Patent US4484283A successfully refreshed from Google Patents.
US4484283A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft roll-yaw fault protocols
Assignee: RTX Corp
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Filing: 1981-03-30
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Granted: 1984-11-20
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Expires: 2001-03-30
Abstract
Abstract In an aircraft automatic flight control system, automatic shutdown (42) of the roll axis thereof (FIG. 1) as a consequence of faults detected therein also provides automatic shutdown of the yaw axis thereof (180) in the same fashion as detection of faults in the yaw axis (171, 167) provides shutdown of the yaw axis. Coupling of the roll axis shutdown into the yaw axis shutdown allows determining which of three axes cause lighting of a single trim shutdown indicator by resetting the yaw shutdown register (145) and simultaneously resetting both the pitch and roll shutdown registers by means of a single cyclic pitch control switch. Automatic yaw trim outer loop and yaw inner loop stability systems are disclosed (FIG. 2).
Inventors
- 👤 David J. Verzella
- 👤 William C. Fischer
- 👤 Don L. Adams
- 👤 Stuart C. Wright
- 👤 Byron Graham, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 22:56
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/08; G05D1/0808; G05D1/0858
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
459 words
An aircraft automatic flight control system, comprising: a roll channel including a roll actuator for positioning roll-axis-controlling aerodynamic surfaces of the aircraft; a yaw channel including a yaw actuator for positioning yaw-axis-controlling aerodynamic surfaces of the aircraft; roll disable means operable in either of two states for enabling operation of said roll actuator in response to roll command signals applied thereto when in a first one of said states and for disabling operation of said roll actuator when set in the other of said states in response to a roll shut down signal provided thereto; yaw disable means operable in either of two states for enabling operation of said yaw actuator in response to yaw command signals applied thereto when in a first one of said states and for disabling operation of said yaw actuator when set in the other of said states in response to a yaw shut down signal provided thereto; means for providing a roll reset signal; means for providing a yaw reset signal; a trim shut down indicator; and signal processing means for providing roll command signals to said roll channel, for providing yaw command signals to said yaw channel, responsive to said roll channel for providing a roll shut down signal to said roll disable means in response to a condition therein indicative of a fault thereof, responsive to said yaw channel for providing a yaw shut down signal to said yaw disable means in response to a condition therein indicative of a fault thereof, for providing said yaw shut down signal in response to said roll shut down signal, for operating said trim shut down indicator in response to the presence of said roll shut down signal concurrently with the absence of said roll reset signal, for operating said trim shut down indicator in response to the presence of said yaw shut down signal concurrently with the absence of said yaw reset signal, for providing a third shut down signal indicative of a third fault and for operating said trim shut down indicator in response to the presence of said third shut down signal concurrently with the absence of said roll reset signal, whereby operation of said trim shut down indicator being interrupted by the absence of said roll reset signal concurrently with the presence of said yaw reset signal is indicative of fault in said yaw channel, and operation of said trim shut down indicator being interrupted by the presence of said roll reset signal concurrently with the absence of said yaw reset signal is indicative of said third fault, and operation of said trim shut down indicator being uninterrupted by the presence of either said roll reset signal or said yaw reset signal being indicative of fault in said roll channel.
Claim 2
Dependent Claim
459 words
An aircraft automatic flight control system, comprising: a roll channel including a roll actuator for positioning roll-axis-controlling aerodynamic surfaces of the aircraft; a yaw channel including a yaw actuator for positioning yaw-axis-controlling aerodynamic surfaces of the aircraft; roll disable means operable in either of two states for enabling operation of said roll actuator in response to roll command signals applied thereto when in a first one of said states and for disabling operation of said roll actuator when set in the other of said states in response to a roll shut down signal provided thereto; yaw disable means operable in either of two states for enabling operation of said yaw actuator in response to yaw command signals applied thereto when in a first one of said states and for disabling operation of said yaw actuator when set in the other of said states in response to a yaw shut down signal provided thereto; means for providing a roll reset signal; means for providing a yaw reset signal; a trim shut down indicator; and signal processing means for providing roll command signals to said roll channel, for providing yaw command signals to said yaw channel, responsive to said roll channel for providing a roll shut down signal to said roll disable means in response to a condition therein indicative of a fault thereof, responsive to said yaw channel for providing a yaw shut down signal to said yaw disable means in response to a condition therein indicative of a fault thereof, for providing said yaw shut down signal in response to said roll shut down signal, for operating said trim shut down indicator in response to the presence of said roll shut down signal concurrently with the absence of said roll reset signal, for operating said trim shut down indicator in response to the presence of said yaw shut down signal concurrently with the absence of said yaw reset signal, for providing a third shut down signal indicative of a third fault and for operating said trim shut down indicator in response to the presence of said third shut down signal concurrently with the absence of said roll reset signal, whereby operation of said trim shut down indicator being interrupted by the absence of said roll reset signal concurrently with the presence of said yaw reset signal is indicative of fault in said yaw channel, and operation of said trim shut down indicator being interrupted by the presence of said roll reset signal concurrently with the absence of said yaw reset signal is indicative of said third fault, and operation of said trim shut down indicator being uninterrupted by the presence of either said roll reset signal or said yaw reset signal being indicative of fault in said roll channel.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-11-20 | 1988-05-21 | 1988-11-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-11-20 | 1992-05-21 | 1992-11-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-11-20 | 1996-05-21 | 1996-11-20 | $7700.00 | Window Closed / Lapsed |