US4227369A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Control systems for apparatus
Assignee: Rolls Royce PLC
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Filing: 1978-05-01
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Granted: 1980-10-14
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Expires: 1998-05-01
Abstract
Abstract Infra-red radiation detectors are used in gas turbine engines to detect radiation produced by the turbine blades giving an indication of blade temperature. Above a given limit the signal produced by the detector is passed to the fuel control system to shut down the fuel supply to the engine. An additional detector is provided which receives the same image as the first detector but is biased to detect radiation in the visible light part of the spectrum. When incandescent particles pass through the field of vision of the detectors both show an increase in signal due to both types of radiation being increased during this transient event. The signal from the second detector is used to reduce the signal from the first detector by an amount sufficient to prevent the fuel supply being temporarily shut down.
Inventors
- 👤 Peter J. Williams
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 19:06
CPC Classifications
F; F23; F23N; F23N5/00; F23N5/02; F23N5/08; F23N5/082; F01; F01D; F01D17/00; F01D17/02; F01D17/08; F01D17/085; F01D21/00; F01D21/12; F23N2229/00; F23N2229/16
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
164 words
A fuel control system for a gas turbine engine comprising: first and second radiation detectors positioned to monitor radiation emanating from combustion equipment of the engine, the first detector being responsive to radiation in the infra-red frequency range to produce a first signal representative of the radiation in the infra-red frequency range, the second detector being responsive to radiation in the visible frequency range produced by a transient radiation event which also produces radiation in the infra-red frequency range to produce a second signal representative of the radiation in the visible frequency range, a function generator operative to receive the second signal and derive therefrom a third signal indicative of the radiation in the infra-red frequency range corresponding to the detected radiation in the visible frequency range, a comparator means for comparing the first and third signals and operative to produce a fourth signal, and control means responsive to said fourth signal for regulating the fuel supplied to the combustion equipment of the engine.
Claim 2
Dependent Claim
164 words
A fuel control system for a gas turbine engine comprising: first and second radiation detectors positioned to monitor radiation emanating from combustion equipment of the engine, the first detector being responsive to radiation in the infra-red frequency range to produce a first signal representative of the radiation in the infra-red frequency range, the second detector being responsive to radiation in the visible frequency range produced by a transient radiation event which also produces radiation in the infra-red frequency range to produce a second signal representative of the radiation in the visible frequency range, a function generator operative to receive the second signal and derive therefrom a third signal indicative of the radiation in the infra-red frequency range corresponding to the detected radiation in the visible frequency range, a comparator means for comparing the first and third signals and operative to produce a fourth signal, and control means responsive to said fourth signal for regulating the fuel supplied to the combustion equipment of the engine.
Claim 3
Dependent Claim
59 words
A control system according to claim 1, wherein at least the first detector monitors the temperature of a turbine blade of the engine and said control means is responsive to the fourth signal to limit the supply of fuel to the combustion apparatus of the engine in dependence upon the temperature of the turbine blade exceeding a predetermined temperature.
Claim 4
Dependent Claim
77 words
A control system according to claim 2 and in which the second detector is responsive to the visible light produced by the passage of hot carbonaceous matter past the turbine blade to produce said second signal, the means responsive to generation of the second signal causing any corresponding increase in the signal from the first detector to be nullified before it affects the control means at least for the duration of the passage of said carbonaceous material.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-10-14 | 1984-04-14 | 1984-10-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-10-14 | 1988-04-14 | 1988-10-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-10-14 | 1992-04-14 | 1992-10-14 | $7700.00 | Window Closed / Lapsed |