Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents

Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents

An aircraft (100) is provided. The aircraft may include, but is not limited to, an accelerometer (160) configured to measure a deceleration experienced by the aircraft (100) and a processor (120) coupled to the accelerometer (160). The processor (120) may be configured to determine if the aircraft (...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Lad, Girish M, Chandran, Nagarajan
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:An aircraft (100) is provided. The aircraft may include, but is not limited to, an accelerometer (160) configured to measure a deceleration experienced by the aircraft (100) and a processor (120) coupled to the accelerometer (160). The processor (120) may be configured to determine if the aircraft (100) experienced a hard landing if the deceleration experienced by the aircraft (100) was greater than a predetermined threshold, and generate a maintenance advisory if the aircraft (100) experienced a hard landing.