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US4218878A
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Acceleration monitoring system for protecting gas turbine against damaging operation at resonant speeds
Assignee: Westinghouse Electric Corp
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Filing: 1978-04-28
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Granted: 1980-08-26
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Expires: 1998-04-28
Abstract
Abstract A fuel control schedules fuel to a gas turbine to produce a scheduled speed profile during startup. The scheduled speed profile is continuously compared to actual turbine speed during startup, and the difference is compared to an alarm setpoint and a trip setpoint. Normally, temperature and surge limit controls prevent the turbine from accelerating too fast; and, if the turbine is accelerating too slowly, an alarm output is generated when the actual/desired speed difference reaches the alarm setpoint and the turbine is tripped when the actual/desired speed difference reaches the trip setpoint.
Inventors
- 👤 Roy W. Kiscaden
- 👤 Kermit R. Wescott
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 19:13
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/26
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
112 words
An improved acceleration monitoring system for protecting a gas turbine against resonant speed operation, said system comprising means for generating a signal representative of actual turbine speed, means for generating a reference signal which substantially represents desired turbine startup speed as a continuous function of time, means for continuously comparing the actual and reference speed signals and for generating an output representing the difference, means for generating an alarm signal when the difference output reaches a first value which indicates the pssibility of an undesired hold at a resonant speed, and means for generating a turbine trip signal when the difference output reaches a predetermined second value higher than the first value.
Claim 2
Dependent Claim
112 words
An improved acceleration monitoring system for protecting a gas turbine against resonant speed operation, said system comprising means for generating a signal representative of actual turbine speed, means for generating a reference signal which substantially represents desired turbine startup speed as a continuous function of time, means for continuously comparing the actual and reference speed signals and for generating an output representing the difference, means for generating an alarm signal when the difference output reaches a first value which indicates the pssibility of an undesired hold at a resonant speed, and means for generating a turbine trip signal when the difference output reaches a predetermined second value higher than the first value.
Claim 3
Dependent Claim
80 words
A system as set forth in claim 1 wherein said reference signal generating means includes first means for generating a first ramp signal having a first slope over a first turbine speed range, second means for generating a second ramp signal having a second slope less than the first slope over a second turbine speed range, and third means for generating a third ramp signal having a third slope less than the second slope over a third turbine speed range.
Claim 4
Dependent Claim
48 words
A system as set forth in claim 2 wherein the first speed range is from 0% rated to about 60% rated, the second speed range is from about 60% rated to about 90% rated and the third speed range is from about 90% rated to about 98% rated.
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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) | 1983-08-26 | 1984-02-25 | 1984-08-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-08-26 | 1988-02-25 | 1988-08-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-08-26 | 1992-02-25 | 1992-08-26 | $7700.00 | Window Closed / Lapsed |