Patent US4569021A successfully refreshed from Google Patents.
US4569021A
Expired / Lapsed
US
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Full flight regime autothrottle control system
Assignee: Boeing Co
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Filing: 1980-05-23
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Granted: 1986-02-04
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Expires: 2000-05-23
Abstract
Abstract A Mach hold control circuit for an aircraft autothrottle system provides capture of a Mach number and control thereto while providing a low level of throttle activity also stabilizing the aircraft at maximum range cruise (MRC) Mach numbers and above. The Mach hold control law utilizes a Mach error signal, flight path acceleration signal, average engine EPR signal, and associated logic inputs and when interfaced with the autothrottle system provides a throttle rate command to the aircraft engines via. the throttle and engine control system thereby modulating engine thrust to provide control to desired flight Mach number.
Inventors
- 👤 Warren R. Larson
- 👤 Henri Peter-Contesse
- 👤 Leonard P. Stephan
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 20:22
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
263 words
A full flight regime autothrottle control system comprising: an EPR command circuit; a speed control circuit; a low speed protection circuit; first summing means having first and second input terminals and an output terminal; a first time variable gain circuit; a second time variable gain circuit; said first time variable gain circuit coupled between said speed control circuit and said first input terminal of said first summing means; said second time variable gain circuit coupled between said low speed protection circuit and said second input terminal of said first summing means; a lowest select circuit having first and second input terminals and an output terminal; a Mach hold control circuit having Mach capture and track submodes; first switching means for coupling said second input terminal of said lowest select circuit to said output terminal of said first summing means when the speed mode of said speed control circuit is selected or when said low speed protection circuit is active and coupling said second input terminal of said lowest select circuit to the output terminal of said Mach hold control circuit when Mach mode is selected and low speed protection circuit is not active; said first input terminal of said lowest select circuit coupled to the output of said EPR command circuit; throttle servo means for controlling throttle lever positioning, said throttle servo means having an input terminal; second switching means for coupling said input terminal of said throttle servo means from said output terminal of said lowest select circuit to the output of said EPR control circuit when the EPR mode is selected.
Claim 2
Dependent Claim
263 words
A full flight regime autothrottle control system comprising: an EPR command circuit; a speed control circuit; a low speed protection circuit; first summing means having first and second input terminals and an output terminal; a first time variable gain circuit; a second time variable gain circuit; said first time variable gain circuit coupled between said speed control circuit and said first input terminal of said first summing means; said second time variable gain circuit coupled between said low speed protection circuit and said second input terminal of said first summing means; a lowest select circuit having first and second input terminals and an output terminal; a Mach hold control circuit having Mach capture and track submodes; first switching means for coupling said second input terminal of said lowest select circuit to said output terminal of said first summing means when the speed mode of said speed control circuit is selected or when said low speed protection circuit is active and coupling said second input terminal of said lowest select circuit to the output terminal of said Mach hold control circuit when Mach mode is selected and low speed protection circuit is not active; said first input terminal of said lowest select circuit coupled to the output of said EPR command circuit; throttle servo means for controlling throttle lever positioning, said throttle servo means having an input terminal; second switching means for coupling said input terminal of said throttle servo means from said output terminal of said lowest select circuit to the output of said EPR control circuit when the EPR mode is selected.
Claim 3
Dependent Claim
126 words
In combination in an autothrottle control system for an aircraft: a Mach hold control circuit for providing aircraft capture and track in the cruise mode to a desired Mach number; an EPR command circuit for providing control of the aircraft during take-off and climb maneuvers; a speed control circuit for providing control of the aircraft during descent, hold, and approach maneuvers; mode selection switching means for selecting one of said Mach hold control, EPR command, or speed control modes for control of the aircraft; and low speed protection circuit means responsive to aircraft angle of attack and Mach number for controlling said autothrottle control system when the speed of said aircraft in the Mach mode is less than the Mach number corresponding to the holding speed.
Claim 4
Dependent Claim
126 words
In combination in an autothrottle control system for an aircraft: a Mach hold control circuit for providing aircraft capture and track in the cruise mode to a desired Mach number; an EPR command circuit for providing control of the aircraft during take-off and climb maneuvers; a speed control circuit for providing control of the aircraft during descent, hold, and approach maneuvers; mode selection switching means for selecting one of said Mach hold control, EPR command, or speed control modes for control of the aircraft; and low speed protection circuit means responsive to aircraft angle of attack and Mach number for controlling said autothrottle control system when the speed of said aircraft in the Mach mode is less than the Mach number corresponding to the holding speed.
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) | 1989-02-03 | 1989-08-05 | 1990-02-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-02-03 | 1993-08-05 | 1994-02-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-02-03 | 1997-08-05 | 1998-02-04 | $7700.00 | Window Closed / Lapsed |