US5900827A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Flight crew response monitor
Assignee: Boeing Co
•
Filing: 1993-05-06
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Granted: 1999-05-04
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Expires: 2013-05-06
Abstract
Abstract Method and apparatus for measuring the alertness level of the flight crew of an aircraft and raising it when necessary. The system also detects departures from the planned flight profile and provides aural warning.
Inventors
- 👤 Donald A. Graham
- 👤 Randall P. Robertson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 21:39
CPC Classifications
G; G08; G08B; G08B21/00; G08B21/02; G08B21/06
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
65 words
A method of flight crew alertness monitoring for an aircraft having a Flight Management computer (FMC) which requires no crew action other than normal flight crew activities comprising a silent visual flight crew response advisory alert when no flight crew actuation of any of the controls monitored by the FMC has been detected by the FMC within a predetermined time period during the cruise segment.
Claim 2
Independent Claim
65 words
A method of flight crew alertness monitoring for an aircraft having a Flight Management computer (FMC) which requires no crew action other than normal flight crew activities comprising a silent visual flight crew response advisory alert when no flight crew actuation of any of the controls monitored by the FMC has been detected by the FMC within a predetermined time period during the cruise segment.
Claim 3
Dependent Claim
15 words
The invention according to claim 1 wherein said predetermined time period is about 20 minutes.
Claim 4
Independent Claim
70 words
A method of flight crew alertness monitoring for an aircraft having a Flight Management Computer (FMC) which requires no crew action other than normal flight crew activities comprising triggering an aural flight crew response alert when no flight crew actuation of any of the controls monitored by the FMC has been detected by the FMC within a predetermined time period after a silent flight crew advisory alert has been issued.
Claim 5
Independent Claim
70 words
A method of flight crew alertness monitoring for an aircraft having a Flight Management Computer (FMC) which requires no crew action other than normal flight crew activities comprising triggering an aural flight crew response alert when no flight crew actuation of any of the controls monitored by the FMC has been detected by the FMC within a predetermined time period after a silent flight crew advisory alert has been issued.
Claim 6
Dependent Claim
15 words
The invention according to claim 3 wherein said predetermined time period is about five minutes.
Claim 7
Independent Claim
133 words
A method of flight crew response monitoring for an aircraft having a Flight Management Computer (FMC) for deriving current aircraft position and a horizontal route over the earth's surface which can be selected and activated by a pilot, to provide an active route to be flown, said method comprising triggering a flight crew response alert when: said aircraft position is not converging with said active route for a predetermined time period with the FMC controlled laterial navigation mode (LNAV) armed, or said aircraft position begins to deviate from a previously captured active route with LNAV engaged, or said aircraft has been in the cruise phase with a route activated in the FMC but without LNAV engaged or armed, and has not been converging with said active route for a further predetermined time period.
Claim 8
Independent Claim
133 words
A method of flight crew response monitoring for an aircraft having a Flight Management Computer (FMC) for deriving current aircraft position and a horizontal route over the earth's surface which can be selected and activated by a pilot, to provide an active route to be flown, said method comprising triggering a flight crew response alert when: said aircraft position is not converging with said active route for a predetermined time period with the FMC controlled laterial navigation mode (LNAV) armed, or said aircraft position begins to deviate from a previously captured active route with LNAV engaged, or said aircraft has been in the cruise phase with a route activated in the FMC but without LNAV engaged or armed, and has not been converging with said active route for a further predetermined time period.
Claim 9
Dependent Claim
16 words
The method according to claim 5 wherein said predetermined time period exceeds about fifteen (15) minutes.
Claim 10
Independent Claim
135 words
A method of flight crew response monitoring for an aircraft having a Flight Management Computer (FMC) controlled vertical navigation mode (VNAV) and an FMC derived flight profile, said method comprising triggering a flight crew response alert during aircraft cruise with the FMC controlled vertical navigation mode (VNAV) engaged when the FMC detects that continued tracking of the FMC derived flight profile is jeopardized by either: a gradual thrust loss to a predetermined percentage on any engine, or a speed deviation from target speed of more than a predetermined amount and said speed deviation is not decreasing for a predetermined time period, or a pitch deviation in excess of a predetermined number of degrees from FMC commanded pitch attitude, or a roll deviation in excess of a predetermined number of degrees from FMC commanded roll attitude.
Claim 11
Independent Claim
135 words
A method of flight crew response monitoring for an aircraft having a Flight Management Computer (FMC) controlled vertical navigation mode (VNAV) and an FMC derived flight profile, said method comprising triggering a flight crew response alert during aircraft cruise with the FMC controlled vertical navigation mode (VNAV) engaged when the FMC detects that continued tracking of the FMC derived flight profile is jeopardized by either: a gradual thrust loss to a predetermined percentage on any engine, or a speed deviation from target speed of more than a predetermined amount and said speed deviation is not decreasing for a predetermined time period, or a pitch deviation in excess of a predetermined number of degrees from FMC commanded pitch attitude, or a roll deviation in excess of a predetermined number of degrees from FMC commanded roll attitude.
Claim 12
Dependent Claim
42 words
The method according to claim 7 wherein said predetermined percentage is about five (5) percent, said predetermined amount is about ten (10) knots, said predetermined time period is five (5) minutes, and said predetermined number of degrees is about five (5) degrees.
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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) | 2002-05-03 | 2002-11-02 | 2003-05-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2006-05-03 | 2006-11-02 | 2007-05-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2010-05-03 | 2010-11-02 | 2011-05-04 | $7700.00 | Window Closed / Lapsed |