Aircraft control architecture, of at least one actuator of a nacelle movable cowl
US-2021285400-A1 · Sep 16, 2021 · US
US12560459B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12560459-B2 |
| Application number | US-202217977207-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 31, 2022 |
| Priority date | Nov 3, 2021 |
| Publication date | Feb 24, 2026 |
| Grant date | Feb 24, 2026 |
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A method of determining the status of a lock. The method includes reading data from a proximity switch and calculating an inductance value from a solenoid, the proximity switch and solenoid located in or around a lock, and processing the data from the proximity switch and the inductance value. The method further includes comparing the processed data with an expected value to confirm the lock status.
Opening claim text (preview).
The invention claimed is: 1 . A method of confirming a lock status of a lock by an engine computer for a thrust reverser prior to deploying the thrust reverser by a thrust reverser actuation system, the method comprising: reading, by the engine computer, data from a proximity switch for a lock, which includes a primary lock and a tertiary lock, of the thrust reverser and calculating an inductance value from a solenoid for the lock, wherein the proximity switch and the solenoid are located in or around the lock; processing, by the engine computer, the data from the proximity switch and the inductance value from the solenoid; and wherein the engine computer is configured for: reading the data from the proximity switch sent to the engine computer; calculating solenoid inductance sent to the engine computer; processing the data sent to the engine computer to compare the data with values to determine whether the lock is unlocked, and thereafter: upon determining that the proximity switch and/or the solenoid inductance show that the lock is unlocked, it is confirmed that the tertiary lock is unlocked and the engine computer proceeds with deployment of the thrust reverser actuation system; and upon determining that the lock is in a locked position, then determining whether the tertiary lock or the primary lock is unlocked, and upon determining that the tertiary lock is not unlocked, reporting a fault and not proceeding to deployment of the thrust reverser actuation system.
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