US4309946A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Laser proximity fuzing device
Assignee: Hughes Missile Systems Co
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Filing: 1967-07-13
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Granted: 1982-01-12
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Expires: 1987-07-13
Abstract
Abstract Broadly, the disclosure is directed to a range-measuring detonating system comprising an air-driven scanning mirror which cooperates with fixed mirrors to project the output of a laser toward a target, the laser being modulated at a given frequency by a local oscillator and modulator circuit. Adjacent the laser is a detecting means which feeds a receiver, the receiver output being in turn delivered to a detector which feeds a phase comparator to which is also applied the output of the local oscillator. The phase comparator output is coupled to an AND circuit to which is also applied the output of the detector. When the light energy returned by a target in the vicinity of the system achieves a given phase and amplitude, the phase comparator output is gated through the AND circuit to ignite a squib, booster and warhead.
Inventors
- 👤 Kenneth A. Block
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 04:57
CPC Classifications
F; F42; F42C; F42C13/00; F42C13/02; F42C13/023; G; G01; G01S; G01S17/00; G01S17/02; G01S17/06; G01S17/08; G01S17/32; G01S17/36
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
365 words
A range-measuring and detonating system comprising: a rolling type air vehicle having a transparent section in the forward portion thereof; air driven propeller means operably mounted in the forward end of said air vehicle for rotation about an axis; a first reflector means operatively mounted in said air vehicle forward of said transparent section and connected to the aft end of said propeller means for rotation with said propeller means about said axis; a second reflector means having a central opening therein operatively mounted in said air vehicle both aft of said transparent section and aft of said first reflector means for directing reflections to said first reflector means and for passing reflections from said first reflector means through said central opening; laser means operably mounted in said air vehicle aft of said second reflector means for directing a beam through said central opening of said second reflector means toward said first reflector means for reflection by said first reflector means; detecting means mounted adjacent said laser means for intercepting and detecting reflections received from said first reflector means through said central opening of said second reflector means and for producing an output signal; receiver means operably connected to said detecting means to receive the output signal from said detecting means and to produce another output signal; detector and threshold assembly means operably connected to said receiver means to receive the output signal from said receiver means and to produce a further output signal; an oscillator mounted in said air vehicle; modulator means operably connected to said detecting means and to said oscillator, said modulator means being responsive to said oscillator; a phase comparator responsive to said oscillator and to the output signal from said detector and threshold assembly means; an AND circuit operatively connected to receive the output from said phase comparator and from said detector and threshold assembly; a trigger generator operably connected to said AND circuit and responsive thereto; a squib operably connected to said trigger generator and responsive thereto; a booster assembly operably connected to said squib and responsive thereto; and an explosive charge operably connected to said booster assembly and responsive thereto, whereby said explosive charge is ignited and detonated.
Claim 2
Dependent Claim
365 words
A range-measuring and detonating system comprising: a rolling type air vehicle having a transparent section in the forward portion thereof; air driven propeller means operably mounted in the forward end of said air vehicle for rotation about an axis; a first reflector means operatively mounted in said air vehicle forward of said transparent section and connected to the aft end of said propeller means for rotation with said propeller means about said axis; a second reflector means having a central opening therein operatively mounted in said air vehicle both aft of said transparent section and aft of said first reflector means for directing reflections to said first reflector means and for passing reflections from said first reflector means through said central opening; laser means operably mounted in said air vehicle aft of said second reflector means for directing a beam through said central opening of said second reflector means toward said first reflector means for reflection by said first reflector means; detecting means mounted adjacent said laser means for intercepting and detecting reflections received from said first reflector means through said central opening of said second reflector means and for producing an output signal; receiver means operably connected to said detecting means to receive the output signal from said detecting means and to produce another output signal; detector and threshold assembly means operably connected to said receiver means to receive the output signal from said receiver means and to produce a further output signal; an oscillator mounted in said air vehicle; modulator means operably connected to said detecting means and to said oscillator, said modulator means being responsive to said oscillator; a phase comparator responsive to said oscillator and to the output signal from said detector and threshold assembly means; an AND circuit operatively connected to receive the output from said phase comparator and from said detector and threshold assembly; a trigger generator operably connected to said AND circuit and responsive thereto; a squib operably connected to said trigger generator and responsive thereto; a booster assembly operably connected to said squib and responsive thereto; and an explosive charge operably connected to said booster assembly and responsive thereto, whereby said explosive charge is ignited and detonated.
Claim 3
Dependent Claim
18 words
The system defined in claim 1, wherein said laser means is a continuous wave type crystal laser assembly.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-01-11 | 1985-07-13 | 1986-01-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-01-11 | 1989-07-13 | 1990-01-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-01-11 | 1993-07-13 | 1994-01-12 | $7700.00 | Window Closed / Lapsed |