Patent US4722061A successfully refreshed from Google Patents.
US4722061A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Establishing synthesis validity between two signal sources
Assignee: RTX Corp
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Filing: 1984-12-20
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Granted: 1988-01-26
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Expires: 2004-12-20
Abstract
Abstract In an electronic engine control (EEC) for a turbine engine, a high rotor speed signal (N2SYNTH) is synthesized from a sensed low rotor speed signal (N1) in a primary control channel (32) so long as the low rotor speed signal is healthy. If the low rotor speed signal (N1) is not healthy, the primary channel is reconfigured (FIG. 3) so that a low rotor speed signal (N1SYNTH) is synthesized from a sensed high rotor speed signal (N2). A secondary control channel 34 provides standby signals for use in the EEC and performs similar logic as in the primary channel, except that signal synthesis (N2 from N1 and vice-versa) is dependent upon N2 health. When the high rotor speed signal (N2) is healthy, a low rotor speed signal (N1SYNTH) is synthesized from a sensed high rotor speed signal (N2). When the high rotor speed signal (N2) is not healthy, a high rotor speed signal (N2SYNTH) is synthesized from a sensed low rotor speed signal (N1). For each of the low and high rotor speeds, redundant signals (N1A, N1B and N2A, N2B, respectively) are available. Primary sensors (10A, 24A) for low and high rotor speeds (N1A, N2A) serve the primary channel, secondary sensors (10B, 24B) for low and high rotor speeds (N2A, N2B) serve the secondary channel, and cross-channel communication is via a link (39).
Inventors
- 👤 Larry B. Carlisle
- 👤 Wayne R. Spock
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 21:09
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/02; F01D17/06; F03; F03B; F03B15/00; F03B15/02; F03B15/04; F03B15/06; F03B15/08; G; G05; G05D; G05D1/00; G05D1/0055; G05D1/0077; Y; Y02; Y02E; Y02E10/00; Y02E10/20
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
95 words
A method of synthesizing signals, comprising: providing a first signal (N1) indicative of and in response to a sensed first parameter; providing a second signal (N2) indicative of and in response to a second parameter related to the first parameter; monitoring the veracity of the first signal and the second signal; providing a first synthesized signal (N1SYNTH) if the veracity of the first signal is less than the veracity of the second signal; providing a second synthesized signal (N2SYNTH) if the veracity of the first signal has at least the veracity of the second signal.
Claim 2
Independent Claim
95 words
A method of synthesizing signals, comprising: providing a first signal (N1) indicative of and in response to a sensed first parameter; providing a second signal (N2) indicative of and in response to a second parameter related to the first parameter; monitoring the veracity of the first signal and the second signal; providing a first synthesized signal (N1SYNTH) if the veracity of the first signal is less than the veracity of the second signal; providing a second synthesized signal (N2SYNTH) if the veracity of the first signal has at least the veracity of the second signal.
Claim 3
Dependent Claim
26 words
A method according to claim 1 wherein the first and second signals are indicative of the low and high rotor speeds in a turbine engine, respectively.
Claim 4
Independent Claim
600 words
A method for controlling a turbine engine based on the low rotor speed and the high rotor speed, comprising: providing primary low and high rotor speed signals (N1A, N2A) in a primary control channel (32); providing secondary low and high rotor speed signals (N1B, N2B) in a secondary control channel (34); communicating the primary low and high rotor speed signals to the secondary channel; communicating the secondary low and high rotor speed signals to the primary channel; measuring the veracity of the primary and secondary low and high turbine speed signals; in the case of greater veracity in the low rotor speed signals (N1A, N1B) than in the high rotor speed signals (N2A, N2B): (a) in the primary channel, providing a first selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the primary and secondary low rotor speed signals (N1A, N1B) has higher veracity; providing a synthesized high rotor speed signal (N2SYNTH) as a function of the first selected low rotor speed signal (N1SEL) and known relationships between high and low rotor speeds in the engine; and providing a first selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the synthesized high rotor speed signal (N2SYNTH), the primary high rotor speed signal (N2A), and the secondary high rotor speed signal (N2B) has the highest veracity; and (b) in the secondary channel, providing a second selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the primary and secondary high rotor speed signals (N2A, N2B) has higher veracity; providing a synthesized low rotor speed signal (N1SYNTH) as a function of the second selected high rotor speed signal (N2SEL) and known relationships between high and low rotor speeds in the engine; and providing a second selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the synthesized low rotor speed signal (N1SYNTH), the primary low rotor speed signal (N1A), and the secondary low rotor speed signal (N1B) has the highest veracity; and in the case of greater veracity in the high rotor speed signals (N2A, N2B) than in the low rotor speed signals (N1A, N1B): (a) in the primary channel, providing a first selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the primary and secondary high rotor speed signals (N2A, N2B) has higher veracity; providing a synthesized low rotor speed signal (N1SYNTH) as a function of the first selected high rotor speed signal (N2SEL) and known relationships between high and low rotor speeds in the engine; and providing a first selected low rotor speed signal (N12SEL), for use in controlling the engine, indicative of which of the synthesized low rotor speed signal (N1SYNTH), the primary low rotor speed signal (N1A), and the secondary low rotor speed signal (N1B) has the highest veracity; and (b) in the secondary channel, providing a second selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the primary and secondary low rotor speed signals (N1A, N1B) has higher veracity; providing a synthesized high rotor speed signal (N2SYNTH) as a function of the second selected low rotor speed signal (N1SEL) and known relationships between high and low rotor speeds in the engine; and providing a second selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the synthesized high rotor speed signal (N2SYNTH), the primary high rotor speed signal (N2A), and the secondary high rotor speed signal (N2B) has the highest veracity.
Claim 5
Independent Claim
600 words
A method for controlling a turbine engine based on the low rotor speed and the high rotor speed, comprising: providing primary low and high rotor speed signals (N1A, N2A) in a primary control channel (32); providing secondary low and high rotor speed signals (N1B, N2B) in a secondary control channel (34); communicating the primary low and high rotor speed signals to the secondary channel; communicating the secondary low and high rotor speed signals to the primary channel; measuring the veracity of the primary and secondary low and high turbine speed signals; in the case of greater veracity in the low rotor speed signals (N1A, N1B) than in the high rotor speed signals (N2A, N2B): (a) in the primary channel, providing a first selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the primary and secondary low rotor speed signals (N1A, N1B) has higher veracity; providing a synthesized high rotor speed signal (N2SYNTH) as a function of the first selected low rotor speed signal (N1SEL) and known relationships between high and low rotor speeds in the engine; and providing a first selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the synthesized high rotor speed signal (N2SYNTH), the primary high rotor speed signal (N2A), and the secondary high rotor speed signal (N2B) has the highest veracity; and (b) in the secondary channel, providing a second selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the primary and secondary high rotor speed signals (N2A, N2B) has higher veracity; providing a synthesized low rotor speed signal (N1SYNTH) as a function of the second selected high rotor speed signal (N2SEL) and known relationships between high and low rotor speeds in the engine; and providing a second selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the synthesized low rotor speed signal (N1SYNTH), the primary low rotor speed signal (N1A), and the secondary low rotor speed signal (N1B) has the highest veracity; and in the case of greater veracity in the high rotor speed signals (N2A, N2B) than in the low rotor speed signals (N1A, N1B): (a) in the primary channel, providing a first selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the primary and secondary high rotor speed signals (N2A, N2B) has higher veracity; providing a synthesized low rotor speed signal (N1SYNTH) as a function of the first selected high rotor speed signal (N2SEL) and known relationships between high and low rotor speeds in the engine; and providing a first selected low rotor speed signal (N12SEL), for use in controlling the engine, indicative of which of the synthesized low rotor speed signal (N1SYNTH), the primary low rotor speed signal (N1A), and the secondary low rotor speed signal (N1B) has the highest veracity; and (b) in the secondary channel, providing a second selected low rotor speed signal (N1SEL), for use in controlling the engine, indicative of which of the primary and secondary low rotor speed signals (N1A, N1B) has higher veracity; providing a synthesized high rotor speed signal (N2SYNTH) as a function of the second selected low rotor speed signal (N1SEL) and known relationships between high and low rotor speeds in the engine; and providing a second selected high rotor speed signal (N2SEL), for use in controlling the engine, indicative of which of the synthesized high rotor speed signal (N2SYNTH), the primary high rotor speed signal (N2A), and the secondary high rotor speed signal (N2B) has the highest veracity.
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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) | 1991-01-25 | 1991-07-27 | 1992-01-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-01-25 | 1995-07-27 | 1996-01-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-01-25 | 1999-07-27 | 2000-01-26 | $7700.00 | Window Closed / Lapsed |