E. Lovelace |
| An optically transparent cylinder having a hemispherical cavity at one endhereof and containing at least one light source and one light detector inside the hemispherical cavity utilizes the prismatic effect of the cylinder to locate an object in space. The light source and detector are located on a disk whose insertion depth into the cavity and tilt angle inside the cavity can be varied to control the sharpness, width and direction of the conical beam output from the cylinder, the beam searching the space for the location of the desired object. | ||||||
| 83 | Optical system for conical beam target detection | US045964 | 1987-05-04 | US4809611A | 1989-03-07 | Roy W. Esplin |
| A passive, infrared, conical beam target sensor having multiple beams which may exhibit a wide variety of half conic angles is disclosed. The sensor may be utilized with a missile by positioning a plurality of optical assemblies adjacent to the skin of the missile and near a corresponding plurality of small windows in the skin of the missile. Each optical assembly includes a detector for each conical beam and a wide-angle lens oriented so that a lens axis parallels the axis of the missile. A preferred lens has a flat entrance aperture surface opposing a spherical surface. Unnecessary material is removed from the lens so that the lens axis may reside as close to the missile skin as possible. Each detector includes a plurality of photoelectric elements arranged to populate at least a portion of an annulus. | ||||||
| 84 | Infrared proximity fuze electronic amplifier | US311921 | 1963-09-26 | US4245558A | 1981-01-20 | Michael Flaherty |
| 1. An electronic proximity fuze for a projectile comprising transducer me for converting infrared radiation to an electrical signal, amplifying means connected to said transducer for amplifying said signal, said amplifying means including automatic gain control means for decreasing the gain of said amplifying means upon occurrence of a slowly rising signal, electronic switch means, a source of electrical energy, a detonator, means connecting said switch means said source and said detonator in electrical series circuit, means connecting said amplifying means and said electronic switch means for closing said switch means upon occurrence of a rapidly rising signal of predetermined magnitude, said last named means operating to reduce said predetermined magnitude of the signal when said automatic gain control has decreased the gain of said amplifying means. | ||||||
| 85 | Optical fuze | US136983 | 1961-09-01 | US4195574A | 1980-04-01 | Stephen M. MacNeille |
| 1. An infra-red detector unit adapted to be mounted on a projectile comprng a nose adaptor having at least one aperture therein, an open "O" unit mounted in said nose adaptor and having at least one aperture that is correlated with the aperture in said nose adaptor, insert means having first and second slit apertures substantially filling the aperture in said "O" unit, a reflector comprising a plurality of strips mounted in said "O" unit and having a parabolic curved surface with a first and second focal point for reflecting infra-red rays from a target source as they pass through said first and second slit apertures, first and second infra-red detecting cells mounted at the first and second focal points of said reflector, said infra-red rays passing through said first and second slit apertures and reflected by said reflector onto said first and second detecting cells thereby providing a first channel for said first infra-red detecting cell and a second channel for said second infra-red detecting cell whereby when the infra-red rays pass through the first and second channels in rapid succession during the flight of the projectile a detonating signal is generated. | ||||||
| 86 | Combination infrared radio fuze | US177617 | 1962-03-13 | US4193072A | 1980-03-11 | Wayne L. McKusick |
| 2. A combination proximity fuze comprising a radio circuit and an infraredircuit, said radio circuit operative to produce a first voltage impulse when a reflected electromagnetic wave is received from a target, said infrared circuit operative to produce a second voltage impulse when a heat source from a target is detected, a first memory circuit connected to said radio circuit for storing said first voltage impulse for a first predetermined time interval, a second memory circuit connected to said infrared circuit for storing said second voltage impulse for a second predetermined time interval, a coincidence firing circuit connected to said first memory circuit and to said second memory circuit whereby a primer may be ignited when said first and second voltage pulses are applied to said coincidence firing circuit simultaneously within said first and second predetermined time intervals. | ||||||
| 87 | Fore and aft fuzing system | US170286 | 1962-01-31 | US4185560A | 1980-01-29 | Mayer Levine |
| 1. In a guided missile fuze system that has optimum kill probability against all sizes of targets, the combination comprising:(a) a fuzing channel for generating an output pulse in response to a received target signal after a predetermined time delay from the time said target signal is received,(b) a guard channel for generating an output pulse in response to the loss of a target signal detected by said guard channel,(c) and a firing circuit coupled to the outputs of said fuzing channel and said guard channel for firing the fuze in response to a firing pulse received from either of said channels. | ||||||
| 88 | Optical switch | US680317 | 1976-04-26 | US4023498A | 1977-05-17 | Paul Harris |
| An optical switch, which may be a part of a fuze for an explosive project, comprises a housing made up of a hollow cylindrical part with two end plates welded thereto and having a pair of aligned glass windows sealed through opposite sides for transmitting light transversely therethrough, a gas piston with O-ring seals slidable in the housing to define an end wall of a variable volume gas chamber therein and adapted to be moved by inertia during projectile launch to decrease the volume of the chamber and thereby increase the gas pressure, means for locking the piston in the new position, a valve in the housing for admitting a light attenuating gas to the chamber, an adjustable pressure relief valve in the housing adapted to open when the internal gas pressure exceeds the external pressure by a given amount, a light source positioned adjacent to the outside of one of the windows to project light through the windows and the attenuating gas, and a light-sensitive device positioned on the other side of the housing to receive the attenuated light. When the intensity of the light received by the device equals a critical value, the device responds by performing a desired function, such as arming a firing circuit of the fuze. The gas pressures in the chamber before and after piston movement are higher than a critical pressure at which the light reaching the output device has the critical value. When the projectile is projected to a desired altitude, the reduced atmospheric pressure causes the relief valve to open, reducing the chamber pressure below the critical pressure, thereby exciting the light sensitive device to arm the fuze.The switch may be used with a gas chamber of fixed volume, with a higher initial gas pressure. | ||||||
| 89 | Passive infra-red proximity fuze | US587568 | 1975-06-17 | US4022132A | 1977-05-10 | Ake Hugo Petrus Blomqvist; Bertil Torbjorn Eriksson |
| Apparatus for use in a projectile-borne passive infra-red proximity fuse for detecting infra-red radiation emitted from a target. The apparatus includes at least one pair of optical means which are respectively located at spaced locations around the periphery of the projectile. The pair of optical means is so located that the beams of infra-red radiation associated therewith, which are both imaged upon a common detector, form an angle therebetween both in a plane through the longitudinal axis of the projectile and in a plane normal to such axis. Logic circuitry is provided and controlled by the detector to provide a distinctive output in response to the signals which are generated by the beams of radiation received from a target which is spinning about its longitudinal axis and is within a predetermined distance of the projectile. With the arrangement as described, the detection apparatus produces either two separate pulses or one long pulse for each revolution of the projectile about its longitudinal axis, whereas only a single pulse is produced for each revolution from distant sources of infra-red radiation such as the sun. | ||||||
| 90 | Radiometric target detection device | US142837 | 1971-04-28 | US3978797A | 1976-09-07 | William W. Harrington; Frederick C. Alpers |
| A radiometer is mounted in a guided missile for detecting electro-magnetichermal power in the microwave region of the spectrum radiated from an area of suspected targets with circuitry coupled thereto to respond to a predetermined change in level of radiation to generate a warhead fuzing signal. | ||||||
| 91 | Optical fuze and/or miss distance indicator | US503998 | 1974-09-06 | US3942446A | 1976-03-09 | Orval R. Cruzan |
| An optical miss distance detector and/or fuzing device for a missle. Four tical ring sensors are disposed around the missile body and the active sensing regions of the first and second sensors are disposed at an angle of 90.degree. to the missile axis thereby forming first and second cones of 90.degree. with respect to the axis while the active sensing regions of the third and fourth sensors are disposed at an angle of other than 90.degree. to the axis thereby forming cones of other than 90.degree. with respect to the axis. The third and fourth sensors are positioned along the axis so that the apices of the third and fourth cones coincide respectively with the apices of the first and second cones. The miss distance and relative velocity of the missile and the target are determined based on the times of interception of the cones and the azimuthal angles of interception. A fuzing arrangement is connected to the sensors which generates a detonation signal responsive to a predetermined order of interception of the cones indicating that the target is crossing the missile within a predetermined range. | ||||||
| 92 | Fuze signal processing circuit | US38095764 | 1964-07-07 | US3908552A | 1975-09-30 | DICK JOHN O |
| 1. In a fuze system having an infrared detector means and a firing circuit means, the improvement comprising a processing circuit that is not influenced by the high degree of modulation present in the signals from said detector means as the result of said detector scanning a jet engine exhaust plume, said processing circuit comprising: A. AN INPUT TERMINAL CONNECTED TO AND TO RECEIVE AN INPUT SIGNAL PROPORTIONAL TO INFRARED ENERGY RECEIVED FROM SAID INFRARED DETECTOR MEANS AS THE JET ENGINE EXHAUST PLUME IS SCANNED BY SAID DETECTOR, B. A FIRST DIODE COUPLED TO SAID INPUT TERMINAL AND BEING POLARIZED TO PASS A NEGATIVE GOING AND TO BLOCK POSITIVE SIGNALS, C. A STORAGE CAPACITOR COUPLED TO SAID DIODE AND BEING CHARGED TO PEAK AMPLITUDE OF SAID INPUT SIGNAL, D. AN OUTPUT TERMINAL CONNECTED TO SAID FIRING CIRCUIT MEANS, E. A NORMALLY CLOSED GATE CIRCUIT COUPLED ACROSS SAID STORAGE CAPACITOR AND COUPLED TO SAID OUTPUT TERMINAL, F. A SECOND DIODE COUPLING SAID INPUT TERMINAL TO SAID GATE CIRCUIT AND BEING POLARIZED TO PASS A POSITIVE VOLTAGE TO OPEN SAID GATE CIRCUIT AND DISCHARGE SAID STORAGE CAPACITOR IN RESPONSE TO A POSITIVE OVERSHOOT AT THE TERMINATION OF SAID INPUT SIGNAL.
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| 93 | Proximity fuse for missiles | US34912473 | 1973-04-09 | US3839963A | 1974-10-08 | NATHAN G; VARAUD C |
| A compact fuse designed to be armed after cessation of acceleration and provided with a plurality of safety means; a cap adapted to be set in an inoperative position by a rotation of 90* with reference to the fuse body, a cover for the cap adapted to collapse towards the striker and to prevent its releasing operation in case of a premature impact, a detonator-carrier adapted to be shifted laterally out of registry with the striker, a weight controlled by inertia and controlling operation of the striker and an arming weight releasing through inertia in striker.
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| 94 | Optical system for an infrared missile fuze | US55636355 | 1955-12-29 | US3621784A | 1971-11-23 | MUNDIE LLOYD G |
| 1. AN INFRARED FUZE COMPRISING AN ANNULAR TOROIDAL LENS, A PAIR OF ANNULAR DETECTORS POSITIONED CONCENTRICALLY WITH RESPECT TO THE AXIS OF SAID LENS AND ON OPPOSITE SIDES OF THE FOCAL POINT OF SAID LENS, SHIELDING AN REFLECTING MEANS ASSOCIATED WITH ONE OF SAID DETECTORS WHEREBY THE ENERGY PASSING THROUGH SAID LENS CROSSES THE AXIS THEREOF BEFORE STRIKING SAID DETECTOR, AND ELECTRONIC MEANS ASSOCIATED WITH SAID DETECTORS AND ADAPTED TO RECEIVE SUCCESSIVE SIGNALS FROM SAID DETECTORS DURING A PREDETERMINED INTERVAL FOR ACTUATING A DETONATION CIRCUIT.
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| 95 | Light energized explosive device | US57479666 | 1966-08-24 | US3408937A | 1968-11-05 | LEWIS DONALD J; COOMBS IVAN G |
| 96 | Gun launched terminal guided projectile | US36521664 | 1964-05-05 | US3282540A | 1966-11-01 | LIPINSKI HENRY S |
| 97 | Proximity fuze with electro-optical apparatus | US48360543 | 1943-04-19 | US3060857A | 1962-10-30 | SMITH KENNETH D |
| 98 | Proximity fuse | US82125959 | 1959-06-18 | US3046892A | 1962-07-31 | CLAUDE COSSE; FERNAND LOY |
| 99 | Electric devices for igniting the charge of a projectile, said devices being especially intended for use on anti-aircraft or anti-armour projectiles | US67486057 | 1957-07-29 | US3043222A | 1962-07-10 | ALFRED KASPAUL |
| 100 | Optical fuze | US1000860 | 1960-02-19 | US3034436A | 1962-05-15 | ARTHABER JOSEF M; MOORE WARD J |
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