US4121194A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Take-off warning system for aircraft
Assignee: Boeing Co
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Filing: 1976-09-30
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Granted: 1978-10-17
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Expires: 1996-09-30
Abstract
Abstract A logic controlled take-off warning system having a circuit for enabling the logic controlled take-off warning system at engine thrust levels exceeding a predetermined value which is less than minimum take-off thrust of the aircraft and greater than trust required for normal ground operations, provided also that the aircraft is on the ground. When the logic controlled take-off warning system is enabled, a take-off warning horn is subsequently energized when any one of a plurality of undesired take-off configurations exists.
Inventors
- 👤 Thomas James Downey
- 👤 Peter Dennis Turnbull
- 👤 James Walter Gayther
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 05:53
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/0083; G08; G08G; G08G5/00; G08G5/20; G08G5/21; G08G5/50; G08G5/52; G08G5/55; G08G5/51
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
236 words
In combination in a multi-engine jet transport: first means associated with a first engine for providing first signals representative of the thrust of said first engine; second means associated with a second engine for providing second signals representative of the trust of said second engine; logic controlled take-off warning circuit means for providing warning signals in the event one or more logical conditions required for take-off configuration of the aircraft are not satisfied; first signal generating means including a phase detection circuit responsive to said first signals for providing third signals representative of thrust levels referenced to a predetermined value equal to or less than required for take-off of said multi-engine jet transport but greater than required for other ground operations of said multi-engine jet transport; second signal generating means including a phase detection circuit responsive to said second signals for providing fourth signals representative of thrust levels referenced to said predetermined value; circuit means responsive to said third and fourth signals for enabling said logic controlled take-off warning circuit to develop warning signals when said third and fourth signals are both representative of thrust levels exceeding said predetermined value and one or more of said logical conditions required for take-off configuration of the aircraft is not satisfied; and said circuit means including thrust reverser sensing circuit means for preventing nuisance warnings in said logic controlled take-off warning circuit means at high levels of reverse thrust.
Claim 2
Dependent Claim
236 words
In combination in a multi-engine jet transport: first means associated with a first engine for providing first signals representative of the thrust of said first engine; second means associated with a second engine for providing second signals representative of the trust of said second engine; logic controlled take-off warning circuit means for providing warning signals in the event one or more logical conditions required for take-off configuration of the aircraft are not satisfied; first signal generating means including a phase detection circuit responsive to said first signals for providing third signals representative of thrust levels referenced to a predetermined value equal to or less than required for take-off of said multi-engine jet transport but greater than required for other ground operations of said multi-engine jet transport; second signal generating means including a phase detection circuit responsive to said second signals for providing fourth signals representative of thrust levels referenced to said predetermined value; circuit means responsive to said third and fourth signals for enabling said logic controlled take-off warning circuit to develop warning signals when said third and fourth signals are both representative of thrust levels exceeding said predetermined value and one or more of said logical conditions required for take-off configuration of the aircraft is not satisfied; and said circuit means including thrust reverser sensing circuit means for preventing nuisance warnings in said logic controlled take-off warning circuit means at high levels of reverse thrust.
Claim 3
Dependent Claim
22 words
The invention according to claim 1 wherein said referenced value thrust level is representative of an engine pressure ratio of about 1.4.
Claim 4
Dependent Claim
125 words
In combination in a take-off warning system for an aircraft having a plurality of engines and a signal path between engine pressure ratio indicator associated with each of said plurality of engines: a plurality of signal generating means responsive to said respective plurality of signal paths for providing a plurality of signals representative of thrust levels referenced to a predetermined value; a squat switch responsive to on-the-ground condition of the aircraft; and, circuit means responsive to said plurality of signals for enabling said take-off warning system to develop warning signals when said plurality of signals representative of thrust levels referenced to a predetermined value are all representative of an engine pressure ratio exceeding about 1.4 and said squat switch is representative of said on-the-ground condition.
Claim 5
Dependent Claim
125 words
In combination in a take-off warning system for an aircraft having a plurality of engines and a signal path between engine pressure ratio indicator associated with each of said plurality of engines: a plurality of signal generating means responsive to said respective plurality of signal paths for providing a plurality of signals representative of thrust levels referenced to a predetermined value; a squat switch responsive to on-the-ground condition of the aircraft; and, circuit means responsive to said plurality of signals for enabling said take-off warning system to develop warning signals when said plurality of signals representative of thrust levels referenced to a predetermined value are all representative of an engine pressure ratio exceeding about 1.4 and said squat switch is representative of said on-the-ground condition.
Claim 6
Dependent Claim
167 words
In combination in a take-off warning system for an multi-engine aircraft having two a.c. signals representative of engine pressure ratio information: means for providing take-off warning system enable signals for enabling said take-off warning system when the aircraft is in an on-the-ground condition; said means including phase detection circuits responsive to said a.c. signals and enabling said take-off warning system in response to engine pressure ratio information representative of engine thrust levels of one or more engines of said multi-engine aircraft of greater than a predetermined value, said predetermined value less than minimum take-off thrust but greater than normal thrust required for ground operations of the aircraft other than take-off condition; said means further including thrust reverser sensing circuit means for preventing nuisance warnings in said take-off warning system at high levels of reverse thrust; and, alarm signalling utilization means for actuating an alarm in response to enabling of said take-off warning system and upon the occurrence of any one of a plurality of undesired take-off conditions.
Claim 7
Dependent Claim
167 words
In combination in a take-off warning system for an multi-engine aircraft having two a.c. signals representative of engine pressure ratio information: means for providing take-off warning system enable signals for enabling said take-off warning system when the aircraft is in an on-the-ground condition; said means including phase detection circuits responsive to said a.c. signals and enabling said take-off warning system in response to engine pressure ratio information representative of engine thrust levels of one or more engines of said multi-engine aircraft of greater than a predetermined value, said predetermined value less than minimum take-off thrust but greater than normal thrust required for ground operations of the aircraft other than take-off condition; said means further including thrust reverser sensing circuit means for preventing nuisance warnings in said take-off warning system at high levels of reverse thrust; and, alarm signalling utilization means for actuating an alarm in response to enabling of said take-off warning system and upon the occurrence of any one of a plurality of undesired take-off conditions.
Claim 8
Dependent Claim
99 words
In combination in an aircraft having a plurality of engines: a logic controlled take-off warning circuit for said aircraft; circuit means for enabling said logic controlled take-off warning circuit when one or more of said plurality of engines of said aircraft has an engine pressure ratio exceeding about 1.4 and said aircraft is in an on-the-ground condition; said logic controlled take-off warning circuit including a plurality of switches representative of undesired take-off configuration conditions for alarm signaling upon enabling of said logic controlled take-off warning circuit and when any one of said plurality of undesired take-off configuration conditions exists.
Claim 9
Dependent Claim
99 words
In combination in an aircraft having a plurality of engines: a logic controlled take-off warning circuit for said aircraft; circuit means for enabling said logic controlled take-off warning circuit when one or more of said plurality of engines of said aircraft has an engine pressure ratio exceeding about 1.4 and said aircraft is in an on-the-ground condition; said logic controlled take-off warning circuit including a plurality of switches representative of undesired take-off configuration conditions for alarm signaling upon enabling of said logic controlled take-off warning circuit and when any one of said plurality of undesired take-off configuration conditions exists.
Claim 10
Dependent Claim
224 words
In combination: a logic controlled take-off warning circuit for an aircraft; and, an enabling circuit having a plurality of input terminals adapted for coupling to a plurality of a.c. voltage signal sources representative of engine pressure ratio information of a plurality of engines of said aircraft and providing at the output terminal thereof a high level logic signal for enabling said logic controlled take-off warning circuit when the aircraft is on the ground and one or more of said plurality of engines has an engine pressure ratio exceeding a predetermined level and providing a low level logic signal when said plurality of engines have engine pressure ratios less than said predetermined level, said enabling circuit including a plurality of series connected phase detection circuit means and Schmitt trigger circuit means connected between said plurality of input terminals and said output terminal, said enable circuit further including a squat switch coupled between said output terminal and a reference potential for preventing enabling of said logic controlled take-off warning circuit when the aircraft is not on the ground; and, a plurality of thrust reverser sensing circuit means coupled in circuit between said plurality of series connected phase detection circuit means and Schmitt trigger circuit means and said output terminal for preventing nuisance warnings in said logic controlled take-off warning circuit at high levels of reverse thrust.
Claim 11
Dependent Claim
224 words
In combination: a logic controlled take-off warning circuit for an aircraft; and, an enabling circuit having a plurality of input terminals adapted for coupling to a plurality of a.c. voltage signal sources representative of engine pressure ratio information of a plurality of engines of said aircraft and providing at the output terminal thereof a high level logic signal for enabling said logic controlled take-off warning circuit when the aircraft is on the ground and one or more of said plurality of engines has an engine pressure ratio exceeding a predetermined level and providing a low level logic signal when said plurality of engines have engine pressure ratios less than said predetermined level, said enabling circuit including a plurality of series connected phase detection circuit means and Schmitt trigger circuit means connected between said plurality of input terminals and said output terminal, said enable circuit further including a squat switch coupled between said output terminal and a reference potential for preventing enabling of said logic controlled take-off warning circuit when the aircraft is not on the ground; and, a plurality of thrust reverser sensing circuit means coupled in circuit between said plurality of series connected phase detection circuit means and Schmitt trigger circuit means and said output terminal for preventing nuisance warnings in said logic controlled take-off warning circuit at high levels of reverse thrust.
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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) | 1981-10-16 | 1982-04-17 | 1982-10-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-16 | 1986-04-17 | 1986-10-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-16 | 1990-04-17 | 1990-10-17 | $7700.00 | Window Closed / Lapsed |