US4122667A
Expired / Lapsed
US
⏱️ 0.0 years remaining
System for detecting abnormality in fuel feed control system of gas turbine engine
Assignee: Nissan Motor Co Ltd
•
Filing: 1976-12-07
•
Granted: 1978-10-31
•
Expires: 1996-12-07
Abstract
Abstract For a gas turbine engine provided with a fuel feed control system that includes an engine speed sensor and provides a fuel feed rate control signal based on the deviation of the sensed engine speed from an intended speed, the invention provides a system for detecting the presence of an abnormality possibly leading to an overrun of the engine shortly after starting of the engine. This system comprises a timer circuit which produces a signal such as logic "1" signal after the lapse of a preset period of time from starting of the engine, a comparison circuit which produces a signal such as logic "1" signal if the amplitude of the actual engine speed signal is below a normally expected level after the lapse of the preset period of time, and a logical operation circuit which provides a warning signal only when, for example, the outputs of the timer and comparison circuits are both "1" signals.
Inventors
- 👤 Akio Hosaka
- 👤 Eiji Tsuruta
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 13:26
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/26; F02C9/00; F02C9/26; F02C9/32
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
227 words
A fuel feed control system for a gas turbine engine, including sensor means to produce an electrical first signal representing actual engine speed and first comparator means for producing a fuel feed rate control signal based on the magnitude of a deviation of the actual engine speed signal from a reference signal representing a variably intended engine speed, a subsystem for detecting the presence of an abnormality in the fuel feed control system shortly after the starting of the engine, said subsystem comprising: timer means for producing an electrical second signal after the lapse of a predetermined period of time from the starting of said engine, said predetermined period of time being chosen such that when said second signal is produced the engine speed is low enough to take preventive action against the occurrence of an overrun if an abnormaility is detected at this moment; second comparator means for producing an electrical third signal if the amplitude of said first signal is below a predetermined value corresponding to an engine speed normally expected after the lapse of said predetermined period of time from the starting of said engine; and logic means, connected to receive said second and third signals from said timer means and said comparing means for producing an electrical warning signal when said third electrical signal has a predetermined relationship to said second electrical signal.
Claim 2
Dependent Claim
227 words
A fuel feed control system for a gas turbine engine, including sensor means to produce an electrical first signal representing actual engine speed and first comparator means for producing a fuel feed rate control signal based on the magnitude of a deviation of the actual engine speed signal from a reference signal representing a variably intended engine speed, a subsystem for detecting the presence of an abnormality in the fuel feed control system shortly after the starting of the engine, said subsystem comprising: timer means for producing an electrical second signal after the lapse of a predetermined period of time from the starting of said engine, said predetermined period of time being chosen such that when said second signal is produced the engine speed is low enough to take preventive action against the occurrence of an overrun if an abnormaility is detected at this moment; second comparator means for producing an electrical third signal if the amplitude of said first signal is below a predetermined value corresponding to an engine speed normally expected after the lapse of said predetermined period of time from the starting of said engine; and logic means, connected to receive said second and third signals from said timer means and said comparing means for producing an electrical warning signal when said third electrical signal has a predetermined relationship to said second electrical signal.
Claim 3
Dependent Claim
39 words
A system as claimed in claim 1, wherein said predetermined period of time is chosen so as to be nearly equal to a period of time normally needed for the rise of the engine speed to an idling speed.
Claim 4
Dependent Claim
51 words
A system as claimed in claim 1, wherein said second and third signals are logic signals individually capable of taking one of logic "1" and logic "0" states, said logical operation circuit being constructed to provide said warning signal only when said second and third signals take the same logic state.
Claim 5
Dependent Claim
144 words
A system as claimed in claim 3, wherein: said timer means comprise a first operational amplifier, a resistor connected to the positive input terminal of said first operational amplifier and a capacitor connected to a junction between said resistor and said positive input terminal, a preset voltage signal as a factor in determining said preset period of time being applied to the negative input terminal of said first operational amplifier, another voltage signal indicating that the engine is in operation being applied to said capacitor through said resistor; said comparison circuit is a second operational amplifier, said first signal and said reference signal being applied to the negative and positive input terminals of said second operational amplifier, respectively; said logical operation circuit is an AND circuit with the input terminals thereof connected respectively to the output terminals of said first and second operational amplifiers.
Claim 6
Dependent Claim
18 words
A system as claimed in claim 4, wherein said second and third signals are respectively logic "1" signals.
Claim 7
Dependent Claim
37 words
A system as claimed in claim 1, further comprising means for giving a warning on the presence of an abnormality to an operator of the engine upon receipt of said warning signal from said logical operation circuit.
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) | 1981-10-30 | 1982-05-01 | 1982-10-31 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-30 | 1986-05-01 | 1986-10-31 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-30 | 1990-05-01 | 1990-10-31 | $7700.00 | Window Closed / Lapsed |