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US3210028A Expired / Lapsed US ⏱️ 0.0 years remaining

Control apparatus

Assignee: Honeywell Inc
•
Filing: 1962-09-27
•
Granted: 1965-10-05
•
Expires: 1982-09-27
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Abstract

No abstract record available.

Inventors

  • 👤 William C Sproull

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 09:35
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/24; G; G05; G05D; G05D1/00; G05D1/02; G05D1/0202

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 153 words
APPARATUS FOR DIRECTING AN AIRCRAFT ON TO AND ALONG A PERDETERMINED PATH DEFINED BY A RADIO BEAM COMPRISING IN COMBINATION WITH AN AUTOPILOT HAVING AN AILERON CHANNEL: A FIRST SOURCE OF SIGNAL HAVING A POLARITY ANF MAGNITUDE DEPENDENT UPON THE LATERAL DISPLACEMENT OF THE AIRCRAFT FROM THE BEAM; A SECOND SOURCE OF SIGNAL HAVING A POLARITY AND MAGNTUDE DEPENDENT UPON THE ROLL ATTITUDE OF THE AIRCRAFT; A SUMMING NETWORK FOR SUMMING THE DISPLACEMENT AND ROLL SIGNALS; A THIRD SOURCE OF SIGNAL HAVING A POLARITY AND A MAGNITUDE DEPENDENT UPON THE HEADING OF THE AIRCRAFT RELATIVE TO THE HEADING OF THE BEAM; A HIGH-PASS NETWORK NORMALLY TRANSMITTING A TRANSIENT HEADING SIGNAL TO THE SUMMING NETWORK; AND MEANS TRANSMITTING THE HEADING SIGNAL DIRECTLY TO THE SUMMING NETWORK, THEREBY SHUNTING THE HIGH-PASS NETWORK, WHENEVER THE HEADING SIGNAL IS GREATER THAN SOME PREDETERMINED AMOUNT, THE SUMMATION SIGNAL BEING EFFECTIVE IN CONTROLLING THE AILERON CHANNEL OF THE AUTOPILOT.
Claim 2
Dependent Claim 153 words
APPARATUS FOR DIRECTING AN AIRCRAFT ON TO AND ALONG A PERDETERMINED PATH DEFINED BY A RADIO BEAM COMPRISING IN COMBINATION WITH AN AUTOPILOT HAVING AN AILERON CHANNEL: A FIRST SOURCE OF SIGNAL HAVING A POLARITY ANF MAGNITUDE DEPENDENT UPON THE LATERAL DISPLACEMENT OF THE AIRCRAFT FROM THE BEAM; A SECOND SOURCE OF SIGNAL HAVING A POLARITY AND MAGNTUDE DEPENDENT UPON THE ROLL ATTITUDE OF THE AIRCRAFT; A SUMMING NETWORK FOR SUMMING THE DISPLACEMENT AND ROLL SIGNALS; A THIRD SOURCE OF SIGNAL HAVING A POLARITY AND A MAGNITUDE DEPENDENT UPON THE HEADING OF THE AIRCRAFT RELATIVE TO THE HEADING OF THE BEAM; A HIGH-PASS NETWORK NORMALLY TRANSMITTING A TRANSIENT HEADING SIGNAL TO THE SUMMING NETWORK; AND MEANS TRANSMITTING THE HEADING SIGNAL DIRECTLY TO THE SUMMING NETWORK, THEREBY SHUNTING THE HIGH-PASS NETWORK, WHENEVER THE HEADING SIGNAL IS GREATER THAN SOME PREDETERMINED AMOUNT, THE SUMMATION SIGNAL BEING EFFECTIVE IN CONTROLLING THE AILERON CHANNEL OF THE AUTOPILOT.

References Cited (Backward Citations)

US2496809A Cited
US2613352A Cited
US3104390A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1968-10-04 1969-04-05 1969-10-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1972-10-04 1973-04-05 1973-10-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1976-10-04 1977-04-05 1977-10-05 $7700.00 Window Closed / Lapsed

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