US4995232A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Running control for a gas turbine engine
Assignee: ZF International UK Ltd
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Filing: 1986-08-04
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Granted: 1991-02-26
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Expires: 2006-08-04
Abstract
Abstract A running control for a gas turbine engine includes a fuel control responsive to an input signal which corresponds to a desired rate of change of engine speed. A speed governor circuit generates a first output signal corresponding to a difference between demanded and actual speeds. Limit signal generators provide second and third signals which correspond to permitted acceleration and deceleration respectively. The second and third signals are integrated and a selected one of the first, second or third signals is applied to the fuel control. At least the integrator for the second signal can be reset by a feedback arrangement which modifies the integrator input in accordance with a difference between the desired rate of change of engine speed and the second signal.
Inventors
- 👤 Arthur E. Sutton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 17:42
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
234 words
In a running control for a gas turbine engine having a fuel flow control which receives as input a signal representing a desired rate of change of engine speed, a speed governor circuit which receives a demand speed signal and an actual speed signal and provides a first output signal determined by the difference between said speed signals, an acceleration control circuit and a deceleration control circuit, each control circuit including a limit signal generator the output of which represents the maximum permitted rate of change of engine speed in current operating conditions and each control circuit also including an integrator connected to integrate the output of the respective limit signal generator and means for generating second and third output signals determined by the difference between the output of the respective one of the integrators and the actual engine speed, selection means for selecting whether the first, second or third output signal is applied to the fuel flow control as the input thereof and means for resetting the integrators of the acceleration and deceleration control circuits, the improvement wherein the integrator resetting means of at least one of the acceleration and deceleration control circuits comprises a feedback arrangement which modifies the input to the integrator of that control circuit in accordance with the difference beween the input to the fuel flow control and the second or third output signal as the case may be.
Claim 2
Dependent Claim
234 words
In a running control for a gas turbine engine having a fuel flow control which receives as input a signal representing a desired rate of change of engine speed, a speed governor circuit which receives a demand speed signal and an actual speed signal and provides a first output signal determined by the difference between said speed signals, an acceleration control circuit and a deceleration control circuit, each control circuit including a limit signal generator the output of which represents the maximum permitted rate of change of engine speed in current operating conditions and each control circuit also including an integrator connected to integrate the output of the respective limit signal generator and means for generating second and third output signals determined by the difference between the output of the respective one of the integrators and the actual engine speed, selection means for selecting whether the first, second or third output signal is applied to the fuel flow control as the input thereof and means for resetting the integrators of the acceleration and deceleration control circuits, the improvement wherein the integrator resetting means of at least one of the acceleration and deceleration control circuits comprises a feedback arrangement which modifies the input to the integrator of that control circuit in accordance with the difference beween the input to the fuel flow control and the second or third output signal as the case may be.
Claim 3
Dependent Claim
23 words
A running control as claimed in claim 1 in which the feedback arrangement further comprises delay means for delaying feedback of said difference.
Claim 4
Dependent Claim
20 words
A running control as claimed in claim 2 in which said feedback arrangement has a gain of greater than unity.
Claim 5
Dependent Claim
61 words
A running control as claimed in any preceding claim in which the fuel flow control incorporates limiting means operable to determine the fuel flow to the engine independently of the input thereto, means being provided to simulate the input which would have been required to obtain the actual resulting fuel flow and for supplying such simulated input to the feedback means.
References Cited (Backward Citations)
US4517797A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-02-25 | 1994-08-27 | 1995-02-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-02-25 | 1998-08-27 | 1999-02-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-02-25 | 2002-08-27 | 2003-02-26 | $7700.00 | Window Closed / Lapsed |