US5303545A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Pressure based close loop thrust control in a turbofan engine
Assignee: RTX Corp
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Filing: 1992-10-05
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Granted: 1994-04-19
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Expires: 2012-10-05
Abstract
Abstract Fuel flow and nozzle area are controlled by a multi-variable control. A requested fan speed is compared with measured fan speed, producing an error signal which is translated in a proportional-integral inner control loop into a requested compressor pressure signal that represents an acceptable rate of change in compressor pressure for difference between requested and measured fan speed. The error signal is compared with measured compressor pressure; the difference being used in a multi-variable control to adjust fuel flow and turbine exhaust area to achieve the requested compressor pressure.
Inventors
- 👤 Louis J. Larkin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 10:26
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/06; F02K1/15; F02K1/16; F02K1/17; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/10; F05D2270/101
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
183 words
A gas turbine engine having an engine control that responds to a thrust required to control fuel flow to an engine burner that powers a fan, the engine control comprising signal processing means responsive to a plurality of engine operating parameters for controlling said fuel flow to control engine thrust, characterized in that said signal processing means comprises: means responsive to the thrust control for producing a first signal manifesting a requested speed for the fan; for producing a second signal manifesting measured speed of the fan; for producing a third signal that manifests the difference between said first and second signals; for producing a fourth signal the magnitude of which is a calculated compressor pressure increase over a selected time interval following the production of said third signal; for producing a fifth signal that manifests measured compressor pressure; for producing a sixth signal that manifests the difference between said fourth and said fifth signals; and for adjusting fuel flow to the burner as a function of the magnitude of said sixth signal to achieve a compressor pressure manifested by said fourth signal.
Claim 2
Dependent Claim
183 words
A gas turbine engine having an engine control that responds to a thrust required to control fuel flow to an engine burner that powers a fan, the engine control comprising signal processing means responsive to a plurality of engine operating parameters for controlling said fuel flow to control engine thrust, characterized in that said signal processing means comprises: means responsive to the thrust control for producing a first signal manifesting a requested speed for the fan; for producing a second signal manifesting measured speed of the fan; for producing a third signal that manifests the difference between said first and second signals; for producing a fourth signal the magnitude of which is a calculated compressor pressure increase over a selected time interval following the production of said third signal; for producing a fifth signal that manifests measured compressor pressure; for producing a sixth signal that manifests the difference between said fourth and said fifth signals; and for adjusting fuel flow to the burner as a function of the magnitude of said sixth signal to achieve a compressor pressure manifested by said fourth signal.
Claim 3
Dependent Claim
28 words
The engine described in claim 1 characterized in that the magnitude of said fourth signal is varied in relation to compressor speed when said third signal is produced.
Claim 4
Dependent Claim
61 words
The engine described in claim 2, characterized by exhaust area control means for adjusting exhaust area of the engine- exhaust and said signal processing means comprising means for providing a signal to said exhaust area control means for adjusting said area as a function of the magnitude of said sixth signal to achieve the compressor pressure manifested by said fourth signal.
Claim 5
Dependent Claim
47 words
The engine described in claim 3, characterized in that said signal processing means comprises means for providing limit signals manifesting limits on compressor pressure during acceleration and deceleration as a function of compressor speed and ambient temperature, said limit signals limiting the magnitude of said fourth signal.
Claim 6
Dependent Claim
52 words
The engine described in claim 4, characterized in that said signal processing means comprises means for providing an augmentation signal to adjust fuel flow and exhaust area as a function of the difference between measured engine exhaust pressure and a requested exhaust pressure, as a function of compressor speed and ambient pressure.
Claim 7
Dependent Claim
22 words
The engine described in claim 4, characterized in that said limits are derived by correcting measured compressor speed for measured ambient temperature.
Claim 8
Dependent Claim
35 words
The engine described in claim 1, characterized in that said signal processing means comprises means for modifying the magnitude of said fourth signal in relation to the speed of the fan corrected for ambient temperature.
Claim 9
Dependent Claim
46 words
The engine described in claim 1, characterized in the said signal processing means comprises means for providing said fourth signal by a proportional plus integral function and varying the gain and time constant of in steps as a function of the magnitude of said third signal.
Claim 10
Dependent Claim
46 words
The engine described in claim 4, characterized in the said signal processing means comprises means for providing said fourth signal by a proportional plus integral function and varying the gain and time constant of said steps as a function of the magnitude of said third signal.
Claim 11
Dependent Claim
46 words
The engine described in claim 7, characterized in the said signal processing means comprises means for providing said fourth signal by a proportional plus integral function and varying the gain and time constant of said steps as a function of the magnitude of said third 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) | 1997-04-18 | 1997-10-18 | 1998-04-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-04-18 | 2001-10-18 | 2002-04-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-04-18 | 2005-10-18 | 2006-04-19 | $7700.00 | Window Closed / Lapsed |