← Back to Patent Explorer
US3240447A Expired / Lapsed US ⏱️ 0.0 years remaining

Vehicle control system

Assignee: North American Aviation Corp
•
Filing: 1965-03-30
•
Granted: 1966-03-15
•
Expires: 1985-03-30
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Olshausen Richard

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 13:03
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0615; G05D1/0623

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 141 words
IN A LONGITUDINAL FLIGHT CONTROL SYSTEM FOR AN AIRCRAFT HAVING A MAIN CONTROL CHANNEL AND AN AUXILIARY CONTROL CHANNEL, INPUT SIGNAL MEANS INCLUDING SIGNAL COMPARISON MEANS FOR APPLYING A CONTROL SIGNAL TO ONE OF SAID CHANNELS; GUST COMPUTING MEANS COMPRISING A HIGH FREQUENCY INTEGRATOR RESPONSIVE TO A PITCH RATE SIGNAL, AND SUMMING MEANS RESPONSIVE TO A NORMAL ACCELERATION SIGNAL AND RESPONSIVELY CONNECTED TO SAID INTEGRATOR; SAID CHANNELS BEING RESPONSIVELY CONNECTED TO SAID COMPUTING MEANS; A PITCHING MOMENT EQUALIZER INTERPOSED BETWEEN THE OTHER OF SAID CHANNELS AND SAID GUST COMPUTING MEANS, SAID EQUALIZER BEING COMPRISED OF A VARIABLE GAIN ELEMENT, AN INTEGRATING DRIVE MEANS RESPONSIVELY CONNECTED TO A SIGNAL MULTIPLIER FOR VARYING THE GAIN OF SAID VARIABLE GAIN ELEMENT, SAID MULTIPLIER BEING RESPONSIVE TO A SIGNAL INDICATIVE OF THE PITCH ACCELERATION OF SAID AIRCRAFT AND TO SAID OUTPUT OF SAID COMPUTING MEANS.
Claim 2
Dependent Claim 141 words
IN A LONGITUDINAL FLIGHT CONTROL SYSTEM FOR AN AIRCRAFT HAVING A MAIN CONTROL CHANNEL AND AN AUXILIARY CONTROL CHANNEL, INPUT SIGNAL MEANS INCLUDING SIGNAL COMPARISON MEANS FOR APPLYING A CONTROL SIGNAL TO ONE OF SAID CHANNELS; GUST COMPUTING MEANS COMPRISING A HIGH FREQUENCY INTEGRATOR RESPONSIVE TO A PITCH RATE SIGNAL, AND SUMMING MEANS RESPONSIVE TO A NORMAL ACCELERATION SIGNAL AND RESPONSIVELY CONNECTED TO SAID INTEGRATOR; SAID CHANNELS BEING RESPONSIVELY CONNECTED TO SAID COMPUTING MEANS; A PITCHING MOMENT EQUALIZER INTERPOSED BETWEEN THE OTHER OF SAID CHANNELS AND SAID GUST COMPUTING MEANS, SAID EQUALIZER BEING COMPRISED OF A VARIABLE GAIN ELEMENT, AN INTEGRATING DRIVE MEANS RESPONSIVELY CONNECTED TO A SIGNAL MULTIPLIER FOR VARYING THE GAIN OF SAID VARIABLE GAIN ELEMENT, SAID MULTIPLIER BEING RESPONSIVE TO A SIGNAL INDICATIVE OF THE PITCH ACCELERATION OF SAID AIRCRAFT AND TO SAID OUTPUT OF SAID COMPUTING MEANS.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-03-14 1969-09-13 1970-03-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-03-14 1973-09-13 1974-03-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-03-14 1977-09-13 1978-03-15 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag