US4954974A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbine engine fan speed monitor
Assignee: Howell Instruments Inc
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Filing: 1988-12-15
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Granted: 1990-09-04
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Expires: 2008-12-15
Abstract
Abstract A turbine fan speed monitor for use with an aircraft engine which monitors actual fan speeds for each of a plurality of aircraft engines. The apparatus also input instantaneous values of total air temperature, pressure altitude, altitude rate, and the position of the wheels. The fan speed monitor calculates an overspeed limit value for the turbine fan as a function of each of the total air temperature, pressure altitude, altitude rate, and position of the wheels data and indicates when the actual fan speed exceeds the overspeed limit value for each monitored engine. The monitor warns the pilot of calculated overspeed conditions that he can control by throttle manipulation. Engine life is related to the calculated speeds at take-off, climb and cruise. The monitor keeps a record of the time and duration of these instances when the actual fan speed exceeds the overspeed limit for any engine. The monitor may also include a display to indicate the value of any of the calculated or sensed parameters including the frequency of the actual fan speed exceeding the overspeed limit for any engine. The monitor may also include data entry controls to manually input engine data previously accumulated for a monitored engine.
Inventors
- 👤 John S. Howell, IV
- 👤 Kenneth P. Widner
- 👤 Gary D. Guenther
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 04:43
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/003; G; G01; G01P; G01P1/00; G01P1/12; G01P1/122; G01P3/00; G01P3/42; G01P3/56; G07; G07C; G07C3/00
Claims Analysis
Total Claims: 17
Claim 1
Independent Claim
141 words
A turbine fan speed monitor for use with at least one aircraft engine having a rotating turbine fan with a variable overspeed limit value comprising: an RPM sensor for continually detecting actual fan rotational speeds of at least one aircraft engine; an environmental condition sensor for continually detecting environmental data defining at least total air temperature, pressure altitude and altitude rate; and a computer, electrically connected to the RPM sensor and the environmental condition sensor, for recording the actual fan speeds, for recording the environmental data, for determining overspeed limit values for each monitored aircraft engine as a function of the environmental data, and for comparing the overspeed limit values with the actual fan rotation speeds, the computer including memory means for recording at least the frequency of the actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 2
Dependent Claim
141 words
A turbine fan speed monitor for use with at least one aircraft engine having a rotating turbine fan with a variable overspeed limit value comprising: an RPM sensor for continually detecting actual fan rotational speeds of at least one aircraft engine; an environmental condition sensor for continually detecting environmental data defining at least total air temperature, pressure altitude and altitude rate; and a computer, electrically connected to the RPM sensor and the environmental condition sensor, for recording the actual fan speeds, for recording the environmental data, for determining overspeed limit values for each monitored aircraft engine as a function of the environmental data, and for comparing the overspeed limit values with the actual fan rotation speeds, the computer including memory means for recording at least the frequency of the actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 3
Dependent Claim
84 words
A monitor as in claim 1 further including: a display, electrically connected to the computer, for indicating the instantaneous values of at least one of: the environmental data, the actual fan speeds for each monitored engine, the overspeed limit values for each monitored engine, the peak actual fan speed for each monitored engine, the frequency of actual fan speeds exceeding the overspeed limit values for each monitored engine, and the duration of actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 4
Dependent Claim
36 words
A monitor as in claim 1 further including: a plurality of warning lamps, electrically connected to the computer, for indicating the occurrence of the actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 5
Dependent Claim
40 words
A monitor as in claim 1 further including: a control panel, electrically connected to the computer, for manually inputting at least data defining a previously monitored frequency of actual fan speeds exceeding the overspeed limit values for any monitored engine.
Claim 6
Dependent Claim
33 words
A turbine fan speed monitor as in claim 1, wherein the memory means also records at least the duration of the actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 7
Dependent Claim
34 words
A monitor as in claim 1 wherein the computer further includes: self-check circuitry for identifying instances when the computer did not receive at least one of the environmental data and the actual fan speed.
Claim 8
Dependent Claim
35 words
A monitor as in claim 6 further including a display for indicating the occurrence of said instances when the computer did not receive at least one of the environmental data and the actual fan speed.
Claim 9
Dependent Claim
35 words
A monitor as in claim 6 further including a display for indicating the duration of said instances when the computer did not receive at least one of the environmental data and the actual fan speed.
Claim 10
Independent Claim
101 words
A method for monitoring at least one aircraft engine having a rotating turbine fan with a variable overspeed limit value comprising the steps of: detecting and recording the actual fan speeds of at least one aircraft engine; detecting and recording environmental data defining at least total air temperature, pressure altitude and altitude rate; determining overspeed limit values for each monitored aircraft engine as a function of the environmental data; comparing the actual fan speeds to the selected overspeed limit values for each monitored engine; and recording the frequency of actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 11
Independent Claim
101 words
A method for monitoring at least one aircraft engine having a rotating turbine fan with a variable overspeed limit value comprising the steps of: detecting and recording the actual fan speeds of at least one aircraft engine; detecting and recording environmental data defining at least total air temperature, pressure altitude and altitude rate; determining overspeed limit values for each monitored aircraft engine as a function of the environmental data; comparing the actual fan speeds to the selected overspeed limit values for each monitored engine; and recording the frequency of actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 12
Dependent Claim
29 words
A method as in claim 9 further including the step of recording the duration of the actual fan speeds exceeding the overspeed limit values for each monitored aircraft engine.
Claim 13
Dependent Claim
79 words
A method as in claim 9 further including the step of displaying the instantaneous values of at least one of: the environmental data, the actual fan speeds for each monitored engine, the overspeed limit values for each monitored engine, the peak actual fan speed for each monitored engine, the frequency of actual fan speeds exceeding the overspeed limit values for each monitored engine, and the duration of actual fan speeds exceeding the overspeed limit values for each monitored engine.
Claim 14
Dependent Claim
27 words
A method as in claim 9 including the step of displaying the occurrence of an actual fan speed exceeding the overspeed limit value for each monitored engine.
Claim 15
Dependent Claim
31 words
A method as in claim 9 further including the steps of monitoring and recording instances when at least one of the environmental data and the actual fan speeds was not detected.
Claim 16
Dependent Claim
33 words
A method as in claim 13 further including the step of indicating the occurrence of said instances when at least one of the environmental data and the actual fan speeds was not detected.
Claim 17
Dependent Claim
33 words
A method as in claim 14 further including the step of indicating the duration of said instances when at least one of the environmental data and the actual fan speeds was not detected.
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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) | 1993-09-03 | 1994-03-05 | 1994-09-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-09-03 | 1998-03-05 | 1998-09-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-09-03 | 2002-03-05 | 2002-09-04 | $7700.00 | Window Closed / Lapsed |