US4209152A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation
Assignee: Boeing Co
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Filing: 1977-11-25
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Granted: 1980-06-24
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Expires: 1997-11-25
Abstract
Abstract Command from engine rating control prevents throttle position from exceeding the value at which the engine operates at its rated power. Flare initiation changes the throttle command signal from a closed loop control signal to a fixed number of degrees per second retard rate, thereby overriding an aft limit switch signal allowing throttles to reach the idle position. A servo feedback arrangement utilizes a tachometer signal and an engine PLA (power level angle) signal to optimize servo performance and overcome undesired control cable characteristics.
Inventors
- 👤 Leonard P. Stephan
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 21:44
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0615; G05D1/063
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
130 words
In the command signal path of an aircraft throttle control system: a first diode having an anode and a cathode and said first diode connected in series with said command signal path, said first diode having the cathode thereof adapted to receive positive polarity signals representative of throttle advance commands from the output of a summing amplifier in said command signal path upstream from said first diode, said summing amplifier including inputs responsive to gust bias and windshear compensated signals; and, a second diode having an anode and a cathode, said cathode of said second diode adapted to receive signals representative of the difference between engine rating and actual engine EPR or N 1 , and said anode of said second diode connected to said anode of said first diode.
Claim 2
Dependent Claim
130 words
In the command signal path of an aircraft throttle control system: a first diode having an anode and a cathode and said first diode connected in series with said command signal path, said first diode having the cathode thereof adapted to receive positive polarity signals representative of throttle advance commands from the output of a summing amplifier in said command signal path upstream from said first diode, said summing amplifier including inputs responsive to gust bias and windshear compensated signals; and, a second diode having an anode and a cathode, said cathode of said second diode adapted to receive signals representative of the difference between engine rating and actual engine EPR or N 1 , and said anode of said second diode connected to said anode of said first diode.
Claim 3
Dependent Claim
106 words
In combination in an aircraft throttle control system having a throttle command signal path for controlling throttle positioning: means for providing a signal representative of airspeed error; means for providing a signal representative of longitudinal acceleration corrected for windshear; means for providing a gust bias signal; combining circuit means responsive to said signal representative of airspeed error, said signal representative of longitudinal acceleration corrected for windshear, and said gust bias signal for providing a first signal; and, lowest select circuit means connected in series circuit in said throttle command signal path, said lowest select circuit means responsive to engine rating control signals and said first signal.
Claim 4
Dependent Claim
106 words
In combination in an aircraft throttle control system having a throttle command signal path for controlling throttle positioning: means for providing a signal representative of airspeed error; means for providing a signal representative of longitudinal acceleration corrected for windshear; means for providing a gust bias signal; combining circuit means responsive to said signal representative of airspeed error, said signal representative of longitudinal acceleration corrected for windshear, and said gust bias signal for providing a first signal; and, lowest select circuit means connected in series circuit in said throttle command signal path, said lowest select circuit means responsive to engine rating control signals and said first signal.
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) | 1983-06-24 | 1983-12-24 | 1984-06-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-06-24 | 1987-12-24 | 1988-06-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-06-24 | 1991-12-24 | 1992-06-24 | $7700.00 | Window Closed / Lapsed |