← Back to Patent Explorer
US3287724A Expired / Lapsed US ⏱️ 0.0 years remaining

Obstacle clearance system for aircraft

Assignee: Individual
•
Filing: 1957-10-24
•
Granted: 1966-11-22
•
Expires: 1977-10-24
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Joseph E Zupanick
  • 👤 Donal R Treffeisen

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 23:44
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/88; G01S13/93; G01S13/933; G01S13/935

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 187 words
IN AN AIRCRAFT GUIDANCE SYSTEM, APPARATUS INCLUDING MEANS FOR DETECTING THE PRESENCE AND ANGULAR ORIENTATION OF AN OBSTACLE LYING ALONG THE PATH OF AIRCRAFT TRAVEL, SAID MEANS FOR DETECTING PRODUCING FIRST AND SECOND SIGNALS, SAID FIRST SIGNAL WHEN PRODUCED BEING INDICATIVE OF THE PRESENCE OF AN OBSTACLE, AND SAID SECOND SIGNAL WHEN PRODUCED BEING PROPORTIONAL TO THE ANGULAR DEVIATION OF THE LONGITUDINAL AXIS OF THE AIRCRAFT FROM THE LINE-OF-SIGHT BETWEEN SAID AIRCRAFT AND THE PEAK OF SAID OBSTACLE, MEANS FOR PRODUCING A REFERENCE SIGNAL, MEANS FOR GENERATING A THIRD SIGNAL PROPORTIONAL TO THE AIRCRAFT ANGLE-OF-ATTACK, MEANS FOR COMPARING SAID SECOND SIGNAL WITH THE SUM OF SAID REFERENCE AND THIRD SIGNAL TO PRODUCE A FOURTH SIGNAL PROPORTIONAL TO THE DIFFERENCE BETWEEN SAID SECOND SIGNAL AND SAID SIGNAL SUM, MEANS HAVING A CONTROL INPUT FOR POSITIONING A CONTROL SURFACE OF SAID AIRCRAFT, AND MEANS FOR SELECTIVELY APPLYING SAID FOURTH SIGNAL TO SAID CONTROL INPUT, SAID MEANS FOR SELECTIVELY APPLYING BEING ADAPTED TO RECEIVE SAID FIRST SIGNAL AND SAID FOURTH SIGNAL AND BEING OPERATIVE TO APPLY SAID FOURTH SIGNAL TO SAID CONTROL INPUT IN THE PRESENCE OF SAID FIRST SIGNAL,
Claim 2
Dependent Claim 187 words
IN AN AIRCRAFT GUIDANCE SYSTEM, APPARATUS INCLUDING MEANS FOR DETECTING THE PRESENCE AND ANGULAR ORIENTATION OF AN OBSTACLE LYING ALONG THE PATH OF AIRCRAFT TRAVEL, SAID MEANS FOR DETECTING PRODUCING FIRST AND SECOND SIGNALS, SAID FIRST SIGNAL WHEN PRODUCED BEING INDICATIVE OF THE PRESENCE OF AN OBSTACLE, AND SAID SECOND SIGNAL WHEN PRODUCED BEING PROPORTIONAL TO THE ANGULAR DEVIATION OF THE LONGITUDINAL AXIS OF THE AIRCRAFT FROM THE LINE-OF-SIGHT BETWEEN SAID AIRCRAFT AND THE PEAK OF SAID OBSTACLE, MEANS FOR PRODUCING A REFERENCE SIGNAL, MEANS FOR GENERATING A THIRD SIGNAL PROPORTIONAL TO THE AIRCRAFT ANGLE-OF-ATTACK, MEANS FOR COMPARING SAID SECOND SIGNAL WITH THE SUM OF SAID REFERENCE AND THIRD SIGNAL TO PRODUCE A FOURTH SIGNAL PROPORTIONAL TO THE DIFFERENCE BETWEEN SAID SECOND SIGNAL AND SAID SIGNAL SUM, MEANS HAVING A CONTROL INPUT FOR POSITIONING A CONTROL SURFACE OF SAID AIRCRAFT, AND MEANS FOR SELECTIVELY APPLYING SAID FOURTH SIGNAL TO SAID CONTROL INPUT, SAID MEANS FOR SELECTIVELY APPLYING BEING ADAPTED TO RECEIVE SAID FIRST SIGNAL AND SAID FOURTH SIGNAL AND BEING OPERATIVE TO APPLY SAID FOURTH SIGNAL TO SAID CONTROL INPUT IN THE PRESENCE OF SAID FIRST SIGNAL,

References Cited (Backward Citations)

US2630283A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-11-21 1970-05-23 1970-11-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-11-21 1974-05-23 1974-11-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-11-21 1978-05-23 1978-11-22 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag