← Back to Patent Explorer
US3902172A Expired / Lapsed US ⏱️ 0.0 years remaining

Infrared gated radio fuzing system

Assignee: United States Department of the Navy
•
Filing: 1962-03-29
•
Granted: 1975-08-26
•
Expires: 1982-03-29
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract 1. In an infrared gated radio fuzing system for use in a guided missile the combination comprising: A. FIRST THERMAL-ENERGY DETECTING MEANS FOR PRODUCING AN OUTPUT SIGNAL IN RESPONSE TO INTERCEPTED THERMAL-ENERGY RADIATED FROM A THERMAL-ENERGY RADIATING OBJECT, B. SECOND CIRCUIT MEANS FOR DETECTING RADIO ENERGY REFLECTED FROM SAID THERMAL-ENERGY RADIATING OBJECT, C. PULSE GENERATOR MEANS COUPLED TO SAID THERMAL-ENERGY DETECTING MEANS FOR GENERATING AN OUTPUT PULSE HAVING A TIME DURATION APPROXIMATELY EQUAL TO THE TIME REQUIRED FOR THE MISSILE TO TRAVERSE A DISTANCE OF HALF THE LENGTH OF THE RADIATING OBJECT, D. SWITCHING MEANS COUPLED TO SAID PULSE GENERATOR MEANS AND TO SAID SECOND CIRCUIT MEANS AND BEING RESPONSIVE TO SAID OUTPUT PULSE FOR ACTIVATING SAID SECOND CIRCUIT MEANS AND BEING RESPONSIVE TO THE CESSATION OF SAID PULSE FOR DE-ACTIVATING SAID SECOND CIRCUIT MEANS, E. THIRD CIRCUIT MEANS RESPONSIVE TO AN OUTPUT SIGNAL FROM SAID SECOND CIRCUIT MEANS IN THE EVENT A DESIRED TARGET IS DETECTED DURING SAID PREDETERMINED TIME INTERVAL FOR ACTUATING A DETONATION CIRCUIT.

Inventors

  • 👤 Albert Weiss
  • 👤 Daniel D Holmes

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 05:29
CPC Classifications
F; F42; F42C; F42C13/00; F42C13/04

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 166 words
In an infrared gated radio fuzing system for use in a guided missile the combination comprising: a. first thermal-energy detecting means for producing an output signal in response to intercepted thermal-energy radiated from a thermal-energy radiating object, b. second circuit means for detecting radio energy reflected from said thermal-energy radiating object, c. pulse generator means coupled to said thermal-energy detecting means for generating an output pulse having a time duration approximately equal to the time required for the missile to traverse a distance of half the length of the radiating object, d. switching means coupled to said pulse generator means and to said second circuit means and being responsive to said output pulse for activating said second circuit means and being responsive to the cessation of said pulse for de-activating said second circuit means, e. third circuit means responsive to an output signal from said second circuit means in the event a desired target is detected during said predetermined time interval for actuating a detonation circuit.
Claim 2
Dependent Claim 166 words
In an infrared gated radio fuzing system for use in a guided missile the combination comprising: a. first thermal-energy detecting means for producing an output signal in response to intercepted thermal-energy radiated from a thermal-energy radiating object, b. second circuit means for detecting radio energy reflected from said thermal-energy radiating object, c. pulse generator means coupled to said thermal-energy detecting means for generating an output pulse having a time duration approximately equal to the time required for the missile to traverse a distance of half the length of the radiating object, d. switching means coupled to said pulse generator means and to said second circuit means and being responsive to said output pulse for activating said second circuit means and being responsive to the cessation of said pulse for de-activating said second circuit means, e. third circuit means responsive to an output signal from said second circuit means in the event a desired target is detected during said predetermined time interval for actuating a detonation circuit.
Claim 3
Dependent Claim 33 words
The system of claim 1 wherein said first circuit means includes an infrared optical detector oriented so that it has a ''''look'''' angle of 45* with respect to the object to be detected.

References Cited (Backward Citations)

US3010102A Cited
US3108270A Cited
US3169726A Cited
US3046892A Cited
US3568185A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-08-25 1979-02-24 1979-08-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-08-25 1983-02-24 1983-08-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-08-25 1987-02-24 1987-08-26 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag