US4204475A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Arming-safing system for airborne weapons
Assignee: United States Department of the Navy
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Filing: 1969-04-29
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Granted: 1980-05-27
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Expires: 1989-04-29
Abstract
Abstract The system of the present invention basically consists of a detector unit unted in each bomb or airborne weapon and operable upon interception of a signal emitted by an aircraft-mounted source. The required signal for arming is present only in a well defined zone below the aircraft and only in response to pilot command during weapon release. The signal consists of mechanically modulated beam of high-energy photons (gamma rays) emitted by a radioisotope source on the aircraft. The weapon must fall well below the aircraft to see the signal. Geiger-Mueller tubes are used for radiation detectors and the resulting signal is processed to initiate the arming or fuzing sequence. Power for the operation of the detector and associated electronics is transferred through the metallic covering of the weapon by means of a split-core transformer at the time of release. The power transferred is capable of operating the unit for the length of time it would normally take the weapon to fall through the signal zone; after which the weapon returns to a dormant, safe, state if no arming signal has been received.
Inventors
- 👤 Ronald J. Fowler
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 02:16
CPC Classifications
F; F42; F42C; F42C15/00; F42C15/40
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
118 words
A system for arming an airborne weapon in time delayed relation with respect to the release of the weapon from an aircraft in flight, the aircraft being provided with a mechanically modulated source of gamma radiation for irradiating a predetermined volume of space below the aircraft, comprising: means for detecting gamma radiation; means for comparing the magnitude of the detected radiation with a predetermined value and for generating a pulse each time the radiation exceeds that value; a low pass filter for receiving the pulses generated by said comparing means; and means operable to initiate the arming sequence for said weapon when the frequency of the filter output equals the frequency at which the radiation source is modulated.
Claim 2
Independent Claim
118 words
A system for arming an airborne weapon in time delayed relation with respect to the release of the weapon from an aircraft in flight, the aircraft being provided with a mechanically modulated source of gamma radiation for irradiating a predetermined volume of space below the aircraft, comprising: means for detecting gamma radiation; means for comparing the magnitude of the detected radiation with a predetermined value and for generating a pulse each time the radiation exceeds that value; a low pass filter for receiving the pulses generated by said comparing means; and means operable to initiate the arming sequence for said weapon when the frequency of the filter output equals the frequency at which the radiation source is modulated.
Claim 3
Dependent Claim
38 words
A system according to claim 1 wherein said detecting means includes: a Geiger-Mueller tube; means for shaping the pulses emitted by said Geiger-Mueller tube; and means for integrating said pulses to provide an input for said comparing means.
Claim 4
Dependent Claim
62 words
A system according to claim 1 wherein said comparing means comprises: a dual level comparor; the lower level of said comparor being set above the anticipated background radiation when said source of gamma radiation is occluded by the mechanical modulator and the higher level of said comparor being set at the radiation level anticipated when said source of gamma radiation is exposed.
Claim 5
Dependent Claim
27 words
A system according to claim 1 wherein said initiating means comprises: an AND gate; and an explosive switch operated by an output pulse from said AND gate.
Claim 6
Dependent Claim
56 words
A system according to claim 4 wherein said low pass filter comprises: a first monostable multivibrator; a plurality of series connected monostable multivibrators connecting the output of said first multivibrator to one input of said AND gate; and a direct connection between the output of said first multivibrator and the other input of said AND gate.
Claim 7
Independent Claim
224 words
A system for arming an airborne weapon in time delayed relation with respect to the release of the weapon from an aircraft in flight, the aircraft being provided with a mechanically modulated source of gamma radiation for irradiating a predetermined volume of space below the aircraft, comprising: a Geiger-Mueller tube for detecting gamma radiation and generating pulses representative thereof; means for shaping the pulses generated by said Geiger-Mueller tube; means for integrating the pulses emitted by said shaping means; means for comparing the magnitude of the integrated signal with a predetermined value and for generating a pulse each time the integrated signal exceeds that value; a first monostable multivibrator for receiving pulses from said comparing means; an AND gate; a direct connection between the output of said first multivibrator and one input of said AND gate; a plurality of series connected monostable multivibrators connecting the output of said first multivibrator and the other input of said AND gate; said direct connection and said series connected multivibrators comprising a low pass filter whereby simultaneous pulses will be applied to said AND gate only when the gamma radiation being detected by said Geiger-Mueller tube is modulated at the frequency of operation of the mechanical modulator; and an explosive switch operable by an output pulse from said AND gate for initiating the arming sequence for said weapon.
Claim 8
Independent Claim
224 words
A system for arming an airborne weapon in time delayed relation with respect to the release of the weapon from an aircraft in flight, the aircraft being provided with a mechanically modulated source of gamma radiation for irradiating a predetermined volume of space below the aircraft, comprising: a Geiger-Mueller tube for detecting gamma radiation and generating pulses representative thereof; means for shaping the pulses generated by said Geiger-Mueller tube; means for integrating the pulses emitted by said shaping means; means for comparing the magnitude of the integrated signal with a predetermined value and for generating a pulse each time the integrated signal exceeds that value; a first monostable multivibrator for receiving pulses from said comparing means; an AND gate; a direct connection between the output of said first multivibrator and one input of said AND gate; a plurality of series connected monostable multivibrators connecting the output of said first multivibrator and the other input of said AND gate; said direct connection and said series connected multivibrators comprising a low pass filter whereby simultaneous pulses will be applied to said AND gate only when the gamma radiation being detected by said Geiger-Mueller tube is modulated at the frequency of operation of the mechanical modulator; and an explosive switch operable by an output pulse from said AND gate for initiating the arming sequence for said weapon.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-05-27 | 1983-11-26 | 1984-05-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-05-27 | 1987-11-26 | 1988-05-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-05-27 | 1991-11-26 | 1992-05-27 | $7700.00 | Window Closed / Lapsed |